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Series: ASM Handbook Archive
Volume: 10
Publisher: ASM International
Published: 01 January 1986
DOI: 10.31399/asm.hb.v10.a0001746
EISBN: 978-1-62708-178-8
... Abstract High-temperature combustion is primarily used to determine carbon and sulfur contained in a variety of materials. This article illustrates the principle of combustion and focuses on the characteristics of accelerators. It provides information on the process of separating oxide...
Series: ASM Handbook
Volume: 18
Publisher: ASM International
Published: 31 December 2017
DOI: 10.31399/asm.hb.v18.a0006427
EISBN: 978-1-62708-192-4
... Abstract This article focuses on friction, lubrication, and wear of internal combustion engine parts, improvements in which provide important gains in energy efficiency, performance, and longevity of the internal combustion (IC) engine systems. It discusses the types, component materials...
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Published: 01 August 2013
Fig. 3 Robotic application of thermal barrier coating on MS6001B combustion liner. Courtesy of GE More
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Published: 01 August 2013
Fig. 11 Combustion chamber gas and wall ature histories. TDC, top dead center More
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Published: 01 January 1994
Fig. 2 Zirconia-coated magnesium-alloy rocket combustion chamber More
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Published: 01 August 2013
Fig. 6 Comparison of shim carbon readings analyzed by the combustion method with the atmosphere carbon potential at 925 °C (1700 °F). (a) 1.1 and (b) 1.4 wt% C atmosphere carbon potential More
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Published: 01 August 2013
Fig. 2 Comparison of shim carbon readings, analyzed by LECO combustion method, with the atmosphere carbon potential at 925 °C (1700 °F). (a) 1.1 and (b) 1.4 wt% C atmosphere carbon potential More
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Published: 01 January 2006
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
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Published: 01 January 1989
Fig. 8 Jet engine combustion chamber housing with electron beam machined holes. Courtesy of MG Industries/Steigerwald More
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Published: 30 September 2014
Fig. 27 Screw conveyor furnace. Courtesy of Surface Combustion More
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Published: 30 September 2014
Fig. 7 Flow diagram of a Surface ® Combustion RX ® Endothermic Gas Generator System More
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Published: 30 September 2014
Fig. 15 Controlled-atmosphere fluidized-bed furnace heated by submerged combustion. 1, burner; 2, combustion tube; 3, tube through which combustion gases and particles rise; 4, particle separators; 5, heat exchanger; 6, gas recycle compressor for fluidization; 7, distributor plate; 8, parts More
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Published: 30 September 2014
Fig. 16 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 More
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Published: 30 September 2014
Fig. 17 Silicon carbide recuperator/burner nozzle. Courtesy of Eclipse Combustion More
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Published: 30 September 2014
Fig. 1 Efficiency losses due to excess air in a typical gas-fired combustion process. Source: Ref 1 = N. Burk and G. Woolbert, Technologies for Low Cost Combustion Control, in Industrial Combustion Technologies , American Society for Metals, 1986, p 213–220 More
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Published: 30 September 2014
Fig. 2 Effects of excess air or fuel on combustion efficiency. (a) General effect on efficiency. (b) Effect on percent of fuel wasted More
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Published: 01 January 1986
Fig. 1 Typical high-frequency combustion configuration. More
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Published: 01 January 2002
Fig. 15 Alloy 718 inner-combustion-chamber case assembly that fractured by fatigue in the weld joining the flange to the case and stiffener. (a) Exterior surface of the assembly showing the circumferential fracture of the case (arrow). 0.5×. (b) Section through the fracture showing the weld More
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Published: 01 January 2003
Fig. 13 Variation in equilibrium composition of the combustion flame as a function of the fuel-to-air ratio when pressure p = 22.1 atm (2.24 MPa) and the inlet temperature T 0 = 811 K (1000 °F) (for fuel jet A + 0.3% S; air, 5 ppm sea salt). (a) The major products formed. (b) Sodium More
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Published: 31 December 2017
Fig. 4 Pressure traces for normal combustion and preignition from LSPI (low-speed preignition) engine test. Source: Ref 25 More