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combustion

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Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490415
EISBN: 978-1-62708-340-9
...Abstract Abstract Combustion turbines consist of a compressor, a combustor, and a turbine. As commonly configured, the compressor and turbine mount on a single shaft that connects directly to a generator. This chapter reviews the materials of construction, damage mechanisms, and life-assessment...
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Published: 01 December 2018
Fig. 1.3 Schematic diagram of a fluidized bed combustion boiler More
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Published: 01 March 2006
Fig. 8 Gas-fired fluidized-bed furnace with internal combustion. 1, insulating lagging; 2, refractory material; 3, air and gas distribution box; 4, fluidized bed; 5, parts to be treated. Source: Ref 6 More
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Published: 01 March 2002
Fig. 14.9 Engine-operated aircraft gas turbine combustion chamber showing metal loss and degradation, owing to oxidation More
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Published: 01 March 2002
Fig. 14.10 Enlarged view of area of combustion chamber showing examples of thermal-mechanical fatigue cracking More
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Published: 01 April 2013
Fig. 8 Schematic of combustion/inert gas fusion apparatus. Source: Ref 1 More
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Published: 01 August 1999
Fig. 4 Aluminum alloy 6061-T6 combustion chamber damaged by cavitation erosion. The chamber rotated in water at moderate speed. (a) Overall view of the chamber. (b) and (c) Micrographs of cross sections of the chamber wall showing typical cavitation damage. 100 and 500×, respectively More
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Published: 01 November 2007
Fig. 8.7 Effect of the test environments (argon and fluidized-bed combustion) on the erosion behavior of HS 1 (Co-30Cr-12W-2.5C) and HS 6B (Co-30Cr-4W-1C) at 760 °C (1400 °F), 42.7 m/s (140 ft/s), with 12 μm alumina (Al 2 O 3 ) as erodent (a) 30° impingement angle and (b) 90° impingement angle More
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Published: 01 November 2007
Fig. 8.8 Effect of the test environments (argon and fluidized-bed combustion) on the erosion behavior of FeCrAlY (Fe-25Cr-4Al-1Y) and IN-100 (Ni-15Co-10Cr-5.5Al-4.7Ti-3Mo) at 760 °C (1400 °F), 42.7 m/s (140 ft/s), with 12 μm alumina (Al 2 O 3 ) as erodent (a) 30° impingement angle and (b) 90 More
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Published: 01 November 2007
Fig. 8.16 Erosion behavior of alloys and coatings under hot, oxidizing combustion gas stream at 815 °C (1500 °F) and 366 m/s (1200 ft/s) with fly-ash as erodent. Source: Ref 25 More
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Published: 01 November 2007
Fig. 10.11 Metal loss data for carbon steel in a simulated combustion atmosphere consisting of N 2 -10CO-10H 2 O-0.5SO 2 containing different levels of HCl (0, 400, and 2000 ppm) at 400 °C. Source: Ref 22 More
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Published: 01 November 2007
Fig. 10.12 Metal loss data for carbon steel in a simulated combustion atmosphere consisting of N 2 -10CO-10H 2 O-0.5SO 2 containing different levels of HCl (0, 400, and 2000 ppm) at 500 °C. Source: Ref 22 More
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Published: 01 December 1989
Fig. 9.1. Typical configuration of a combustion turbine (General Electric Model MS7001F) ( Ref 1 ; courtesy of G.A. Cincotta, General Electric Co., Schenectady, NY). More
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Published: 01 December 1989
Fig. 9.5. Combustion turbine blades ( Ref 5 ). More
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Published: 01 December 1989
Fig. 9.6. Air-cooled combustion turbine blades ( Ref 5 ; original source, Westinghouse Electric Corp.). More
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Published: 01 December 2015
Fig. 23 Corrosion rate in a combustion environment versus time as monitored using electrochemical methods is plotted with a key process variable. Fireside corrosion of boiler tubes in coal-fired utilities and waste incineration plants is an expensive and difficult problem to deal with. Special More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2018
DOI: 10.31399/asm.tb.fibtca.t52430001
EISBN: 978-1-62708-253-2
... combustion boilers, oil- and gas-fired boilers, waste heat boilers, and black liquor recovery boilers. It also describes the operation and working principle of utility or power plant boilers, covering conventional subcritical and advanced supercritical types. black liquor recovery boilers electric...
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Published: 01 November 2007
Fig. 9.7 Test specimens alloy HR-160, 625, 800H, RA330, and Type 310 at 900 °C (1650 °F) in the combustion gas stream generated by a burner rig using No. 2 fuel oil (0.4% S) for combustion at 35:1 air-to-fuel ratio and with injection of 50 ppm sea salt into the combustion gas stream. During More
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 April 2013
DOI: 10.31399/asm.tb.imub.t53720139
EISBN: 978-1-62708-305-8
...Abstract Abstract The overall chemical composition of metals and alloys is most commonly determined by x-ray fluorescence (XRF) and optical emission spectroscopy (OES). High-temperature combustion and inert gas fusion methods are typically used to analyze dissolved gases (oxygen, nitrogen...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080259
EISBN: 978-1-62708-304-1
...Abstract Abstract This chapter discusses material-related problems associated with coal-fired burners. It explains how high temperatures affect heat-absorbing surfaces in furnace combustion areas and in the convection pass of superheaters and reheaters. It describes how low-NOx combustion...