Results 91 to 100 of about 49,628 (234)
Performance and emission characteristics of swirl-can combustors to near-stoichiometric fuel-air ratio [PDF]
Emissions and performance characteristics were determined for two full annular swirl-can combustors operated to near stoichiometric fuel-air ratio. Test condition variations were as follows: combustor inlet-air temperatures, 589, 756, 839, and 894 K ...
Diehl, L. A., Trout, A. M.
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Diesel engine catalytic combustor system [PDF]
A low compression turbocharged diesel engine is provided in which the turbocharger can be operated independently of the engine to power auxiliary equipment.
Ream, L. W.
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Analytical fuel property effects--small combustors [PDF]
The consequences of using broad-property fuels in both conventional and advanced state-of-the-art small gas turbine combustors are assessed. Eight combustor concepts were selected for initial screening, of these, four final combustor concepts were chosen
Miles, G. A. +2 more
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Techniques for enhancing durability and equivalence ratio control in a rich-lean, three-stage ground power gas turbine combustor [PDF]
Rig tests of a can-type combustor were performed to demonstrate two advanced ground power engine combustor concepts: steam cooled rich-burn combustor primary zones for enhanced durability; and variable combustor geometry for three stage combustion ...
Schultz, D. F.
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Gas turbine engine emission reduction technology program [PDF]
Progress in the development of combustor technology to meet the standards for the allowable pollutant emission levels of aircraft gas turbine engines is reported.
Diehl, L. A., Petrash, D. A.
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Test fires of a rotating detonation engine (RDE) annular combustor operating on a methane–oxygen mixture were conducted. Compared to the original RDE combustor previously tested, it was modified in terms of changing the layout of the water cooling system,
Sergey M. Frolov +3 more
doaj +1 more source
In this work, a numerical study has been carried out in order to investigate the effects of a micro combustor size on the exergy and energy efficiencies of a premixed hydrogen/air for a micro thermophotovoltaic system. For this purpose, six combustors in
E. Nadimi, S. Jafarmadar
doaj
NASA/General Electric broad-specification fuels combustion technology program, phase 1 [PDF]
The use of broad specification fuels in aircraft turbine engine combustion systems was examined. Three different combustor design concepts were evaluated for their ability to use broad specification fuels while meeting several specific emissions ...
Dodds, W. J.
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Gas turbine combustor insensitive to compressor outlet distortion [PDF]
Short-length annular combustor for turbojet engines eliminates change of exit temperature profile. Individual scoops of full annular height control air distribution so that shifts in the radial velocity profile of air entering the combustor will not ...
Humenik, F., Norgren, C. T.
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Fuel distribution measurements in a model low NOx double annular combustor using laser induced fluorescence [PDF]
Planar laser induced fluorescence (PLIF) was employed in a three sector, low NOx double annular combustor in order to characterise the combusting fuel spray.
Greenhalgh, D. A., Lockett, R. D.
core

