EP3080318A2 - Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties and distributor for this method - Google Patents
Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties and distributor for this methodInfo
- Publication number
- EP3080318A2 EP3080318A2 EP14828176.9A EP14828176A EP3080318A2 EP 3080318 A2 EP3080318 A2 EP 3080318A2 EP 14828176 A EP14828176 A EP 14828176A EP 3080318 A2 EP3080318 A2 EP 3080318A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- fabric
- casting
- wall
- weight
- liquid
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000004744 fabric Substances 0.000 claims description 49
- 238000005266 casting Methods 0.000 claims description 40
- 229910001338 liquidmetal Inorganic materials 0.000 claims description 32
- 239000007788 liquid Substances 0.000 claims description 26
- 238000000034 method Methods 0.000 claims description 25
- 229910052760 oxygen Inorganic materials 0.000 claims description 19
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 18
- 239000001301 oxygen Substances 0.000 claims description 18
- 229910045601 alloy Inorganic materials 0.000 claims description 17
- 239000000956 alloy Substances 0.000 claims description 17
- 229910000838 Al alloy Inorganic materials 0.000 claims description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 11
- 238000001914 filtration Methods 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 10
- 230000008018 melting Effects 0.000 claims description 10
- 238000007789 sealing Methods 0.000 claims description 10
- 238000007711 solidification Methods 0.000 claims description 10
- 230000008023 solidification Effects 0.000 claims description 10
- 229910052726 zirconium Inorganic materials 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 8
- 229910052744 lithium Inorganic materials 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 7
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 7
- 239000001257 hydrogen Substances 0.000 claims description 7
- 229910052739 hydrogen Inorganic materials 0.000 claims description 7
- 150000003839 salts Chemical class 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 238000009749 continuous casting Methods 0.000 claims description 6
- 238000012423 maintenance Methods 0.000 claims description 6
- 239000011261 inert gas Substances 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 238000009941 weaving Methods 0.000 claims description 5
- 238000007872 degassing Methods 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 3
- 238000005242 forging Methods 0.000 claims description 3
- 229910002804 graphite Inorganic materials 0.000 claims description 3
- 239000010439 graphite Substances 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 2
- 238000009987 spinning Methods 0.000 claims 1
- 239000011572 manganese Substances 0.000 description 10
- 239000010949 copper Substances 0.000 description 7
- 239000010936 titanium Substances 0.000 description 7
- -1 Aluminum - copper - lithium Chemical compound 0.000 description 6
- 229910052782 aluminium Inorganic materials 0.000 description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 6
- 238000009434 installation Methods 0.000 description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000001989 lithium alloy Substances 0.000 description 6
- 239000011777 magnesium Substances 0.000 description 6
- 230000003068 static effect Effects 0.000 description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 5
- 229910000733 Li alloy Inorganic materials 0.000 description 5
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 229910052709 silver Inorganic materials 0.000 description 5
- 239000004332 silver Substances 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- 239000012080 ambient air Substances 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- KWGKDLIKAYFUFQ-UHFFFAOYSA-M lithium chloride Chemical compound [Li+].[Cl-] KWGKDLIKAYFUFQ-UHFFFAOYSA-M 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000000523 sample Substances 0.000 description 3
- 239000003351 stiffener Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 238000012512 characterization method Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- 229910017539 Cu-Li Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 239000001768 carboxy methyl cellulose Substances 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 229920002313 fluoropolymer Polymers 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 238000009210 therapy by ultrasound Methods 0.000 description 1
- 229940089401 xylon Drugs 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/057—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with copper as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/22—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/21—Presses specially adapted for extruding metal
- B21C23/212—Details
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
- B22D11/003—Aluminium alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/0408—Moulds for casting thin slabs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/041—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds for vertical casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/059—Mould materials or platings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/103—Distributing the molten metal, e.g. using runners, floats, distributors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/11—Treating the molten metal
- B22D11/116—Refining the metal
- B22D11/119—Refining the metal by filtering
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
- B22D21/04—Casting aluminium or magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
- B21B2003/001—Aluminium or its alloys
Definitions
- the invention relates to wrought products aluminum alloys - copper - lithium, more particularly, such products, their manufacturing processes and use, intended in particular for aeronautical and aerospace construction.
- Aluminum alloy rolled products are developed to produce structural elements for the aerospace industry and the aerospace industry in particular.
- Aluminum - copper - lithium alloys are particularly promising for this type of product.
- the specifications imposed by the aeronautical industry for fatigue performance are high.
- Thick products of Al-Cu-Li alloy are described in particular in applications US2005 / 0006008 and US2009 / 0159159.
- this type of treatment remains difficult to perform for the quantities necessary for the manufacture of thick plates.
- a first object of the invention is a method of manufacturing an aluminum alloy product comprising the steps in which
- the hydrogen content of said liquid metal bath (1) is less than 0.4 ml / 100 g, the oxygen content measured above the liquid surface (14, 15) is less than 0.5% by volume ,
- the distributor used (7) for the casting is made of fabric comprising essentially carbon, that it comprises a lower face (76), an upper face defining the orifice through which the liquid metal is introduced (71) and a wall; of substantially rectangular section, the wall comprising two longitudinal parts parallel to the width W (720, 721) and two transverse parts parallel to the thickness T (730, 731) said portions transverse and longitudinal being formed of at least two tissues, a first substantially obturating and semi-rigid tissue (77) ensuring the maintenance of the dispenser shape during casting and a second non-sealing fabric (78) allowing the passage and filtration liquid, said first and second webs being bonded to each other without overlapping or overlapping and without gap between them, said first fabric continuously covering at least 30% of the area of said wall portions (720,721, 730 731) and being positioned so that the liquid surface is in contact with it over the entire section.
- Another object of the invention is a dispenser for the semi-continuous casting of fabric aluminum alloy plates comprising essentially carbon, comprising a lower face (76), an upper face defining the orifice through which the metal liquid is introduced (71) and a wall of substantially rectangular section, the wall comprising two longitudinal portions parallel to the width W (720, 721) and two transverse portions parallel to the thickness T (730, 731) said transverse and longitudinal portions being formed of at least two fabrics, a first substantially obturating and semi-rigid fabric (77) ensuring the maintenance of the shape of the dispenser during casting and a second non-sealing fabric (78) permitting the passage and filtration of the liquid, said first and second webs being bonded to one another without overlapping or overlapping and without interstices separating them, said first web covering continuously at least 30% of the area of said wall portions (720, 721, 730, 731) being positioned so that the liquid surface is in contact therewith throughout the section.
- Figure 1 is the diagram of the test pieces used for the tests in smooth fatigue (Fig la) and in fatigue with hole (Fig lb). Dimensions are given in mm.
- Figure 2 is a general diagram of the solidification device used in one embodiment of the invention.
- Figure 3 is a general diagram of the dispenser used in the process according to the invention.
- Figure 4 shows representations of the bottom and the lateral and longitudinal parts of the distributor wall according to one embodiment of the invention.
- Figure 5 shows the relationship between the smooth fatigue performance and the hydrogen content of the liquid metal bath during solidification (Fig. 5a) or the oxygen content measured above the liquid surface during solidification (Fig. 5b).
- Figure 6 shows the Wohler curves obtained with tests 3, 7 and 8 in the direction L-T ( Figure 6a) and T-L ( Figure 6b).
- the static mechanical characteristics in tension in other words the tensile strength R m , the conventional yield stress at 0.2% elongation R p0.2 , and the elongation at break A% are determined by a tensile test according to standard NF EN ISO 6892-1, the sampling and the direction of the test being defined by the EN 485-1 standard.
- the test conditions follow the ASTM E466 standard.
- the logarithmic average of the results obtained on at least 4 test pieces is determined.
- N the number of cycles to failure
- N 0 the number of cycles to failure
- n -4.5.
- the IQF corresponding to the median is reported, ie 50% rupture per 100,000 cycles.
- a thick wrought product is a product whose thickness is at least 6 mm.
- the thickness of the products according to the invention is at least 80 mm and preferably at least 100 mm.
- the thickness of the wrought products is at least 120 mm or preferably 140 mm.
- the thickness of the thick products according to the invention is typically at most 240 mm, generally at most 220 mm and preferably at most 180 mm.
- a sheet is according to the invention a laminated product of rectangular cross section whose uniform thickness is at least 6 mm and does not exceed 1 / 10th of the width.
- a "structural element” or “structural element” of a mechanical construction is called a mechanical part for which the static and / or dynamic mechanical properties are particularly important for the performance of the structure, and for which a structural calculation is usually prescribed or realized.
- These are typically elements whose failure is likely to endanger the safety of said construction, its users, its users or others.
- these structural elements include the elements that make up the fuselage (such as fuselage skin (fuselage skin in English), stiffeners or stringers, bulkheads, fuselage (circumferential frames), the wings (such as the wing skin), the stiffeners (stringers or stiffeners), the ribs (ribs) and spars) and the empennage composed in particular of stabilizers Horizontal and vertical (horizontal or vertical stabilizers), as well as floor beams, seat rails and doors.
- fuselage such as fuselage skin (fuselage skin in English
- stiffeners or stringers such as the wing skin
- the stiffeners stringers or stiffeners
- ribs ribs
- spars spars
- empennage composed in particular of stabilizers Horizontal and vertical (horizontal or vertical stabilizers), as well as floor beams, seat rails and doors.
- a casting plant is here referred to as the set of devices making it possible to transform a metal in any form into a semi-product of raw form via the liquid phase.
- a casting plant may include a number of devices such as one or more ovens required for melting the metal (“melting furnace") and / or maintaining it (“holding furnace”) in temperature and / or preparation of the liquid metal and adjustment of the composition (“preparation furnace”), one or more tanks (or “pockets") intended to carry out a treatment for the removal of impurities dissolved and / or suspended in the liquid metal this treatment may consist of filtering the liquid metal on a filter medium in a "filtration bag” or introducing into the bath a so-called “treatment” gas that can be inert or reactive in a "degassing bag", a device for solidification of the liquid metal (or “casting loom”) by vertical semi-continuous casting by direct cooling in a casting well, which may comprise devices such as a mold (or “mold”) a liquid metal supply device (or "nozzle”)
- the present inventors have found that, surprisingly, thick wrought products of copper lithium aluminum alloy with improved fatigue performance can be obtained by preparing these sheets by the following method.
- an alloy liquid metal bath comprising, in% by weight Cu: 2.0 - 6.0; Li: 0.5 - 2.0; Mg: 0-1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one member selected from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if selected, being from 0.05 to 0.20% by weight for Zr, 0.05 to 0 , 8% by weight for Mn, 0.05 to 0.3% by weight for Cr and for Se, 0.05 to 0.5% by weight for Hf and from 0.01 to 0.15% by weight for Ti , Si ⁇ 0,1; Fe ⁇ 0.1; others ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum.
- An advantageous alloy for the process according to the invention comprises, in% by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element selected from Zr, Mn and Ti, the amount of said element, if selected, being from 0.06 to 0.15% by weight for Zr, 0.05 to 0.8% by weight for Mn and from 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ⁇ 0.25; If ⁇ 0.08; Fe ⁇ 0.10; others ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum.
- the copper content is at least 3.2% by weight.
- the lithium content is preferably between 0.85 and 1.15% by weight and preferably between 0.90 and 1.10% by weight.
- the magnesium content is preferably between 0.20 and 0.6% by weight.
- the simultaneous addition of manganese and zirconium is generally advantageous.
- the manganese content is between 0.20 and 0.50% by weight and the zirconium content is between 0.06 and 0.14% by weight.
- the silver content is between 0.20 and 0.7% by weight. It is advantageous that the silver content is at least 0.1% by weight. In one embodiment of the invention the silver content is at least 0.20% by weight. Preferably, the silver content is at most 0.5% by weight. In one embodiment of the invention, the silver content is limited to 0.3% by weight.
- the silicon content is at most 0.05% by weight and the iron content is at most 0.06% by weight.
- the titanium content is between 0.01 and 0.08% by weight.
- the zinc content is at most 0.15% by weight.
- a preferred aluminum-copper-lithium alloy is AA2050 alloy.
- This liquid metal bath is prepared in a furnace of the casting plant. It is known, for example from US Pat. No. 5,415,220, to use lithium-containing molten salts such as KCl / LiCl mixtures in the melting furnace to passivate the alloy during its transfer to the casting plant.
- the present inventors have obtained excellent fatigue properties for thick plates without using molten salt containing lithium in the melting furnace, but maintaining in this furnace a low oxygen atmosphere and believe that the presence of salt in the furnace Melting furnace could have in some cases a detrimental effect on the fatigue properties of thick wrought products.
- molten salt containing lithium is not used throughout the casting installation. In an advantageous embodiment, no molten salt is used throughout the casting installation.
- an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume is maintained.
- the furnace or furnaces of the casting installation are induction furnaces. The present inventors have found that this type of oven is advantageous despite the stirring generated by the induction heating.
- This bath of liquid metal is then treated with a degassing bag and in a filtration bag so that its hydrogen content is less than 0.4 ml / 100g and preferably less than 0.35 ml / 100g .
- the hydrogen content of the liquid metal is measured using a commercial apparatus such as the apparatus marketed under the tradename ALSCAN TM, known to those skilled in the art, the probe being maintained under a nitrogen sweep.
- the oxygen content of the atmosphere in contact with the liquid metal bath in the melting furnace during the degassing steps, filtration is less than 0.5% by volume and preferably less than 0.3% by volume.
- the oxygen content of the atmosphere in contact with the liquid metal bath is less than 0.5% by volume and preferably less than 0% by volume for the entire casting plant.
- a plate is an aluminum block of substantially parallelepipedic shape, length L, width W and thickness T.
- the atmosphere is controlled above the liquid surface during solidification.
- An example of a device for controlling the atmosphere above the liquid surface during solidification is shown in Figure 2.
- the liquid metal coming from a trough (63) is introduced into a nozzle (4) controlled by a stopper rod (8) which can move upwards and downwards (81), in an ingot mold (31) placed on a false bottom (21).
- the aluminum alloy is solidified by direct cooling (5).
- the aluminum alloy (1) has at least one solid surface (1 1, 12, 13) and at least one liquid surface (14, 15).
- An elevator (2) makes it possible to maintain the level of the liquid surface (14, 15) substantially constant.
- a distributor (7) allows the distribution of the liquid metal.
- a cover (62) covers the liquid surface.
- the cover may include seals (61) for sealing with the casting table (32).
- the liquid metal in the trough (63) can be advantageously protected by a cover (64).
- An inert gas (9) is introduced into the chamber (65) defined between the cover and the pouring table.
- the inert gas is advantageously chosen from rare gases, nitrogen and carbon dioxide or mixtures of these gases.
- a preferred inert gas is argon.
- the oxygen content is measured in the chamber (65) above the liquid surface. The flow of inert gas can be adjusted to achieve the desired oxygen content.
- the suction of the pump (101) is such that the pressure in the enclosure (10) is lower than the pressure in the chamber (65), which can preferably be obtained by imposing a speed of the atmosphere through the open surfaces of the casting well of at least 2 m / s and preferably at least 2.5 m / s.
- the pressure in the chamber (65) is close to atmospheric pressure and the pressure in the chamber (10) is lower than atmospheric pressure, typically 0.95 times the atmospheric pressure.
- the chamber (65) is maintained, thanks to the devices described, with an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume.
- the dispenser according to the invention is made of a fabric essentially comprising carbon, it comprises a lower face (76), an upper face typically vacuum defining the orifice through which the liquid metal is introduced (71) and wall of substantially rectangular cross section typically substantially constant and of height h typically substantially constant, the wall comprising two longitudinal parts parallel to the width W of the plate (720, 721 ) and two transverse parts parallel to the thickness T of the plate (730, 731), said transverse and longitudinal portions being formed of at least two tissues, a first substantially obturating and semi-rigid tissue (77) ensuring the maintenance of the shape of the dispenser during the casting and a second non sealing device (78) for passage and filtration of the liquid, said first and second webs being bonded to one another without overlapping or overlapping and without interstices separating them, said first fabric continuously covering at least 30% of the surface of said wall portions (720, 721, 730, 731) and being positioned so that
- the dispenser is semi-rigid and does not deform substantially during casting.
- the first fabric has a height, hl, measured from the upper face on the circumference of the wall (720, 721, 730, 731) such that h1> 0.3 h and preferably h1> 0, 5 h, where h denotes the total height of the distributor wall.
- the liquid surface being in contact with said first liquid-sealing fabric passes through the dispenser only under the liquid surface in certain directions of each part of the wall.
- the height immersed in the liquid wall metal (720, 721, 730, 731) of the distributor (7) covered by the first fabric is at least 20%, preferably 40% and preferably 60% of the height. total submerged wall.
- Figure 4 shows the bottom and the longitudinal wall portions.
- the bottom (76) is typically covered by the first and / or second fabric.
- the first fabric is at least located in the central part of the bottom (76) along a length L1 and / or in the central part of the longitudinal parts (720) and (721) over the entire height h and over a length L2.
- the surface portion covered by the first fabric is between 30 and 90% and preferably between 50 and 80% for the longitudinal portions (720) and (721), and / or between 30 and 70% and preferably between 40 and 60% for the side parts (730, 731) and / or between 30 and 100% and preferably between 50 and 80% for the bottom (76). It is advantageous if the length L1 of the first tissue located in the bottom (76) is greater than the length L2 of the first tissue situated in the part of the longitudinal walls (720) and (721) in contact with the bottom.
- the present inventors believe that the geometry of the dispenser makes it possible in particular to improve the quality of the flow of the liquid metal, to reduce turbulence and to improve the temperature distribution.
- the first fabric and the second fabric are advantageously obtained by weaving a yarn essentially comprising carbon.
- the weaving of graphite yarn is particularly advantageous.
- the tissues are typically sewn to each other. It is also possible instead of first and second fabrics to use a single diffuser fabric having at least two weaving areas, more or less dense.
- the wire comprising carbon is coated with a layer facilitating sliding.
- This layer may for example comprise a fluorinated polymer such as Teflon or a polyamide such as xylon.
- the first fabric is substantially obturant. Typically it is a fabric having mesh size of less than 0.5 mm, preferably less than 0.2 mm.
- the second fabric is non-sealing and allows the passage of the molten metal. Typically, it is a fabric having mesh sizes of between 1 and 5 mm, preferably 2 to 4 mm.
- the first tissue locally covers the second tissue, while being in intimate contact so as not to leave a gap between the two tissues.
- the plate thus obtained is then transformed to obtain a wrought product.
- the plate thus obtained is then homogenized before or after having been optionally machined to obtain a shape that can be deformed while hot.
- the plate is machined as a rolling plate so as to be hot deformed by rolling.
- the plate is machined as a forging blank so as to be hot deformed by forging.
- the plate is machined in the form of billets so as to then be hot deformed by extrusion.
- the homogenization is carried out at a temperature between 470 and 540 ° C for a period of between 2 and 30 hours.
- the shape thus homogenized is deformed hot and optionally cold so as to obtain a wrought product.
- the heat-forming temperature is advantageously at least 350 ° C and preferably at least 400 ° C.
- the rate of deformation hot and optionally cold that is to say the ratio between the difference between the initial thickness, before deformation but after the possible machining, and the final thickness and on the other hand, the initial thickness is less than 85% and preferably less than 80%. In one embodiment, the deformation rate during the deformation is less than 75% and preferably less than 70%.
- the wrought product thus obtained is then dissolved and quenched.
- the dissolution temperature is advantageously between 470 and 540 ° C and preferably between 490 and 530 ° C and the duration is adapted to the thickness of the product.
- the wrought product thus solubilized is de-tensioned by plastic deformation with a deformation of at least 1%.
- the income is made in one or more steps at a temperature advantageously between 130 and 160 ° C for a period of 5 to 60 hours.
- a metallurgical state T8 such as in particular T851, T83, T84, or T85.
- the wrought products obtained by the process according to the invention have advantageous properties.
- the logarithmic fatigue mean of the wrought products whose thickness is at least 80 mm, obtained by the method according to the invention, measured at mid-thickness in the direction TL on smooth test pieces according to Figure la at a maximum amplitude stress of 242 MPa, a frequency of 50 Hz, a stress ratio R 0.1 is at least 250,000 cycles, advantageously the fatigue property is obtained for the wrought products obtained by the process according to the invention, the thickness of which is at least 100 mm or preferably at least 120 mm or even at least 140 mm.
- the products obtained by the process according to the invention have advantageous static mechanical characteristics.
- wrought products whose thickness is at least 80 mm comprising in% by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element selected from Zr, Mn and Ti, the amount of said element, if selected, being from 0.06 to 0.15% by weight for Zr, O, From 0.5 to 0.8% by weight for Mn and from 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ⁇ 0.25; If ⁇ 0.08; Fe ⁇ 0.10; other ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum, the yield strength measured at quarter-thickness in the direction L is at least 450 MPa and preferably at least 470 MPa and / or the breaking strength measured is at least 480 MPa and preferably at least 500 MPa and / or the elongation is at least 5% and preferably at least 6%.
- the wrought products obtained by the process according to the invention can advantageously be used to produce structural elements, preferably aircraft structural elements.
- Preferred aircraft structural elements are spars, ribs or frames.
- the invention is particularly advantageous for parts of complex shape obtained by integral machining, used in particular for the manufacture of aircraft wings and for any other use for which the properties of the products according to the invention are advantageous. .
- AA2050 alloy plates were prepared. AA2050 alloy plates were cast by direct cooling vertical semi-continuous casting. The alloy was prepared in a melting furnace. For Examples 1 to 7, a KCL / LiCl mixture was used on the surface of the liquid metal in the melting furnace. For Examples 8 to 9 no salt was used in the melting furnace. For Examples 8 to 9 the atmosphere in contact with the liquid metal with an oxygen content of less than 0.3% by volume for the entire casting installation.
- the casting installation included a hood disposed above the pouring well to limit the oxygen content.
- an aspiration (101) was also used such that the pressure in the chamber (10) was lower than the pressure in the chamber (65) and such that the speed of the atmosphere through the open surfaces of the casting well was at least 2 m / s.
- Oxygen content was measured with an oximeter during casting.
- the hydrogen content in the liquid aluminum was measured using an Alscan TM type probe under nitrogen flushing.
- Two types of liquid metal dispensers were used.
- a first "Combo Bag” type dispenser as described for example in Figures 2 to 6 of the international application WO99 / 44719 but made of fabric comprising essentially carbon, referenced below "distributor A" and a second distributor such as described in Figure 3 referenced below “distributor B" is made of graphite wire cloth.
- the plates were homogenized for 12 hours at 505 ° C., machined to a thickness of about 365 mm, hot-rolled to sheets with a final thickness of between 154 and 158 mm, dissolved at 504 ° C. , quenched and relieved by controlled traction with a permanent elongation of 3.5%.
- the sheets thus obtained have an 18 hour income at 155 ° C.
- Static mechanical properties and toughness were characterized at quarter-thickness. Static mechanical characteristics and toughness are given in Table 2.
- the fatigue properties were characterized on smooth test specimens and hole test specimens for some samples taken at mid-thickness.
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Abstract
Description
Procédé de fabrication de produits en alliage d'aluminium - cuivre - lithium à propriétés en fatigue améliorées Process for producing aluminum alloy - copper - lithium products with improved fatigue properties
Domaine de l'invention Field of the invention
L'invention concerne les produits corroyés alliages aluminium - cuivre - lithium, plus particulièrement, de tels produits, leurs procédés de fabrication et d'utilisation, destinés notamment à la construction aéronautique et aérospatiale. The invention relates to wrought products aluminum alloys - copper - lithium, more particularly, such products, their manufacturing processes and use, intended in particular for aeronautical and aerospace construction.
Etat de la technique State of the art
Des produits laminés en alliage d'aluminium sont développés pour produire des éléments structuraux destinés notamment à l'industrie aéronautique et à l'industrie aérospatiale.Aluminum alloy rolled products are developed to produce structural elements for the aerospace industry and the aerospace industry in particular.
Les alliages aluminium - cuivre - lithium sont particulièrement prometteurs pour fabriquer ce type de produit. Les spécifications imposées par l'industrie aéronautique pour la tenue en fatigue sont élevées. Pour les produits épais elles sont particulièrement difficiles à atteindre. En effet compte tenu des épaisseurs possibles des plaques coulées, la réduction d'épaisseur par déformation à chaud est assez faible et par conséquent les sites liés à la coulée sur lesquels s'initient les fissures de fatigue ne voient pas leur taille réduite au cours de la déformation à chaud. Aluminum - copper - lithium alloys are particularly promising for this type of product. The specifications imposed by the aeronautical industry for fatigue performance are high. For thick products they are particularly difficult to reach. Indeed, given the possible thicknesses of the cast slabs, the thickness reduction by hot deformation is quite low and therefore the sites related to the casting on which the fatigue cracks are initiated do not see their reduced size during hot deformation.
Le lithium étant particulièrement oxydable, la coulée des alliages aluminium-cuivre-lithium génère d'une manière générale des sites d'initiation de fissure en fatigue plus nombreux que pour les alliages de type 2XXX sans lithium ou 7XXX. Ainsi les solutions habituellement trouvées pour l'obtention de produits laminés épais en alliages de type 2XXX sans lithium ou 7XXX ne permettent pas d'obtenir des propriétés en fatigue suffisantes pour les alliages aluminium - cuivre - lithium. Since lithium is particularly oxidizable, the casting of aluminum-copper-lithium alloys generally generates more fatigue crack initiation sites than for 2XXX lithium-free or 7XXX-type alloys. Thus the solutions usually found for obtaining thick rolled products of 2XXX type alloys without lithium or 7XXX do not make it possible to obtain sufficient fatigue properties for aluminum-copper-lithium alloys.
Des produits épais en alliage Al-Cu-Li sont notamment décrits dans les demandes US2005/0006008 et US2009/0159159. Dans la demande WO2012/110717, il est proposé pour améliorer les propriétés, notamment en fatigue, des alliages d'aluminium contenant en particulier au moins 0,1 % de Mg et/ou 0,1 % de Li de réaliser lors de la coulée un traitement ultrason. Cependant ce type de traitement reste difficile à effectuer pour les quantités nécessaires à la fabrication de tôles épaisses. Thick products of Al-Cu-Li alloy are described in particular in applications US2005 / 0006008 and US2009 / 0159159. In the application WO2012 / 110717, it is proposed to improve the properties, especially in fatigue, aluminum alloys containing in particular at least 0.1% Mg and / or 0.1% Li to achieve during casting an ultrasound treatment. However, this type of treatment remains difficult to perform for the quantities necessary for the manufacture of thick plates.
Il existe un besoin pour des produits épais en alliage aluminium - cuivre - lithium présentant des propriétés améliorées par rapport à celles des produits connus, en particulier en termes de propriétés en fatigue tout en ayant des propriétés de ténacité et des propriétés de résistance mécanique statique avantageuses. Par ailleurs il existe un besoin pour un procédé simple et économique d'obtention de ces produits. There is a need for thick aluminum-copper-lithium alloy products having improved properties over those of the known products, particularly in terms of fatigue properties while having advantageous toughness properties and static strength properties. . Moreover, there is a need for a simple and economical method of obtaining these products.
Objet de l'inveution Object of the inveution
Un premier objet de l'invention est un procédé de fabrication d'un produit en alliage d'aluminium comprenant les étapes dans lequelles A first object of the invention is a method of manufacturing an aluminum alloy product comprising the steps in which
(a) on élabore un bain de métal liquide en alliage comprenant, en % en poids, Cu : 2,0 - 6,0 ; Li : 0,5 - 2,0 ; Mg : 0- 1,0 ; Ag : 0 - 0,7 ; Zn 0 - 1,0 ; et au moins un élément choisi parmi Zr, Mn, Cr, Se, Hf et Ti, la quantité dudit élément, s'il est choisi, étant de 0,05 à 0,20 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn, 0,05 à 0,3 % en poids pour Cr et pour Se, 0,05 à 0,5 % en poids pour Hf et de 0,01 à 0, 15 % en poids pour Ti, Si < 0, 1 ; Fe < 0, 1 ; autres < 0,05 chacun et < 0,15 au total, (a) forming an alloy molten metal bath comprising, in% by weight, Cu: 2.0 - 6.0; Li: 0.5 - 2.0; Mg: 0-1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one member selected from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if selected, being from 0.05 to 0.20% by weight for Zr, 0.05 to 0 , 8% by weight for Mn, 0.05 to 0.3% by weight for Cr and for Se, 0.05 to 0.5% by weight for Hf and from 0.01 to 0.15% by weight for Ti , Si <0, 1; Fe <0, 1; others <0.05 each and <0.15 in total,
(b) on coule ledit alliage par coulée semi-continue verticale pour obtenir une plaque d'épaisseur T et de largeur W de telle façon que, lors de la solidification, (b) pouring said alloy by vertical semi-continuous casting to obtain a plate of thickness T and width W such that, during solidification,
- la teneur en hydrogène dudit bain de métal liquide (1) soit inférieure à 0,4 ml/ 100g, - la teneur en oxygène mesurée au-dessus de la surface liquide (14,15) soit inférieure à 0,5 % en volume, the hydrogen content of said liquid metal bath (1) is less than 0.4 ml / 100 g, the oxygen content measured above the liquid surface (14, 15) is less than 0.5% by volume ,
- le distributeur utilisé (7) pour la coulée soit réalisé en tissu comprenant essentiellement du carbone, qu'il comprenne une face inférieure (76), une face supérieure définissant l'orifice par lequel le métal liquide est introduit (71) et une paroi de section substantiellement rectangulaire, la paroi comprenant deux parties longitudinales parallèles à la largeur W (720, 721) et deux parties transversales parallèles à l'épaisseur T (730, 731) lesdites parties transversales et longitudinales étant formées d'au moins deux tissus, un premier tissu sensiblement obturant et semi-rigide (77) assurant le maintien de la forme du distributeur pendant la coulée et un second tissu non obturant (78) permettant le passage et la filtration du liquide, lesdits premier et deuxième tissu étant liés l'un à l'autre sans recouvrement ou avec recouvrement et sans interstice les séparant, ledit premier tissu couvrant de façon continue au moins 30 % de la surface desdites parties de paroi (720,721 , 730, 731) et étant positionné de manière à ce que la surface liquide soit en contact avec lui sur l'ensemble de la section. the distributor used (7) for the casting is made of fabric comprising essentially carbon, that it comprises a lower face (76), an upper face defining the orifice through which the liquid metal is introduced (71) and a wall; of substantially rectangular section, the wall comprising two longitudinal parts parallel to the width W (720, 721) and two transverse parts parallel to the thickness T (730, 731) said portions transverse and longitudinal being formed of at least two tissues, a first substantially obturating and semi-rigid tissue (77) ensuring the maintenance of the dispenser shape during casting and a second non-sealing fabric (78) allowing the passage and filtration liquid, said first and second webs being bonded to each other without overlapping or overlapping and without gap between them, said first fabric continuously covering at least 30% of the area of said wall portions (720,721, 730 731) and being positioned so that the liquid surface is in contact with it over the entire section.
Un autre objet de l'invention est un distributeur destiné à la coulée semi-continue de plaques en alliage d'aluminium en tissu comprenant essentiellement du carbone, comprennant une face inférieure (76), une face supérieure définissant l'orifice par lequel le métal liquide est introduit (71) et une paroi de section substantiellement rectangulaire, la paroi comprenant deux parties longitudinales parallèles à la largeur W (720, 721) et deux parties transversales parallèles à l'épaisseur T (730, 731) lesdites parties transversales et longitudinales étant formées d'au moins deux tissus, un premier tissu sensiblement obturant et semi-rigide (77) assurant le maintien de la forme du distributeur pendant la coulée et un second tissu non obturant (78) permettant le passage et la filtration du liquide, lesdits premier et deuxième tissu étant liés l'un à l'autre sans recouvrement ou avec recouvrement et sans interstice les séparant, ledit premier tissu couvrant de façon continue au moins 30 % de la surface desdites parties de paroi (720,721, 730, 731) et étant positionné de manière à ce que la surface liquide soit en contact avec lui sur l'ensemble de la section. Another object of the invention is a dispenser for the semi-continuous casting of fabric aluminum alloy plates comprising essentially carbon, comprising a lower face (76), an upper face defining the orifice through which the metal liquid is introduced (71) and a wall of substantially rectangular section, the wall comprising two longitudinal portions parallel to the width W (720, 721) and two transverse portions parallel to the thickness T (730, 731) said transverse and longitudinal portions being formed of at least two fabrics, a first substantially obturating and semi-rigid fabric (77) ensuring the maintenance of the shape of the dispenser during casting and a second non-sealing fabric (78) permitting the passage and filtration of the liquid, said first and second webs being bonded to one another without overlapping or overlapping and without interstices separating them, said first web covering continuously at least 30% of the area of said wall portions (720, 721, 730, 731) being positioned so that the liquid surface is in contact therewith throughout the section.
Description des figures Description of figures
La Figure 1 est le schéma des éprouvettes utilisées pour les essais en fatigue lisse (Fig la) et en fatigue à trou (Fig lb). Les dimensions sont données en mm. Figure 1 is the diagram of the test pieces used for the tests in smooth fatigue (Fig la) and in fatigue with hole (Fig lb). Dimensions are given in mm.
La Figure 2 est un schéma général du dispositif de solidification utilisé dans un mode de réalisation de l'invention. Figure 2 is a general diagram of the solidification device used in one embodiment of the invention.
La Figure 3 est un schéma général du distributeur utilisé dans le procédé selon l'invention. La Figure 4 présente des représentations du fond et des parties latérales et longitudinales de la paroi du distributeur selon un mode de réalisation de l'invention. Figure 3 is a general diagram of the dispenser used in the process according to the invention. Figure 4 shows representations of the bottom and the lateral and longitudinal parts of the distributor wall according to one embodiment of the invention.
La Figure 5 montre la relation entre la performance en fatigue lisse et la teneur en hydrogène du bain de métal liquide lors de la solidification (Fig 5 a) ou la teneur en oxygène mesurée au-dessus de la surface liquide lors de la solidification (Fig. 5b). Figure 5 shows the relationship between the smooth fatigue performance and the hydrogen content of the liquid metal bath during solidification (Fig. 5a) or the oxygen content measured above the liquid surface during solidification (Fig. 5b).
La Figure 6 montre les courbes de Wôhler obtenues avec les essais 3, 7 et 8 dans la direction L-T (Figure 6a) et T-L (figure 6b). Figure 6 shows the Wohler curves obtained with tests 3, 7 and 8 in the direction L-T (Figure 6a) and T-L (Figure 6b).
Description de l'invention Description of the invention
Sauf mention contraire, toutes les indications concernant la composition chimique des alliages sont exprimées comme un pourcentage en poids basé sur le poids total de l'alliage. L'expression 1,4 Cu signifie que la teneur en cuivre exprimée en % en poids est multipliée par 1,4. La désignation des alliages se fait en conformité avec les règlements de The Aluminium Association, connus de l'homme du métier. Sauf mention contraire les définitions des états métallurgiques indiquées dans la norme européenne EN 515 s'appliquent. Unless stated otherwise, all the information concerning the chemical composition of the alloys is expressed as a percentage by weight based on the total weight of the alloy. The expression 1.4 Cu means that the copper content expressed in% by weight is multiplied by 1.4. The designation of alloys is in accordance with the regulations of The Aluminum Association, known to those skilled in the art. Unless otherwise stated, the definitions of the metallurgical states given in the European standard EN 515 apply.
Les caractéristiques mécaniques statiques en traction, en d'autres termes la résistance à la rupture Rm, la limite d'élasticité conventionnelle à 0,2% d'allongement Rp0,2, et l'allongement à la rupture A%, sont déterminés par un essai de traction selon la norme NF EN ISO 6892-1, le prélèvement et le sens de l'essai étant définis par la norme EN 485-1. Les propriétés en fatigue sur éprouvettes lisses sont mesurées à l'air ambiant à une contrainte d'amplitude maximale de 242 MPa, une fréquence de 50 Hz, un rapport de contrainte R = 0,1, sur des éprouvettes telles que représentées sur la Figure la, prélevées à mi-largeur et à mi-épaisseur des tôles dans la direction TL. Les conditions de test obéissent à la norme ASTM E466. On détermine la moyenne logarithmique des résultats obtenus sur au moins 4 éprouvettes. The static mechanical characteristics in tension, in other words the tensile strength R m , the conventional yield stress at 0.2% elongation R p0.2 , and the elongation at break A% are determined by a tensile test according to standard NF EN ISO 6892-1, the sampling and the direction of the test being defined by the EN 485-1 standard. The fatigue properties on smooth specimens are measured in ambient air at a maximum amplitude stress of 242 MPa, a frequency of 50 Hz, a stress ratio R = 0.1, on specimens as shown in FIG. la, taken at mid-width and at mid-thickness of the sheets in the direction TL. The test conditions follow the ASTM E466 standard. The logarithmic average of the results obtained on at least 4 test pieces is determined.
Les propriétés en fatigue sur éprouvettes à trou sont mesurées à l'air ambiant pour des niveaux de contrainte variables, à une fréquence de 50 Hz, un rapport de contrainte R = 0,1, sur des éprouvettes telles que représentées sur la Figure lb, Kt = 2,3, prélevées au centre et à mi-épaisseur des tôles dans la direction L-T et T-L. L'équation de Walker a été utilisée pour déterminer une valeur de contrainte maximale représentative de 50 % de non rupture à 100 000 cycles. Pour ce faire un indice de qualité fatigue (IQF) est calculé pour chaque point de la courbe de Wôhler avec la formule The fatigue properties on hole specimens are measured in the ambient air for variable stress levels, at a frequency of 50 Hz, a stress ratio R = 0.1, on specimens as shown in FIG. K t = 2,3, taken at the center and at mid-thickness of the sheets in the direction LT and TL. Walker's equation was used to determine a maximum stress value representative of 50% of non-rupture at 100,000 cycles. To do this a fatigue quality index (IQF) is calculated for each point of the Wôhler curve with the formula
où amax est la contrainte maximale appliquée à un échantillon donné, N est le nombre de cycles jusqu'à la rupture, N0 est égale à 100 000 et n = -4,5. On rapporte l'IQF correspondant à la médiane, soit 50% rupture pour 100 000 cycles. where a max is the maximum stress applied to a given sample, N is the number of cycles to failure, N 0 is equal to 100,000 and n = -4.5. The IQF corresponding to the median is reported, ie 50% rupture per 100,000 cycles.
Dans le cadre de l'invention, un produit corroyé épais est un produit dont l'épaisseur est au moins 6 mm. De préférence l'épaisseur des produits selon l'invention est au moins 80 mm et de manière préférée au moins 100 mm. Dans un mode de réalisation de l'invention l'épaisseur des produits corroyés est au moins 120 mm ou de préférence 140 mm. L'épaisseur des produits épais selon l'invention est typiquement au plus de 240 mm, généralement au plus de 220 mm et préférentiellement au plus de 180 mm. In the context of the invention, a thick wrought product is a product whose thickness is at least 6 mm. Preferably the thickness of the products according to the invention is at least 80 mm and preferably at least 100 mm. In one embodiment of the invention the thickness of the wrought products is at least 120 mm or preferably 140 mm. The thickness of the thick products according to the invention is typically at most 240 mm, generally at most 220 mm and preferably at most 180 mm.
Sauf mention contraire, les définitions de la norme EN 12258 s'appliquent. Notamment, une tôle est selon l'invention un produit laminé de section transversale rectangulaire dont l'épaisseur uniforme est au moins de 6 mm et n'excède pas l/10ème de la largeur. Unless otherwise specified, the definitions of EN 12258 apply. In particular, a sheet is according to the invention a laminated product of rectangular cross section whose uniform thickness is at least 6 mm and does not exceed 1 / 10th of the width.
On appelle ici « élément de structure » ou « élément structural » d'une construction mécanique une pièce mécanique pour laquelle les propriétés mécaniques statiques et/ou dynamiques sont particulièrement importantes pour la performance de la structure, et pour laquelle un calcul de structure est habituellement prescrit ou réalisé. Il s'agit typiquement d'éléments dont la défaillance est susceptible de mettre en danger la sécurité de ladite construction, de ses utilisateurs, de ses usagers ou d' autrui. Pour un avion, ces éléments de structure comprennent notamment les éléments qui composent le fuselage (tels que la peau de fuselage (fuselage skin en anglais), les raidisseurs ou lisses de fuselage (stringers), les cloisons étanches (bulkheads), les cadres de fuselage (circumferential frames), les ailes (tels que la peau de voilure (wing skin), les raidisseurs (stringers ou stiffeners), les nervures (ribs) et longerons (spars)) et l'empennage composé notamment de stabilisateurs horizontaux et verticaux (horizontal or vertical stabilisers), ainsi que les profilés de plancher (floor beams), les rails de sièges (seat tracks) et les portes. Here, a "structural element" or "structural element" of a mechanical construction is called a mechanical part for which the static and / or dynamic mechanical properties are particularly important for the performance of the structure, and for which a structural calculation is usually prescribed or realized. These are typically elements whose failure is likely to endanger the safety of said construction, its users, its users or others. For an aircraft, these structural elements include the elements that make up the fuselage (such as fuselage skin (fuselage skin in English), stiffeners or stringers, bulkheads, fuselage (circumferential frames), the wings (such as the wing skin), the stiffeners (stringers or stiffeners), the ribs (ribs) and spars) and the empennage composed in particular of stabilizers Horizontal and vertical (horizontal or vertical stabilizers), as well as floor beams, seat rails and doors.
On appelle ici « ensemble de l'installation de coulée » l'ensemble des dispositifs permettant de transformer un métal sous forme quelconque en demi-produit de forme brute en passant par la phase liquide. Une installation de coulée peut comprendre de nombreux dispositifs tels que un ou plusieurs fours nécessaires à la fusion du métal (« four de fusion ») et/ou à son maintien (« four de maintien ») en température et/ou à des opérations de préparation du métal liquide et d'ajustement de la composition (« four d'élaboration »), une ou plusieurs cuves (ou « poches ») destinées à effectuer un traitement d'élimination des impuretés dissoutes et/ou en suspension dans le métal liquide, ce traitement pouvant consister à filtrer le métal liquide sur un média filtrant dans une « poche de filtration » ou à introduire dans le bain un gaz dit « de traitement » pouvant être inerte ou réactif dans une « poche de dégazage », un dispositif de solidification du métal liquide (ou « métier de coulée »), par coulée semi-continue verticale par refroidissement direct dans un puits de coulée, pouvant comprendre des dispositifs tels que un moule (ou « lingotière ») un dispositif d'approvisionnement du métal liquide (ou « busette ») et un système de refroidissement, ces différents fours, cuves et dispositifs de solidification étant reliés entre eux par des dispositifs de transfert ou chenaux appelés « goulottes » dans lesquels le métal liquide peut être transporté. The term "set of the casting plant" is here referred to as the set of devices making it possible to transform a metal in any form into a semi-product of raw form via the liquid phase. A casting plant may include a number of devices such as one or more ovens required for melting the metal ("melting furnace") and / or maintaining it ("holding furnace") in temperature and / or preparation of the liquid metal and adjustment of the composition ("preparation furnace"), one or more tanks (or "pockets") intended to carry out a treatment for the removal of impurities dissolved and / or suspended in the liquid metal this treatment may consist of filtering the liquid metal on a filter medium in a "filtration bag" or introducing into the bath a so-called "treatment" gas that can be inert or reactive in a "degassing bag", a device for solidification of the liquid metal (or "casting loom") by vertical semi-continuous casting by direct cooling in a casting well, which may comprise devices such as a mold (or "mold") a liquid metal supply device (or "nozzle") and a cooling system, these different furnaces, tanks and solidification devices being interconnected by transfer devices or channels called "chutes" in which the liquid metal can to be transported.
Les présents inventeurs ont constaté que de manière surprenante on peut obtenir des produits corroyés épais en alliage aluminium cuivre lithium présentant une performance en fatigue améliorée en préparant ces tôles à l'aide du procédé suivant. The present inventors have found that, surprisingly, thick wrought products of copper lithium aluminum alloy with improved fatigue performance can be obtained by preparing these sheets by the following method.
Dans une première étape on élabore un bain de métal liquide en alliage comprenant, en % en poids Cu : 2,0 - 6,0 ; Li : 0,5 - 2,0 ; Mg : 0- 1,0 ; Ag : 0 - 0,7 ; Zn 0 - 1,0 ; et au moins un élément choisi parmi Zr, Mn, Cr, Se, Hf et Ti, la quantité dudit élément, s'il est choisi, étant de 0,05 à 0,20 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn, 0,05 à 0,3 % en poids pour Cr et pour Se, 0,05 à 0,5 % en poids pour Hf et de 0,01 à 0,15 % en poids pour Ti, Si < 0,1 ; Fe < 0,1; autres < 0,05 chacun et < 0,15 au total, reste aluminium. In a first step, an alloy liquid metal bath comprising, in% by weight Cu: 2.0 - 6.0; Li: 0.5 - 2.0; Mg: 0-1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one member selected from Zr, Mn, Cr, Se, Hf and Ti, the amount of said element, if selected, being from 0.05 to 0.20% by weight for Zr, 0.05 to 0 , 8% by weight for Mn, 0.05 to 0.3% by weight for Cr and for Se, 0.05 to 0.5% by weight for Hf and from 0.01 to 0.15% by weight for Ti , Si <0,1; Fe <0.1; others <0.05 each and <0.15 in total, remains aluminum.
Un alliage avantageux pour le procédé selon l'invention comprend, en % en poids, Cu : 3,0 - 3,9 ; Li : 0,7 - 1,3 ; Mg : 0,1 - 1,0, au moins un élément choisi parmi Zr, Mn et Ti, la quantité dudit élément, s'il est choisi, étant de 0,06 à 0,15 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn et de 0,01 à 0,15 % en poids pour Ti ; Ag : 0 - 0,7 ; Zn < 0,25 ; Si < 0,08 ; Fe < 0,10 ; autres < 0,05 chacun et < 0,15 au total, reste aluminium. An advantageous alloy for the process according to the invention comprises, in% by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element selected from Zr, Mn and Ti, the amount of said element, if selected, being from 0.06 to 0.15% by weight for Zr, 0.05 to 0.8% by weight for Mn and from 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn <0.25; If <0.08; Fe <0.10; others <0.05 each and <0.15 in total, remains aluminum.
Avantageusement la teneur en cuivre est au moins de 3,2 % en poids. La teneur en lithium est de préférence comprise entre 0,85 et 1,15 % en poids et de préférence entre 0,90 et 1,10 % en poids. La teneur en magnésium est de préférence comprise entre 0,20 et 0,6 % en poids. L'addition simultanée de manganèse et de zirconium est généralement avantageuse. De façon préférée la teneur en manganèse est comprise entre 0,20 et 0,50 % en poids et la teneur en zirconium est comprise entre 0,06 et 0,14 % en poids. Avantageusement la teneur en argent est comprise entre 0,20 et 0,7 % en poids. Il est avantageux que la teneur en argent soit au moins 0,1 % en poids. Dans un mode de réalisation de l'invention la teneur en argent est au moins 0,20 % en poids. Préférentiellement la teneur en argent est au plus 0,5 % en poids. Dans un mode de réalisation de l'invention la teneur en argent est limitée à 0,3 % en poids. Préférentiellement la teneur en silicium est au plus de 0,05 % en poids et la teneur en fer est au plus de 0,06 % en poids. Avantageusement la teneur en titane est comprise entre 0,01 et 0,08 % en poids. Dans un mode de réalisation de l'invention la teneur en zinc est au plus de 0,15 % en poids. Advantageously, the copper content is at least 3.2% by weight. The lithium content is preferably between 0.85 and 1.15% by weight and preferably between 0.90 and 1.10% by weight. The magnesium content is preferably between 0.20 and 0.6% by weight. The simultaneous addition of manganese and zirconium is generally advantageous. Preferably, the manganese content is between 0.20 and 0.50% by weight and the zirconium content is between 0.06 and 0.14% by weight. Advantageously, the silver content is between 0.20 and 0.7% by weight. It is advantageous that the silver content is at least 0.1% by weight. In one embodiment of the invention the silver content is at least 0.20% by weight. Preferably, the silver content is at most 0.5% by weight. In one embodiment of the invention, the silver content is limited to 0.3% by weight. Preferably, the silicon content is at most 0.05% by weight and the iron content is at most 0.06% by weight. Advantageously, the titanium content is between 0.01 and 0.08% by weight. In one embodiment of the invention, the zinc content is at most 0.15% by weight.
Un alliage aluminium-cuivre-lithium préféré est l'alliage AA2050. A preferred aluminum-copper-lithium alloy is AA2050 alloy.
Ce bain de métal liquide est préparé dans un four de l'installation de coulée. Il est connu, par exemple de US 5,415,220 d'utiliser des sels fondus contenant du lithium tels que des mélanges KCl/LiCl dans le four de fusion pour passiver l'alliage lors de son transfert vers l'installation de coulée. Les présents inventeurs ont cependant obtenu d'excellentes propriétés de fatigue pour des tôles épaisses sans utiliser de sel fondu contenant du lithium dans le four de fusion, mais en maintenant dans ce four une atmosphère pauvre en oxygène et pensent que la présence de sel dans le four de fusion pourrait avoir dans certains cas un effet néfaste sur les propriétés en fatigue des produits corroyés épais. Avantageusement, on n'utilise pas de sel fondu contenant du lithium dans l'ensemble de l'installation de coulée. Dans un mode de réalisation avantageux on n'utilise pas de sel fondu dans l'ensemble de l'installation de coulée. Préférentiellement on maintient dans le ou les fours de l'installation de coulée une teneur en oxygène inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume. Cependant on peut tolérer une teneur en oxygène d'au moins 0,05 % en volume et même d'au moins 0,1 % en volume dans le ou les fours de l'installation de coulée, ce qui est avantageux notamment pour les aspects économiques du procédé. Avantageusement le ou les fours de l'installation de coulée sont des fours à induction. Les présents inventeurs ont constaté que ce type de four est avantageux malgré le brassage généré par le chauffage par induction. This liquid metal bath is prepared in a furnace of the casting plant. It is known, for example from US Pat. No. 5,415,220, to use lithium-containing molten salts such as KCl / LiCl mixtures in the melting furnace to passivate the alloy during its transfer to the casting plant. The present inventors, however, have obtained excellent fatigue properties for thick plates without using molten salt containing lithium in the melting furnace, but maintaining in this furnace a low oxygen atmosphere and believe that the presence of salt in the furnace Melting furnace could have in some cases a detrimental effect on the fatigue properties of thick wrought products. Advantageously, molten salt containing lithium is not used throughout the casting installation. In an advantageous embodiment, no molten salt is used throughout the casting installation. Preferably, in the furnace or furnaces of the casting installation, an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume is maintained. However one can tolerate an oxygen content at least 0.05% by volume and even at least 0.1% by volume in the furnace (s) of the casting plant, which is advantageous especially for the economic aspects of the process. Advantageously, the furnace or furnaces of the casting installation are induction furnaces. The present inventors have found that this type of oven is advantageous despite the stirring generated by the induction heating.
Ce bain de métal liquide est ensuite traité avec dans une poche de dégazage et dans une poche de filtration de façon notamment à ce que sa teneur en hydrogène soit inférieure à 0,4 ml/100g et de préférence inférieure à 0,35 ml/100g. La teneur en hydrogène du métal liquide est mesurée à l'aide d'un appareillage commercial tel que l'appareil commercialisé sous la marque ALSCAN™, connu de l'homme du métier, la sonde étant maintenue sous un balayage d'azote. Avantageusement la teneur en oxygène de l'atmosphère en contact avec le bain de métal liquide dans le four de fusion lors des étapes de dégazage, filtration est inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume. De préférence, la teneur en oxygène de l'atmosphère en contact avec le bain de métal liquide est inférieure est inférieure à 0,5 % en volume et de préférence inférieure à 0 % en volume pour l'ensemble de l'installation de coulée. Cependant on peut tolérer une teneur en oxygène d'au moins 0,05 % en volume et même d'au moins 0,1 % en volume pour l'ensemble de l'installation de coulée ce qui est avantageux notamment pour les aspects économiques du procédé. This bath of liquid metal is then treated with a degassing bag and in a filtration bag so that its hydrogen content is less than 0.4 ml / 100g and preferably less than 0.35 ml / 100g . The hydrogen content of the liquid metal is measured using a commercial apparatus such as the apparatus marketed under the tradename ALSCAN ™, known to those skilled in the art, the probe being maintained under a nitrogen sweep. Advantageously, the oxygen content of the atmosphere in contact with the liquid metal bath in the melting furnace during the degassing steps, filtration is less than 0.5% by volume and preferably less than 0.3% by volume. Preferably, the oxygen content of the atmosphere in contact with the liquid metal bath is less than 0.5% by volume and preferably less than 0% by volume for the entire casting plant. However, it is possible to tolerate an oxygen content of at least 0.05% by volume and even at least 0.1% by volume for the entire casting plant, which is advantageous especially for the economic aspects of the casting. process.
Le bain de métal liquide est ensuite solidifié sous forme de plaque. Une plaque est un bloc d'aluminium de forme substantiellement parallélépipédique, de longueur L, de largeur W et d'épaisseur T. On contrôle l'atmosphère au-dessus de la surface liquide lors de la solidification. Un exemple de dispositif permettant de contrôler l'atmosphère au-dessus de la surface liquide lors de la solidification est présenté sur la Figure 2. The liquid metal bath is then solidified in the form of a plate. A plate is an aluminum block of substantially parallelepipedic shape, length L, width W and thickness T. The atmosphere is controlled above the liquid surface during solidification. An example of a device for controlling the atmosphere above the liquid surface during solidification is shown in Figure 2.
Dans cet exemple de dispositif approprié, le métal liquide provenant d'une goulotte (63) est introduit dans une busette (4) contrôlée par une quenouille (8) pouvant se déplacer vers le haut et vers le bas (81), dans une lingotière (31) placée sur un faux fond (21). L'alliage d'aluminium est solidifié par refroidissement direct (5). L'alliage d'aluminium (1) a au moins une surface solide (1 1, 12, 13) et au moins une surface liquide (14, 15). Un ascenseur (2) permet de maintenir le niveau de la surface liquide (14, 15) sensiblement constant. Un distributeur (7) permet la répartition du métal liquide. Un couvercle (62) recouvre la surface liquide. Le couvercle peut comprendre des joints (61) pour assurer une étanchéité avec la table de coulée (32). Le métal liquide dans la goulotte (63) peut être avantageusement protégé par un couvercle (64). Un gaz inerte (9) est introduit dans la chambre (65) définie entre le couvercle et la table de coulée. Le gaz inerte est avantageusement choisi parmi les gaz rares, l'azote et le dioxyde de carbone ou des mélanges de ces gaz. Un gaz inerte préféré est l'argon. La teneur en oxygène est mesurée dans la chambre (65) au-dessus de la surface liquide. Le débit de gaz inerte peut être ajusté pour atteindre la teneur en oxygène désirée. Cependant il est avantageux de maintenir une aspiration suffisante dans le puits de coulée (10) grâce à une pompe (101). En effet les présents inventeurs ont constaté qu'il n'existe pas en général une étanchéité suffisante entre la lingotière (31) et le métal solidifié (5) ce qui conduit à une diffusion de l'atmosphère du puits de coulée (10) vers la chambre (65). Avantageusement l'aspiration de la pompe (101) est telle que la pression dans l'enceinte (10) soit inférieure à la pression dans la chambre (65), ce qui est peut être obtenu de préférence en imposant une vitesse de l'atmosphère au travers des surfaces ouvertes du puits de coulée d'au moins de 2 m/s et de préférence d'au moins de 2,5 m/s. Typiquement la pression dans la chambre (65) est proche de la pression atmosphérique et la pression dans l'enceinte (10) est inférieure à la pression atmosphérique, typiquement 0,95 fois la pression atmosphérique. Dans le cadre du procédé selon l'invention, on maintient dans la chambre (65), grâce aux dispositifs décrits, une teneur en oxygène inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume. In this example of a suitable device, the liquid metal coming from a trough (63) is introduced into a nozzle (4) controlled by a stopper rod (8) which can move upwards and downwards (81), in an ingot mold (31) placed on a false bottom (21). The aluminum alloy is solidified by direct cooling (5). The aluminum alloy (1) has at least one solid surface (1 1, 12, 13) and at least one liquid surface (14, 15). An elevator (2) makes it possible to maintain the level of the liquid surface (14, 15) substantially constant. A distributor (7) allows the distribution of the liquid metal. A cover (62) covers the liquid surface. The cover may include seals (61) for sealing with the casting table (32). The liquid metal in the trough (63) can be advantageously protected by a cover (64). An inert gas (9) is introduced into the chamber (65) defined between the cover and the pouring table. The inert gas is advantageously chosen from rare gases, nitrogen and carbon dioxide or mixtures of these gases. A preferred inert gas is argon. The oxygen content is measured in the chamber (65) above the liquid surface. The flow of inert gas can be adjusted to achieve the desired oxygen content. However, it is advantageous to maintain sufficient suction in the casting well (10) by means of a pump (101). Indeed the present inventors have found that there is generally no sufficient seal between the mold (31) and the solidified metal (5) which leads to a diffusion of the atmosphere of the casting well (10) to the room (65). Advantageously, the suction of the pump (101) is such that the pressure in the enclosure (10) is lower than the pressure in the chamber (65), which can preferably be obtained by imposing a speed of the atmosphere through the open surfaces of the casting well of at least 2 m / s and preferably at least 2.5 m / s. Typically the pressure in the chamber (65) is close to atmospheric pressure and the pressure in the chamber (10) is lower than atmospheric pressure, typically 0.95 times the atmospheric pressure. In the context of the process according to the invention, the chamber (65) is maintained, thanks to the devices described, with an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume.
Un exemple de distributeur (7) du procédé selon l'invention est présenté sur les figures 3 et 4. Le distributeur selon l'invention est réalisé en tissu comprenant essentiellement du carbone, il comprend une face inférieure (76), une face supérieure typiquement vide définissant l'orifice par lequel le métal liquide est introduit (71) et paroi de section substantiellement rectangulaire typiquement substantiellement constante et de hauteur h typiquement substantiellement constante, la paroi comprenant deux parties longitudinales parallèles à la largeur W de la plaque (720, 721) et deux parties transversales parallèles à l'épaisseur T de la plaque (730, 731) lesdites parties transversales et longitudinales étant formées d'au moins deux tissus, un premier tissu sensiblement obturant et semi-rigide (77) assurant le maintien de la forme du distributeur pendant la coulée et un second tissu non obturant (78) permettant le passage et la filtration du liquide, lesdits premier et deuxième tissu étant liés l'un à l'autre sans recouvrement ou avec recouvrement et sans interstice les séparant, ledit premier tissu couvrant de façon continue au moins 30 % de la surface desdites parties de paroi (720,721, 730, 731) et étant positionné de manière à ce que la surface liquide soit en contact avec lui sur l'ensemble de la section du distributeur. Les premier et deuxième tissus étant cousus l'un à l'autre sans recouvrement ou avec recouvrement et sans interstice les séparant, c'est-à-dire en contact, le métal liquide ne peut pas traverser le premier tissu et être dévié par le second tissu comme c'est le cas par exemple dans un combo-bag tel que décrit dans la demande WO 99/44719 Fig 2 à 5. Grâce au maintien assuré par le premier tissu, le distributeur est semi-rigide et ne se déforme pas sensiblement lors de la coulée. Dans une réalisation avantageuse le premier tissu a une hauteur, hl, mesurée à partir de la face supérieure sur la circonférence de la paroi (720, 721, 730, 731) telle que hl > 0,3 h et de préférence hl > 0,5 h, où h désigne la hauteur totale de la paroi du distributeur. An example of a dispenser (7) of the process according to the invention is shown in FIGS. 3 and 4. The dispenser according to the invention is made of a fabric essentially comprising carbon, it comprises a lower face (76), an upper face typically vacuum defining the orifice through which the liquid metal is introduced (71) and wall of substantially rectangular cross section typically substantially constant and of height h typically substantially constant, the wall comprising two longitudinal parts parallel to the width W of the plate (720, 721 ) and two transverse parts parallel to the thickness T of the plate (730, 731), said transverse and longitudinal portions being formed of at least two tissues, a first substantially obturating and semi-rigid tissue (77) ensuring the maintenance of the shape of the dispenser during the casting and a second non sealing device (78) for passage and filtration of the liquid, said first and second webs being bonded to one another without overlapping or overlapping and without interstices separating them, said first fabric continuously covering at least 30% of the surface of said wall portions (720, 721, 730, 731) and being positioned so that the liquid surface is in contact with it over the entire section of the dispenser. The first and second fabrics being sewn together without overlapping or overlapping and without interstices separating them, i.e., in contact, the liquid metal can not pass through the first fabric and be deflected by the second fabric as is the case for example in a combo-bag as described in the application WO 99/44719 Fig 2 to 5. Thanks to the maintenance provided by the first fabric, the dispenser is semi-rigid and does not deform substantially during casting. In an advantageous embodiment, the first fabric has a height, hl, measured from the upper face on the circumference of the wall (720, 721, 730, 731) such that h1> 0.3 h and preferably h1> 0, 5 h, where h denotes the total height of the distributor wall.
La surface liquide étant en contact avec ledit premier tissu obturant le métal liquide ne traverse le distributeur que sous la surface liquide dans certaines directions de chaque partie de la paroi. De préférence la hauteur immergée dans le métal liquide de paroi (720, 721, 730, 731) du distributeur (7) couverte par le premier tissu est au moins égale à 20 %, préférentiellement 40 % et de manière préférée 60 % de la hauteur totale de paroi immergée. The liquid surface being in contact with said first liquid-sealing fabric passes through the dispenser only under the liquid surface in certain directions of each part of the wall. Preferably the height immersed in the liquid wall metal (720, 721, 730, 731) of the distributor (7) covered by the first fabric is at least 20%, preferably 40% and preferably 60% of the height. total submerged wall.
La figure 4 représente le fond et les parties de paroi longitudinales. Le fond (76) est typiquement couvert par le premier et/ou le second tissu. Avantageusement le premier tissu est au moins situé dans la partie centrale du fond (76) sur une longueur Ll et/ou dans la partie centrale des parties longitudinales (720) et (721) sur l'ensemble de la hauteur h et sur une longueur L2. Figure 4 shows the bottom and the longitudinal wall portions. The bottom (76) is typically covered by the first and / or second fabric. Advantageously, the first fabric is at least located in the central part of the bottom (76) along a length L1 and / or in the central part of the longitudinal parts (720) and (721) over the entire height h and over a length L2.
Avantageusement, la portion de surface couverte par le premier tissu est comprise entre 30 et 90 % et de préférence entre 50 et 80 % pour les parties longitudinales (720) et (721), et/ou entre 30 et 70 % et de préférence entre 40 et 60 % pour les parties latérales (730, 731) et/ou entre 30 et 100 % et de préférence entre 50 et 80 % pour le fond (76). Il est avantageux que la longueur Ll de premier tissu situé dans le fond (76) soit supérieure à la longueur L2 de premier tissu situé dans la partie des parois longitudinales (720) et (721) en contact avec le fond. Advantageously, the surface portion covered by the first fabric is between 30 and 90% and preferably between 50 and 80% for the longitudinal portions (720) and (721), and / or between 30 and 70% and preferably between 40 and 60% for the side parts (730, 731) and / or between 30 and 100% and preferably between 50 and 80% for the bottom (76). It is advantageous if the length L1 of the first tissue located in the bottom (76) is greater than the length L2 of the first tissue situated in the part of the longitudinal walls (720) and (721) in contact with the bottom.
Les présents inventeurs pensent que la géométrie du distributeur permet notamment d'améliorer la qualité du flux du métal liquide, de réduire les turbulences et d'améliorer la distribution de température. The present inventors believe that the geometry of the dispenser makes it possible in particular to improve the quality of the flow of the liquid metal, to reduce turbulence and to improve the temperature distribution.
Le premier tissu et le deuxième tissu sont avantageusement obtenus par tissage d'un fil comprenant essentiellement du carbone. Le tissage de fil graphite est particulièrement avantageux. Les tissus sont typiquement cousus l'un à l'autre. Il est possible également en lieu et place d'un premier et deuxième tissus d'utiliser un tissu diffuseur unique présentant au moins deux zones de tissage, plus ou moins denses. The first fabric and the second fabric are advantageously obtained by weaving a yarn essentially comprising carbon. The weaving of graphite yarn is particularly advantageous. The tissues are typically sewn to each other. It is also possible instead of first and second fabrics to use a single diffuser fabric having at least two weaving areas, more or less dense.
Il est avantageux pour la facilité du tissage que le fil comprenant du carbone soit revêtu d'une couche facilitant le glissement. Cette couche peut par exemple comprendre un polymère fluoré tel que le Teflon ou une polyamide telle que le xylon. It is advantageous for the ease of weaving that the wire comprising carbon is coated with a layer facilitating sliding. This layer may for example comprise a fluorinated polymer such as Teflon or a polyamide such as xylon.
Le premier tissu est sensiblement obturant. Typiquement il s'agit d'un tissu présentant des mailles de dimension inférieure à 0,5 mm, de préférence inférieure à 0,2 mm. Le second tissu est non obturant et permet le passage du métal en fusion. Typiquement, il s'agit d'un tissu présentant des mailles de dimension comprise entre 1 et 5 mm, de préférence de 2 à 4 mm. Dans un mode de réalisation de l'invention le premier tissu recouvre localement le second tissu, tout en étant en contact intime de façon à ne pas laisser d'interstice entre les deux tissus. The first fabric is substantially obturant. Typically it is a fabric having mesh size of less than 0.5 mm, preferably less than 0.2 mm. The second fabric is non-sealing and allows the passage of the molten metal. Typically, it is a fabric having mesh sizes of between 1 and 5 mm, preferably 2 to 4 mm. In one embodiment of the invention the first tissue locally covers the second tissue, while being in intimate contact so as not to leave a gap between the two tissues.
Avantageusement la plaque ainsi obtenue est ensuite transformée pour obtenir un produit corroyé. Advantageously, the plate thus obtained is then transformed to obtain a wrought product.
La plaque ainsi obtenue est ensuite homogénéisée avant ou après avoir optionnellement été usinée pour obtenir une forme pouvant être déformée à chaud. Dans un mode de réalisation, la plaque est usinée sous forme de plaque de laminage de façon à ensuite être déformée à chaud par laminage. Dans un autre mode de réalisation, la plaque est usinée sous forme de d'ébauche de forge de façon à ensuite être déformée à chaud par forgeage. Dans encore une autre mode de réalisation la plaque est usinée sous forme de billettes de façon à ensuite être déformée à chaud par extrusion. De préférence l'homogénéisation est réalisée à une température comprise entre 470 et 540 °C pendant une durée comprise entre 2 et 30 heures. The plate thus obtained is then homogenized before or after having been optionally machined to obtain a shape that can be deformed while hot. In one embodiment, the plate is machined as a rolling plate so as to be hot deformed by rolling. In another embodiment, the plate is machined as a forging blank so as to be hot deformed by forging. In yet another embodiment, the plate is machined in the form of billets so as to then be hot deformed by extrusion. Preferably the homogenization is carried out at a temperature between 470 and 540 ° C for a period of between 2 and 30 hours.
On déforme à chaud et optionnellement à froid ladite forme ainsi homogénéisée pour obtenir un produit corroyé. La température de déformation à chaud est avantageusement au moins 350 °C et de préférence au moins 400 °C. Le taux de déformation à chaud et optionnellement à froid, c'est-à-dire le rapport entre d'une part la différence entre l'épaisseur initiale, avant déformation mais après l'éventuel usinage, et l'épaisseur finale et d'autre part l'épaisseur initiale est inférieur à 85% et de préférence inférieur à 80 %. Dans un mode de réalisation lequel le taux de déformation lors de la déformation est inférieur à 75% et de préférence inférieur à 70 %. The shape thus homogenized is deformed hot and optionally cold so as to obtain a wrought product. The heat-forming temperature is advantageously at least 350 ° C and preferably at least 400 ° C. The rate of deformation hot and optionally cold, that is to say the ratio between the difference between the initial thickness, before deformation but after the possible machining, and the final thickness and on the other hand, the initial thickness is less than 85% and preferably less than 80%. In one embodiment, the deformation rate during the deformation is less than 75% and preferably less than 70%.
Le produit corroyé ainsi obtenu est ensuite mis en solution et trempé. La température de mise en solution est avantageusement comprise entre 470 et 540 °C et de préférence entre 490 et 530 °C et la durée est adaptée à l'épaisseur du produit. The wrought product thus obtained is then dissolved and quenched. The dissolution temperature is advantageously between 470 and 540 ° C and preferably between 490 and 530 ° C and the duration is adapted to the thickness of the product.
Optionnellement on détensionne ledit produit corroyé ainsi mis en solution par déformation plastique avec une déformation d'au moins 1%. Dans le cas des produits laminés il est avantageux de détensionner par traction contrôlée ledit produit corroyé ainsi mis en solution avec un allongement permanent d'au moins 1% et de préférence compris entre 2 et 5 %. Optionally, the wrought product thus solubilized is de-tensioned by plastic deformation with a deformation of at least 1%. In the case of rolled products, it is advantageous to detension by controlled traction said wrought product thus put into solution with a permanent elongation of at least 1% and preferably between 2 and 5%.
Enfin on fait subir un revenu au produit ainsi mis en solution et optionnellement détensionné. Le revenu est effectué en un ou plusieurs paliers à une température avantageusement comprise entre 130 et 160 °C pendant une durée de 5 à 60 heures. De préférence on obtient à l'issue du revenu un état métallurgique T8, tel que notamment T851, T83, T84, ou T85. Finally, we make an income to the product thus put in solution and optionally relieved. The income is made in one or more steps at a temperature advantageously between 130 and 160 ° C for a period of 5 to 60 hours. Preferably one obtains at the end of the income a metallurgical state T8, such as in particular T851, T83, T84, or T85.
Les produits corroyés obtenus par le procédé selon l'invention présentent des propriétés avantageuses. The wrought products obtained by the process according to the invention have advantageous properties.
La moyenne logarithmique de fatigue des produits corroyés dont l'épaisseur est au moins 80 mm, obtenus par le procédé selon l'invention, mesurée à mi-épaisseur dans la direction TL sur éprouvettes lisses selon la Figure la à une contrainte d'amplitude maximale de 242 MPa, une fréquence de 50 Hz, un rapport de contrainte R = 0,1 est au moins 250 000 cycles, avantageusement la propriété en fatigue est obtenue pour les produits corroyés obtenus par le procédé selon l'invention dont l'épaisseur est au moins 100 mm ou de préférence au moins 120 mm ou même au moins 140 mm. The logarithmic fatigue mean of the wrought products whose thickness is at least 80 mm, obtained by the method according to the invention, measured at mid-thickness in the direction TL on smooth test pieces according to Figure la at a maximum amplitude stress of 242 MPa, a frequency of 50 Hz, a stress ratio R = 0.1 is at least 250,000 cycles, advantageously the fatigue property is obtained for the wrought products obtained by the process according to the invention, the thickness of which is at least 100 mm or preferably at least 120 mm or even at least 140 mm.
Les produits corroyés selon l'invention d'épaisseur au moins 80 mm présentent également des propriétés en fatigue avantageuse pour des éprouvettes à trou, ainsi l'indice de qualité fatigue IQF obtenu sur des éprouvettes à trou Kt = 2,3 selon la Figure lb à une fréquence de 50 Hz à l'air ambiant avec une valeur R— 0,1 est au moins 180 MPa et de préférence est au moins 190 MPa dans le sens T-L. The wrought products according to the invention having a thickness of at least 80 mm also have advantageous fatigue properties for hole specimens, thus the fatigue quality index IQF obtained on specimens with a hole Kt = 2.3 according to FIG. at a frequency of 50 Hz to ambient air with an R-0.1 value is at least 180 MPa and preferably is at least 190 MPa in the TL direction.
De plus les produits obtenus par le procédé selon l'invention ont des caractéristiques mécaniques statiques avantageuses. Ainsi pour les produits corroyés dont l'épaisseur est au moins 80 mm comprenant en % en poids, Cu : 3,0 - 3,9 ; Li : 0,7 - 1,3 ; Mg : 0,1 - 1 ,0, au moins un élément choisi parmi Zr, Mn et Ti, la quantité dudit élément, s'il est choisi, étant de 0,06 à 0,15 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn et de 0,01 à 0,15 % en poids pour Ti,; Ag : 0 - 0,7 ; Zn < 0,25 ; Si < 0,08 ; Fe < 0,10 ; autres < 0,05 chacun et < 0,15 au total, reste aluminium, la limite d'élasticité mesurée à quart épaisseur dans le sens L est au moins 450 MPa et de préférence au moins 470 MPa et/ou la résistance à la rupture mesurée est au moins 480 MPa et de préférence au moins 500 MPa et/ou l'allongement est au moins 5% et de préférence au moins 6%. In addition, the products obtained by the process according to the invention have advantageous static mechanical characteristics. Thus for wrought products whose thickness is at least 80 mm comprising in% by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element selected from Zr, Mn and Ti, the amount of said element, if selected, being from 0.06 to 0.15% by weight for Zr, O, From 0.5 to 0.8% by weight for Mn and from 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn <0.25; If <0.08; Fe <0.10; other <0.05 each and <0.15 in total, remains aluminum, the yield strength measured at quarter-thickness in the direction L is at least 450 MPa and preferably at least 470 MPa and / or the breaking strength measured is at least 480 MPa and preferably at least 500 MPa and / or the elongation is at least 5% and preferably at least 6%.
Les produits corroyés obtenus par le procédé selon l'invention peuvent de manière avantageuse être utilisées pour réaliser des éléments de structure, de préférence des éléments de structure d'avion. Des éléments de structure d'avion préférés sont les longerons, nervures ou un cadres. L'invention est particulièrement avantageuse pour des pièces de forme complexe obtenues par usinage intégral, utilisées en particulier pour la fabrication d'ailes d'avion ainsi que pour n'importe quel autre usage pour lequel les propriétés des produits selon l'invention sont avantageuses. The wrought products obtained by the process according to the invention can advantageously be used to produce structural elements, preferably aircraft structural elements. Preferred aircraft structural elements are spars, ribs or frames. The invention is particularly advantageous for parts of complex shape obtained by integral machining, used in particular for the manufacture of aircraft wings and for any other use for which the properties of the products according to the invention are advantageous. .
Exemple Example
Dans cet exemple, on a préparé des tôles fortes en alliage AA2050. Des plaques en alliage AA2050 ont été coulées par coulée semi-continue verticale à refroidissement direct. L'alliage a été préparé dans un four de fusion. Pour les exemples 1 à 7 on a utilisé un mélange KCL/LiCl en surface du métal liquide dans le four de fusion. Pour les exemples 8 à 9 on n'a pas utilisé de sel dans le four de fusion. Pour les exemples 8 à 9 l'atmosphère en contact avec le métal liquide avec une teneur en oxygène inférieure à 0,3 % en volume pour l'ensemble de l'installation de coulée. L'installation de coulée comprenait un capot disposé au-dessus du puits de coulée permettant de limiter la teneur en oxygène. Pour les essais 8 et 9 on avait en plus utilisé une aspiration (101) telle que la pression dans l'enceinte (10) était inférieure à la pression dans la chambre (65) et telle que la vitesse de l'atmosphère au travers des surfaces ouvertes du puits de coulée était au moins de 2 m/s. La teneur en oxygène a été mesurée à l'aide d'un oxymètre lors de la coulée. Par ailleurs, la teneur en hydrogène dans l'aluminium liquide a été mesurée à l'aide d'une sonde de type Alscan™sous balayage d'azote. Deux types de distributeurs de métal liquide ont été utilisés. Un premier distributeur de type « Combo Bag » tel que décrit par exemple dans les Figures 2 à 6 de la demande internationale W099/44719 mais réalisé en tissu comprenant essentiellement du carbone, référencé ci-dessous « distributeur A » et un second distributeur tel que décrit figure 3 référencé ci-dessous « distributeur B » est réalisé en tissu de fil de graphite. In this example, AA2050 alloy plates were prepared. AA2050 alloy plates were cast by direct cooling vertical semi-continuous casting. The alloy was prepared in a melting furnace. For Examples 1 to 7, a KCL / LiCl mixture was used on the surface of the liquid metal in the melting furnace. For Examples 8 to 9 no salt was used in the melting furnace. For Examples 8 to 9 the atmosphere in contact with the liquid metal with an oxygen content of less than 0.3% by volume for the entire casting installation. The casting installation included a hood disposed above the pouring well to limit the oxygen content. For tests 8 and 9, an aspiration (101) was also used such that the pressure in the chamber (10) was lower than the pressure in the chamber (65) and such that the speed of the atmosphere through the open surfaces of the casting well was at least 2 m / s. Oxygen content was measured with an oximeter during casting. Furthermore, the hydrogen content in the liquid aluminum was measured using an Alscan ™ type probe under nitrogen flushing. Two types of liquid metal dispensers were used. A first "Combo Bag" type dispenser as described for example in Figures 2 to 6 of the international application WO99 / 44719 but made of fabric comprising essentially carbon, referenced below "distributor A" and a second distributor such as described in Figure 3 referenced below "distributor B" is made of graphite wire cloth.
Les conditions de coulée des différents essais réalisés sont données dans le tableau 1. The casting conditions of the various tests carried out are given in Table 1.
Table 1 - Conditions de coulée pour les différents essais Table 1 - Casting conditions for different tests
Les plaques ont été homogénéisées 12 heures à 505 °C, usinées jusqu'à une épaisseur d'environ 365 mm, laminées à chaud jusqu'à des tôles d'épaisseur finale comprise entre 154 et 158 mm, mises en solution à 504 °C, trempées et détensionnée par traction contrôlée avec un allongement permanent de 3,5%. Les tôles ainsi obtenues ont subi un revenu de 18 heures à 155 °C. The plates were homogenized for 12 hours at 505 ° C., machined to a thickness of about 365 mm, hot-rolled to sheets with a final thickness of between 154 and 158 mm, dissolved at 504 ° C. , quenched and relieved by controlled traction with a permanent elongation of 3.5%. The sheets thus obtained have an 18 hour income at 155 ° C.
Les propriétés mécaniques statiques et de ténacité ont été caractérisées à quart-épaisseur. Les caractéristiques mécaniques statiques et la ténacité sont données dans le Tableau 2. Static mechanical properties and toughness were characterized at quarter-thickness. Static mechanical characteristics and toughness are given in Table 2.
Tableau 2 Caractéristiques mécaniques Table 2 Mechanical characteristics
Les propriétés en fatigue ont été caractérisées sur des éprouvettes lisses et sur des éprouvettes à trou pour certains échantillons prélevées à mi-épaisseur. The fatigue properties were characterized on smooth test specimens and hole test specimens for some samples taken at mid-thickness.
Pour les caractérisations de fatigue lisse, quatre éprouvettes, dont le schéma est donné en Figure la, ont été testées à mi-épaisseur et mi-largeur dans le sens TL, les conditions de test étant σ = 242 MPa, R = 0,1. Certains tests ont été arrêtés après 200 000 cycles et d'autres tests ont été arrêtés après 300 000 cycles. For the smooth fatigue characterizations, four test pieces, whose diagram is given in Figure la, were tested at mid-thickness and half-width in the TL direction, the test conditions being σ = 242 MPa, R = 0.1 . Some tests were stopped after 200,000 cycles and other tests were stopped after 300,000 cycles.
Pour les caractérisations de fatigue à trou, on a utilisé l'éprouvette reproduite sur la Figure lb, dont la valeur Kt est 2,3. Les éprouvettes ont été testées à une fréquence de 50 Hz à l'air ambiant avec une valeur R = 0,1. Les courbes de Wôhler correspondantes sont présentées sur les Figures 6a et 6b. On a calculé l'indice de qualité de fatigue IQF. Tableau 3 - Résultats des essais en fatigue For hole fatigue characterizations, the specimen reproduced in Figure 1b, whose K t value is 2.3, was used. The test pieces were tested at a frequency of 50 Hz in ambient air with a value R = 0.1. The corresponding Wohler curves are shown in Figures 6a and 6b. The IQF fatigue quality index was calculated. Table 3 - Fatigue Test Results
La combinaison d'une teneur en hydrogène inférieure à 0,4 ml/100g d'une teneur en oxygène mesurée au-dessus de la surface liquide inférieure à 0,3 % en volume et du distributeur B permet d'atteindre un excellent niveau de performance en fatigue. Ces résultats sont présentés sur la Figure 5. The combination of a hydrogen content of less than 0.4 ml / 100g of an oxygen content measured above the liquid surface of less than 0.3% by volume and of the distributor B makes it possible to achieve an excellent level of fatigue performance. These results are shown in Figure 5.
Claims
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PCT/FR2014/000273 WO2015086922A2 (en) | 2013-12-13 | 2014-12-11 | Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties |
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CA2932991C (en) | 2021-10-26 |
WO2015086921A3 (en) | 2015-08-20 |
WO2015086921A2 (en) | 2015-06-18 |
CN105814222B (en) | 2019-07-23 |
JP2017505378A (en) | 2017-02-16 |
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