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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...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1981) 30 (7): Ni-269.
Published: 01 July 1981
... and stress-rupture properties up to about 1500 F. Typical applications are gas-turbine components, airframes and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature...
Journal Articles
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...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1984) 33 (3): SA-398.
Published: 01 March 1984
... range of highly-stressed, fracture-critical applications such as airframe structural components, landing gear components and light armor plate. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes...
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
Publisher: Journals Gateway
Alloy Digest (2001) 50 (9): Ti-120.
Published: 01 September 2001
..., although the latter methods can be used only if the material is protected from atmospheric contamination. This grade is used in airframe and chemical process applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and bend strength...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2006) 55 (8): Al-400.
Published: 01 August 2006
... Aluminum 7xxx series alloys contain zinc as the main alloying element, usually in combination with magnesium and copper. High-strength 7020 alloy is widely used in aerospace structures and is approved by the world’s leading airframe builders. For engineering applications this alloy is generally...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1969) 18 (6): Ti-58.
Published: 01 June 1969
... Ti-5A1-4FeCr is an alpha-beta type titanium alloy recommended for airframe components. It responds to an age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (5): SA-209.
Published: 01 May 1967
... Republic RSM-200 is a high strength, tough maraging steel recommended for airframe and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (8): Ti-52.
Published: 01 August 1967
... Ti-6Al-2Sn-4Zr-2Mo is a super-alpha titanium alloy providing an excellent combination of creep strength, tensile strength, toughness and stability to 1050 F. It is recommended for airframe and gas turbine engine requirements. This datasheet provides information on composition, physical 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 (1986) 35 (12): Al-274.
Published: 01 December 1986
... cases, gear cases, oil pans, airframe fittings and instrument housings. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1993) 42 (1): Ti-103.
Published: 01 January 1993
... TIMETAL 622 is useful for damages tolerant designs in airframes and engines. It offers fracture mechanics properties comparable to Ti-6A1-4V Beta Annealed, but with higher strength. Metallurgically, it is an ELI alpha-beta alloy. This datasheet provides information on composition, physical...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1973) 22 (11): Ni-197.
Published: 01 November 1973
... 41 is a precipitation-hardening nickel- base alloy possessing high strength in the 1200/18OOoF tem- perature range. The alloy is designed for severely stressed high temperature applications. Its high temperature strength makes it useful for jet engine and high speed airframe components...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1963) 12 (5): SA-146.
Published: 01 May 1963
... with excellent ductiliry and norchediunnocched ratios. Superior hot and cold workability, ease of heat rrear- ment weldability and adequate properties at cryogenic temperatures, make this material suitable for wide ap- plications in aircraft and rocket engines, airframe and missile systems. Srrength...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1972) 21 (6): Ti-65.
Published: 01 June 1972
... shapes must be warm formed for satisfactory results. These materials are weldable by both electrical resistance and fusion procedures although the latter methods can be used only if the material is protected from atmospheric contamination. These grades are used in airframe and chemical process...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1965) 14 (3): Ti-4.
Published: 01 March 1965
... and is the strongest titanium-base aRoy now in production. The impact strength remains neatly constant with increasing temperature from 500 deg. F to 1100 deg. F. Forms Available: Ingots, forgings, bars, rods, plates, and extrusions. Applications: Airframe and jet engine forgings and fittings, airframe extruded shapes...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1958) 7 (1): Ti-14.
Published: 01 January 1958
..., rods, forgings and billets. Applications: Jet engine discs and blades! airframe forgings, airframe fasteners, special ordnance equrpmeot. Manufacturer: Rem-&t Titanium Corporation Midland, Pennsylvania ...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (2004) 53 (8): Cu-722.
Published: 01 August 2004
... this product. The machinability of this alloy has been rated superior by customers from major airframes to small machine shops. The alloy is cost effective since AMS 4880 is commonly allowed as a substitute for AMS 4640, saving weight and machining time. Applications: This material, specified as AMS 4880...
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1970) 19 (12): SS-247.
Published: 01 December 1970
...: AMS 5595 and AMS 5656. General Characteristics: Pyromet 538 is a solid-solution-strengthened, austenitic stainless steel with a desirable combination of strength, corrosion resistance. oxidation resistance, and economy. This combination lends itself to various airframe and aircraft engine applications...