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Axles
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Image
Published: 01 October 2011
Fig. 9.33 Deep case hardening of 20-foot axles. Courtesy of Ajax Tocco Magnethermic
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Published: 01 January 2022
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2008
DOI: 10.31399/asm.tb.fahtsc.t51130351
EISBN: 978-1-62708-284-6
..., inboard flap hinge bolt, nose landing gear piston axle, multiple-leg aircraft-handling sling, aircraft hoist sling, internal spur gear, and MLG axle. In addition, the chapter provides information on full-scale fatigue testing, nondestructive testing, and failure analysis of fin attach bolts. high...
Abstract
This chapter presents various case histories that illustrate a variety of failure mechanisms experienced by the high-strength steel components in aerospace applications. The components covered are catapult holdback bar, AISI 420 stainless steel roll pin, main landing gear (MLG) lever, inboard flap hinge bolt, nose landing gear piston axle, multiple-leg aircraft-handling sling, aircraft hoist sling, internal spur gear, and MLG axle. In addition, the chapter provides information on full-scale fatigue testing, nondestructive testing, and failure analysis of fin attach bolts.
Image
Published: 01 December 1999
Fig. 8.14 Comparison of bending fatigue strength of conventionally processed (cut/harden/lap) versus CBN ground (cut/harden/lap) spiral bevel gears. Test gear design specifications: hypoid design, 4.286 dp, 11 by 45 ratio, 1.60 in. face. Gears were installed in axles using a 4-square loaded
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in Metallographic Evaluation—Guidelines for Performing and Reporting
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 18.1 The region where the fatigue fracture of the axle presented in Fig. 15.24 (Chapter 15, “Engineered Special Bar Quality Steel (Engineered Steels),” in this book) started. (a) The radial aspect of the marks inside the defect that started the fatigue failure. (b) A view of the region
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Published: 01 September 2008
Fig. 28 Component drawing of the intermediate I axle. Highlighted are the section change region where the fracture developed and the crack propagation path for the total fracture of the axle.
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Published: 30 November 2013
Fig. 24 Large axle shaft of medium-carbon steel with fatigue fracture across most of the cross section before final rupture. Note the smooth origin region (arrow) and gradually coarsening fracture surface as the fatigue crack progressed. Note that there was a thread groove running around
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Published: 30 November 2013
Fig. 25 (a) Fracture surface of a 3.6-in.-diam axle housing tube showing four major fatigue-fracture origins (arrows) at the bottom. (b) Origin areas at higher magnification. Beach marks are clearly seen. Small areas of postfracture damage are present, but in general, the fracture
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Published: 30 November 2013
Fig. 34 Torsional fatigue fracture of a 1050 steel axle shaft induction-hardened to about 50 HRC. The arrow indicates the longitudinal shear fatigue origin, which then changed direction and grew to the small circular beach mark, or “halo.” Final brittle fracture (note chevron marks in the case
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in Tribology of Plastics and Elastomers
> Tribomaterials: Properties and Selection for Friction, Wear, and Erosion Applications
Published: 30 April 2021
Fig. 11.23 Model showing how walking is rolling. The knee joint is the axle of the wheel, the foot is part of the rim of a wheel, and the lower leg is a spoke on a wheel.
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in Engineered Special Bar Quality Steel (Engineering Steels)
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 15.24 Fatigue failure in a forged railway axle. The wheel is still mounted in the axle. The fracture started at the radius transition corresponding to the area of the axis where the wheel is assembled. The arrow indicates the initiation. Beach marks indicate that the crack propagated
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in Engineered Special Bar Quality Steel (Engineering Steels)
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 15.26 Region of the axle close to the point where the fatigue crack started, shown in the macrograph of Fig. 15.25 . Weld deposited metal (upper region of the image), heat affected zone in base metal similar to AISI 1050 (lower region of the image). Metallography by I. C. Abud, INT
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Published: 01 January 2022
Fig. 12.103 Rear axle housing for a highway heavy-duty vehicle
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in Applications of Iron and Steel Castings and the Impact of Electric Vehicles
> Iron and Steel Castings Engineering Guide
Published: 01 January 2022
Fig. 13.12 Vehicle center of gravity and axle load distributions
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Published: 01 January 2022
Fig. 12.11 Underside of a truck showing an axle housing. Source: Ref 5
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Published: 01 January 2022
Fig. 12.27 Truck axle housing; pouring orientation and parting plane. Source: Ref 15
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Published: 01 September 2008
Fig. 29 Complete cross-sectional fracture surface of the intermediate I axle. The white arrow shows the nucleating site of the fatigue crack. The surface generated by the fatigue crack propagation is identified by “F,” while the final fracture of the remaining section is indicated by “FF.”
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Published: 01 September 2008
Fig. 30 Microstructure of the axle according to a longitudinal cut plane. Etched with 2% nital
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