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Series: ASM Handbook
Volume: 4B
Publisher: ASM International
Published: 30 September 2014
DOI: 10.31399/asm.hb.v04b.a0005966
EISBN: 978-1-62708-166-5
... at the surface, the presence of decarburization generally lowers the fatigue strength of a steel component, especially in the case of cyclic bending and torsion. In the best of circumstances, the fatigue limit for high cycle fatigue of steel is only about 50% of the ultimate tensile strength. Thus, a gross loss...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006821
EISBN: 978-1-62708-329-4
... Abstract This article focuses on failure analyses of aircraft components from a metallurgical and materials engineering standpoint, which considers the interdependence of processing, structure, properties, and performance of materials. It discusses methodologies for conducting aircraft...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006840
EISBN: 978-1-62708-329-4
... Abstract This glossary is a compilation of terms related to the analysis and prevention of component and equipment failures. It is intended to help promote clear thinking and useful failure analysis. The definitions presented are those used in this Volume and reflect a common and modern...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.9781627083294
EISBN: 978-1-62708-329-4
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Published: 01 November 2010
Fig. 5 Distorted airframe component. This component was machined flat. The material stress and machining-induced stress are causing it to distort More
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Published: 01 August 2013
Fig. 1 Component and service considerations More
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Published: 01 August 2013
Fig. 11 Example of thermal barrier coating on nozzle guide vane component. Courtesy of Rolls-Royce plc More
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Published: 01 August 2013
Fig. 3 Magnetic confinement fusion plasma facing component test sample with a thick (10 mm, or 400 mils) plasma-sprayed beryllium coating on a water-cooled copper substrate More
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Published: 01 January 1994
Fig. 4 Effect of shot peening on the fatigue strength of a ground component. A part designed for a gentle grinding operation could be salvaged by shot peening after a severe grinding operation. Source: Ref 6 More
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Published: 01 January 1994
Fig. 1 Schematic cross section of the surface of a cast iron component as it is modified by cleaning in a molten salt bath. (a) As-cast. Note surface scale, burned-in core/mold sand particles, and flake graphite extending to surface. (b) After first reduction cycle. Exposed sand particles have More
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Published: 01 August 2013
Fig. 15 Stretcher-strain marks (Lüders bands) on the surface of a range component after forming. Original magnification: 0.25× More
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Published: 09 June 2014
Fig. 16 Three-component resonant output networks. (a) Series tuned parallel resonant. (b) Parallel tuned series resonant More
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Published: 09 June 2014
Fig. 14 Diagram showing relationship between current ( i ), static component of force ( F c ), and dynamic force ( F ). Source: Ref 17 More
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Published: 01 January 1990
Fig. 5 Typical microstructure of a high-carbon through-hardened bearing component More
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Published: 01 January 1990
Fig. 2 Principal zones and component parts of an iron blast furnace. Source: Ref 1 More
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Published: 01 January 1990
Fig. 3 Principal zones and component parts of a basic oxygen furnace for the production of steel in a melt shop. (a) Typical plant layout. (b) BOF vessel More
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Published: 01 August 2013
Fig. 23 Intergranular oxidation at the surface of a carburized component. Unetched. Original magnification: 500× More
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Published: 01 August 2013
Fig. 21 Component manufacturing with central hardening shop and with one-piece flow (integrated manufacturing lines applying high-temperature low-pressure carburizing, or LPC). Source: Ref 21 More
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Published: 01 August 2013
Fig. 15 Schematic concentration-depth profile of the interstitial component k in the compound layer of the I/II (here: ϵ/γ′) double-layer morphology. The concentration profiles in both sublayers have been taken linearly. The dark-gray area represents the amount of component k per unit area More
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Published: 01 December 2008
Fig. 4 Cross ribbing (left) should be avoided in cast component design due to the hot spots and potential shrinkage defects it creates in casting solidification. Staggered ribs (right) provide for better manufacturing. More