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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
... Abstract This article illustrates typical wear and friction issues encountered in gas and steam turbines and their consequences as well as commonly adopted materials solutions. It contains tables that present the summary of wear and friction related issues encountered in steam turbines and gas...
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
... Abstract This article provides an overview of key thermal spray coatings used in compressors, combustors, and turbine sections of a power-generation gas turbine. It describes the critical components, including combustors, transition ducts, inlet nozzle guide vanes, and first-stage rotating...
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Published: 01 August 2013
Fig. 7 Temperature profile through gas turbine ngine. Gas temperatures exceed melting point of structural materials. LPC, low-pressure compressor; HPC, high-pressure compressor; HPT, high-pressure turbine; LPT, low-pressure turbine More
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Published: 01 August 2013
Fig. 1 Gas turbine components. TBCs, thermal barrier coatings. Courtesy of Siemens More
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Published: 01 January 1990
Fig. 24 Dynamic oxidation, 1177 °C (2150 °F), cyclic. Source: Allison Gas Turbine Division, General Motors Corporation More
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Published: 01 January 1990
Fig. 15 Typical investment cast titanium alloy components used for gas turbine applications More
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Published: 01 January 2006
Fig. 27 High-temperature oxidation of the tip of an industrial gas turbine blade. Below the tip, a coating is protecting the base metal. See the article “Corrosion of Industrial Gas Turbines” in this Volume. More
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Published: 01 January 2006
Fig. 28 Severe attack of an aeroderivative gas turbine blade by hot corrosion. See the article “Corrosion of Industrial Gas Turbines” in this Volume. More
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Published: 01 January 2006
Fig. 5 Severe attack of an aeroderivative gas turbine blade by hot corrosion More
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Published: 01 January 2006
Fig. 2 Titanium alloy gas-turbine ring that was produced by compression forming. Dimensions given in inches More
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Published: 01 December 2008
Fig. 13 Typical investment cast titanium components used for gas turbine applications More
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Published: 01 January 1997
Fig. 8 Gas turbine engine and components. Scroll and rotor are made from structural ceramics. Courtesy of Allison Engine Company More
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Published: 01 November 1995
Fig. 18 Duty cycles and lifetime requirements for different types of gas turbine engines. Lifetime is given in hours. More
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Published: 01 November 1995
Fig. 20 Cutaway view of the Garrett AGT101 ceramic gas turbine test engine More
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Published: 31 December 2017
Fig. 1 (a) Schematic illustration of a gas turbine with key components and examples of wear. Source: Ref 2 , 3 , 4 . (b) Fretting damage location on dovetail joint, Courtesy of Lambda Technologies Group. (c) Microcracks on dovetail joint, Courtesy of Lambda Technologies Group. (d) Droplet More
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Published: 31 December 2017
Fig. 4 Schematic illustration of a 7EA gas turbine showing sealing locations. Source: Ref 24 More
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Published: 01 January 1993
Fig. 1 Furnace brazed MA 754 gas turbine vane More
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Published: 01 January 1987
Fig. 835 Segment of a fractured second-stage gas-turbine wheel, cast from alloy 713C, that broke from fatigue in service. (About half of the disk portion of the wheel was never recovered.) The fracture origin (at arrow) was in a grinding-relief groove adjacent to the wheel-balancing pad More
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Published: 30 August 2021
Fig. 1 Failed gas turbine rotor. From left to right: first-, second-, and third-stage turbine blades. The failure originated in the second stage; fragments