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Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270095
EISBN: 978-1-62708-301-0
... to overheating, possibly as a result of misalignment compounded by insufficient lubrication and high speeds. aircraft engine bearings high-temperature wear microstructural analysis visual examination Summary In an aircraft engine, two center support ball bearings failed. In one, the inner ring...
Abstract
A pair of bearings mounted side by side in an aircraft engine failed in service. Photographs show that the inner rings were either broken or deformed, the balls were worn and flattened, and the cages severely damaged. The bearing races were damaged as well, but only on one side indicating a directional thrust. In addition to their examination, investigators also conducted metallographic studies and hardness tests, which indicated that the balls and inner rings reached temperatures above 825 °C (1520 °F). Based on their findings, investigators concluded that the bearings failed due to overheating, possibly as a result of misalignment compounded by insufficient lubrication and high speeds.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270180
EISBN: 978-1-62708-301-0
... Abstract The nose landing gear on an aircraft malfunctioned during landing roll. After the incident, two fractured studs were found in the retraction jack support beam. Based on visual examination and the results of SEM fractography, investigators concluded that the studs failed by fatigue...
Abstract
The nose landing gear on an aircraft malfunctioned during landing roll. After the incident, two fractured studs were found in the retraction jack support beam. Based on visual examination and the results of SEM fractography, investigators concluded that the studs failed by fatigue, a vulnerability because of the way they were mounted. A sketch showing the correct mounting configuration is included in the report.
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Published: 01 September 2011
Fig. 7.10 Superconducting-supercolliding magnet support post
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Published: 01 December 2006
Fig. 2.50 AlMgSi0.5 support and housing sections for the scanner of a carpet tufting machine. Source: Alusuisse
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Published: 01 December 2006
Fig. 2.90 Special sections as support tubes in a walking beam furnace for heating steel slabs
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Published: 01 December 2006
Fig. 5.29 Formation of a hollow space (gas pocket) under the mandrel support leg at a low extrusion ratio (a) and a dead metal zone at a higher extrusion ratio (b). On the left, flow lines; right, lines of equal strain rate [ Wel 95 ]
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Published: 01 August 2015
Fig. 12.1 Steady rest support for long workpieces. Source: Ref 3
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Published: 01 August 2015
Fig. 12.2 Anvil support for cylindrical workpieces. (a) Correct method places the specimen centrally under indenter and prevents movement of the specimen under testing loads. (b) Incorrect method of supporting cylindrical work on spot anvil. The test piece is not firmly secured, and rolling
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Published: 01 December 2004
Fig. 3.15 One-piece alloy D357.0 main landing gear door uplock support for the 767 airplane. The casting replaced a sheet metal assembly; the conversion eliminated 27 separate parts and reduced assembly time by 65%. Source: Ref 5
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Published: 01 December 2003
Fig. 13 Workpiece in furnace. (a) Component mounted on support points. (b) Detail showing the effect of support on local case formation
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Published: 01 December 2003
Fig. 1 Core support of the nitrided case on a forging die. Source: Ref 1
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Published: 01 October 2011
Fig. 13 Example of unusable indentation curves due to an unfavorable support of the sample
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Published: 01 June 1983
Figure 3.2 Fiberglass/epoxy support cone for a superconducting electrical motor.
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Published: 01 June 1983
Figure 12.32 Experimental pressure vessel thermal standoff support strap for liquid-hydrogen fuel tank ( Barclay et al., 1975 ).
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Published: 01 October 2012
Fig. 12.7 Unit cost (1961 prices) of roller support made by machining from bar stock compared with machining a blank made by investment casting. Material, AISI 8630 steel. Weight of finished part, 0.5 lb. Part dimensions in inches. Source: Ref 12.11
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in Static and Dynamic Fracture Toughness of Metals
> Mechanics and Mechanisms of Fracture: An Introduction
Published: 01 August 2005
Fig. 4.31 Drop-weight tear test specimen and support dimensions
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Published: 01 January 2015
Fig. 15.9 Titanium support structure for a jet engine thrust reverser from a Rolls-Royce RB199 engine. Source: Ref 15.14
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Published: 01 November 2007
Fig. 4.1 Alloy X (Ni-22Cr-18.5Fe-9Mo-0.6W) catalyst grid support structure bar after 2 years of service in a nitric acid plant. (a) Internal nitride precipitates (about 20 mils in depth) containing mainly chromium-rich nitrides along with some carbides formed during thermal aging. (b
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Published: 30 April 2020
Fig. 7.36 Schematic of batch catalytic debinding, where the compacts rest on support trays in a hot nitrogen atmosphere that is doped with nitric acid
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