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Journal Articles
Alloy Digest (1980) 29 (6): Ni-264.
Published: 01 June 1980
... CARPENTER 80-20 ALLOY is a nickel-chromium alloy intended for service at high temperatures. It offers good corrosion resistance to exhaust gases in aircraft piston engines. Considerable quantities of this alloy have been used as welded overlays on valve heads for aircraft engine exhaust valves...
Journal Articles
Alloy Digest (1983) 32 (7): Ti-85.
Published: 01 July 1983
... CABOT Ti-3A1-2.5V alloy is both lightweight and strong. It has a high strength-to-weight ratio which provides a major design advantage saving weight. It can be formed readily and it has good weldability. Seamless tubing of CABOT Ti-3A1-2.5V was developed for aircraft hydraulic and fuel systems...
Journal Articles
Alloy Digest (2022) 71 (7): SS-1349.
Published: 01 July 2022
... sufficient ductility in conditions up to 1/2 Hard and allows it to be roll or brake formed into aircraft, architectural, and particularly rail car structural components. However, 3/4 Hard to Full Hard tempers should be used whenever high wear resistance and spring features are required in components...
Journal Articles
Alloy Digest (1972) 21 (2): SS-268.
Published: 01 February 1972
... CARPENTER C-XB is a hardenable high-carbon high-silicon high-chromium stainless steel offering good high-temperature strength and corrosion resistance to combustion products of automotive gas engines. It is also available in aircraft quality. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1975) 24 (4): Ni-216.
Published: 01 April 1975
... PYROMET 901 is a nickel-chromium super alloy designed for high strength and corrosion resistance in the temperature range of 1000-1400 F. Compounds of Ni3 (Al, Ti) type produce the precipitation hardening. It is used in a variety of high-temperature applications such as components in aircraft...
Journal Articles
Alloy Digest (1976) 25 (5): Al-223.
Published: 01 May 1976
... and components for aircraft and missiles. 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 resistance as well as casting, heat treating...
Journal Articles
Alloy Digest (2004) 53 (4): Fe-128.
Published: 01 April 2004
... Rotelloy 3 has the same composition as Permandur 49 and was specifically developed for aircraft generator rotor and stator laminations. In addition to a slightly improved magnetic performance, this grade is supplied with guaranteed minimum mechanical properties. This alloy complies...
Journal Articles
Alloy Digest (2004) 53 (7): Al-391.
Published: 01 July 2004
... Originally developed as a high-strength alloy for the aircraft industry, this alloy was further developed and optimized to satisfy the most demanding applications of the mold construction industry. The resulting mold construction alloy, Hokotol, exhibits very high strength and wear resistance...
Journal Articles
Alloy Digest (2006) 55 (5): Ni-637.
Published: 01 May 2006
.... The advanced, wrought, gamma-prime strengthened superalloy Haynes 282 could also potentially be used in aircraft manufacturing and other highperformance, high-temperature environments. The alloy contains 58% Ni, 19% Cr, 10% Co, 8.5% Mo, 1.5% Al, and 2.1% Ti. This datasheet provides information on composition...
Journal Articles
Alloy Digest (2006) 55 (11): Al-402.
Published: 01 November 2006
... Aluminum alloy 7449 in the T7651 temper is solution heat treated, stress relieved, and overaged. This processing produces an alloy of high strength, good corrosion/exfoliation resistance, and good toughness. An application of interest is the upper-wing skin of aircraft structures. This datasheet...
Journal Articles
Alloy Digest (2007) 56 (5): Ni-650.
Published: 01 May 2007
... Boehler L311 VMR is a nickel alloy having high creep and rupture strength up to 760 deg C (1400 deg F) and scaling resistance in air to 850 deg C (1560 deg F). It is used in the aircraft and gas turbine industries as shafts, blades, and discs. This datasheet provides information on composition...
Journal Articles
Alloy Digest (2007) 56 (5): Ni-649.
Published: 01 May 2007
... deg C (1800 deg F). It is typically used in aircraft turbine and structural components. 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...
Journal Articles
Alloy Digest (2008) 57 (1): Ti-145.
Published: 01 January 2008
... Haynes Ti-3Al-2.5V alloy is used where the strength/weight ratio is of prime importance; the alloy is 43% lighter than 21-6-9 stainless steel. It is most often used in the form of seamless tubing for aircraft hydraulic systems. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (2008) 57 (5): Al-413.
Published: 01 May 2008
... Kaiser aluminum alloy 2124 is a high-purity version of 2024 with tighter controls on the iron and silicon for an increase in strength and toughness. It is primarily used as plate in the aircraft industry. This data sheet applies to sheet, coil, and plate in the T851 temper. This datasheet provides...
Journal Articles
Alloy Digest (2008) 57 (6): Al-414.
Published: 01 June 2008
... Kaiser Aluminum alloy 7175/7475 is a high-purity version of 7075 and is heavily used by the aircraft and ordinance industries because of its superior strength. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information...
Journal Articles
Alloy Digest (1957) 6 (12): Ni-38.
Published: 01 December 1957
... INCOLOY 901 is a nickel-base alloy having creep and rupture strength at 1000 to 1400 F. It is recommended for use in aircraft and industrial gas turbine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also...
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 (1960) 9 (1): Ti-23.
Published: 01 January 1960
... REPUBLIC RS-130 is a good general purpose bar and forging alloy having the two phase alpha-beta microstructure. It is widely used in aircraft fasteners and related applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties...
Journal Articles
Alloy Digest (1960) 9 (4): Mg-46.
Published: 01 April 1960
... MAGNESIUM HM21A is a magnesium alloy sheet, plate, and forging material developed for high temperature service as in aircraft and missile applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bearing...