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stress-rupture strength

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Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (3): Co-51.
Published: 01 March 1967
... UMCo-51 is a cobalt-base alloy having high stress-rupture strength. It is recommended for high temperature applications where the mechanical stresses are high, and where resistance to abrasion, thermal shock and oxidation are required. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1977) 26 (4): Ni-243.
Published: 01 April 1977
... and zirconium additions also have been made to obtain optimum stress-rupture strength. It has excellent strength and good resistance to corrosion and oxidation at least to 1600 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (5): Ni-124.
Published: 01 May 1967
... UDIMET M-252 is a vacuum induction method alloy recommended for heavy-duty high temperature applications in the range 1300-1600 F. It has good stress-rupture strength, fatigue strength and mechanical strength at elevated temperatures. The alloy responds to an age-hardening heat treatment...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1978) 27 (9): Ni-257.
Published: 01 September 1978
... UDIMET WASPALOY is a nickel-base, austenitic, precipitation-hardenable alloy. It features outstanding tensile and stress-rupture strength up to 1400 F and high oxidation resistance up to 1600 F. It is used widely in gas turbine engines, airframe assemblies and missile systems. This datasheet...
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Publisher: Journals Gateway
Alloy Digest (1981) 30 (9): Ni-271.
Published: 01 September 1981
... AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile...
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Publisher: Journals Gateway
Alloy Digest (1995) 44 (8): SS-604.
Published: 01 August 1995
... CENTRALLOY 4848 (HK-40) is a cast austenitic 25% chromium-20% nickel-stainless steel. A balanced composition provides excellent structural stability, high stress rupture strength and good resistance to oxidation and carburization. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1995) 44 (9): SS-609.
Published: 01 September 1995
... CENTRALLOY 4852 (HP + Nb) is a cast austenitic 35% nickel-25% chromium alloy plus niobium (columbium). The alloy possesses excellent structural stability, high temperature stress rupture strength, oxidation and carburization resistance. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1995) 44 (11): SS-621.
Published: 01 November 1995
... CENTRALLOY 4859 is a cast austenitic iron base alloy with 32% nickel and 20% chromium plus niobium. Despite a low carbon content it has a very stable austenitic structure, sufficient stress rupture strength, excellent thermal shock resistance, and is not susceptible to embrittlement. CENTRALLOY...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1996) 45 (4): SS-643.
Published: 01 April 1996
... Sandvik Sanicro 31HT is an austenitic Fe-Ni-Cr alloy developed for high-temperature service. The alloy is highly resistant to oxidation and carburization, has high creep and stress-rupture strength, and possesses good structural stability. This datasheet provides information on composition...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1994) 43 (2): Fe-105.
Published: 01 February 1994
... THERMO-SPAN ALLOY is a precipitation-hardenable superalloy with a low coefficient of expansion combined with tensile and stress-rupture strength. Thermal fatigue resistance is inherent. This datasheet provides information on composition, physical properties, elasticity, and tensile properties...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2000) 49 (3): Ni-560.
Published: 01 March 2000
... Haynes Waspaloy is a specially vacuum melted, nickel-base alloy having outstanding tensile and stress-rupture strength up to 760 deg C (1400 deg F) combined with high oxidation resistance up to 871 deg C (1600 deg F). It is recommended for gas turbine engines, airframe assemblies, and missile...
Journal Articles
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Alloy Digest (1966) 15 (10): Ni-118.
Published: 01 October 1966
... ALLOY 713LC is a nickel-base alloy possessing high stress-rupture strength up to 1700 F combined with excellent resistance to thermal fatigue. It is recommended for turbine wheels. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (11): Ni-129.
Published: 01 November 1967
... WASPALOY is a vacuum induction melted nickel-base alloy having outstanding tensil and stress-rupture strength up to 1400 F combined with high oxidation resistance up to 1600 F. It is recommended for gas turbine engines, airframe assemblies and missile systems. This datasheet provides information...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1961) 10 (10): Mo-3.
Published: 01 October 1961
... Climelt Molybdenum-0.5 Ti-0.08 Zr is a molybdenum-base alloy that offers substantial benefits for high temperature applications. It has higher recrystallization temperature, and better stress-rupture strength than unalloyed molybdenum and the Mo-0.5% Ti alloy. This datasheet provides information...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1993) 42 (6): Ni-434.
Published: 01 June 1993
... P/M RENE 95 is a high strength, high temperature alloy used for rotating jet turbine components. Supersolvus P/M Rene 95 provides even higher temperature creep and stress-rupture resistance than standard Rene 95. Both are available as-HIP performs. A typical application is a high pressure turbine...
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Alloy Digest (1961) 10 (12): Ni-28.
Published: 01 December 1961
... 17 192000 16 190000 15 185000 11 175000 11 I55000 20 100000 21 46000 22 25000 22.5 Propeniec in the temperature range of 200-800 deg. F. are not definia. Table 2 - STRESS-RUPTURE STRENGTH 22 22 22 21 20 16 16 28 36 41 42 10 hours Stress. psi for Rupture in 100 hours 1000 hours Table 3 - SIRESRUPTURE...
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Publisher: Journals Gateway
Alloy Digest (1991) 40 (6): Ni-177.
Published: 01 June 1991
... UNITEMP 901, a nickel/iron/chromium base austenitic, precipitation-hardenable alloy has high tensile, stress-rupture and creep strengths in the range 1000 to 1400 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1993) 42 (5): SS-543.
Published: 01 May 1993
... element and despite the low carbon content has a very stable austen- itic structure, sufficient stress rupture strength, excellent thermal shock resistance and is not susceptible to embrittlement. Marker G4859 is applied under condi- tions where moderate stress rupture strength, good duc- tility...
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Alloy Digest (1962) 11 (9): Ni-74.
Published: 01 September 1962
... or less nose radius. Chip breakers will aid chip control. Workability: The optimum temperature range for forging is between 21500F and 1800oF. Below 1800oF the material will be hot-cold worked, with a re- sultant decrease in stress rupture strength. Liberal soaking time between rounds is advised...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1976) 25 (6): SS-329.
Published: 01 June 1976
... UNITEMP 1420WM is a hardenable 12% chromium stainless steel containing nickel, molybdenum, tungsten and vanadium additions to attain high strength up to 1200 F. Its good creep-rupture properties and resistance to stress-corrosion cracking make this steel well suited for jet engines and many other...