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gas turbine components

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Series: ASM Handbook
Volume: 18
Publisher: ASM International
Published: 31 December 2017
DOI: 10.31399/asm.hb.v18.a0006428
EISBN: 978-1-62708-192-4
... and gas turbines. The article outlines the differences in the operating conditions and the nature of the components involved in gas and steam turbines. It discusses the constraints and applicable coating solutions for wear and friction issues, and concludes with a broad set of challenges that need...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003060
EISBN: 978-1-62708-200-6
... in detailed design procedure. The article provides information on the proof testing of ceramics, and presents a short note on public domain software that helps determine the reliability of a loaded ceramic component. The article concludes with several design scenarios for gas turbine components, turbine...
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
... Abstract This article provides a discussion on the structural ceramics used in gas turbine components, the automotive and aerospace industries, or as heat exchangers in various segments of the chemical and power generation industries. It covers the fundamental aspects of chemical corrosion...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004124
EISBN: 978-1-62708-184-9
..., and nuclear), land-based gas turbine and diesel engines, gas turbine engines for aircraft, marine gas turbine engines for shipboard use, waste incineration, high-temperature fuel cells, and missile components. This article discusses high-temperature corrosion in boilers, diesel engines, gas turbines...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005737
EISBN: 978-1-62708-171-9
... Fig. 1 Gas turbine components. TBCs, thermal barrier coatings. Courtesy of Siemens Fig. 2 Robotic application of thermal barrier coating on MS7001E transition piece. Courtesy of GE Fig. 3 Robotic application of thermal barrier coating on MS6001B combustion liner. Courtesy...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003061
EISBN: 978-1-62708-200-6
... and valve components, rolling elements and bearings, paper and wire manufacturing, biomedical implants, heat exchangers, adiabatic diesel engines, advanced gas turbines, and aerospace applications. advanced ceramics aerospace applications mineral processing equipment structural applications...
Book Chapter

Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001293
EISBN: 978-1-62708-170-2
... Abstract This article describes the widespread use of diffusion coatings for elevated-temperature protection of the turbine components for aircraft engines and gas turbines. The principles of pack diffusion coating, namely, aluminizing, chromizing, and siliconizing, are discussed. The article...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003170
EISBN: 978-1-62708-199-3
..., poured into a mold, and allowed to solidify. Typical uses of castings include municipal hardware, water distribution systems (pipes, pumps, and valves), automotive components (engine blocks, brakes, steering and suspension components, etc.), prosthetics, and gas turbine engine hardware. This introduction...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003517
EISBN: 978-1-62708-180-1
... Abstract This article focuses on the life assessment methods for elevated-temperature failure mechanisms and metallurgical instabilities that reduce life or cause loss of function or operating time of high-temperature components, namely, gas turbine blade, and power plant piping and tubing...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003140
EISBN: 978-1-62708-199-3
... Applications Physical Metallurgy Alloy Systems Information Sources on Titanium Gas Turbine Engine Components Aerospace Pressure Vessels Applications Requiring Corrosion Resistance and High Strength Optic-System Support Structures Prosthetic Devices Consumer Goods Unalloyed...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005706
EISBN: 978-1-62708-171-9
... applications. Figure 2 also shows the influence aircraft engine applications have had on the growth of the industry. Thermal spray coatings have been used for advanced gas turbine components such as compressor blades, compressor stator vanes, bearing housings, and labyrinth seals since the early 1960s...
Book: Casting
Series: ASM Handbook
Volume: 15
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.hb.v15.a0005341
EISBN: 978-1-62708-187-0
... nitride bearing elements Various materials, turbines Gas turbine components (not yet in production) PCRT is effective on materials that are stiff and resonant. This includes most metals, ceramics, and a few composites. Metals that are not suitable include very soft metals, such as lead...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005734
EISBN: 978-1-62708-171-9
... (>1000, <1500 °F) WC/CoCr, CoCrMo, NiCr-Cr 3 C 2 , CoNiCrAlY/HBN PS, HVOF, HVAF, DG Various aerospace/industrial gas turbine components in compressor/turbine section: air seals, air seal rings, air seal spacers, baffle dampeners, exhaust struts, inner nozzle supports (a) PS, plasma spray...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003555
EISBN: 978-1-62708-180-1
... , p 511 65. Streiff R. , Cerelier O. , and Boone D.H. , Surf. Coat. Technol. , Vol 32 , 1987 , p 111 66. McMordie B.G and Isaacs A.K. , “Slurry Aluminide Coating Processes for Gas Turbine Components at Overhaul,” presented at The Annual Gas Turbine...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006787
EISBN: 978-1-62708-295-2
... failures, molten salts for energy storage, and degradation and failures in gas turbines. The article describes the effects of environment on aero gas turbine engines and provides an overview of aging, diffusion, and interdiffusion phenomena. It also discusses the processes involved in high-temperature...
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006094
EISBN: 978-1-62708-175-7
... of HIP Consolidated P/M Superalloys for Conventional Forging to Gas Turbine Engine Components , Superalloys 1996 , Kissinger R.D. et al. , Ed., The Minerals, Metals, and Materials Society , 1996 , p 645 – 652 21. Locq D. and Caron P. , On Some Advanced Nickel-Based...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001072
EISBN: 978-1-62708-162-7
... to 815 °C (1200 to 1500 °F) as the rotor turned at speeds of 20,000 to 30,000 rpm, led to improved precipitation-hardened alloys Hastelloy alloy B and Hastelloy alloy X The production of the first gas turbine engine led to developments in new alloys for blades, vanes, and disks with improved creep...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002476
EISBN: 978-1-62708-194-8
... Components. Advanced Gas Turbine Systems for Automobiles,” SP-465, Society of Automotive Engineers , 1980 , p 69 – 77 10.4271/800194 20. Dukes W.H. , Handbook of Brittle Material Design Technology , AGARDograph 152, AGARD, Paris, France , 1971 21. Batdorf S.B. , Fundamentals...
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001052
EISBN: 978-1-62708-161-0
... the superior strength of the bond. In addition, the rupture lives of the combinations were always equal to or greater than that for alloy 901 alone. These results imply that a dual-alloy concept is viable for enhancing the local properties of gas turbine components and for conserving costly strategic materials...
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003619
EISBN: 978-1-62708-182-5
..., heat treatment components N06075 Nimonic 75 19.5 75.0 … … … 0.4 0.15 2.5 0.12 0.25 max Cu Gas turbines, heat treatment equipment N06230 Haynes 230 22.0 55.0 5.0 max 2.0 … … 0.35 3.0 max 0.10 14.0 W, 0.015 max B, 0.02 La Gas turbines, superheater tubes N06600 Inconel...