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aircraft brake linings

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Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0004037
EISBN: 978-1-62708-185-6
... direction must be reduced proportionately, and additional stress reduction must be allowed for assurance against stress corrosion. Nevertheless, a major portion of failures attributable to material, or material processing, in forged aircraft parts are located in trim lines and are frequently initiated by...
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000608
EISBN: 978-1-62708-181-8
..., sulfide stress-corrosion failure, stress-corrosion cracking, and hitch post shaft failure of these steels. The components considered in the article include tail-rotor drive-pinion shafts, pinion gears, outboard-motor crankshafts, bull gears, diesel engine bearing cap bolts, splined shafts, aircraft...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005339
EISBN: 978-1-62708-187-0
... aircraft. For instance, the use of MMCs reduces the maximum deflection of the leading-edge tip of the ventral fin in an F-l6 aircraft by over 50%, reducing the aerodynamic loads and increasing the service life from 400 to 8000 h. Aluminum alloy skins used in the honeycomb structure of the fin were replaced...
Book Chapter

By Nabil Zaki
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001257
EISBN: 978-1-62708-170-2
... alloys plated from alkaline baths have shown potential as substitutes for cadmium coatings in aircraft and military applications. Available chromates are clear, iridescent, bronze, and black. Typical zinc-nickel bath compositions and process parameters are given in Table 2 . Alkaline formulations are...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003177
EISBN: 978-1-62708-199-3
... X X X X X X Transfer X X X X X X X X X X X X X X X Flat-edge trimming X X X X X X X X Hydraulic X X X X X X X X X X X X X X X X X X Press brake X X X X X X...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003121
EISBN: 978-1-62708-199-3
... processing equipment. Also for nameplates, fan blades, flue lining, sheet metal work, spun holloware, and fin stock 1350 Electrical conductors 2011 Screw machine products. Appliance parts and trim, ordnance, automotive, electronic, fasteners, hardware, machine parts 2014 Truck frames, aircraft...
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0003827
EISBN: 978-1-62708-183-2
... corrosion of the beryllium brake shoe pads of bombers on military aircraft carriers has been reported. The brake shoes were typical of those that have performed well for years on the C5A military transport in less corrosive environments. The salt-laden environment of the aircraft carrier caused the brake...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005265
EISBN: 978-1-62708-187-0
... precombustion chambers, fuel injection components, rocker arms, and others. Parts are supplied to the aircraft and aerospace industries, such as temperature probes, fuel pump impellers, missile wings, brake parts, pump housings, and structural parts. Other applications include golf club heads, machine...
Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.9781627081863
EISBN: 978-1-62708-186-3
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003043
EISBN: 978-1-62708-200-6
... F-15 has boron-epoxy composites and horizontal stabilizers with composite materials that transmit flight loads to the fuselage through primary structural adhesively bonded joints. In addition, the composite speed brake in the aircraft is an all-bonded structure. The C-17 aircraft contains extensive...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003031
EISBN: 978-1-62708-200-6
... steel. Heat sink properties of carbon-carbon composites designed for brakes, combined with dimensional stability, light weight, and friction characteristics, have resulted in their acceptance for high-performance aircraft and racing cars. Thermal expansion characteristics of composites can be...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005186
EISBN: 978-1-62708-187-0
... Motor vehicles Metalworking machinery Other major markets include steel manufacturing, spring goods, heating and air conditioning, recreation equipment, industrial materials handling equipment, ships and boats, and aircraft and aerospace (a) Nonferrous castings Aluminum Auto and light...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003154
EISBN: 978-1-62708-199-3
... include aircraft magnetos, alternators, magnetos for lawn mowers, garden tractors, and outboard motors; small and large direct current (dc) motors (including automotive motors); acoustic transducers; magnetic couplings; magnetic resonance imaging; magnetic focusing systems; ammeters and voltmeters; and...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003005
EISBN: 978-1-62708-200-6
... of ferrous alloys is relatively high density (∼7.8 g/cm 3 ), which contributes to a low strength-to-density ratio and precludes extensive use in aircraft/aerospace applications. In addition, irons and steels with lower alloy contents are not highly corrosion resistant, as evidenced by the galvanic...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0003981
EISBN: 978-1-62708-185-6
... producing parts that vary widely in sizes and shapes. Usually the length of the roll forged products is limited by the roll size (i.e., circumference). Large rotor blade halves (up to 1620 mm long) for aircraft applications to crankshafts (up to 200 kg) for automobiles have been produced by incorporating...
Book Chapter

By Ted Kostilnik
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001235
EISBN: 978-1-62708-170-2
... Institute for Iron, Steel and Other Metals , Tohoku University, Sendai, Japan, 1959. (aj) H.C. Burnett, Proc. ASTM , 58, 515 (1958). (ak) “Effect of Chromium Plate on Torsion Fatigue Life of Shot Peened 4340 Steel,” Douglas Aircraft Co. Report No. MP 20.005 (Sept. 13, 1960); available through SAE...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0009021
EISBN: 978-1-62708-187-0
... superalloys. For this reason, most aircraft castings made of these materials are produced in shell, ceramic or baked sand molds. An analytical approach to the design of thin-wall steel castings to be produced in green sand molds necessitates an understanding of four major production problems involved: mold...
Book Chapter

Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003047
EISBN: 978-1-62708-200-6
... compared with the total surface area (automotive body sheet, aircraft assembly, furniture). Laminating: Loads are usually small, and the bond covers a large fraction of the surface (plywood, multilayer packaging, labelling, decals). Pressure-Sensitive: Usage could be structural or laminating, but...
Book Chapter

Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005287
EISBN: 978-1-62708-187-0
....) Across parting line Sand ±0.38 (±0.015) …. Die …. …. Permanent mold ±0.38 (±0.015) +0.051 (+0.002) Plaster mold ±0.25 (±0.010) +0.038 (+0.0015) Shell mold ±0.25 (±0.010) +0.030 (+0.0012) Centrifugal (a) ±0.25 (±0.010) (b) +0.025 (+0.001) (c) Investment...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003089
EISBN: 978-1-62708-199-3
... permanent deformation of the structure. In many structures, any permanent deformation destroys the usefulness of the. structure; for example, the aerodynamic efficiency of an aircraft wing can be substantially reduced by only 1 to 1 1 2 % deformation. The amount of ductility required for processing...