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Image
in Cold Spray Applications in the Defense Industry
> High Pressure Cold Spray: Principles and Applications
Published: 01 June 2016
Fig. 9.23 Cargo bay door where the hinge fittings are located. Source: Ref 9.27
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Image
Hinge fittings made from Al-7075-T6 that can be repaired without being remo...
Available to Purchase
in Cold Spray Applications in the Defense Industry
> High Pressure Cold Spray: Principles and Applications
Published: 01 June 2016
Fig. 9.24 Hinge fittings made from Al-7075-T6 that can be repaired without being removed from the aircraft. Courtesy of South Dakota School of Mines and Technology
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Image
Published: 01 December 2006
Fig. 2.79 Furniture fittings in extruded brass sections. Source: Wieland-Werke AG
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Water supplies and bath fittings in extruded lead-free brass tubes. Source:...
Available to PurchasePublished: 01 December 2006
Fig. 2.87 Water supplies and bath fittings in extruded lead-free brass tubes. Source: Wieland-Werke AG
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Image
Published: 01 December 1995
Fig. 2-91 Stainless CF-8 cast steel fittings of several sizes
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Book Chapter
Fracture Mechanics and Service Fitness of Welds
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 July 1997
DOI: 10.31399/asm.tb.wip.t65930163
EISBN: 978-1-62708-359-1
... into the categories of fracture, fatigue, environmental cracking, and high-temperature creep. This article discusses each of these categories, as well as the benefits of a fitness-for-service approach. brittle fracture buckling corrosion ductile fracture environmental cracking fatigue fitness-for-service...
Abstract
Depending on the operating environment and the nature of the applied loading, a structure can fail by a number of different modes, including brittle fracture, ductile fracture, plastic collapse, fatigue, creep, corrosion, and buckling. These failure modes can be broken down into the categories of fracture, fatigue, environmental cracking, and high-temperature creep. This article discusses each of these categories, as well as the benefits of a fitness-for-service approach.
Book Chapter
Failure of a Throttle End Fitting in an Aircraft
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270065
EISBN: 978-1-62708-301-0
... of the investigation, which included the use of scanning electron fractography, along with recommendations on acceptable hole patterns for rivets. fatigue fracture fractography Summary An aircraft was forced to land after the engine did not respond to throttle movement. The throttle end fitting did...
Abstract
An aircraft was heavily damaged when it was forced to land due to a throttle malfunction. Investigators determined that one of the studs linking the throttle to the engine fractured from fatigue, initiated by cracks formed during a riveting procedure. This chapter provides a summary of the investigation, which included the use of scanning electron fractography, along with recommendations on acceptable hole patterns for rivets.
Book Chapter
Cracking in the Wing Root Fitting in an Aircraft
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270146
EISBN: 978-1-62708-301-0
... Abstract During a major servicing of an aircraft, cracks were found in the bottom wing root fitting. Based on dye penetrant inspection and the results of SEM fractography and chemical analysis, investigators concluded that the cracks were due to stress corrosion. They also recommended...
Abstract
During a major servicing of an aircraft, cracks were found in the bottom wing root fitting. Based on dye penetrant inspection and the results of SEM fractography and chemical analysis, investigators concluded that the cracks were due to stress corrosion. They also recommended an inspection of all other aircraft with similar fittings and the consideration of alternate materials that are less prone to stress-corrosion cracking.
Image
Elastic stress distribution: interference fit (press or shrink). T, tension...
Available to PurchasePublished: 30 November 2013
Fig. 5 Elastic stress distribution: interference fit (press or shrink). T, tension. C, compression.
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Example of snap fit connection: (a) before assembly, and (b) with parts sna...
Available to PurchasePublished: 01 November 2011
Fig. 8.23 Example of snap fit connection: (a) before assembly, and (b) with parts snapped together
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Image
Best-fit fatigue curves for aluminum alloy A201-T7 at various strain rates ...
Available to Purchase
in Properties and Performance of Aluminum Castings
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. 8.9 Best-fit fatigue curves for aluminum alloy A201-T7 at various strain rates at 75 °F (24 °C). Source: Ref 14
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Image
in Induction Heating Power Supplies
> Elements of Induction Heating: Design, Control, and Applications
Published: 01 June 1988
Fig. 4.10 “Split-yoke” system used to expand locomotive tires for shrink fitting Source: Cheltenham Induction Heating, Ltd.
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Image
Tool stack for the direct extrusion of copper alloys fitted in an axially m...
Available to PurchasePublished: 01 December 2006
Fig. 7.66 Tool stack for the direct extrusion of copper alloys fitted in an axially moving die head acting as the die holder. 1, container; 2, die holder; 3, extrusion die; 4, backer; 5, bolster; 6, pressure bolster and die head. Source: Wieland-Werke AG
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Toot set for the direct extrusion of copper alloys fitted in the tool holde...
Available to PurchasePublished: 01 December 2006
Fig. 7.67 Toot set for the direct extrusion of copper alloys fitted in the tool holder of a die slide. (a) Axial section through the tool stock. 1, container; 2, die holder; 3, extrusion die; 4, backer; 5, bolster; 6, pressure ring; 7, pressure ring as support in the press platen 8, press
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Image
Malleable iron applications, (a) pole line iron fitting; (b) malleable fitt...
Available to PurchasePublished: 01 January 2022
Fig. 8.1 Malleable iron applications, (a) pole line iron fitting; (b) malleable fitting. Source: Ref 1 . Courtesy of American Foundry Society (AFS)
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Image
As-received portion of the failed aft right-hand fitting for the hoist slin...
Available to Purchase
in Case Studies of Steel Component Failures in Aerospace Applications
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 47 As-received portion of the failed aft right-hand fitting for the hoist sling
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Image
Example of the fitted correlation between the solid thickness, and time fro...
Available to Purchase
in Solidification, Segregation, and Nonmetallic Inclusions
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 8.63 Example of the fitted correlation between the solid thickness, and time from the steel entering the caster mold, for AISI 304 stainless steel. The slope of 0.5 in the log thickness versus log time graph corresponds to a square root of time dependence of the solid thickness. Source
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Picture of the spiral detail that fits inside the extrusion press to form a...
Available to PurchasePublished: 30 April 2020
Fig. 6.14 Picture of the spiral detail that fits inside the extrusion press to form a rotating structure in the extrusion product
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Image
Examples of machine vision applications. (a) Measuring fit and gap of autom...
Available to PurchasePublished: 01 April 2013
Fig. 3 Examples of machine vision applications. (a) Measuring fit and gap of automotive fender. Courtesy of Diffracto Limited. (b) Reading box labels in sorting application. Courtesy of Cognex Corporation. (c) Reading part numbers on silicon wafers. Courtesy of Cognex Corporation. (d) Vision
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Image
Forging sequence of the titanium fitting. Part geometry courtesy of Weber M...
Available to Purchase
in Process Modeling in Impression-Die Forging Using Finite-Element Analysis
> Cold and Hot Forging: Fundamentals and Applications
Published: 01 February 2005
Fig. 16.15 Forging sequence of the titanium fitting. Part geometry courtesy of Weber Metals Inc.
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