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wing control cable

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Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270158
EISBN: 978-1-62708-301-0
... their observations and the results of SEM fractography, investigators concluded that tensile overload was the predominate cause of failure. fractography visual examination wing control cable A failed wing control cable of an aircraft was investigated. There was general...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2015
DOI: 10.31399/asm.tb.cpi2.t55030247
EISBN: 978-1-62708-282-2
... Abstract This chapter discusses the particular corrosion problems encountered and the methods of control used in petroleum production and the storage and transportation of oil and gas up to the refinery. It begins by describing those aspects of corrosion that tend to be unique to corrosion as...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550033
EISBN: 978-1-62708-307-2
... joining, and includes a section on the causes and effects of corrosion and how they are typically controlled. aluminum alloys castability composition corrosion forgeability formability heat treatability machinability weldability wrought aluminum alloys ALUMINUM is an industrial and...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270053
EISBN: 978-1-62708-301-0
... was procured for use in the fabrication of aircraft wings. During inspection for acceptance, blisters were noticed on their surface. When the extrusions were solution treated, the blisters were found to increase in size and number. Sectional metallography revealed the presence of cavities below the...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2012
DOI: 10.31399/asm.tb.ffub.t53610001
EISBN: 978-1-62708-303-4
... wing pivot fitting 1969 Fatigue failure due to material defect in high-strength steel Improved inspection techniques Change from fatigue “safe-life” to damage-tolerant design philosophy Development of materials with improved toughness Seam-welded high-energy piping failures 1986–2000 Cavitation...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.smnm.t52140039
EISBN: 978-1-62708-264-8
..., the crack becomes large enough to break the axle, a process known as fatigue failure. Fatigue failures occur in metal parts subjected to cyclic stresses, as often occurs in rotating machinery, valve and coil springs, or vibrating parts, such as airplane wings. Fig. 5.13 Development of...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 May 2018
DOI: 10.31399/asm.tb.hma.t59250107
EISBN: 978-1-62708-287-7
...-strength alloys from Alcoa are used on the Boeing 777 ( FIG. 8.17 ). The major structure of the plane is constructed with two basic aluminum alloys. The upper wings, because they are the most highly stressed components, are built of 7055 alloy. The lower wings are constructed of modified versions of 2024...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2012
DOI: 10.31399/asm.tb.smfpa.t53500083
EISBN: 978-1-62708-317-1
.... Aluminum has been used for large surface panels for the roof, hood, rear panels, and rear wings. Magnesium has been employed for the inner door panels and seat frames, and plastic moldings have been used for secondary components such as the trunk lid, spare wheel well, and front wings. A weight savings of...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2011
DOI: 10.31399/asm.tb.mnm2.t53060315
EISBN: 978-1-62708-261-7
... aerospace structures such as airplane fuselage and wing components, and rivets. The aluminum alloys in such structures have a high strength-to-weight ratio, and being both strong and light is particularly advantageous in machines and the transportation of people and goods. The use of aluminum alloys in...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550385
EISBN: 978-1-62708-307-2
... molding compound made by compression molding. For high-performance Formula 1 racing cars, where cost is not an impediment, most of the chassis, including the monocoque, suspension, wings, and engine cover, is made from carbon-fiber composites. Fig. 8.8 Composite transportation applications. Source...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170351
EISBN: 978-1-62708-297-6
..., aircraft fuselage and wing skins, structural parts, and those parts requiring good strength at temperatures up to 150 °C (300 °F). Figure 1 shows the relationships between some of the more commonly used alloys in the 2 xxx series. Fig. 1 Relationships among commonly used alloys in the 2 xxx...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2011
DOI: 10.31399/asm.tb.mnm2.t53060333
EISBN: 978-1-62708-261-7
... necessary mechanical strength and electrical conductivity. The resulting hardness and strength depend on the effectiveness of the solution quench and the control of the precipitation (aging) treatment. Cold working prior to precipitation aging tends to improve heat-treated hardness. Table 14.6 is a...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1984
DOI: 10.31399/asm.tb.mpp.9781627082600
EISBN: 978-1-62708-260-0
Series: ASM Technical Books
Publisher: ASM International
Published: 30 April 2021
DOI: 10.31399/asm.tb.tpsfwea.9781627083232
EISBN: 978-1-62708-323-2