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in Failure of Tail Boom Attachments in a Helicopter
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH42.2 Snapped tail rotor pitch control cables
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Book Chapter
Failure of an Aileron Control Cable in an Aircraft
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270090
EISBN: 978-1-62708-301-0
... Abstract This chapter discusses the failure of an aircraft control cable and the investigation that followed. It explains how visual examination showed that the failure occurred in a heavily worn section that runs over a pulley. Further examination under a stereoscope and in a SEM found that 40...
Abstract
This chapter discusses the failure of an aircraft control cable and the investigation that followed. It explains how visual examination showed that the failure occurred in a heavily worn section that runs over a pulley. Further examination under a stereoscope and in a SEM found that 40 out of 49 wires had thinned and broke apart, and that the remaining nine wires failed in tension evidenced by cup and cone fracture and the presence of dimples on the fracture surface. Based on their findings, investigators concluded that cable snapped because of excessive thinning due to contact wear.
Book Chapter
Failure of an Aileron Control Cable in an Aircraft
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270152
EISBN: 978-1-62708-301-0
... Abstract This chapter discusses the failure of an aileron control cable in an aircraft and explains how investigators determined the cause. Based on their observations and the results of SEM fractography, investigators concluded that the cable had been damaged by a shearing tool, leading to its...
Abstract
This chapter discusses the failure of an aileron control cable in an aircraft and explains how investigators determined the cause. Based on their observations and the results of SEM fractography, investigators concluded that the cable had been damaged by a shearing tool, leading to its failure.
Book Chapter
Failure of a Wing Control Cable in an Aircraft
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270158
EISBN: 978-1-62708-301-0
... Abstract This chapter discusses the failure of a control cable on an aircraft and the findings of an investigation that followed. The cable was made of stranded steel wire that was visibly worn. All seven strands had snapped and bore evidence of corrosion, pitting, nicks, and rubbing. Based...
Abstract
This chapter discusses the failure of a control cable on an aircraft and the findings of an investigation that followed. The cable was made of stranded steel wire that was visibly worn. All seven strands had snapped and bore evidence of corrosion, pitting, nicks, and rubbing. Based on their observations and the results of SEM fractography, investigators concluded that tensile overload was the predominate cause of failure.
Image
Principle of cable sheathing. 1, extrusion stem; 2, container; 3, cable she...
Available to PurchasePublished: 01 December 2006
Fig. 3.84 Principle of cable sheathing. 1, extrusion stem; 2, container; 3, cable sheathing material; 4, die head; 5, cable sheath; 6, cable core; 7, die; 8, hollow mandrel; 9, detachable point. The billet is placed in the container and pushed into a feeder chamber. The cable slips through
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Image
in Failure of an Aileron Control Cable in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
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in Overview of Wafer-level Electrical Failure Analysis Process for Accelerated Yield Engineering
> Microelectronics Failure Analysis: Desk Reference
Published: 01 November 2019
Figure 5 (a) Pogo tower (hard dock) and (b) cable docking (soft dock) solution.
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Image
Arresting gear hook-point showing vertical cracking in the cable groove and...
Available to Purchase
in Overview of the Mechanisms of Failure in Heat Treated Steel Components
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 30 Arresting gear hook-point showing vertical cracking in the cable groove and evidence of localized heating (from the temper colors in the cable groove)
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Image
Semiflexible coaxial cable used to transmit power between medium- or low-fr...
Available to PurchasePublished: 01 June 1988
Fig. 8.66 Semiflexible coaxial cable used to transmit power between medium- or low-frequency power supplies and heat stations: (a) cross section of coaxial cable and (b) cable “broken out” for assembly Source: American Induction Heating Corp.
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Water-cooled flexible coaxial cable used in radio-frequency induction heati...
Available to PurchasePublished: 01 June 1988
Fig. 8.67 Water-cooled flexible coaxial cable used in radio-frequency induction heating to connect the inductor to the power supply Source: L. C. Miller Co.
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Image
Extruded solder with several flux cores, lead sheathed cable, and window sp...
Available to PurchasePublished: 01 December 2006
Fig. 2.3 Extruded solder with several flux cores, lead sheathed cable, and window spacer sections in lead alloys for double glazed windows, as well as lead lines for fishing nets and curtain weights. Source: Collin
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Image
Published: 01 December 2006
Fig. 3.79 Cable sheathing with the conform process [ Lan 85 , Par 86 ]
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Aluminum electrical cable produced with the conform system (Source: Holton ...
Available to PurchasePublished: 01 December 2006
Fig. 3.82 Aluminum electrical cable produced with the conform system (Source: Holton Machinery Ltd.)
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Image
Press for continuous cable sheathing. (a) Extrusion. (b) Loading [ Rie 72 ]...
Available to PurchasePublished: 01 December 2006
Fig. 3.86 Press for continuous cable sheathing. (a) Extrusion. (b) Loading [ Rie 72 ]
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Image
Published: 01 December 2006
Fig. 3.87 30 MN cable sheathing press for aluminum [ Rie 72 ]
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Galvanic corrosion of aluminum shielding in buried telephone cable coupled ...
Available to PurchasePublished: 01 August 1999
Fig. 2 Galvanic corrosion of aluminum shielding in buried telephone cable coupled to buried copper plates
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Galvanic corrosion of aluminum in buried power cable splice (copper to alum...
Available to PurchasePublished: 01 August 1999
Fig. 3 Galvanic corrosion of aluminum in buried power cable splice (copper to aluminum)
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Image
in Failure of a Wing Control Cable in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH40.1 Strands of wires found snapped in a wing control cable
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Image
in Failure of Tail Boom Attachments in a Helicopter
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH42.5 Broken strands of the tail rotor pitch control cable
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Image
Galvanic corrosion of aluminum shielding in buried telephone cable coupled ...
Available to PurchasePublished: 01 December 2015
Fig. 2 Galvanic corrosion of aluminum shielding in buried telephone cable coupled to buried copper plates. Courtesy of R. Baboian, Texas Instruments, Inc.
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