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pin fasteners

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Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001812
EISBN: 978-1-62708-180-1
...Abstract Abstract This article discusses different types of mechanical fasteners, including threaded fasteners, rivets, blind fasteners, pin fasteners, special-purpose fasteners, and fasteners used with composite materials. It describes the origins and causes of fastener failures...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.mech.c0048634
EISBN: 978-1-62708-225-9
... was stripped from the pins, which were then baked and repeated with a dull, porous cadmium layer that allowed outward diffusion of hydrogen. The pins were baked again after deposition of the porous cadmium layer. This eliminated the problem. Electroplating Fasteners Hydrogen embrittlement 8740 UNS...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c9001260
EISBN: 978-1-62708-235-8
...Abstract Abstract One percent Cr-Mo low alloy constructional steel is widely used for high tensile applications, e.g., for manufacture of high tensile fasteners, heat treated shafts and axles, for automobile applications such as track pins for high duty tracked vehicles etc. The steel is fairly...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.usage.c9001660
EISBN: 978-1-62708-236-5
... of fastener is designed so that during installation, the nuts (collars) separate in half (torque off) leaving a portion of the collar tight against the bolt (pin) at a specified torque ( Figures 1 ). Pins from three different commercial sources were evaluated in the present investigation and are referred...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0048665
EISBN: 978-1-62708-217-4
... substitution Pitting corrosion 300M UNS K44220 Stress-corrosion cracking Both jackscrew drive pins on a landing-gear bogie failed suddenly when the other bogie on the same side of the airplane was kneeled for a tire change. The pins were smooth cylindrical tubes that fastened the top tubular ends...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001080
EISBN: 978-1-62708-214-3
... design was responsible for the loosening of the nut. It was recommended that the locking mechanism be redesigned and changed in all existing turbines. Locking Nuts (fasteners) Turbine disks Turbine steel (Other, miscellaneous, or unspecified) failure Background A290 mm (10 in.) diam...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.bldgs.c0089530
EISBN: 978-1-62708-219-8
...Abstract Abstract A sand-cast steel eye connector used to link together two 54,430 kg capacity floating-bridge pontoons failed prematurely in service. The pontoons were coupled by upper and lower eye and clevis connectors that were pinned together. The eye connector was found to be cast from...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001815
EISBN: 978-1-62708-241-9
... the sealed compressor chamber. A unique combination of applied stress, residual stress, stress riser, and grain size helped isolate the failure mechanism to a single production lot of material. fastening pin corrosion stress concentration copper alloys grain size variations scanning electron...
Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001353
EISBN: 978-1-62708-215-0
... was made of two separate flap pieces fastened together at the outer periphery using bolts and spacers. The flap pieces were elliptical, with an approximate size of 1927 × 1187 × 80 mm (76 × 47 × 3 in.). The bolted flap body was mounted using a dowel pin on the central shaft, which passed through a central...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003543
EISBN: 978-1-62708-180-1
... installation torque. Investigation Typical failed fasteners are shown in Fig. 2(a) . Substantial necking accompanied all of the fractures. The fractographic features were consistent with dimple rupture, and the macroscopic necking is shown metallographically in Fig. 2(b) . The chemical composition...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006778
EISBN: 978-1-62708-295-2
... at the normal installation torque. Investigation Typical failed fasteners are shown in Fig. 2(a) . All fractures showed substantial necking. Fractographic features were consistent with dimple rupture, and macroscopic necking is shown metallographically in Fig. 2(b) . The chemical composition...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006794
EISBN: 978-1-62708-295-2
... Synergy during a Corrosive Sliding Wear Test , Tribol. Lett. , Vol 29 , 2008 , p 45 – 52 10.1007/s11249-007-9280-3 27. “ Standard Test Method for Wear Testing with a Pin-on-Disk Apparatus ,” G 99, Corrosion of Metals; Wear and Erosion , Vol 03.02 , Annual Book of ASTM Standards , ASTM...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001026
EISBN: 978-1-62708-214-3
... for the wing leading edge flap are fastened ( Fig. 1 ). The outboard and inboard supports had fractured, leading to loss of the flap in flight. Despite this, the aircraft was able to land safely. Analysis of the fracture was first performed by the materials engineering laboratory of the aircraft overhaul...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003500
EISBN: 978-1-62708-180-1
... in failures, such as the use of cadmium plating on an A286 superalloy fastener, subjected to service temperatures above 315 °C (600 °F) (the melting temperature of cadmium is 320 °C, or 610 °F). Two metals specified for use in a wear application could sustain galling if the metals are incompatible...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006753
EISBN: 978-1-62708-295-2
... plating on an A286 superalloy fastener subjected to service temperatures above 315 °C (600 °F) (the melting temperature of cadmium is 320 °C, or 610 °F). Two metals specified for use in a wear application could sustain galling if the metals are similar (atomic number) and mutually soluble, such as sliding...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006791
EISBN: 978-1-62708-295-2
.... (a) Pin-on-disk test. (b) Modified cylinder-on-cylinder test. Adapted from Ref 89 Fig. 15 Twist compression test setup. Source: Ref 101 Fig. 16 Slider-on-flat-surface testing rig. (a) Overview. (b) Tool holder with load cells and actuator (A, normal load; B, friction force; C, load...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001081
EISBN: 978-1-62708-214-3
..., the fatigue crack growth curves for the spin-pit cracks were also determined. Fig. 15 Spin-pit crack growth history of bolt hole crack in disk 1 using idle-max-idle loading. Fig. 16 Striations in typical pin-pit fracture area of bolt hole crack, 4.3 mm (0.17in.) from crack initiation site...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001808
EISBN: 978-1-62708-180-1
..., but sometimes hollow—that is used to support rotating components or to transmit power or motion by rotary or axial movement. Even fasteners, such as bolts or studs, can be considered to be stationary shafts, usually with tensile forces, but sometimes combined with bending and/or torsional forces. In addition...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003518
EISBN: 978-1-62708-180-1
.... This is still a useful task, perhaps more useful than something that pins “blame” on a particular individual or group. Understanding the factors that promoted a failure can lead to an understanding of what is required to have a real improvement in durability of products, equipment, or structures. Understanding...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006754
EISBN: 978-1-62708-295-2
... involved in allowing conditions that promoted the likelihood of failure. This is still a useful task, perhaps more useful than something that pins “blame” on a particular individual or group. Understanding the factors that promoted a failure can lead to an understanding of what is required to realize...