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Combustion
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Book Chapter
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...
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 techniques for nozzles and buckets. It also presents key information from a detailed review of the literature and the results of a survey on combustion-turbine material problems.
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in Introduction to Boiler Technology
> Failure Investigation of Boiler TubesA Comprehensive Approach
Published: 01 December 2018
Fig. 1.3 Schematic diagram of a fluidized bed combustion boiler
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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
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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
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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
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Published: 01 April 2013
Fig. 8 Schematic of combustion/inert gas fusion apparatus. Source: Ref 1
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in Erosion, Cavitation, Impingement, and Fretting Corrosion
> Corrosion of Aluminum and Aluminum Alloys
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
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in Applications of Iron and Steel Castings and the Impact of Electric Vehicles
> Iron and Steel Castings Engineering Guide
Published: 01 January 2022
Fig. 13.7 Schematic of an internal combustion engine and motors and generators
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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
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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
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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
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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
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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
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
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).
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.5. Combustion turbine blades ( Ref 5 ).
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.6. Air-cooled combustion turbine blades ( Ref 5 ; original source, Westinghouse Electric Corp.).
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in Corrosion in Petroleum Refining and Petrochemical Operations[1]
> Corrosion in the Petrochemical Industry
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
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Book Chapter
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...
Abstract
Boilers are engineered systems designed to convert the chemical energy in fuel into heat to generate hot water or steam. This chapter describes boiler applications and types, including firetube boilers, watertube boilers, electric boilers, packaged boilers, fluidized bed 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.
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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
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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...
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, and hydrogen) and, in some cases, carbon and sulfur in metals. This chapter discusses the operating principles of XRF, OES, combustion and inert gas fusion analysis, surface analysis, and scanning auger microprobe analysis. The details of equipment set-up used for chemical composition analysis as well as the capabilities of related techniques of these methods are also covered.