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creep elongation
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Journal Articles
Alloy Digest (2019) 68 (1): Ni-749.
Published: 01 January 2019
... Manaurite XMR is a heat resistant alloy for hydrocarbon processing. It is a modified version of Manaurite XM (Alloy Digest Ni-748, December 2018) designed to withstand creep elongation at high temperature, while also being able to be welded after aging. This datasheet provides information...
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Manaurite XMR is a heat resistant alloy for hydrocarbon processing. It is a modified version of Manaurite XM (Alloy Digest Ni-748, December 2018) designed to withstand creep elongation at high temperature, while also being able to be welded after aging. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on joining. Filing Code: Ni-749. Producer or source: Manoir Pîtres.
Journal Articles
Alloy Digest (1977) 26 (10): Zn-32.
Published: 01 October 1977
... (Smooth, no notch), ft-lb As-Cast Heat Treated 5800064000 4500047000 53000 40000 3-6 8-11 110-120 90-l 00 42000 32000 11 13 Table 2 - CREEP DATA AT 680F Stress, psi Creep elongation in 105 hours, % 9000* 0.1 *Design stress. Heat Treatment: If more than 3 - 6% elongation is required, an optional...
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ZA-27 is a zinc-aluminum-copper alloy that offers exceptionally high strength (58,000 to 64,000 psi tensile strength as cast) at modest cost. It performs best in thin-walled castings (down to 0.10 inch) which means reduced weight and lower material costs when castings are redesigned. It is similar to the general-purpose ZA-12 alloy (Alloy Digest Zn-31, September 1977) except for its higher strength and elongation, but with higher casting temperatures and poor heavy-section castability. This datasheet provides information on composition, physical properties, hardness, tensile properties, and shear strength as well as fracture toughness and creep. It also includes information on corrosion and wear resistance as well as casting, forming, heat treating, machining, and surface treatment. Filing Code: Zn-32. Producer or source: Eastern Alloys Inc.. See also Alloy Digest Zn-50, June 1990.
Journal Articles
Alloy Digest (2021) 70 (11): Mo-21.
Published: 01 November 2021
... that is stable at temperatures up to 2000 °C (3630 °F). After recrystallization, the elongated grain structure with jagged grain boundaries provides a measurable increase in ductility and creep resistant strength over that seen with pure molybdenum. Ed Fagan Molybdenum Lanthanum Oxide is the preferred material...
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Ed Fagan Molybdenum Lanthanum Oxide, often referred to as lanthanated molybdenum, MoLa or ML, is an oxide dispersion strengthened alloy. It is produced by combining small amounts of lanthanum oxide (La2O3) particles with molybdenum. This creates a special stacked fiber microstructure that is stable at temperatures up to 2000 °C (3630 °F). After recrystallization, the elongated grain structure with jagged grain boundaries provides a measurable increase in ductility and creep resistant strength over that seen with pure molybdenum. Ed Fagan Molybdenum Lanthanum Oxide is the preferred material when embrittlement after recrystallization must be avoided. This alloy maintains its dimensional shape stability at high-temperatures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on wear resistance as well as heat treating and machining. Filing Code: Mo-21. Producer or source: Ed Fagan Inc.
Journal Articles
Alloy Digest (1975) 24 (7): Zn-20.
Published: 01 July 1975
... NJZ ALLOY No. 10 is an alloy with medium tensile strength and elongation. It is produced from a high-grade zinc base by additions of cadmium, iron, and lead. It combines good ductility with stiffness and its applications include hardware and laundry tags. This datasheet provides information...
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NJZ ALLOY No. 10 is an alloy with medium tensile strength and elongation. It is produced from a high-grade zinc base by additions of cadmium, iron, and lead. It combines good ductility with stiffness and its applications include hardware and laundry tags. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep and fatigue. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Zn-20. Producer or source: New Jersey Zinc Company.
Journal Articles
Alloy Digest (1995) 44 (7): Al-336.
Published: 01 July 1995
...: Various aluminum companies. Producer or Source: Various aluminum companies Copyright © ASM International® 1996 1996 ASM International aluminum alloy 201.0 cast aluminum alloys castability chemical composition creep properties elasticity elongation fatigue properties heat treatability...
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ALUMINUM ALLOY 201.0 is a structural casting alloy available as sand, permanent mold and investment castings. It is used in structural casting members, applications requiring high tensile and yield strengths with moderate elongation, and where high strength and energy-absorption capacity are needed. This datasheet provides information on composition, physical properties, and elasticity as well as creep and fatigue. It also includes information on high temperature performance as well as casting, heat treating, machining, joining, and surface treatment. Filing Code: AL-336. Producer or source: Various aluminum companies.
Journal Articles
Alloy Digest (2018) 67 (12): ni-748.
Published: 01 December 2018
... Published by ASM International® :: Data shown are typical, not to be used for specification or final design. Specification Equivalents EN 1.4852 ASTM HP+MA General Characteristics Manaurite XM was designed to withstand creep elongation at high temperature, while also being able to be welded after aging...
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Manaurite XM is a heat resistant alloy for hydrocarbon processing. It is a microalloyed evolution of Manaurite 36X (Alloy Digest SS-1296, May 2018). This datasheet provides information on composition and physical properties as well as creep. It also includes information on joining. Filing Code: Ni-748. Producer or source: Manoir Pîtres.
Journal Articles
Alloy Digest (1988) 37 (11): Zn-44.
Published: 01 November 1988
...), ft-lb 11 43 Fatigue strength (rotary bend), psi (5 x 108 cycles) 15000 Table 2 - CREEP DATA AT 68 F Stress, psi Creep elongation in 105 hours, % *Design stress. 9ooo* 0.1 Heat Treatment: Machinability: If more than 3-6% elongation is required, an optional...
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UNS No. Z35840 is a zinc-aluminum-copper alloy that offers exceptionally high strength (58,000 to 64,000 psi tensile strength as cast) at modest cost. It performs best in thin-walled castings (down to 0.10 inch) which means reduced weight and lower material costs when castings are redesigned. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fracture toughness, creep, and fatigue. It also includes information on corrosion and wear resistance as well as forming, heat treating, machining, and surface treatment. Filing Code: Zn-44. Producer or source: Zinc alloy producers.
Journal Articles
Alloy Digest (1988) 37 (7): Ni-358.
Published: 01 July 1988
... tensile properties. solution annealed. 1170°C. water quench. Temperature. Oc sm?oDapos33laonm .E . Rio loo n :SOP 5; .mjj . lom Temperature. OF Fig. 2 - Typical 1 %-creep elongation, solution annealed, 1170 C, water quench. 45000 (310) 30 40000 (276) 35 35000 (240) 35 40000 (276) 35 Temperan~aoC 600 700...
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NICROFER 4722 Co is a high-strength matrix-stiffened nickel-chromium-molybdenum-iron alloy with cobalt and tungsten additions. It has excellent oxidation resistance up to 2190 F (1200 C). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-358. Producer or source: Vereingte Deutsche Metallwerke AG.
Journal Articles
Alloy Digest (1975) 24 (3): Co-41.
Published: 01 March 1975
... hr Tempcr- alure Table 3 - CREEP DATA (As-forged condition) Stress. psi, to Cause 1%. Creep Elongation in As-Cast 1740 As-Forged 1290 1470 1650 1740 1830 01: 5000 2400 1600 I 29n 1380 5W0 I69W 1370 15300 10300 6800 1560 6800 3300 1600 16.511 4300 2700 I7O(l I740 3000 1830 10 hr Ion hr 1000 hr 10.000...
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UMCo-50 is a cobalt-chromium-iron heat-resistant alloy with good resistance to thermal shock, oxidatoin, and corrosion by hot gases, slags and molten copper. These characteristics make it highly suitable for use in the metallurgical and glass industries. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-41. Producer or source: United States Pipe and Foundry Company. Originally published January 1965, revised March 1975.
Journal Articles
Alloy Digest (1975) 24 (4): SS-309.
Published: 01 April 1975
... for its production and by all of the conventional fabricating methods such as drawing and spinning. Creep elongation tests at 1700°F show that Crutemp 25 has better creep resistance than the 25Cr-20Ni and 2oCr-35Ni stainless steels and it appears to be comparable to alloys such as INCONEL* 60 1 alloy...
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CRUTEMP 25 is a fully austenitic stainless steel with outstanding resistance to scaling at elevated temperatures. It also has high strength at elevated temperatures and its weldability is excellent. It is used in such applications as automotive emission control systems and gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-309. Producer or source: Crucible Stainless Steel Division, Colt Industries.
Journal Articles
Alloy Digest (1956) 5 (12): SS-50.
Published: 01 December 1956
... Test Temperature, OF. 1200°F. 65.000 1350°F. Rupture elong., % - . 100~hrs. Creep Rupture, Rupture stress, psi 9o:ooo 52?00 Rupture elong., % 705000 6 500~hrs. Creep Rupture, Rupture stress, psi Rupture elong., % i 47,000 5 Table 3 - CREEP-RUFTURE PROPERTIES (Specimens from disc forging 13.5 dia. x 3...
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DISCALOY is an iron-base heat treatable alloy having good high temperature strength and oxidation resistance. It is corrosion and heat resistant. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SS-50. Producer or source: Westinghouse Electric Corporation.
Journal Articles
Alloy Digest (1965) 14 (11): Ti-46.
Published: 01 November 1965
... ELEVATED TEMPERATURE PROPERTIES - Sheer Test Tensile Yield Reducrion Temperature Strength Strength Elongation of Area oF psi psi (0.2%) % in 2 % 400 96000- 79200- 24 6 888 110000 04 30000 8 4& 800 84000-100000 63800-82000 61600-75000 :: 45-46 1000 80400- 96000 48 Table 5 - TYPICAL CREEP DATA Test...
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Ti-7AI-12Zr is an alpha-type titanium alloy recommended for high temperature applications in the 800-1100 F range where minimum creep and high Creep strength are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-46. Producer or source: Reactive Metals Corporation.
Journal Articles
Alloy Digest (1958) 7 (9): SA-75.
Published: 01 September 1958
... CHATILLON 709 is a low-carbon low-alloy structural steel having good high temperature creep resistance. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on low and high...
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CHATILLON 709 is a low-carbon low-alloy structural steel having good high temperature creep resistance. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on low and high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SA-75. Producer or source: Societe des Usines St. Jacques.
Journal Articles
Alloy Digest (1974) 23 (1): Zr-6.
Published: 01 January 1974
... as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Zr-6. Producer or source: Teledyne Wah Chang Albany. Producer or Source: Teledyne Wah Chang Albany Copyright © ASM...
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Zr-3Nb-1Sn was developed to provide improved elevated temperature mechanical properties over the Zircaloys without reducing corrosion resistance. It is used in nuclear applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Zr-6. Producer or source: Teledyne Wah Chang Albany.
Journal Articles
Alloy Digest (1973) 22 (10): Ti-69.
Published: 01 October 1973
... specified by producer through 2rh in. thick at 700F: 130,000 psi tensile strength, 120.000 psi yield (O.t 10% elongation (2 in.) and 20% reduction of area. * 1950oF 15 min. AC + 13OOoF 1 hr AC. 13OOoFl hrQQ+llOOoF8hrAC. l * 15OOoF 1 hr OQ + 1 lOOoF 8 hr AC. 1300oF 1 hr AC. Table 2 - CREEP DATA AND STABILITY...
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Ti-11 is a super alpha litanium alloy with excellent properties up to at least 1000 F; it has useful properties as high as 1100 F. It offers a good combination of creep resistance and metallurgical and surface stability. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-69. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1964) 13 (3): Ti-38.
Published: 01 March 1964
... in &he alpha-beta field.) Test Tensile Temperature Strength oF psi Alpha Anneal 600 89200 800 82900 1000 80000 Alpha-Beta Anneal 600 90200 800 85200 1000 96000 Table 4 - TYPICAL CREEP PROPERTIES Test Temperature oF Stress, psi to Produce 0.2% Elongation in 150 hours Alpha Anneal Alpha-Beta Anneal 850...
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Ti-5A1-5Sn-5Zr is an alpha type titanium alloy recommended for high temperature applications in the 800-1100 F range where minimum creep is desired. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-38. Producer or source: Titanium Metals Corporation of America.
Journal Articles
Alloy Digest (1958) 7 (4): Ti-15.
Published: 01 April 1958
... MST 821 is a weldable titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fracture...
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MST 821 is a weldable titanium-base alloy having a favorable combination of strength, formability and resistance to creep at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ti-15. Producer or source: Mallory-Sharon Titanium Corporation.
Journal Articles
Alloy Digest (2019) 68 (4): SS-1305.
Published: 01 April 2019
... MANAURITE 900X is a casting alloy with good creep strength and high thermal shock resistance. This alloy is evolution from Manaurite 900 (Alloy Digest SS-1304, March 2019). This datasheet provides information on composition and physical properties as well as creep. It also includes information...
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MANAURITE 900X is a casting alloy with good creep strength and high thermal shock resistance. This alloy is evolution from Manaurite 900 (Alloy Digest SS-1304, March 2019). This datasheet provides information on composition and physical properties as well as creep. It also includes information on high temperature performance as well as joining. Filing Code: SS-1305. Producer or source: Manoir Industries, Manoir Pîtres.
Journal Articles
Alloy Digest (2001) 50 (8): Ti-118.
Published: 01 August 2001
... tensile test, min(a) Test temperature Stress Yield strength, 0.2% Tensile strength °C °F Time, h MPa ksi Total plastic strain, % MPa ksi MPa ksi Elongation, 5D, % Reduction in area, % 540 1004 100 300 44 0.048 820 119 930 135 7 12 (a)The creep test piece is subjected to a room temperature tensile test...
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TIMETAL 829 is a Ti-5.5Al-3.5Sn-3Zr-1Nb-0.25Mo-0.3Si near-alpha titanium alloy that is weldable and has high strength and is a creep resistant high temperature alloy. The major application is as gas turbine engine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on forming and heat treating. Filing Code: TI-118. Producer or source: Timet.
Journal Articles
Alloy Digest (2001) 50 (7): Ti-116.
Published: 01 July 2001
... Elongation, Reduction °C °F MPa ksi MPa ksi 5D, % in area, % 20 68 932 135 1039 151 12 21 100 212 837 121 957 139 12 24 200 392 743 108 887 129 13 28 300 572 697 101 832 121 13 31 400 752 663 96 797 116 13 37 500 932 605 88 771 112 14 42 600 1112 500 73 654 95 15 50 Table 2 Creep Rupture Properties Creep...
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TIMETAL 834 is a Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.35Si-0.06C alloy with high strength and creep resistance up to 593 C (1100 F). The alloy is workable and weldable. It is used in the aerospace industry for rings and compressor disks. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as heat treating. Filing Code: TI-116. Producer or source: Timet.
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