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aircraft structural applications

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Journal Articles
Alloy Digest (2016) 65 (10): Al-447.
Published: 01 October 2016
... aircraft structural applications chemical composition compressive strength elasticity fatigue properties heat treatability KAISER ALLOY 7099-T7651 physical properties tensile properties workability Kaiser Alloy 7099-T7651 is used in aircraft wing structures as well as fuselage frames. The alloy...
Journal Articles
Alloy Digest (2000) 49 (9): Al-372.
Published: 01 September 2000
... International aircraft structural applications Alcoa 2024 chemical composition corrosion-resistant alloys fatigue resistance physical properties tensile properties thermal properties Alcoa 2024 was introduced by Alcoa in 1931 as the first alloy to have a yield strength approaching 345 MPa (50 ksi...
Journal Articles
Alloy Digest (1999) 48 (1): Al-357.
Published: 01 January 1999
... Kaiser Aluminum Alloy 2024 has good machinability and good mechanical properties. The alloy is typically used in aircraft structures, rivets, connectors, hydraulic valve bodies, and miscellaneous structural applications. This datasheet provides information on composition, physical properties...
Journal Articles
Alloy Digest (1986) 35 (7): Al-269.
Published: 01 July 1986
... UNS No. A97075 is a wrought precipitation-hardenable aluminum alloy. It has excellent mechanical properties, workability and response to heat treatment and refrigeration. Its typical uses comprise aircraft structural parts and other highly stressed structural applications where very high strength...
Journal Articles
Alloy Digest (1977) 26 (7): SA-335.
Published: 01 July 1977
... Aircraft) GM 1013 (Grumman Aircraft) 4MDS-20701 (U.T.C.) RB016&800 (Rocketdyne, N.A.A.) SP-35 1 (Thlokol) General Characteristics: Lescalloy D6AC Vat Arc is a medium-carbon, low-alloy, ultra-high-strength steel primarily designed for high-strength structural applications requiring strength levels up...
Journal Articles
Alloy Digest (1964) 13 (10): TS-152.
Published: 01 October 1964
... Pyromet 882 is an air-hardening 5% chromium tool steel recommended for high temperature applications up to 1000 F. It has extremely high tensile and creep strength. It is used for such critical applications as structural components in aircraft and missiles which require either extremely high...
Journal Articles
Alloy Digest (1962) 11 (5): SA-129.
Published: 01 May 1962
... or vacuum melting practices. Forms Available: Kods, bars and forgings (Conventional or vacuum melted.) Applications: .\ircrufr landing gear components, aircraft structural componenrs. rocket motor cases. solid fuel rocker engine cases, thin walled pressure vessels, die blocks, tlummies, backer blocks...
Journal Articles
Alloy Digest (1970) 19 (2): SS-234.
Published: 01 February 1970
... ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet...
Journal Articles
Alloy Digest (1968) 17 (4): SA-225.
Published: 01 April 1968
... for applications such as rocket motor cases and accessories, bolts and fasteners and aircraft structural components- particularly landing gear. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes...
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 (1993) 42 (2): SA-321.
Published: 01 February 1993
... optimum cleanliness and preferred ingot structure. Its applications include aircraft components, pressure vessels and fasteners. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information...
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 (1979) 28 (7): SA-361.
Published: 01 July 1979
... structure. It is used for aircraft components including retainer rings for critical bearings and other heavy-duty applications. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on forming, heat treating, machining, and joining. Filing Code...
Journal Articles
Alloy Digest (1981) 30 (4): Ti-82.
Published: 01 April 1981
... in applications requiring high w&weight ratios at temperatures up to 7OOOF. Its uses include aircraft sheet components and structural parts. l RMI is a M trademark of the RMI Company. Composition: Carbon u= Nitrogen OxYgen Hydrogen Sheet Titanium 0.08 max. 6.5-9.0 0.05 max. 0.20 max. 0.015 max. Remainder Physical...
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 (1984) 33 (2): SS-440.
Published: 01 February 1984
... of corrosion resistance. cold formability. high strength and hardness. excellent fatigue properties and minimum distortion upon heat treatment. Typical applications include aircraft structural members and equipment for rhe process industries. *JESSOP and JSI7Cr-7Ni are registered trademarks of Jessop Steel...
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 (1983) 32 (1): Ni-282.
Published: 01 January 1983
... up to 501b (23kg). Consult the manufacturer for tolerances. Applications: METGLAS MBF-I5! l5A is used widely for joining aircraft engine components. It is also recommended for other brazing applications that require high joint strength with good corrosion and oxidation resistance aI elevated...
Journal Articles
Alloy Digest (2008) 57 (5): Al-413.
Published: 01 May 2008
..., A Division of Kaiser Aluminum Copyright © ASM International® 2008 2008 ASM International aircraft applications chemical composition coil corrosion-resistant alloys elasticity heat treatability joinability KAISER aluminum alloy 2124 machinability physical properties plates sheets...