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UNS S17700

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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c0006394
EISBN: 978-1-62708-217-4
... a different heat treatment (which would offer lower strength but higher toughness) could be used for this part. Grain boundaries Precipitates Scanning electron microscopy Sensitizing 17-7 PH UNS S17700 Intergranular corrosion Stress-corrosion cracking Heat treating-related failures Brittle...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.design.c0048169
EISBN: 978-1-62708-233-4
... engines Design Engine components Service life 17-7 PH UNS S17700 Fatigue fracture The part shown in the “original design” portion of Fig. 1 was a valve-seat retainer spring from a fuel control on an aircraft engine. This spring was found to be broken during disassembly of the fuel control...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.mech.c9001547
EISBN: 978-1-62708-225-9
... S17700 Custom 455 UNS S45500 Fatigue fracture Stress-corrosion cracking Mechanical springs go into a variety of aerospace systems where both efficiency and reliability are required. Typical applications range from the control of switching characteristics of miniature switches to the deployment...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001707
EISBN: 978-1-62708-217-4
...: A286 (S66286) semi-austenitic: 17-7 PH (S17700), PH 15-7 Mo (S15700), AM 350 (S35000), AM 355 (S35500) martensitic: PH 13-8 Mo (S13800), 15-5 PH (S15500), 17-4 PH (S17400), Custom 450 (S45000), Custom 455(S45500). The martensitic alloys only require a single step heat treatment...