1-20 of 597 Search Results for

aircraft

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
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 (2012) 61 (9): Al-439.
Published: 01 September 2012
... Alcoa has developed this Al-Li alloy with the benefits of excellent corrosion resistance, a good spectrum of fatigue crack growth performance, a good strength and toughness combination, and compatibility with standard manufacturing techniques for aircraft internal structures. This datasheet...
Journal Articles
Alloy Digest (2016) 65 (7): Al-443.
Published: 01 July 2016
... Kaiser Alloy 7X49 is used in aircraft structural parts. The alloy has characteristics of high strength and good machinability. Good resistance to stress-corrosion cracking in –T7 type temper. X represents either or 1 or 0 as noted in the tex This datasheet provides information on composition...
Journal Articles
Alloy Digest (2016) 65 (8): Al-444.
Published: 01 August 2016
... Kaiser Alloy 7099-T7451 is used in aircraft wing structurals. The alloy has characteristics of high strength, high toughness, and good resistance to stress-corrosion cracking. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well...
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 (1978) 27 (5): Ti-70.
Published: 01 May 1978
... CORONA 5 is a titanium alloy developed for applications in fracture-controlled aircraft components. Plane strain fracture toughnesses of 110,000 to 150,000 psi sq.rt. in. (120 to 165 MPa sq.rt. m) have been produced in this alloy at 135,00 psi (930 MPa) tensile strength through a variety...
Journal Articles
Alloy Digest (1989) 38 (11): Al-232.
Published: 01 November 1989
... ALCOA 7475 was developed for sheet and plate applications that require high strength and a high level of guaranteed fracture toughness. It has the highest toughness for a given strength of the commercially available high-strength aircraft alloys. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1991) 40 (11): Ni-104.
Published: 01 November 1991
... NIMONIC alloy 115 is a nickel/chromium/cobalt based alloy developed as a vacuum processed creep resisting alloy for service at temperatures up to about 1010 C (1850 F) as a turbine blade material for aircraft turbines. This datasheet provides information on composition, physical properties...
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 (1977) 26 (7): SA-335.
Published: 01 July 1977
... as 210 F in impact tests. It is produced by the vacuum consumable electrode melting process to provide optimum cleanliness and preferred ingot structure. Its uses include fasteners, shafting and aircraft components. This datasheet provides information on composition, physical properties, hardness...
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 (1967) 16 (1): SS-190.
Published: 01 January 1967
... AISI No. 634 is a transformation and precipitation hardening stainless steel. It is used for applications such as pressure vessels, aircraft constructural components and jet engine compressor components. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (1967) 16 (3): Al-164.
Published: 01 March 1967
... BA.704 is a heat treatable aluminum extrusion alloy having high tensile and fatigue strengths. It is recommended for aircraft components, gears, fittings and machinery parts. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties...
Journal Articles
Alloy Digest (1967) 16 (6): Mg-63.
Published: 01 June 1967
... Magnesium MSR-B is a heat-treatable magnesium alloy with highest yield strength of any cast magnesium alloy up to 480 F. It is pressure tight and weldable by argon-arc. It is recommended for aircraft nose wheels, missile components, transmission cases, etc. This datasheet provides information...
Journal Articles
Alloy Digest (1967) 16 (10): Ni-128.
Published: 01 October 1967
... NIMONIC 110 is a highly alloyed nickel-base alloy having high creep and oxidation resistance. It is recommended for aircraft gas turbine components to resist the stresses at the very high temperatures of operation. This datasheet provides information on composition, physical properties, elasticity...
Journal Articles
Alloy Digest (1967) 16 (11): Co-54.
Published: 01 November 1967
... MAR-M Alloy 509 is a vacuum melted, cobalt-base alloy having high strength, low creep rates, and resistance to oxidation and thermal shock. It is recommended for aircraft and industrial gas turbine applications. This datasheet provides information on composition, physical properties, hardness...
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...