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Ellen E. Wright, Suzanne F. Uchneat
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Book Chapter
Steel Decarburization—Mechanisms, Models, Prevention, Correction, and Effects on Component Life
Available to PurchaseSeries: 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...
Abstract
This article focuses on the mechanisms, models, prevention, correction, and effects associated with decarburization inherited from semi-finished product processing prior to induction heating. It discusses the diffusion of carbon in austenitic iron, which has a face-centered cubic crystal structure that provides an interstitial path for the migration of the relatively small carbon atoms. The article describes the evolution of steel microstructure with progressive decarburization (in air) to a steady-state carbon gradient using an iron-iron carbide phase diagram. It provides useful information on the impact of alloying on vulnerability to decarburization, and the impact of decarburization on the mechanical properties of steels and cast irons. The article also describes the technological operations that potentially cause decarburization and the practical implications for induction hardening.
Book Chapter
An Overview of Aircraft Accident Investigation and Component Failures
Available to PurchaseSeries: 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...
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 investigations and inspections and emphasizes cases where metallurgical or materials contributions were causal to an accident event. The article highlights how the failure of a component or system can affect the associated systems and the overall aircraft. The case studies in this article provide examples of aircraft component and system-level failures that resulted from various factors, including operational stresses, environmental effects, improper maintenance/inspection/repair, construction and installation issues, manufacturing issues, and inadequate design.
Book Chapter
Glossary of Terms—Analysis and Prevention of Component and Equipment Failures
Available to PurchaseSeries: 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...
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 understanding of these terms as used in the literature and in reports by practicing failure analysts.
Book
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
Image
Distorted airframe component. This component was machined flat. The materia...
Available to Purchase
in Modeling of Residual Stress and Machining Distortion in Aerospace Components
> Metals Process Simulation
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
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Image
Example of thermal barrier coating on nozzle guide vane component. Courtesy...
Available to PurchasePublished: 01 August 2013
Fig. 11 Example of thermal barrier coating on nozzle guide vane component. Courtesy of Rolls-Royce plc
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Image
Magnetic confinement fusion plasma facing component test sample with a thic...
Available to PurchasePublished: 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
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Image
Effect of shot peening on the fatigue strength of a ground component. A par...
Available to PurchasePublished: 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
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Image
Schematic cross section of the surface of a cast iron component as it is mo...
Available to PurchasePublished: 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
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Image
Stretcher-strain marks (Lüders bands) on the surface of a range component a...
Available to PurchasePublished: 01 August 2013
Fig. 15 Stretcher-strain marks (Lüders bands) on the surface of a range component after forming. Original magnification: 0.25×
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Image
Three-component resonant output networks. (a) Series tuned parallel resonan...
Available to Purchase
in Power Supplies for Induction Heat Treating, Brazing, and Soldering
> Induction Heating and Heat Treatment
Published: 09 June 2014
Fig. 16 Three-component resonant output networks. (a) Series tuned parallel resonant. (b) Parallel tuned series resonant
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Image
Diagram showing relationship between current ( i ), static component of for...
Available to Purchase
in Design and Fabrication of Inductors for Induction Heat Treating
> Induction Heating and Heat Treatment
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
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Image
Published: 01 January 1990
Fig. 5 Typical microstructure of a high-carbon through-hardened bearing component
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Image
in Steel Processing Technology
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 2 Principal zones and component parts of an iron blast furnace. Source: Ref 1
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Image
Principal zones and component parts of a basic oxygen furnace for the produ...
Available to Purchase
in Steel Processing Technology
> Properties and Selection: Irons, Steels, and High-Performance Alloys
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
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Image
Intergranular oxidation at the surface of a carburized component. Unetched....
Available to PurchasePublished: 01 August 2013
Fig. 23 Intergranular oxidation at the surface of a carburized component. Unetched. Original magnification: 500×
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Image
Component manufacturing with central hardening shop and with one-piece flow...
Available to PurchasePublished: 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
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Image
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
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Image
Cross ribbing (left) should be avoided in cast component design due to the ...
Available to PurchasePublished: 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.
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