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aircraft landing gear

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Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005739
EISBN: 978-1-62708-171-9
... used base metals in airframe structures. This article summarizes the results of materials and component testing. It also presents a cost/benefit analysis of HVOF WC/17Co and WC/10Co4Cr coatings on aircraft landing gear components. aircraft landing gears corrosion cost assessment fatigue hard...
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001366
EISBN: 978-1-62708-173-3
... flash-welding applications, including chain links, transmission bands, automotive flywheel ring gears, aircraft landing gear, band-saw blades, and crankshaft counter weights. It describes the components of a typical flash-welding machine. The article provides information on the electrical controls...
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000621
EISBN: 978-1-62708-181-8
... Fig. 1004 An aluminum alloy 7075-T736 aircraft main landing gear forging, similar to that described in Fig. 1002 and 1003 , which was shot peened on its inner-diameter surface to enhance fatigue resistance. The shot-peened part withstood cycles far beyond the number required for acceptance...
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000612
EISBN: 978-1-62708-181-8
... of aircraft main landing gears, and aircraft engine mount beams. aircraft main landing gear fatigue fracture fractograph high-pressure compressors intergranular fracture intergranular stress-corrosion cracking precipitation-hardening stainless steel tension-overload fracture Fig. 720...
Book Chapter

Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001377
EISBN: 978-1-62708-173-3
... be used to temper the weld zone. Other metals welded by forge welding include high-alloy steels, nickel-base alloys, cobalt-base alloys, aluminum alloys, titanium alloys, and tungsten. Applications of this process include welding rods, bars, tubes, rails, aircraft landing gear, chains, and cans. The forge...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003101
EISBN: 978-1-62708-199-3
... is available as bar, sheet, plate, wire, tubing, forgings, and castings, are aircraft landing gear, airframe parts, fasteners, and pressure vessels. Variations in hardness and mechanical properties of 300M with tempering temperature are presented in Table 3 . Typical mechanical properties of 300M steel...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005732
EISBN: 978-1-62708-171-9
... Technology Growth in Gas Turbine Applications” “Abradable Thermal Spray Applications and Technology” “Replacement for Hard Chromium Plating on Aircraft Landing Gear” “Automotive Coatings and Applications” “Biomedical Coatings Made by Thermal Spraying for Orthopedic Joint Applications...
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001261
EISBN: 978-1-62708-170-2
... Co. Cosmetic or decorative applications involve parts that range in size from jewelry to large exterior structural domes and lobby interiors. Corrosion protection applications allow touchup of small rusted or corroded areas without disassembly. Examples include aircraft landing gears...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002442
EISBN: 978-1-62708-194-8
... with nonspherical, asymmetric cores Fig. 2 Accurate simulation of ball performance as it contacts the pins Fig. 4 Taxi simulations that predict loads from the landing gear into the aircraft Fig. 5 Landing gear mechanism geometry changes significantly during taxi or landing Fig...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003227
EISBN: 978-1-62708-199-3
... of the 4340 steel axle of Fig. 1 in the region of crack origin, showing the weld metal, the heat-affected zone adjacent to the weld metal, and the Rockwell C hardness at various locations. Etched in 2% nital. 12× Fig. 3 Aluminum alloy 7079-T6 aircraft landing-gear actuator beam fractured because...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003227
EISBN: 978-1-62708-199-3
... often shows some evidence of ductility, such as a shear lip or a herringbone pattern emanating from the zone of slow cracking. Fig. 3 Aluminum alloy 7079-T6 aircraft landing-gear actuator beam fractured because of stress-corrosion cracking (a) Portion of a broken aircraft landing-gear actuator...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006553
EISBN: 978-1-62708-210-5
..., milling machines, and grinding mills, and as hydraulic pump bushings. Aircraft landing gear assemblies, power shovels, and track rollers utilize solid aluminum bearings to withstand high-shock loads. Rolling mill bearings are cast of aluminum alloys to increase load and speed capability. Important...
Series: ASM Handbook
Volume: 6A
Publisher: ASM International
Published: 31 October 2011
DOI: 10.31399/asm.hb.v06a.a0005567
EISBN: 978-1-62708-174-0
... by forge welding include high-alloy steels, nickel-base alloys, cobalt-base alloys, aluminum alloys, titanium alloys, and tungsten. Applications of this process include welding rods, bars, tubes, rails, aircraft landing gear, chains, and cans. The forge welding process is competitive with flash welding...
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001325
EISBN: 978-1-62708-170-2
... testing to protect the aircraft from corrosion and provide required marking during flight test evaluation. Impact-resistant coating protects aerospace components such as aircraft landing gear, landing gear components, and other surfaces subject to erosion, abrasion, or impact from runway debris...
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
.... 413 Surface of a low-cycle fatigue fracture in an aircraft landing-gear cylinder made of AISI 4340 steel that was hardened and tempered to a tensile strength of 1793 to 1931 MPa (260 to 280 ksi). The cylinder was stressed in the laboratory to its tensile strength four times and broke at a stress...
Series: ASM Handbook
Volume: 4A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v04a.a0005802
EISBN: 978-1-62708-165-8
..., 1.04 m (41 in.). (e) Automatically controlled to ±3 °C (±5 °F) Equipment requirements for salt martempering aircraft landing-gear parts of 4330 steel Table 15 Equipment requirements for salt martempering aircraft landing-gear parts of 4330 steel Production requirements...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003516
EISBN: 978-1-62708-180-1
... factor to obtain a replacement time for the component. For aircraft components, such as landing gear, control surfaces, or engine rotor blades, the replacement time is usually defined in terms of allowable flight hours or landings, after which the component must be discarded and replaced with a new one...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006554
EISBN: 978-1-62708-210-5
... for Alloys 201.0 and A201.0 include structural casting members, truck and trailer castings, cylinder heads, pistons, gear and pump housings, aerospace housings, and aircraft landing gear components, as well as other applications where high strength and high energy-absorption capacity are required. Due...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004119
EISBN: 978-1-62708-184-9
... process and often leads to serious cause-and-effect situations where fatigue is involved; it is particularly damaging to critical aircraft structures such as landing and arresting gears, hinges, and load-bearing struts. Figure 2 shows the reactions and mechanisms of how a material corrodes and forms...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003190
EISBN: 978-1-62708-199-3
.... Grinding burns on high-strength steel aircraft landing gear components Untempered martensite in drilled holes in steel components Grinding cracks in the root sections of cast nickel-base gas turbine buckets Lowering of fatigue strength of parts processed by electrical discharge machining...