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Journal Articles
Alloy Digest (1968) 17 (4): SS-208.
Published: 01 April 1968
... Fifth-Vickers F.V. 520(S) is a corrosion resistant martensitic steel which is readily weldable and capable of being hardened by low temperature heat treatment. It is recommended for turbine components and supersonic aircraft parts. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1970) 19 (7): Ti-59.
Published: 01 July 1970
... CRUCIBLE BETA III is a heat-treatable beta titanium alloy offering outstanding cold formability and simple heat treatment to high strengths. It is recommended for aircraft parts and fasteners. This datasheet provides information on composition, physical properties, elasticity, tensile properties...
Journal Articles
Alloy Digest (1981) 30 (1): Ti-81.
Published: 01 January 1981
... are equipment requiring resistance to corrosion and aircraft parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating...
Journal Articles
Alloy Digest (1982) 31 (1): Bi-27.
Published: 01 January 1982
... characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1983) 32 (10): Bi-32.
Published: 01 October 1983
...-shrinkage characteristics make it of great use in industry for such applications as sprinkler and fire safety devices, support for bending pipe and tubing, anchoring aircraft parts for machining, and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1958) 7 (5): Ti-16.
Published: 01 May 1958
... REM-CRU A-70 is the grade of unalloyed titanium used where higher strength is required. It is specified for many moderately stressed aircraft parts. (Formerly known as RC-70.) This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive...
Journal Articles
Alloy Digest (1959) 8 (10): Al-84.
Published: 01 October 1959
... ALUMINUM 7079 is a high strength alloy especially applicable to highly stressed aircraft parts in thick sections. It responds to age-hardening heat treatment. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes...
Journal Articles
Alloy Digest (1984) 33 (12): SS-455.
Published: 01 December 1984
... of such parts are aircraft components and gears. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-455. Producer...
Journal Articles
Alloy Digest (1968) 17 (10): SA-232.
Published: 01 October 1968
... ISO-CAST 8 is a cast chromium-molybdenum steel recommended as a general purpose structural alloy of wide application with wide range of mechanical properties. It is used for aircraft and railroad car parts, machine tool and hammermill equipment, gears and shafts. This datasheet provides...
Journal Articles
Alloy Digest (1983) 32 (2): Al-243.
Published: 01 February 1983
.... Its applications include propeller gear boxes, crankcases and stressed structural parts in aircraft. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature...
Journal Articles
Alloy Digest (1965) 14 (5): SS-168.
Published: 01 May 1965
... AISI No. 631 is chromium-nickel-aluminum precipitation hardening stainless steel recommended for aircraft, missile and jet engine parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also...
Journal Articles
Alloy Digest (1964) 13 (6): SS-156.
Published: 01 June 1964
... AISI No. 630 is a precipitation hardening stainless steel which is used in a variety of applications requiring strength combined with corrosion resistance. It is recommended for chemical process equipment, valve parts, aircraft fittings, pump shafts, etc. This datasheet provides information...
Journal Articles
Alloy Digest (2002) 51 (5): SS-853.
Published: 01 May 2002
... and improves weldability. Typical uses include furnace parts, heating elements, aircraft and jet engine parts, heat exchangers, carburizing-annealing boxes, sulfite liquor handling equipment, kiln liners, boiler baffles, refinery and chemical processing equipment, and auto exhaust parts. This datasheet...
Journal Articles
Alloy Digest (1978) 27 (1): SS-346.
Published: 01 January 1978
... and ductility plus a higher degree of forgeability. Its wide range of uses include valve parts, engine parts and aircraft components; it is especially useful where high transverse strength and toughness are required. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (1983) 32 (5): SS-426.
Published: 01 May 1983
... worked. Among its many applications are aircraft-engine exhaust manifolds, furnace parts and expansion joints. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information...
Journal Articles
Alloy Digest (1998) 47 (9): SS-729.
Published: 01 September 1998
... and 816 C (800 and 1500 F). This grade is nonmagnetic in the annealed condition but is slightly magnetic when cold worked. Among its many applications are aircraft engine exhaust manifolds, furnace parts, and fasteners. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (2008) 57 (5): Al-413.
Published: 01 May 2008
... for structural aircraft parts. Corrosion resistance and anodizability are only fair. Alloy 2124 is also the basic alloy for cold finished square and rectangular bar. The alloy has high strength and good machinability, which are essential for precision fittings and parts. Comparative characteristics in the T851...
Journal Articles
Alloy Digest (1987) 36 (2): Al-277.
Published: 01 February 1987
... many uses include aircraft components, gears, machinery parts, fittings, valves and ornamental products. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat...
Journal Articles
Alloy Digest (1987) 36 (4): Al-279.
Published: 01 April 1987
... properties. It has good castability, excellent machinability and high resistance to corrosion. TERNALLOY 7 has many uses including aircraft components, gears machinery parts, fittings, valves and ornamental products. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (1987) 36 (9): Ti-88.
Published: 01 September 1987
.... This alloy is tough and has attractive elevated-temperature properties. It is used widely for applications at temperatures up to 800 F. Typical applications are parts for jet engines, aircraft components and pressure vessels. This datasheet provides information on composition, physical properties, hardness...