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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
... the microarcing. Arcing Pitting (wear) Surgical implants Wire Ti-6Al-4V Titanium nitride coating UNS R56406 Surface treatment related failures (Other, miscellaneous, or unspecified) wear Background Observations and Results Discussion And Conclusion Selected Reference Selected...
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
... reduction in welding 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...
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
... further resulted 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...
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
.... golf club fracture atmospheric contamination titanium alloy cracking concentric grooves SEM/EDS analysis grain size Ti6Al4V (titanium-aluminum-vanadium alloy) UNS R56406 Introduction The relative low density, high strength, and corrosion resistance of titanium alloys make them well...
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
... R56406 Stress-corrosion cracking Background Cracks were discovered between interference-fit fasteners (MoS 2 -coated Ti-6Al-4V) that had been incorporated into a fighter aircraft primary structural frame (D6ac steel) to enhance structural fatigue life. Applications Modern fighter aircraft...
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
... of the bolt 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...
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
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001803
EISBN: 978-1-62708-241-9
... discussed. orthopedic implant devices fracture corrosion inclusions and stress gaps medical materials 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
... implants. 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...
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
... stress 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 Failure Analysis Topics and Techniques...