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Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003515
EISBN: 978-1-62708-180-1
... to understand how safe and reliable that equipment or structure might be over this additional time of service. Common Measurement Techniques Life Assessment Strategies The Role of NDE Non-Aerospace Applications Implementation Guidance Conclusions References References 1. “Standard...
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
... to obtain maximum strength. Of these alloys, PH 13-8 Mo has often been specified for aerospace applications requiring high strengths (i.e. tensile strengths as high as 235 ksi (1620 MPa) can be achieved), good transverse mechanical properties, high fracture toughness, corrosion resistance, and oxidation...
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.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
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001030
EISBN: 978-1-62708-214-3
.... and Impellizzeri L.F. , “Fatigue Analysis of Cold Worked and Interference Fit Fastener Holes,” MCAIR 76-007, in STP 637, ASTM , 1976 . 10.1520/STP27993S 3. Shigley , Mechanical Engineering Design , 1977 . 4. Aerospace Structural Metals Handbook , Battelle Columbus Laboratories , 1983...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006805
EISBN: 978-1-62708-329-4
... with aluminum because the galvanic characteristics of cadmium are more favorable than those of zinc. Chromate coatings are also used over cadmium coatings for the reasons given for zinc-plated fasteners. Cadmium as a corrosion coating is now mostly limited to the military and aerospace applications due...
Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001299
EISBN: 978-1-62708-215-0
... be used to cheek for cracks during periodic maintenance overhauls. Aerospace engines Airplanes Nonmetallic inclusions 4340 UNS G43400 Fatigue fracture Background Visual Examination of General Physical Features Testing Procedure and Results Discussion Conclusion...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003519
EISBN: 978-1-62708-180-1
... has been used in commercial applications with great success when replacing nonplated UNS 52100 martensitic steel bearings. However, once that component moved into aerospace applications as a low-cost replacement for American Iron and Steel Institute 440C stainless steel, the requirements changed...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003503
EISBN: 978-1-62708-180-1
... Applications,” ARP 5580, Society of Automotive Engineers Aerospace Recommended Practice , July 2001 12. Bowles J.B. , The New SAE FMECA Standard , Proc. Annual Reliability and Maintainability Symposium , 1998 , p 48 – 53 10.1109/RAMS.1998.653561 13. Goddard P.L. , Validating...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003516
EISBN: 978-1-62708-180-1
... from the aerospace industry. References References 1. Nondestructive Evaluation and Quality Control , Vol 17 , ASM Handbook , ASM International , 1987 2. Metallic Materials and Elements for Aerospace Vehicle Structures , MIL-HDBK-5F, Department of Defense, Nov 1990 , p 3 – 104...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001023
EISBN: 978-1-62708-214-3
.... The wear had been caused by incorrect machining of the shaft splines, which prevented the bevel gear nut from locating correctly against the gear. Aerospace engines Aircraft components Bevel gears Drives Engine components Jet planes Military planes Splines 16 NCD 13 Fretting wear...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006800
EISBN: 978-1-62708-329-4
... can be an emulative process, whereby a successful design is adapted for a similar but separate service application. Emulative design assumes that the new intended service is analogous, that the materials and processing are the same, and that the knowledge of the prior design is complete. Using prior...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003501
EISBN: 978-1-62708-180-1
.... This article cannot detail the many particulars of materials selection, because every industry or component application has many specific requirements, guidelines, or procedures, some of which may be mandated by federal or state statute. Therefore, coverage is more conceptual with general discussions...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001504
EISBN: 978-1-62708-217-4
... Data Center , Traverse City, Michigan ( 1977 ) 3. MIL-HDBK-5C “Metallic Materials and Elements for Aerospace Vehicle Structures” , p. 2 – 58 , Dept. of Defence , U.S.A. , ( Jan . 1984 ) 4. “Advanced Material for Landing Gear” , Aerospace Engineering Journal, Vol. 10 , No. 7 , pp. 17...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001781
EISBN: 978-1-62708-241-9
.... Shackelford J.C. , Development of a short range tracking system using an inertial measurement unit . Master’s Thesis , Department of Aerospace Engineering, Mississippi State University 2011 7. McGinnis R.S. , Nesbit S. , Open Sports Sci. J. 3 , 155 – 164 ( 2010 ) 10.2174...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003551
EISBN: 978-1-62708-180-1
...) … … (a) A, resistant to attack up to temperature indicated; B, some reaction at temperature indicated; C, appreciable attack at temperature indicated Abstract Abstract This article provides a discussion on the structural ceramics used in gas turbine components, the automotive and aerospace industries...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006835
EISBN: 978-1-62708-329-4
... Because of their low density and high potential strength, aluminum forgings are found in automotive and aerospace applications. Like titanium, aluminum is highly strain-rate sensitive. In production with high-strain-rate tools such as hammers and mechanical presses, the rapid delivery of energy can cause...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001813
EISBN: 978-1-62708-180-1
... touched down and the vertical load has decreased to the static load of the aircraft, the continuing application of side and drag loads during taxiing causes a tensile stress at the top surface of the spring. Compressive stresses in the top surface of the spring at the support are generally localized...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001706
EISBN: 978-1-62708-217-4
... Preventive Compounds-Solvent Cutback Cold Application, (1993) 7. Military Handbook 5F , Metallic Materials & Elements for Aerospace Vehicle structures, Vol.1 , pp 2 –31 to 2– 51 ( 1990 ) Selected References Selected References • Forms of Corrosion , Failure Analysis and Prevention...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001028
EISBN: 978-1-62708-214-3
... fatigue fracture was caused by engine vibrations during operation of the aircraft. Fracture characteristics indicated that the fatigue would not have occurred if the initial damage had not taken place. Aerospace engines Engine components Gas turbine engines Lubrication systems Tanks Tearing...