US20050013723A1 - Formation of metallic thermal barrier alloys - Google Patents
Formation of metallic thermal barrier alloys Download PDFInfo
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- US20050013723A1 US20050013723A1 US10/776,473 US77647304A US2005013723A1 US 20050013723 A1 US20050013723 A1 US 20050013723A1 US 77647304 A US77647304 A US 77647304A US 2005013723 A1 US2005013723 A1 US 2005013723A1
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- alloy
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- 229910045601 alloy Inorganic materials 0.000 title abstract description 34
- 239000000956 alloy Substances 0.000 title abstract description 34
- 230000004888 barrier function Effects 0.000 title description 5
- 230000015572 biosynthetic process Effects 0.000 title 1
- 229910001092 metal group alloy Inorganic materials 0.000 claims abstract description 24
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 14
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 13
- 239000010703 silicon Substances 0.000 claims abstract description 13
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052796 boron Inorganic materials 0.000 claims abstract description 7
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 6
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 claims abstract description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 25
- 238000005275 alloying Methods 0.000 claims description 25
- 239000010953 base metal Substances 0.000 claims description 15
- 238000000034 method Methods 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 15
- 239000003574 free electron Substances 0.000 claims description 14
- 229910052742 iron Inorganic materials 0.000 claims description 11
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 5
- 229910052757 nitrogen Inorganic materials 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 4
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 239000011733 molybdenum Substances 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 239000010937 tungsten Substances 0.000 claims description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 4
- 229910052721 tungsten Inorganic materials 0.000 claims description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 3
- 229910002065 alloy metal Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 229910052759 nickel Inorganic materials 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 2
- MUBKMWFYVHYZAI-UHFFFAOYSA-N [Al].[Cu].[Zn] Chemical compound [Al].[Cu].[Zn] MUBKMWFYVHYZAI-UHFFFAOYSA-N 0.000 claims description 2
- 230000003247 decreasing effect Effects 0.000 claims description 2
- 229910052735 hafnium Inorganic materials 0.000 claims description 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims description 2
- 238000002156 mixing Methods 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 239000010955 niobium Substances 0.000 claims description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 2
- 229910052720 vanadium Inorganic materials 0.000 claims description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 238000000576 coating method Methods 0.000 abstract description 17
- 239000011248 coating agent Substances 0.000 abstract description 14
- 238000007792 addition Methods 0.000 abstract description 4
- 239000012720 thermal barrier coating Substances 0.000 abstract description 2
- 229910052751 metal Inorganic materials 0.000 description 16
- 239000002184 metal Substances 0.000 description 16
- 239000000843 powder Substances 0.000 description 8
- 239000000919 ceramic Substances 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 7
- 238000007749 high velocity oxygen fuel spraying Methods 0.000 description 5
- 239000000758 substrate Substances 0.000 description 5
- 239000000446 fuel Substances 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 239000010935 stainless steel Substances 0.000 description 4
- 229910001220 stainless steel Inorganic materials 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 229910000975 Carbon steel Inorganic materials 0.000 description 3
- 239000010962 carbon steel Substances 0.000 description 3
- 239000011651 chromium Substances 0.000 description 3
- 239000000470 constituent Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 150000002500 ions Chemical group 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000007921 spray Substances 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 238000000889 atomisation Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000001747 exhibiting effect Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- 239000010965 430 stainless steel Substances 0.000 description 1
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 229910001060 Gray iron Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001037 White iron Inorganic materials 0.000 description 1
- 150000001450 anions Chemical group 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 150000001768 cations Chemical group 0.000 description 1
- 229910002110 ceramic alloy Inorganic materials 0.000 description 1
- 238000005524 ceramic coating Methods 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000009689 gas atomisation Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- XWHPIFXRKKHEKR-UHFFFAOYSA-N iron silicon Chemical compound [Si].[Fe] XWHPIFXRKKHEKR-UHFFFAOYSA-N 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000696 magnetic material Substances 0.000 description 1
- 238000002074 melt spinning Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910021645 metal ion Inorganic materials 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 230000027756 respiratory electron transport chain Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 238000007783 splat quenching Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/06—Making metallic powder or suspensions thereof using physical processes starting from liquid material
- B22F9/08—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying
- B22F9/082—Making metallic powder or suspensions thereof using physical processes starting from liquid material by casting, e.g. through sieves or in water, by atomising or spraying atomising using a fluid
- B22F2009/088—Fluid nozzles, e.g. angle, distance
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
Definitions
- This invention is directed at metallic alloys, and more particularly at unique metallic alloys having low electrical and thermal conductivity. In coating form, when applied, such alloys present the ability to provide thermal barrier characteristics to a selected substrate.
- Metals and metallic alloys have metallic bonds consisting of metal ion cores surrounded by a sea of electrons. These free electrons which arise from an unfilled outer energy band allow the metal to have high electrical and thermal conductivity which makes this class of materials conductors. Due to the nature of the metallic bonds, metals and metallic alloys may exhibit a characteristic range of properties such as electrical and thermal conductivity. Typical metallic materials may exhibit values of electrical resistivity that generally fall in a range of between about 1.5 to 145 10 ⁇ 8 ⁇ m, with iron having an electrical resistivity of about 8.6 10 ⁇ 8 ⁇ m. Typical values of thermal conductivity for metallic materials may be in a range of between about 0.2 to 4.3 watts/cm° C., with iron exhibiting a thermal conductivity of about 0.8 watts/cm° C.
- ceramics are a class of materials which typically contain positive ions and negative ions resulting from electron transfer from a cation atom to an anion atom. All of the electron density in ceramics is strongly bonded resulting in a filled outer energy band. Ceramic alloys, due to the nature of their ionic bonding, will exhibit a different characteristic range of properties such as electrical and thermal conductivity. Because of the lack of free electrons, ceramics generally have poor electrical and thermal conductivity and are considered insulators. Thus, ceramics may be suitable for use in applications such as thermal barrier coatings while metals are not.
- a metal alloy comprising an alloy metal and greater than about 4 atomic % of at least one P-group alloying element.
- a method of reducing the thermal and/or electrical conductivity of a metal alloy composition comprising supplying a base metal with a free electron density, supplying a P-group alloying element and combining said P-group alloying element with said base metal and decreasing the free electron density of the base metal.
- a metallic alloy which exhibits relatively low thermal conductivity and a low electrical conductivity.
- the alloy may include primary alloying metals, such as iron, nickel, cobalt, aluminum, copper, zinc, titanium, zirconium, niobium, molybdenum, tantalum, vanadium, hafnium, tungsten, manganese, and combinations thereof, and increased fractions of P-Group elemental additions in the alloy composition.
- P-group elements are the non-metal and semi-metal constituents of groups IIIA, IVA, VA, VIA, and VIIA found in the periodic table, including but not limited to phosphorous, carbon, boron, silicon, sulfur, and nitrogen.
- the metallic alloy exhibiting relatively low thermal conductivity and electrical conductivity may be provided as a coating suitable for thermal and/or electrical barrier applications on a variety of substrates.
- metallic alloys are provided that exhibit relatively low thermal and electrical conductivity.
- the alloys according to the present invention may include relatively high fractions of P-group elemental alloying additions in admixture with a metal.
- the added P-group elements may include, but are not limited to, carbon, nitrogen, phosphorus, silicon, sulfur and boron.
- the P-group elements may be alloyed with the metal according to such methods as by the addition of the P-group elements to the metal in a melt state.
- an alloy according to the present invention may include P-group alloying constituents. Such constituents are preferably present at a level of at least 4 at % (atomic percent) of the alloy. Desirably, the alloy consistent with the present invention may include more than one alloying component selected from P-group elements, such that the collective content of all of the P-group elements is between about 4 at % to 50 at %.
- the alloy may include relatively large fractions of silicon in the alloy composition.
- an iron/silicon coating alloy can be prepared according to the present invention which coating may be applied, e.g., to any given substrate.
- the metal alloy may be applied as coating using a thermal spray process.
- the resulting coating maybe employed to provide a thermal and/or electrical barrier coating.
- the coating provides thermal and/or electrical barrier properties exhibited similar to a ceramic material, however without the associated brittleness of conventional ceramic coatings.
- the alloy of the present invention may also be processed by any know means to process a liquid melt including conventional casting (permanent mold, die, injection, sand, continuous casting, etc.) or higher cooling rate, i.e. rapid solidification, processes including melt spinning, atomization (centrifugal, gas,. water, explosive), or splat quenching.
- a liquid melt including conventional casting (permanent mold, die, injection, sand, continuous casting, etc.) or higher cooling rate, i.e. rapid solidification, processes including melt spinning, atomization (centrifugal, gas,. water, explosive), or splat quenching.
- melt spinning centrifugal, gas,. water, explosive
- splat quenching atomization to produce powder in the target size range for various thermal spray coating application devices.
- the present invention provides a metal alloy that behaves similar to a ceramic with respect to electrical and thermal conductivity.
- An exemplary alloy consistent with the present invention was prepared containing a combination of several alloying elements present at a total level of 25.0 atomic % P-group alloying elements in combination with, e.g. iron.
- the experimental alloy was produced by combining multiple P group elements according to the following distribution: 16.0 atomic % boron, 4.0 atomic % carbon, and 5.0 atomic % silicon with 54.5 atomic % iron, 15.0 atomic % chromium, 2.0 atomic % manganese, 2.0 atomic % molybdenum, and 1.5 atomic % tungsten.
- the experimental alloy was prepared by mixing the alloying elements at the disclosed ratios and then melting the alloying ingredients using radio frequency induction in a ceramic crucible. The alloy was then process into a powder form by first aspirating molten alloy to initiate flow, and then supplying high pressure argon gas to the melt stream in a close coupled gas atomization nozzle. The power which was produced exhibited a Gaussian size distribution with a mean particle size of 30 microns. The atomized powder was further air classified to yield preferred powder sized either in the range of 10-45 microns or 22-53 microns. These preferred size feed stock powders were then sprayed onto selected metal substrates using high velocity oxy-fuel thermal spray systems to provide a coating on the selected substrates.
- conventional metals and metallic alloys typically cool rapidly from a melt state on a conventional water cooled copper arc-melter, and can be safely handled in a matter of a few minutes.
- the experimental alloy prepared as described above required in excess of 30 minutes to cool from a melt state down to a safe handling temperature after being melted on a water cooled copper hearth arc-melter.
- the experimental alloy powder does not transfer heat sufficiently using conventional operating parameters due to its relatively low conductivity and inability to absorb heat.
- conventional alloys can be sprayed with equivalence ratios (kerosene fuel/oxygen fuel flow rate) equal to 0.8. Because of the low thermal conductivity of the modified experimental alloys, much higher equivalence ratios, in the range of 0.9-1.2, are necessary in order to provide sufficient heating of the power.
- the very thin deposit (225 ⁇ m thick weld) took excessive time before another layer can be deposited since it glows red hot for an extended time.
- alloy compositions of the following are to be noted, with the numbers reflecting atomic %: SHS717 Powder, with an alloy composition of Fe (52.3), Cr (19.0), Mo (2.5), W (1.7), B (16.0), C (4.0), Si (2.5) and Mn (2.0); SHS717 wire, with an alloy composition of Fe (55.9), Cr (22.0), Mo (0.6), W (0.4), B (15.6), C (3.5), Si (1.2) and Mn (0.9).
- the thermal conductivity data for the SHS717 coatings was measured by a Laser Flash method and the results are given in Table 1. Note that the wire-arc conductivity is generally lower than the HVOF due to the higher porosity in the wire-arc coating. Note that the conductivity of the coatings is lower than that of titanium which is the lowest thermal conductivity metal and at room temperature are even lower than alumina ceramic (see Table 2).
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Coating By Spraying Or Casting (AREA)
- Conductive Materials (AREA)
- Chemical Vapour Deposition (AREA)
Abstract
Metal alloys having low electrical and thermal conductivity including relatively large fractions of P-Group element additions. The P-Group elements may be selected from the group including phosphorous, carbon, boron, and silicon. The resultant alloys do not exhibit significantly increased brittleness, and are applied as a coating that provides a metallic thermal barrier coating.
Description
- This application claims priority to U.S. Provisional Application No. 60/446,610 filed Feb. 11, 2003.
- This invention is directed at metallic alloys, and more particularly at unique metallic alloys having low electrical and thermal conductivity. In coating form, when applied, such alloys present the ability to provide thermal barrier characteristics to a selected substrate.
- Metals and metallic alloys have metallic bonds consisting of metal ion cores surrounded by a sea of electrons. These free electrons which arise from an unfilled outer energy band allow the metal to have high electrical and thermal conductivity which makes this class of materials conductors. Due to the nature of the metallic bonds, metals and metallic alloys may exhibit a characteristic range of properties such as electrical and thermal conductivity. Typical metallic materials may exhibit values of electrical resistivity that generally fall in a range of between about 1.5 to 145 10−8 Ωm, with iron having an electrical resistivity of about 8.6 10−8 Ωm. Typical values of thermal conductivity for metallic materials may be in a range of between about 0.2 to 4.3 watts/cm° C., with iron exhibiting a thermal conductivity of about 0.8 watts/cm° C.
- By contrast, ceramics are a class of materials which typically contain positive ions and negative ions resulting from electron transfer from a cation atom to an anion atom. All of the electron density in ceramics is strongly bonded resulting in a filled outer energy band. Ceramic alloys, due to the nature of their ionic bonding, will exhibit a different characteristic range of properties such as electrical and thermal conductivity. Because of the lack of free electrons, ceramics generally have poor electrical and thermal conductivity and are considered insulators. Thus, ceramics may be suitable for use in applications such as thermal barrier coatings while metals are not.
- Designing a metal alloy to exhibit ceramic like electrical and thermal conductivities is unique. The only area where this has been utilized in material science is in the design of soft magnetic materials for transformer core applications. In such applications, extra silicon is added to iron in order to specifically reduce the electrical conductivity to minimize eddy current losses. However, iron-silicon alloys utilized for transformer cores typically contain a maximum of 2.5 at % (atomic percent) silicon because any additional silicon embrittles the alloy. Additionally, attempts to reduce electrical conductivity of iron transformer cores have not addressed reduced thermal conductivity.
- A metal alloy comprising an alloy metal and greater than about 4 atomic % of at least one P-group alloying element. In method form, a method of reducing the thermal and/or electrical conductivity of a metal alloy composition comprising supplying a base metal with a free electron density, supplying a P-group alloying element and combining said P-group alloying element with said base metal and decreasing the free electron density of the base metal.
- A metallic alloy is provided which exhibits relatively low thermal conductivity and a low electrical conductivity. The alloy may include primary alloying metals, such as iron, nickel, cobalt, aluminum, copper, zinc, titanium, zirconium, niobium, molybdenum, tantalum, vanadium, hafnium, tungsten, manganese, and combinations thereof, and increased fractions of P-Group elemental additions in the alloy composition. P-group elements are the non-metal and semi-metal constituents of groups IIIA, IVA, VA, VIA, and VIIA found in the periodic table, including but not limited to phosphorous, carbon, boron, silicon, sulfur, and nitrogen. The metallic alloy exhibiting relatively low thermal conductivity and electrical conductivity may be provided as a coating suitable for thermal and/or electrical barrier applications on a variety of substrates.
- Consistent with the present invention, metallic alloys are provided that exhibit relatively low thermal and electrical conductivity. The alloys according to the present invention may include relatively high fractions of P-group elemental alloying additions in admixture with a metal. The added P-group elements may include, but are not limited to, carbon, nitrogen, phosphorus, silicon, sulfur and boron. The P-group elements may be alloyed with the metal according to such methods as by the addition of the P-group elements to the metal in a melt state.
- Preferably, an alloy according to the present invention may include P-group alloying constituents. Such constituents are preferably present at a level of at least 4 at % (atomic percent) of the alloy. Desirably, the alloy consistent with the present invention may include more than one alloying component selected from P-group elements, such that the collective content of all of the P-group elements is between about 4 at % to 50 at %.
- Consistent with the present invention, the alloy may include relatively large fractions of silicon in the alloy composition. For example, an iron/silicon coating alloy can be prepared according to the present invention which coating may be applied, e.g., to any given substrate. For example, it has been found that 5.0 atomic % of silicon, and greater, may be incorporated into the alloy without any measurable loss of toughness when employed in a coating application.
- As alluded to above, consistent with the present invention, the metal alloy may be applied as coating using a thermal spray process. The resulting coating maybe employed to provide a thermal and/or electrical barrier coating. The coating provides thermal and/or electrical barrier properties exhibited similar to a ceramic material, however without the associated brittleness of conventional ceramic coatings.
- In addition to the use as a coating, the alloy of the present invention may also be processed by any know means to process a liquid melt including conventional casting (permanent mold, die, injection, sand, continuous casting, etc.) or higher cooling rate, i.e. rapid solidification, processes including melt spinning, atomization (centrifugal, gas,. water, explosive), or splat quenching. One especially preferred method is to utilize atomization to produce powder in the target size range for various thermal spray coating application devices.
- While not limiting the invention to any particular theory, it is believed at the time of filing that by alloying metals with P-group elements, including but not limited to carbon, nitrogen, phosphorus, and silicon, covalent bonds may be formed between the electrons in the P-group alloying element and the free electrons in the base metal, which base metal, as noted, may include iron. The interaction of the free electrons in the base metal in covalent bonds with the P-group alloying elements apparently act to reduce the free electron density of the base metal, and the outer electron energy band of the base metal is progressively filled. Accordingly, by adding significant quantities of P-group elements, the free electron density of the base metal can be continually reduced and the outer electron energy band can be progressively filled. Because the relatively high thermal conductively and electrical conductivity arise from the free electrons in the unfilled outer energy bands of the metal, as the free electron density is reduced, so are the electrical conductivity and the thermal conductivity. Therefore, the present invention provides a metal alloy that behaves similar to a ceramic with respect to electrical and thermal conductivity.
- An exemplary alloy consistent with the present invention was prepared containing a combination of several alloying elements present at a total level of 25.0 atomic % P-group alloying elements in combination with, e.g. iron. The experimental alloy was produced by combining multiple P group elements according to the following distribution: 16.0 atomic % boron, 4.0 atomic % carbon, and 5.0 atomic % silicon with 54.5 atomic % iron, 15.0 atomic % chromium, 2.0 atomic % manganese, 2.0 atomic % molybdenum, and 1.5 atomic % tungsten.
- The experimental alloy was prepared by mixing the alloying elements at the disclosed ratios and then melting the alloying ingredients using radio frequency induction in a ceramic crucible. The alloy was then process into a powder form by first aspirating molten alloy to initiate flow, and then supplying high pressure argon gas to the melt stream in a close coupled gas atomization nozzle. The power which was produced exhibited a Gaussian size distribution with a mean particle size of 30 microns. The atomized powder was further air classified to yield preferred powder sized either in the range of 10-45 microns or 22-53 microns. These preferred size feed stock powders were then sprayed onto selected metal substrates using high velocity oxy-fuel thermal spray systems to provide a coating on the selected substrates.
- Reduced thermal behavior was observed for the exemplary alloy in a variety of experiments. Specifically, a small 5 gram ingot of the exemplary alloy was arc-melted on a water cooled copper hearth. It was observed that the alloy ingots took longer time for cooling back to room temperature, relative to other alloys which did not contain the P-group composition noted herein. More specifically, the increased time for cooling was on the order of about 20 times longer.
- Additionally, while conventional metals and alloys that have been heated to high temperatures cool below their red hot radiance level in a few seconds, it was observed that when the exemplary alloy herein was heated to a temperature above the red hot radiance level of the alloy, the red hot radiance persisted for several minutes after removal of the heat source.
- Similarly, conventional metals and metallic alloys typically cool rapidly from a melt state on a conventional water cooled copper arc-melter, and can be safely handled in a matter of a few minutes. The experimental alloy prepared as described above required in excess of 30 minutes to cool from a melt state down to a safe handling temperature after being melted on a water cooled copper hearth arc-melter.
- Finally, when thermally sprayed the experimental alloy powder does not transfer heat sufficiently using conventional operating parameters due to its relatively low conductivity and inability to absorb heat. When using high velocity oxy-fuel thermal spray system, conventional alloys can be sprayed with equivalence ratios (kerosene fuel/oxygen fuel flow rate) equal to 0.8. Because of the low thermal conductivity of the modified experimental alloys, much higher equivalence ratios, in the range of 0.9-1.2, are necessary in order to provide sufficient heating of the power. Additionally, when deposited via the LENS (Laser Engineered Net Shape) process, in which a high powered laser is used to melt metal powder supplied to the focus of the laser by a deposition head, the very thin deposit (225 μm thick weld) took excessive time before another layer can be deposited since it glows red hot for an extended time.
- In the broad context of the present invention alloy compositions of the following are to be noted, with the numbers reflecting atomic %: SHS717 Powder, with an alloy composition of Fe (52.3), Cr (19.0), Mo (2.5), W (1.7), B (16.0), C (4.0), Si (2.5) and Mn (2.0); SHS717 wire, with an alloy composition of Fe (55.9), Cr (22.0), Mo (0.6), W (0.4), B (15.6), C (3.5), Si (1.2) and Mn (0.9).
- The thermal conductivity data for the SHS717 coatings was measured by a Laser Flash method and the results are given in Table 1. Note that the wire-arc conductivity is generally lower than the HVOF due to the higher porosity in the wire-arc coating. Note that the conductivity of the coatings is lower than that of titanium which is the lowest thermal conductivity metal and at room temperature are even lower than alumina ceramic (see Table 2).
TABLE 1 Thermal Conductivity Data for SHS717 Coatings Temperature Conductivity Coating Type (° C.) (W/m-K) HVOF 25 5.07 HVOF 200 6.93 HVOF 400 10.0 HVOF 600 14.2 Wire-Arc 25 4.14 Wire-Arc 200 4.78 Wire-Arc 400 5.48 Wire-Arc 600 6.94 -
TABLE 2 Comparative Thermal Conductivity Data 600° C. 25° C. (298 K) 400° C. (673 K) (873 K) Alloy W/m-K W/m-K W/m-K Al 239 227.5 213.5 Au 311 270.5 258* Cu 383 367* 352* Fe 79.1 49.11 39.8 Ni 74.9 63.0 72* Ti 22.0* 14.0 13.3 .31 wt % 69.5* 26.5 20.0 Carbon Steel .65 wt % 64.7* 23.8 18.7 Carbon Steel .88 wt % 59.0* 22.6 18.5 Carbon Steel British Steel #7 49.6* 38.1 29.9 White Cast Iron 12.8* 21.8 19.8 Grey Cast Iron 29.5* 34.1 23.8 717HV 5.07 10.00 14.20 717WA 4.14 5.48 6.94 302 Stainless Steel 12.3 18.6 22.1 303 Stainless Steel 14.4* 19.7 23.0 310 Stainless Steel 13.3* 20.1 25.1 430 Stainless Steel 22.0* 23.3 24.0 446 Stainless Steel 17.6* 19.8 21.0 Alumina Ceramic 24.5* 8.2 6.69
*Approximated Value
Claims (10)
1. A metal alloy comprising an alloy metal and greater than about 4 atomic % of at least one P-group alloying element.
2. A metal alloy of claim 1 wherein the P-group alloying element is present at a level of 4 atomic % to 50 atomic %.
3. The metal alloy of claim 1 wherein said P-group alloying element is selected from the group consisting of carbon, nitrogen, phosphorous, silicon, boron, and mixtures thereof.
4. A metal alloy according to claim 1 , wherein said at least one P-group alloying element comprises 16.0 atomic % B, 4.0 atomic % C, and 5.0 atomic % Si.
5. A metal alloy according to claim 1 wherein the alloy metal is selected from the group consisting of iron, chrome, molybdenum, tungsten, manganese, cobalt, nickel, copper, and mixtures thereof.
6. A method for reducing the thermal and/or electrical conductivity of a metal alloy composition comprising:
(a) supplying a metal alloy composition; and
(b) supplying a P-group alloying element;
(c) mixing said metal alloy composition and said P-group alloying element wherein said P-group alloying element is present at a level to reduce the thermal/and or electrical conductivity of said metal alloy composition.
7. A method of reducing the thermal and/or electrical conductivity of a metal alloy composition comprising:
(a) supplying a base metal with a free electron density
(b) supplying a P-group alloying element
(c) combining said P-group alloying element with said base metal and decreasing the free electron density of the base metal.
8. The method of claim 7 wherein the free electron density of the base metal is reduced from its base metal value, and wherein said free electron density is generally representative of a fully filled outer shell after combination with said P-group alloying element.
9. The method of claim 7 wherein said P-group alloying element is selected from the group consisting of carbon, nitrogen, phosphorous, silicon, boron, and mixtures thereof.
10. The method of claim 7 wherein the base metal is selected from the group consisting of iron, nickel, cobalt, aluminum, copper, zinc. titanium, zirconium, niobium, molybdenum, tantalum, vanadium, hafnium, tungsten, manganese, and combinations thereof.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/776,473 US20050013723A1 (en) | 2003-02-11 | 2004-02-11 | Formation of metallic thermal barrier alloys |
| US11/324,576 US7803223B2 (en) | 2003-02-11 | 2006-01-03 | Formation of metallic thermal barrier alloys |
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| US44661003P | 2003-02-11 | 2003-02-11 | |
| PCT/US2004/004026 WO2004072313A2 (en) | 2003-02-11 | 2004-02-11 | Formation of metallic thermal barrier alloys |
| US10/776,473 US20050013723A1 (en) | 2003-02-11 | 2004-02-11 | Formation of metallic thermal barrier alloys |
| WOPCT/US04/04026 | 2004-02-11 |
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| US11/324,576 Continuation US7803223B2 (en) | 2003-02-11 | 2006-01-03 | Formation of metallic thermal barrier alloys |
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| US11/324,576 Expired - Lifetime US7803223B2 (en) | 2003-02-11 | 2006-01-03 | Formation of metallic thermal barrier alloys |
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| US (2) | US20050013723A1 (en) |
| EP (1) | EP1594644B1 (en) |
| JP (1) | JP5367944B2 (en) |
| CN (1) | CN1758972A (en) |
| CA (1) | CA2515739C (en) |
| WO (1) | WO2004072313A2 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040140017A1 (en) * | 2000-11-09 | 2004-07-22 | Branagan Daniel J. | Hard metallic materials |
| US20050104867A1 (en) * | 1998-01-26 | 2005-05-19 | University Of Delaware | Method and apparatus for integrating manual input |
| US20070107809A1 (en) * | 2005-11-14 | 2007-05-17 | The Regents Of The Univerisity Of California | Process for making corrosion-resistant amorphous-metal coatings from gas-atomized amorphous-metal powders having relatively high critical cooling rates through particle-size optimization (PSO) and variations thereof |
| US20070107810A1 (en) * | 2005-11-14 | 2007-05-17 | The Regents Of The University Of California | Amorphous metal formulations and structured coatings for corrosion and wear resistance |
| US20070243335A1 (en) * | 2004-09-16 | 2007-10-18 | Belashchenko Vladimir E | Deposition System, Method And Materials For Composite Coatings |
| US20070281102A1 (en) * | 2006-06-05 | 2007-12-06 | The Regents Of The University Of California | Magnetic separation of devitrified particles from corrosion-resistant iron-based amorphous metal powders |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3986867A (en) * | 1974-01-12 | 1976-10-19 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Iron-chromium series amorphous alloys |
| US4067732A (en) * | 1975-06-26 | 1978-01-10 | Allied Chemical Corporation | Amorphous alloys which include iron group elements and boron |
| US4290808A (en) * | 1979-03-23 | 1981-09-22 | Allied Chemical Corporation | Metallic glass powders from glassy alloys |
| US4381943A (en) * | 1981-07-20 | 1983-05-03 | Allied Corporation | Chemically homogeneous microcrystalline metal powder for coating substrates |
| US4515870A (en) * | 1981-07-22 | 1985-05-07 | Allied Corporation | Homogeneous, ductile iron based hardfacing foils |
| US4523621A (en) * | 1982-02-18 | 1985-06-18 | Allied Corporation | Method for making metallic glass powder |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5827338B2 (en) * | 1974-01-12 | 1983-06-08 | 東北大学金属材料研究所長 | Fe-Cr amorphous alloy |
| JPS5841343B2 (en) * | 1974-07-01 | 1983-09-12 | トウホクダイガク キンゾクザイリヨウケンキユウシヨチヨウ | High strength Fe-Cr amorphous alloy |
| US4067932A (en) * | 1976-06-02 | 1978-01-10 | Stauffer Chemical Company | Derivatives of phosphorus-containing aldehydes and ketones |
| JPS58213857A (en) * | 1982-06-04 | 1983-12-12 | Takeshi Masumoto | Amorphous iron alloy having superior fatigue characteristic |
| US4822415A (en) * | 1985-11-22 | 1989-04-18 | Perkin-Elmer Corporation | Thermal spray iron alloy powder containing molybdenum, copper and boron |
| SE459863B (en) * | 1986-07-04 | 1989-08-14 | Hoeganaes Ab | HEAT-INSULATING SINTERED COMPONENT OF YEAR-BASED POWDER AND SET TO MANUFACTURE THIS |
| DE3876529T2 (en) * | 1987-07-31 | 1993-06-24 | Tdk Corp | MAGNETIC SOFT IRON POWDER FOR SHAPING MAGNETIC SHIELDING, CONNECTION AND METHOD FOR PRODUCING IT. |
| SU1615222A1 (en) * | 1988-10-31 | 1990-12-23 | Московский станкоинструментальный институт | Method of working surface subject to friction |
| US4965139A (en) * | 1990-03-01 | 1990-10-23 | The United States Of America As Represented By The Secretary Of The Navy | Corrosion resistant metallic glass coatings |
| JP3075331B2 (en) * | 1993-12-28 | 2000-08-14 | ボルボ コンストラクション イクイップメントコリア カンパニー リミテッド | Wear-resistant, corrosion-resistant, heat-resistant mechanical seal |
| RO111513B1 (en) * | 1995-12-27 | 1999-12-30 | Institutul Naţional De Cercetare - Dezvoltare Pentru Fizică Tehnică-Ift Iaşi | Amorphous and nano-crystalline magnetic yarns which are covered with glass and preparation process therefor |
| EP0818549B1 (en) * | 1996-06-25 | 2004-02-04 | Castolin S.A. | Nickel-based material in powder- or wireform for coating as well as the processes thereof |
| US6258185B1 (en) * | 1999-05-25 | 2001-07-10 | Bechtel Bwxt Idaho, Llc | Methods of forming steel |
-
2004
- 2004-02-11 US US10/776,473 patent/US20050013723A1/en not_active Abandoned
- 2004-02-11 CA CA 2515739 patent/CA2515739C/en not_active Expired - Fee Related
- 2004-02-11 CN CNA2004800062977A patent/CN1758972A/en active Pending
- 2004-02-11 WO PCT/US2004/004026 patent/WO2004072313A2/en not_active Ceased
- 2004-02-11 JP JP2006503500A patent/JP5367944B2/en not_active Expired - Fee Related
- 2004-02-11 EP EP20040710240 patent/EP1594644B1/en not_active Expired - Lifetime
-
2006
- 2006-01-03 US US11/324,576 patent/US7803223B2/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3986867A (en) * | 1974-01-12 | 1976-10-19 | The Research Institute For Iron, Steel And Other Metals Of The Tohoku University | Iron-chromium series amorphous alloys |
| US4067732A (en) * | 1975-06-26 | 1978-01-10 | Allied Chemical Corporation | Amorphous alloys which include iron group elements and boron |
| US4290808A (en) * | 1979-03-23 | 1981-09-22 | Allied Chemical Corporation | Metallic glass powders from glassy alloys |
| US4381943A (en) * | 1981-07-20 | 1983-05-03 | Allied Corporation | Chemically homogeneous microcrystalline metal powder for coating substrates |
| US4515870A (en) * | 1981-07-22 | 1985-05-07 | Allied Corporation | Homogeneous, ductile iron based hardfacing foils |
| US4523621A (en) * | 1982-02-18 | 1985-06-18 | Allied Corporation | Method for making metallic glass powder |
Cited By (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050104867A1 (en) * | 1998-01-26 | 2005-05-19 | University Of Delaware | Method and apparatus for integrating manual input |
| US8097095B2 (en) | 2000-11-09 | 2012-01-17 | Battelle Energy Alliance, Llc | Hardfacing material |
| US7785428B2 (en) | 2000-11-09 | 2010-08-31 | Battelle Energy Alliance, Llc | Method of forming a hardened surface on a substrate |
| US20040140017A1 (en) * | 2000-11-09 | 2004-07-22 | Branagan Daniel J. | Hard metallic materials |
| US20100015348A1 (en) * | 2000-11-09 | 2010-01-21 | Branagan Daniel J | Method of forming a hardened surface on a substrate |
| US20070243335A1 (en) * | 2004-09-16 | 2007-10-18 | Belashchenko Vladimir E | Deposition System, Method And Materials For Composite Coatings |
| US7670406B2 (en) | 2004-09-16 | 2010-03-02 | Belashchenko Vladimir E | Deposition system, method and materials for composite coatings |
| US20100019817A1 (en) * | 2005-09-06 | 2010-01-28 | Broadcom Corporation | Current-controlled CMOS (C3MOS) fully differential integrated delay cell with variable delay and high bandwidth |
| US7618500B2 (en) | 2005-11-14 | 2009-11-17 | Lawrence Livermore National Security, Llc | Corrosion resistant amorphous metals and methods of forming corrosion resistant amorphous metals |
| US8187720B2 (en) | 2005-11-14 | 2012-05-29 | Lawrence Livermore National Security, Llc | Corrosion resistant neutron absorbing coatings |
| US8778459B2 (en) | 2005-11-14 | 2014-07-15 | Lawrence Livermore National Security, Llc. | Corrosion resistant amorphous metals and methods of forming corrosion resistant amorphous metals |
| US20100084052A1 (en) * | 2005-11-14 | 2010-04-08 | The Regents Of The University Of California | Compositions of corrosion-resistant Fe-based amorphous metals suitable for producing thermal spray coatings |
| US20070107810A1 (en) * | 2005-11-14 | 2007-05-17 | The Regents Of The University Of California | Amorphous metal formulations and structured coatings for corrosion and wear resistance |
| US20110014353A1 (en) * | 2005-11-14 | 2011-01-20 | Jor-Shan Choi | Corrosion resistant neutron absorbing coatings |
| US20110165348A1 (en) * | 2005-11-14 | 2011-07-07 | Lawrence Livermore National Security, Llc | Compositions of Corrosion-resistant Fe-Based Amorphous Metals Suitable for Producing Thermal Spray Coatings |
| US8075712B2 (en) | 2005-11-14 | 2011-12-13 | Lawrence Livermore National Security, Llc | Amorphous metal formulations and structured coatings for corrosion and wear resistance |
| US20070107809A1 (en) * | 2005-11-14 | 2007-05-17 | The Regents Of The Univerisity Of California | Process for making corrosion-resistant amorphous-metal coatings from gas-atomized amorphous-metal powders having relatively high critical cooling rates through particle-size optimization (PSO) and variations thereof |
| US20100021750A1 (en) * | 2005-11-14 | 2010-01-28 | Farmer Joseph C | Corrosion resistant amorphous metals and methods of forming corrosion resistant amorphous metals |
| US8778460B2 (en) | 2005-11-14 | 2014-07-15 | Lawrence Livermore National Security, Llc. | Amorphous metal formulations and structured coatings for corrosion and wear resistance |
| US8480864B2 (en) | 2005-11-14 | 2013-07-09 | Joseph C. Farmer | Compositions of corrosion-resistant Fe-based amorphous metals suitable for producing thermal spray coatings |
| US8524053B2 (en) | 2005-11-14 | 2013-09-03 | Joseph C. Farmer | Compositions of corrosion-resistant Fe-based amorphous metals suitable for producing thermal spray coatings |
| US8580350B2 (en) | 2005-11-14 | 2013-11-12 | Lawrence Livermore National Security, Llc | Corrosion resistant neutron absorbing coatings |
| US8245661B2 (en) | 2006-06-05 | 2012-08-21 | Lawrence Livermore National Security, Llc | Magnetic separation of devitrified particles from corrosion-resistant iron-based amorphous metal powders |
| US20070281102A1 (en) * | 2006-06-05 | 2007-12-06 | The Regents Of The University Of California | Magnetic separation of devitrified particles from corrosion-resistant iron-based amorphous metal powders |
| CN103898434A (en) * | 2014-04-01 | 2014-07-02 | 北京工业大学 | Heat-insulating coating material for preventing hot-end component of automobile engine, and preparation method thereof |
| US20220028589A1 (en) * | 2018-10-16 | 2022-01-27 | Magneto B.V. | Magnetocaloric effect of Mn-Fe-P-Si-B-V alloy and use thereof |
| US11972883B2 (en) * | 2018-10-16 | 2024-04-30 | Magneto B.V. | Magnetocaloric effect of Mn—Fe—P—Si—B—V alloy and use thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| JP5367944B2 (en) | 2013-12-11 |
| US7803223B2 (en) | 2010-09-28 |
| CN1758972A (en) | 2006-04-12 |
| CA2515739A1 (en) | 2004-08-26 |
| WO2004072313A3 (en) | 2005-06-23 |
| EP1594644A2 (en) | 2005-11-16 |
| EP1594644B1 (en) | 2013-05-15 |
| EP1594644A4 (en) | 2008-03-26 |
| WO2004072313A2 (en) | 2004-08-26 |
| US20060110278A1 (en) | 2006-05-25 |
| CA2515739C (en) | 2012-08-14 |
| JP2006517616A (en) | 2006-07-27 |
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