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US2963129A - Dissimilar metal welded joint with protective overlay - Google Patents

Dissimilar metal welded joint with protective overlay Download PDF

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Publication number
US2963129A
US2963129A US474175A US47417554A US2963129A US 2963129 A US2963129 A US 2963129A US 474175 A US474175 A US 474175A US 47417554 A US47417554 A US 47417554A US 2963129 A US2963129 A US 2963129A
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ferritic
austenitic
alloy steel
deposit
weld
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US474175A
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Fritz T Eberle
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Babcock and Wilcox Co
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Babcock and Wilcox Co
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K9/00Arc welding or cutting
    • B23K9/23Arc welding or cutting taking account of the properties of the materials to be welded
    • B23K9/232Arc welding or cutting taking account of the properties of the materials to be welded of different metals
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/939Molten or fused coating
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12486Laterally noncoextensive components [e.g., embedded, etc.]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12639Adjacent, identical composition, components
    • Y10T428/12646Group VIII or IB metal-base
    • Y10T428/12653Fe, containing 0.01-1.7% carbon [i.e., steel]
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12958Next to Fe-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12958Next to Fe-base component
    • Y10T428/12965Both containing 0.01-1.7% carbon [i.e., steel]

Definitions

  • This invention relates to the production of a welded joint between austenitic and ferritic materials suitable for high temperatures, high "pressure service under conditions involving thermal shock and cyclic temperature and load applications.
  • Such conditions are encountered in high temperature process plants such. as, for example, oil refineries, in vapor or steam generators, and in heat exchangers of various types.
  • the particular problems in any one type of installation may differ in one or more aspects from those in another type.
  • refineries involve high temperatures but only moderate pressures, in conjunction with alternating oxidation and reducing conditions, corrosive environments and the like.
  • steam generators a more complex stress condition exists due to the combined actions of high operating pressures and high operating temperatures, which are further aggravated by cyclic variations in these factors.
  • the invention is of general application under high temperature, high stress conditions in any type of installation, particular reference will be made, by way of example only, to thehigh temperature and high stress conditions encountered in steam generators.
  • the external surface and the superheater support lugs are at a higher temperature than'the internal surface of the superheater tubes, due to the higher temperatures of the heat- ;ing gases as compared to the temperature of the steam flowing through the superheater. The reverse is true with respect to the steam line leading to the turbine.
  • the present invention is particularly directed to the production of a welded joint, between austenitic and ferritic materials, which has the requisite strength, ductility, and oxidation resistance to assure satisfactory performance under conditions of high stresses occasioned by thermal shock, cyclic temperature and load application, and differential thermal expansion. It has been found that these objectives can be obtained by Weld uniting a low alloy ferritic member to an austenitic member by a weld deposit which is carbide-stabilized, has an oxidation resistance which is higher than that of the ferritic member, and a coeflicient of thermal expansion intermediate the coefficients of thermal expansion of the two members, the weld deposit including an overlying heat resistant oxygen barrier.
  • the welded joint is a composite deposit of two or more metals, at least one of which is a carbidestabilized and oxidation-resistant ferritic metal and at least one more of which is an austenitic, heat-and-oxidation-resistant metal.
  • the weld groove forming surface of the austenitic member is buttered with a carbide-stabilized, ferritic metal having an oxidation resistance higher than that of the ferritic member.
  • the remainder of the weld groove is then filled with a ferritic metal of substantially the same composition as that of the ferritic member, and which may be carbidestabilized.
  • At least the ferritic-austenitic junction of the welded joint is then covered with a weld deposit overlay of an austenitic heat-resisting metal having a heat expansion coefiicient which is intermediate the heat expansion coeflicients of the two base members.
  • the weld groove between the ferritic and austenitic base members is filled with a carbide-stabilized, ferritic metal having a higher oxidation resistance than that of the ferritic base member. At least the ferritic-austenitic junction of the Welded point is then provided with substantially the same overlay as in the first embodiment.
  • the weld groove forming surface of the ferritic member is buttered with a carbide-stabilized, ferritic metal having an oxidation 'resistance higher than that of the ferritic member.
  • the remainder of the weld groove is then filled with anaustenitic, heat-resisting metal having a coeflicient of thermal expansion intermediate those of the base members, the weld depositio'n of this latter metal being continued to form an overlay thereof across the ferritic austenitic junction.
  • Figs. 1, 2 and 3 are partial transverse sectional views of welded points, each weld uniting a low alloy. ferritic base member to an austenitic base member, and embodying the invention. a
  • austenitic alloy refers to alloys known to those skilled in the art as 18-8 (18 Cr-8 Ni), 18-8 Cb, 18-8 Ti, 25-12, "25-20, or any other alloy-steel which is predominantly austenitic in structure.
  • a predominantly ferritic alloy steel workpiece 10 such as a pressure tube or pipe
  • a predominantly austenitic alloy steel workpiece 20 such as a pressure tube or pipe
  • a fusion deposited, carbide-stabilized, welded joint 30' having an oxidation resistance which is higher than that of member 10 and a coefiicient of thermal expansion intermediate the corresponding coefficients of members 10 and 20, joint 30 including an overlying heat-resistant oxidation barrier 35.
  • ferritic member 10 may be an alloy steel containing 2%% chromium and 1% molybdenum, this .steel being known commercially as fCroloy 2%, and austenitic member 20 may be an 188Ti alloy steel.
  • the facing end surfaces of members 10 and 20 are suitably bevelled, as at 11 and 21, respectively, to form a weld groove, a backing member 15 being arranged to bridge the open lower end of the welding groove.
  • the 'weld groove forming surface 21 of austenitic alloy steel member 20 is first buttered with a fusion deposit 31 of carbide- .stabilized ferritic metal having an oxidation resistance higher than that of ferritic alloy steel member 10.
  • This deposit or layer 31 resists carbon migration, due to its being carbide-stabilized, and also resists oxidation at the relatively high and cyclically varying working temperatures to which joint 30 is exposed in practice.
  • member 10 is a low alloy steel containing 2%% Cr and 1% M or 3% Cr and 1% M0
  • the metal deposited to form buttering layer 31 may be a 5% Cr0.5% Mo alloy steel stabilized with Cb (a S Cr.5 .MoCb steel).
  • deposit 32 may be a 2%.% Cr1% Mo ferritic alloy steel.
  • Deposit 32 may also be of carbide-stabilized ferritic alloy steel such as 254% Cr1% Mo-Cb alloy steel, for example.
  • the protective overlay 35 is fusion deposited at least across the ferritic-austenitic junction, which latter .is the junction of buttered layer 31 and surface 21 of member 20.
  • This weld overlay is deposited of an austenitic heat resisting steel alloy having a coefficient of thermal expansion intermediate the corresponding coefficients of members 10 and 20.
  • a suitable austenitic steel alloy for overlay 35 is a 25 -Cr-20 Ni steel, for example, or a 77 Ni15 Cr steel .known as Inconel. Another suitable austenitic steel'is an 80 Ni Cr steel.
  • the cotficients of thermal expansion, from room temperature to 1200 F. are 7.69 X 10 for the Croloy 2% member 10, and 10.41 x 10 for the :18-8Ti member 20.
  • the corresponding coefiicient for a Cr-20 Ni overlay is 9.20 x 10*, which is inter- -mediate the coefiicients of the base members '10 and 20.
  • the heat resistant overlay 35 protects the relatively .vulnerable ferritic-austenitic junction (21-31) from the extreme effects of cyclically varying elevated temperatures during service. As the expansion of the overlay, -with change in temperature, is intermediate the expan- -sions of members 10 and 20, the tendency of the joint 'to fail due to differential thermal expansion of the base members is substantially eliminated. Welded joints between dissimilar metal members, including overlay 35, -have a life as much as five times the life of corresponding -joints without the overlay, when subjected to cyclically -.varying elevated, temperatures, 1
  • the entire welding groove is filled with a fusion deposit 33 of carbide stabilized ferritic metal having an oxidation resistance higher than that of ferritic alloy steel member 10.
  • deposit 33 may be the 5 Cr--.5 Mo-Cb ferritic steel useful for the butten'ng layer 31 of Fig. 1.
  • Deposit 33 resists carbon migration, due to its carbide stabilization by the Cb, and resists oxidation at the filatively high and cyclical-1y varying temperatures to which the 10 joint is subjected in service.
  • At least the ferritic-austenitic junction 2133) is then covered with the fusion deposited overlay 35 in the same manner as in the embodiment of Fig. l.
  • Overlay 35 may be one of the same heat resistant austenitic alloys as 15 used in forming the overlay 35 of Fig. 1.
  • the weld groove forming surface 11 of ferritic member 10 is first buttered with a fusion deposit 34 ,of a carbide-stabilized ferritic steel alloy, such as the 5 Cr-.5 Mo-Cb steel previously 20 mentioned.
  • the remainder of the weld groove is then filled with a fusion deposit of an austenitic, heat resisting, steel alloy having a coeflicient of thermal expansion intermediate those of members 10 and 20.
  • this may be the 25 Cr 20 Ni austenitic steel alloy, or
  • the deposit 36 is continued to form the overlay deposit 35 so that the austenitic-ferritic junction 3436 is covered by such heat resistant austenitic steel alloy.
  • the carbide-stabilized ferriticalloy steel deposit having higher oxidation resistance than that of the ferritic alloy steel member 10 such as deposits 31, 33 and 34- may, in general, have a higher chromium or silicon content than those of member 10, and may also have a slightly lower coefficient of thermal expansion. While this is less favorable than would be the case witha coefficient of thermal expansion somewhat higher than that of member 10, the slight decrease is insignificant and is out-balanced by the higher oxidation resistance.
  • the combination of the carbide-stabilized and higher oxida- 40 tion resistance deposit with the oxygen barrier over the dissimilar junction provides an effective safeguard against stress-oxidation or stress-oxidation-fatigue cracking.
  • a composite welded assembly having an extended service life when subjected to cyclically varying elevated temperatures of the order of 1100 F. and higher, said assembly comprising, in combination, a ferritic alloy steel member having a weldv groove forming surface; an austenitic alloy steel member having a weld groove forming surface; and a fusion welded joint uniting said members comprising afusionweld deposit fused to .bothof said surfaces and including afusion weld section of a carbide stabilized ferritic alloy steel having an oxidation resistance .higher than that of said ferritic steel member, and a fusion weld section of a heat and oxidation resistant austenitic alloy steeljsaid ferritic alloysteel section of said deposit beingfu sedtoatleast one of said surfaces and said austenitic alloy steel section of said deposit being fused to said ferritic alloy steelsection of-saiddepositand overlyingand overlapping theferritic-austenitic junction of said assembly.
  • a composite welded assembly having an extended service life when subjected to cyclically-varying elevated temperatures of the order of l100 F. andhigher, said -assembly comprising, in combination, a ferritic alloy steel member. having a weld'groove forming surface;.,an austenitic alloy steel-memberhavinga weld groove forming surface; and a fusionwel dedjointunitingsaiimemhers comprising a fusion weld deposit.
  • ferritic alloy steel section of said deposit being fused to at least one of said surfaces and said austenitic alloy steel section of said deposit being fused to said ferritic alloy steel section of said deposit and overlying and overlapping the ferritic-austenitic junction of said assembly.
  • a composite welded assembly having an extended service life when subjected to cyclically varying elevated temperatures of the order of 1100 F. and higher, said assembly comprising, in combination, a ferritic alloy steel member having a weld groove forming surface; an austenitic alloy steel member having a weld groove forming surface; and a fusion welded joint uniting said members comprising a fusion weld deposit fused to both of said surfaces and including a fusion weld section of a carbide stabilized ferritic alloy steel having an oxidation resistance higher than that of said ferritic alloy steel member, and
  • a composite welded assembly as claimed in claim 1 in which said ferritic alloy steel section of said deposit is deposited against the groove forming surface of said austenitic member; and including a fusion deposit of a ferritic alloy steel, of substantially the same composition as the ferritic alloy member, deposited between said first deposit and the groove forming surface of said ferritic member.
  • a composite welded assembly as claimed in claim 1 in which said ferritic alloy steel section of said deposit is deposited against the groove forming surfaces of both of said members.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
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Description

Dec. 6, 1960 F. T. EBERLE 2,963,129
DISSIMILAR METAL WELDED JOINT WITH PROTECTIVE OVERLAY Filed Dec. 9, 1954 FERRITIC ALLOY STEEL AUSTENITIC ALLOY STEEL FIG. 2
FERRITIC ALLOY STEEL AUSTENITIC ALLOY STEEL FERRITIC ALLOY STEEL AUSTENITIC ALLOY STEEL INVENTOR FRITZ T. EBERLE' ATTORNEY of the steam generators.
lot the "pile, those due DISSIMILAR METAL WELDED JOINT WITH PROTECTIVE OVERLAY Filed Dec. 9, 1954, Ser. No. 474,175 7 Claims. Cl. 189-36 This invention relates to the production of a welded joint between austenitic and ferritic materials suitable for high temperatures, high "pressure service under conditions involving thermal shock and cyclic temperature and load applications.
Such conditions are encountered in high temperature process plants such. as, for example, oil refineries, in vapor or steam generators, and in heat exchangers of various types. The particular problems in any one type of installation may differ in one or more aspects from those in another type. Thus, refineries involve high temperatures but only moderate pressures, in conjunction with alternating oxidation and reducing conditions, corrosive environments and the like. In steam generators a more complex stress condition exists due to the combined actions of high operating pressures and high operating temperatures, which are further aggravated by cyclic variations in these factors. While the invention is of general application under high temperature, high stress conditions in any type of installation, particular reference will be made, by way of example only, to thehigh temperature and high stress conditions encountered in steam generators.
In order to obtain higher efficiencies, the outlet steam temperatures and the operating pressures of central station steam generators have been constantly increasing, and presently some central station steam generating units have outlet temperatures of 1050 F. and operating pressures of over 2000 p.s.i. The increasing useof such high temperatures and pressures has brought with it problems .of providing materials and joints between such materials which will successfully withstand the stresses encountered ithereat.
The long time load carrying characteristics of metals at high temperatures, together with the economics in- "volved, have led steam generator designers to use both austenitic and ferritic materials for the outlet components material may be used in the superheater and its supports, and in the main steam line from the generator to the turbine. Use of both types of materials in the same component requires that'particular attention be given to the junctions between these materials, which junctions must operate under the particular temperature and stress conditions encountered in producingsteam at relatively high temperatures. In a superheater, for example, the external surface and the superheater support lugs are at a higher temperature than'the internal surface of the superheater tubes, due to the higher temperatures of the heat- ;ing gases as compared to the temperature of the steam flowing through the superheater. The reverse is true with respect to the steam line leading to the turbine.
Operation under stress at such high temperatures intro- 'c luces many problems due to the difierential expansion and contraction of the dissimilar materials on either side joint, their relative surface and structural stability, Aside from mechanical stresses, such as, for exam- For example, both types of Patented Dec, 6, 1960 traction, the factors influencing the service life of welded basically of a metallurgical nature, such as carbon depletion in the heat affected zone of the ferritic material, notching due to oxide penetration occurring therein, micro-fissuring in the weld junction, and accelerated creep due to these conditions. Examples of joints between ferritic and austenitic materials, with which these problems are encountered, are the joining of a ferritic alloy having substantially 2%% chromium to an austenitic alloy of the 18-8 or 25-20 type.
The present invention is particularly directed to the production of a welded joint, between austenitic and ferritic materials, which has the requisite strength, ductility, and oxidation resistance to assure satisfactory performance under conditions of high stresses occasioned by thermal shock, cyclic temperature and load application, and differential thermal expansion. It has been found that these objectives can be obtained by Weld uniting a low alloy ferritic member to an austenitic member by a weld deposit which is carbide-stabilized, has an oxidation resistance which is higher than that of the ferritic member, and a coeflicient of thermal expansion intermediate the coefficients of thermal expansion of the two members, the weld deposit including an overlying heat resistant oxygen barrier. The welded joint is a composite deposit of two or more metals, at least one of which is a carbidestabilized and oxidation-resistant ferritic metal and at least one more of which is an austenitic, heat-and-oxidation-resistant metal.
In one embodiment of the invention, the weld groove forming surface of the austenitic member is buttered with a carbide-stabilized, ferritic metal having an oxidation resistance higher than that of the ferritic member. The remainder of the weld groove is then filled with a ferritic metal of substantially the same composition as that of the ferritic member, and which may be carbidestabilized. At least the ferritic-austenitic junction of the welded joint is then covered with a weld deposit overlay of an austenitic heat-resisting metal having a heat expansion coefiicient which is intermediate the heat expansion coeflicients of the two base members.
In another embodiment, the weld groove between the ferritic and austenitic base members is filled with a carbide-stabilized, ferritic metal having a higher oxidation resistance than that of the ferritic base member. At least the ferritic-austenitic junction of the Welded point is then provided with substantially the same overlay as in the first embodiment. L
In a further embodiment, the weld groove forming surface of the ferritic member is buttered with a carbide-stabilized, ferritic metal having an oxidation 'resistance higher than that of the ferritic member. The remainder of the weld groove is then filled with anaustenitic, heat-resisting metal having a coeflicient of thermal expansion intermediate those of the base members, the weld depositio'n of this latter metal being continued to form an overlay thereof across the ferritic austenitic junction.
For a more complete understanding of the invention principles, reference is made to the following description of a typical embodiment thereof as illustrated in the accompanying drawings.
In the drawings:
Figs. 1, 2 and 3 are partial transverse sectional views of welded points, each weld uniting a low alloy. ferritic base member to an austenitic base member, and embodying the invention. a
' -In the following description of the invention, the term 1 ferriticalloy' is used to designate alloys having compositions such as carbon--0.5% molybdenum, 2% Crto differential thermal expansion and con- =3 similar predominantly ferritic alloy steels. Similarly, the term austenitic alloy refers to alloys known to those skilled in the art as 18-8 (18 Cr-8 Ni), 18-8 Cb, 18-8 Ti, 25-12, "25-20, or any other alloy-steel which is predominantly austenitic in structure.
Referring to Fig. 1 of the drawing, a predominantly ferritic alloy steel workpiece 10, such as a pressure tube or pipe, is illustrated as weld united to a predominantly austenitic alloy steel workpiece 20, such as a pressure tube or pipe, by a fusion deposited, carbide-stabilized, welded joint 30'having an oxidation resistance which is higher than that of member 10 and a coefiicient of thermal expansion intermediate the corresponding coefficients of members 10 and 20, joint 30 including an overlying heat-resistant oxidation barrier 35. By way of example only, ferritic member 10 may be an alloy steel containing 2%% chromium and 1% molybdenum, this .steel being known commercially as fCroloy 2%, and austenitic member 20 may be an 188Ti alloy steel. The facing end surfaces of members 10 and 20 are suitably bevelled, as at 11 and 21, respectively, to form a weld groove, a backing member 15 being arranged to bridge the open lower end of the welding groove.
In this embodiment of the invention, the 'weld groove forming surface 21 of austenitic alloy steel member 20 is first buttered with a fusion deposit 31 of carbide- .stabilized ferritic metal having an oxidation resistance higher than that of ferritic alloy steel member 10. This deposit or layer 31 resists carbon migration, due to its being carbide-stabilized, and also resists oxidation at the relatively high and cyclically varying working temperatures to which joint 30 is exposed in practice. If, by way of example, member 10 is a low alloy steel containing 2%% Cr and 1% M or 3% Cr and 1% M0, the metal deposited to form buttering layer 31 may be a 5% Cr0.5% Mo alloy steel stabilized with Cb (a S Cr.5 .MoCb steel).
The remainder of the weld groove between surface 11 of member and layer 31 is then filled with a fusion deposit 32 of ferritic alloy steel having about the composition of member 10. In the specific example given, deposit 32 may be a 2%.% Cr1% Mo ferritic alloy steel. Deposit 32 may also be of carbide-stabilized ferritic alloy steel such as 254% Cr1% Mo-Cb alloy steel, for example.
As the final step in forming the welded joint or weld deposit 30, the protective overlay 35 is fusion deposited at least across the ferritic-austenitic junction, which latter .is the junction of buttered layer 31 and surface 21 of member 20. This weld overlay is deposited of an austenitic heat resisting steel alloy having a coefficient of thermal expansion intermediate the corresponding coefficients of members 10 and 20.
A suitable austenitic steel alloy for overlay 35 is a 25 -Cr-20 Ni steel, for example, or a 77 Ni15 Cr steel .known as Inconel. Another suitable austenitic steel'is an 80 Ni Cr steel. In the specific welded joint given by way of example, the cotficients of thermal expansion, from room temperature to 1200 F., are 7.69 X 10 for the Croloy 2% member 10, and 10.41 x 10 for the :18-8Ti member 20. The corresponding coefiicient for a Cr-20 Ni overlay is 9.20 x 10*, which is inter- -mediate the coefiicients of the base members '10 and 20.
The heat resistant overlay 35 protects the relatively .vulnerable ferritic-austenitic junction (21-31) from the extreme effects of cyclically varying elevated temperatures during service. As the expansion of the overlay, -with change in temperature, is intermediate the expan- -sions of members 10 and 20, the tendency of the joint 'to fail due to differential thermal expansion of the base members is substantially eliminated. Welded joints between dissimilar metal members, including overlay 35, -have a life as much as five times the life of corresponding -joints without the overlay, when subjected to cyclically -.varying elevated, temperatures, 1
In the embodiment of Fig. 2, the entire welding groove is filled with a fusion deposit 33 of carbide stabilized ferritic metal having an oxidation resistance higher than that of ferritic alloy steel member 10. By way of ex- 5 ample, deposit 33 may be the 5 Cr--.5 Mo-Cb ferritic steel useful for the butten'ng layer 31 of Fig. 1. Deposit 33 resists carbon migration, due to its carbide stabilization by the Cb, and resists oxidation at the filatively high and cyclical-1y varying temperatures to which the 10 joint is subjected in service.
At least the ferritic-austenitic junction 2133) is then covered with the fusion deposited overlay 35 in the same manner as in the embodiment of Fig. l. Overlay 35 may be one of the same heat resistant austenitic alloys as 15 used in forming the overlay 35 of Fig. 1.
In the embodiment of Fig. 3, the weld groove forming surface 11 of ferritic member 10 is first buttered with a fusion deposit 34 ,of a carbide-stabilized ferritic steel alloy, such as the 5 Cr-.5 Mo-Cb steel previously 20 mentioned. The remainder of the weld groove is then filled with a fusion deposit of an austenitic, heat resisting, steel alloy having a coeflicient of thermal expansion intermediate those of members 10 and 20. For example, this may be the 25 Cr 20 Ni austenitic steel alloy, or
25 the Inconel" alloy, previously mentioned. The deposit 36 is continued to form the overlay deposit 35 so that the austenitic-ferritic junction 3436 is covered by such heat resistant austenitic steel alloy.
i The carbide-stabilized ferriticalloy steel deposit having higher oxidation resistance than that of the ferritic alloy steel member 10such as deposits 31, 33 and 34- may, in general, have a higher chromium or silicon content than those of member 10, and may also have a slightly lower coefficient of thermal expansion. While this is less favorable than would be the case witha coefficient of thermal expansion somewhat higher than that of member 10, the slight decrease is insignificant and is out-balanced by the higher oxidation resistance. The combination of the carbide-stabilized and higher oxida- 40 tion resistance deposit with the oxygen barrier over the dissimilar junction provides an effective safeguard against stress-oxidation or stress-oxidation-fatigue cracking.
While specific embodiments of the inventionhave been shown and described in detail to illustrate the application 5 of the invention principles, it should be understood that the invention may be otherwise embodied without departing from such principles.
What is claimed is: a
1. A composite welded assembly having an extended service life when subjected to cyclically varying elevated temperatures of the order of 1100 F. and higher, said assembly comprising, in combination, a ferritic alloy steel member having a weldv groove forming surface; an austenitic alloy steel member having a weld groove forming surface; and a fusion welded joint uniting said members comprising afusionweld deposit fused to .bothof said surfaces and including afusion weld section of a carbide stabilized ferritic alloy steel having an oxidation resistance .higher than that of said ferritic steel member, and a fusion weld section of a heat and oxidation resistant austenitic alloy steeljsaid ferritic alloysteel section of said deposit beingfu sedtoatleast one of said surfaces and said austenitic alloy steel section of said deposit being fused to said ferritic alloy steelsection of-saiddepositand overlyingand overlapping theferritic-austenitic junction of said assembly.
2. A composite welded assembly having an extended service life when subjected to cyclically-varying elevated temperatures of the order of l100 F. andhigher, said -assembly comprising, in combination, a ferritic alloy steel member. having a weld'groove forming surface;.,an austenitic alloy steel-memberhavinga weld groove forming surface; and a fusionwel dedjointunitingsaiimemhers comprising a fusion weld deposit. fused to both of said Surfaces and including a fusion weld section bfj-a carbide stabilized ferritic alloy steel having an oxidation resistance higher than that of said ferritic alloy steel member, and a fusion weld section of a heat and oxidation resistant austenitic alloy steel having a coeflicient of thermal expansion intermediate those of said members; said ferritic alloy steel section of said deposit being fused to at least one of said surfaces and said austenitic alloy steel section of said deposit being fused to said ferritic alloy steel section of said deposit and overlying and overlapping the ferritic-austenitic junction of said assembly.
3. A composite welded assembly having an extended service life when subjected to cyclically varying elevated temperatures of the order of 1100 F. and higher, said assembly comprising, in combination, a ferritic alloy steel member having a weld groove forming surface; an austenitic alloy steel member having a weld groove forming surface; and a fusion welded joint uniting said members comprising a fusion weld deposit fused to both of said surfaces and including a fusion weld section of a carbide stabilized ferritic alloy steel having an oxidation resistance higher than that of said ferritic alloy steel member, and
' a fusion weld section of a heat and oxidation resistant austenitic alloy steel having a coefficient of thermal expansion itnermediate those of said members; said ferritic alloy steel section of said deposit being fused to said austenitic alloy steel member surface and said austenitic alloy steel section of said deposit being also fused to said austenitic alloy steel member surface and overlying and overlapping the ferritic-austenitic junction of said asscmbly.
4. A composite welded assembly as claimed in claim 1 in which said ferritic alloy steel section of said deposit is deposited against the groove forming surface of said austenitic member; and including a fusion deposit of a ferritic alloy steel, of substantially the same composition as the ferritic alloy member, deposited between said first deposit and the groove forming surface of said ferritic member.
5. A composite welded assembly as claimed in claim 1 in which said ferritic alloy steel section of said deposit is deposited against the groove forming surfaces of both of said members. 1
6. A composite welded assembly as claimed in claim 2 in which the fusion weld deposit further includes a fusion weld section of a ferritic alloy steel having substantially the same composition as said ferritic member.
7. A composite welded assembly as claimed in claim 3 in which said weld deposit further includes a fusion weld section of a ferritic alloy steel having substantially the same composition as said ferritic member.
References Cited in the file of this patent UNITED STATES PATENTS 1,808,205 Bryant et al. June 2, 1931 1,959,791 Kautz June 22, 1934 2,054,939 Larson Sept. 22, 1936 2,158,799 Larson May 16, 1939 2,209,290 Watts Jan 23, 1940 2,240,672 Scherer et a1 May 6, 1941 2,759,249 Eberle Aug. 21, 1956 2,769,227 Sykes et al. Nov. 6, 1956
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US3163501A (en) * 1961-10-13 1964-12-29 Bbc Brown Boveri & Cie Process for the production of welded seams in niobium and vanadium steels, and welded joints produced thereby
US3194642A (en) * 1960-04-22 1965-07-13 Westinghouse Electric Corp Welding structure and method of making such structure
US3484930A (en) * 1965-03-04 1969-12-23 Ishikawajima Harima Heavy Ind Welding process for high tensile strength steel
US3693240A (en) * 1969-08-27 1972-09-26 Sandvikens Jernverks Ab Method of manufacturing filler material for welding
US3712317A (en) * 1966-09-29 1973-01-23 Messrs Mitsubishi Jukogyo Kk Corrosion resistant boiler tube for chemical recovery vapor generating unit
US3915666A (en) * 1971-04-28 1975-10-28 Voest Ag Steel composite having resistance to carbon diffusion
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US4049186A (en) * 1976-10-20 1977-09-20 General Electric Company Process for reducing stress corrosion in a weld by applying an overlay weld
US4135739A (en) * 1978-02-27 1979-01-23 The Babcock & Wilcox Company Off-set welding ring
FR2402107A1 (en) * 1977-09-06 1979-03-30 Bbc Brown Boveri & Cie ASSEMBLY PROCEDURE OF TWO SHAFT PARTS
US4178417A (en) * 1977-03-23 1979-12-11 The Japan Steel Works, Ltd. Clad steel
US4256518A (en) * 1978-03-16 1981-03-17 Smith International, Inc. Welding and austenitizing earth boring apparatus
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US4298053A (en) * 1974-03-18 1981-11-03 Metallurgie Hoboken-Overpelt Casting belts for machines for the continuous casting of metals
US4318966A (en) * 1980-03-31 1982-03-09 Imperial Chemical Industries Limited Welded structures
DE3406314A1 (en) * 1983-02-28 1984-08-30 Ishikawajima-Harima Jukogyo K.K., Tokio/Tokyo METHOD FOR RELIEVING RESIDUAL TENSIONS BY WELDING AN ORDER OVER THE EXTERNAL SURFACE OF A TUBE
US4624402A (en) * 1983-01-18 1986-11-25 Nutech, Inc. Method for applying an overlay weld for preventing and controlling stress corrosion cracking
US4700863A (en) * 1986-01-09 1987-10-20 The United States Of America As Represented By The United States Department Of Energy Seal welded cast iron nuclear waste container
US4702406A (en) * 1986-10-16 1987-10-27 Carolina Power & Light Company Forming stable welded joints between dissimilar metals
US4703885A (en) * 1985-11-15 1987-11-03 Ga Technologies Inc. Method of welding austenitic steel to ferritic steel with filler alloys
US5536050A (en) * 1995-01-23 1996-07-16 Usx Corporation Connection for fabricating mandrel bar from used segments
FR2742369A1 (en) * 1995-12-18 1997-06-20 Framatome Sa METHOD FOR CONNECTING HETEROGENEOUS WELDING OF TWO PIECES AND USE
WO2000056498A1 (en) * 1999-03-23 2000-09-28 Exxonmobil Upstream Research Company Welding process and welded joints
US20100006545A1 (en) * 2005-12-22 2010-01-14 Macia Mario L Welding of Pipeline to Enhance Strain Performance
WO2012096937A1 (en) * 2011-01-10 2012-07-19 Arcelormittal Investigacion Y Desarrollo S.L. Method of welding nickel-aluminide
US20120237287A1 (en) * 2009-12-04 2012-09-20 Ryuichi Honma Butt-welded joint and method for manufacturing same
US20120301309A1 (en) * 2011-05-23 2012-11-29 Hitachi, Ltd. Dissimilar metal welds and its manufacturing method of large welded structures such as the turbine rotor
US20120325898A1 (en) * 2005-07-29 2012-12-27 Areva Np Gmbh Method for repairing a welded connection
CN103733453A (en) * 2012-05-31 2014-04-16 古河电气工业株式会社 Structure and method for connecting former of superconducting cable
DE102014226492A1 (en) * 2014-12-18 2016-06-23 Sitech Sitztechnik Gmbh Method for connecting fittings for a FeMn-based seat back adjuster
US20180126437A1 (en) * 2012-03-28 2018-05-10 Nippon Steel & Sumitomo Metal Corporation Tailored blank for hot stamping, hot stamped member, and methods for manufacturing same
US20180245616A1 (en) * 2015-09-15 2018-08-30 Panasonic Intellectual Property Management Co., Ltd. Weld structure of metal member and welding process
US11065705B2 (en) * 2015-09-14 2021-07-20 Nippon Steel Corporation Fillet welding method and fillet welded joint
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Cited By (48)

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Publication number Priority date Publication date Assignee Title
US3194642A (en) * 1960-04-22 1965-07-13 Westinghouse Electric Corp Welding structure and method of making such structure
US3163501A (en) * 1961-10-13 1964-12-29 Bbc Brown Boveri & Cie Process for the production of welded seams in niobium and vanadium steels, and welded joints produced thereby
US3484930A (en) * 1965-03-04 1969-12-23 Ishikawajima Harima Heavy Ind Welding process for high tensile strength steel
US3712317A (en) * 1966-09-29 1973-01-23 Messrs Mitsubishi Jukogyo Kk Corrosion resistant boiler tube for chemical recovery vapor generating unit
US3693240A (en) * 1969-08-27 1972-09-26 Sandvikens Jernverks Ab Method of manufacturing filler material for welding
US3915666A (en) * 1971-04-28 1975-10-28 Voest Ag Steel composite having resistance to carbon diffusion
US3956809A (en) * 1972-05-30 1976-05-18 Allegheny Ludlum Industries, Inc. Pressure bonded composite material with low yield strength
US4298053A (en) * 1974-03-18 1981-11-03 Metallurgie Hoboken-Overpelt Casting belts for machines for the continuous casting of metals
US4049186A (en) * 1976-10-20 1977-09-20 General Electric Company Process for reducing stress corrosion in a weld by applying an overlay weld
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US4178417A (en) * 1977-03-23 1979-12-11 The Japan Steel Works, Ltd. Clad steel
US4208003A (en) * 1977-09-06 1980-06-17 Bbc Brown Boveri & Company Limited Method of joining shaft sections
FR2402107A1 (en) * 1977-09-06 1979-03-30 Bbc Brown Boveri & Cie ASSEMBLY PROCEDURE OF TWO SHAFT PARTS
US4135739A (en) * 1978-02-27 1979-01-23 The Babcock & Wilcox Company Off-set welding ring
US4256518A (en) * 1978-03-16 1981-03-17 Smith International, Inc. Welding and austenitizing earth boring apparatus
US4273159A (en) * 1978-03-16 1981-06-16 Smith International, Inc. Earth boring apparatus with multiple welds
US4318966A (en) * 1980-03-31 1982-03-09 Imperial Chemical Industries Limited Welded structures
US4624402A (en) * 1983-01-18 1986-11-25 Nutech, Inc. Method for applying an overlay weld for preventing and controlling stress corrosion cracking
DE3406314A1 (en) * 1983-02-28 1984-08-30 Ishikawajima-Harima Jukogyo K.K., Tokio/Tokyo METHOD FOR RELIEVING RESIDUAL TENSIONS BY WELDING AN ORDER OVER THE EXTERNAL SURFACE OF A TUBE
US4703885A (en) * 1985-11-15 1987-11-03 Ga Technologies Inc. Method of welding austenitic steel to ferritic steel with filler alloys
US4700863A (en) * 1986-01-09 1987-10-20 The United States Of America As Represented By The United States Department Of Energy Seal welded cast iron nuclear waste container
US4702406A (en) * 1986-10-16 1987-10-27 Carolina Power & Light Company Forming stable welded joints between dissimilar metals
EP0264292A1 (en) * 1986-10-16 1988-04-20 CAROLINA POWER & LIGHT COMPANY Forming stable welded joints between dissimilar metals
US5536050A (en) * 1995-01-23 1996-07-16 Usx Corporation Connection for fabricating mandrel bar from used segments
FR2742369A1 (en) * 1995-12-18 1997-06-20 Framatome Sa METHOD FOR CONNECTING HETEROGENEOUS WELDING OF TWO PIECES AND USE
US6080960A (en) * 1995-12-18 2000-06-27 Framatome Method for joining two parts by heterogeneous welding and use thereof
WO1997022432A1 (en) * 1995-12-18 1997-06-26 Framatome Method for joining two parts by heterogeneous welding and use thereof
WO2000056498A1 (en) * 1999-03-23 2000-09-28 Exxonmobil Upstream Research Company Welding process and welded joints
US6336583B1 (en) 1999-03-23 2002-01-08 Exxonmobil Upstream Research Company Welding process and welded joints
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US20120325898A1 (en) * 2005-07-29 2012-12-27 Areva Np Gmbh Method for repairing a welded connection
US8729418B2 (en) * 2005-07-29 2014-05-20 Areva Gmbh Method for repairing a welded connection
US20100006545A1 (en) * 2005-12-22 2010-01-14 Macia Mario L Welding of Pipeline to Enhance Strain Performance
US8653403B2 (en) * 2009-12-04 2014-02-18 Nippon Steel & Sumitomo Metal Corporation Butt-welded joint and method for manufacturing same
US20120237287A1 (en) * 2009-12-04 2012-09-20 Ryuichi Honma Butt-welded joint and method for manufacturing same
US9623509B2 (en) 2011-01-10 2017-04-18 Arcelormittal Method of welding nickel-aluminide
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US20120301309A1 (en) * 2011-05-23 2012-11-29 Hitachi, Ltd. Dissimilar metal welds and its manufacturing method of large welded structures such as the turbine rotor
US20180126437A1 (en) * 2012-03-28 2018-05-10 Nippon Steel & Sumitomo Metal Corporation Tailored blank for hot stamping, hot stamped member, and methods for manufacturing same
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US20150107867A1 (en) * 2012-05-31 2015-04-23 International Superconductivity Technology Center Structure and method for connecting formers of superconducting cables
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