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UNS R56406

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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.med.c9001573
EISBN: 978-1-62708-226-6
.... Arcing Pitting (wear) Surgical implants Wire Ti-6Al-4V Titanium nitride coating UNS R56406 Surface treatment related failures (Other, miscellaneous, or unspecified) wear Background The TiN coated back surgery wires were made of Ti6A14V. The reported failure was the presence of pits...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.power.c0047681
EISBN: 978-1-62708-229-7
... current to reduce the temperature, by an increase in the electrode force, or both. Compressors Gas turbine engines Welding parameters Ti-6Al-4V UNS R56406 Joining-related failures Fatigue fracture A fluorescent liquid-penetrant inspection of an experimental stator vane of a first-stage...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c0047641
EISBN: 978-1-62708-235-8
... contamination. Contaminants Gas tungsten arc welding Heat affected zone Oxygen Stress concentration Thermal stresses Ti-6Al-4V UNS R56406 Joining-related failures A Ti-6Al-4V alloy pressure vessel failed during a proof-pressure test, fracturing along the center girth weld. The pressure vessel...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0091726
EISBN: 978-1-62708-217-4
.... Recommendations included revising the specification to require a minimum NO content of 0.6%. Nitrogen dioxide Pressure vessels Propellant tanks Ti-6Al-4V UNS R56406 Stress-corrosion cracking Nitrogen tetroxide, a storable hypergolic oxidizer, was used in the service propulsion system (SPS...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0091727
EISBN: 978-1-62708-217-4
... in the imposition of a control specification (MF0004-018) for all fluids that contact titanium for existing and future space designs. Pressure Vessels Propellant tanks Surface pretreatments Ti-6Al-4V UNS R56406 Stress-corrosion cracking The storable hypergolic fuel used for the SPS on the Apollo...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001782
EISBN: 978-1-62708-241-9
... concentric grooves SEM/EDS analysis grain size Ti6Al4V (titanium-aluminum-vanadium alloy) UNS R56406 ...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001030
EISBN: 978-1-62708-214-3
..., corrosion Fasteners Jet planes Marine environments Military planes Solid lubricants Ti-6Al-4V UNS R56406 Stress-corrosion cracking Handbook of Case Histories in Failure Analysis, Volume 1 Copyright ┬ę 1992 ASM International┬« K.A. Esaklul, editor All rights reserved DOI: 10.31399/asm.fach.v01...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.modes.c9001649
EISBN: 978-1-62708-234-1
... at the time of re-torque and at the time of initial torque application several years earlier. Aerospace fasteners Fractography Ti-6Al-4V UNS R56406 Ductile fracture As in many industries, aerospace systems and components are subject to time-dependent degradation. The ongoing structural...
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
... are discussed along with potential methods to eliminate these microstructural in homogeneities. Shear bands Threaded fasteners Ti-6Al-4V UNS R56406 Ductile fracture Threaded Ti-6Al-4V fasteners are used extensively by the aerospace industry for joining structural components. One popular type...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001636
EISBN: 978-1-62708-217-4
... history could have been more severe than anticipated. This possibility was subsequently supported by a separate investigation of the assumed and actual fatigue loads and stresses. Rotor blade Ti-6Al-4V UNS R56406 Fatigue fracture Introduction On 10 November 1998, a Royal Netherlands Navy...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001803
EISBN: 978-1-62708-241-9
... cracking fretting pitting fractography fracture toughness Ti6Al4V (titanium-aluminum-vanadium alloy) UNS R56406 316L stainless steel (austenitic wrought stainless steel) UNS S31603 ...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.med.c9001690
EISBN: 978-1-62708-226-6
.... Corrosion Fracture mechanisms Metallic surgical implants Retrieval analysis Ti-6Al-4V UNS R56406 316L UNS S31603 ISO 5832-2 grade 1 Nitinol (Other, general, or unspecified) corrosion (Other, general, or unspecified) fracture Worldwide data indicate that approximately 100 million metallic...