SMALL GAS-TURBINE COMBUSTOR STUDY - FUEL INJECTOR EVALUATION.

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作者：
Norgren, Carl T.
Riddlebaugh, Stephen M.
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NASA Technical Memorandum | 1981年
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摘要：
An investigation was undertaken of fuel injection technique and effect of fuel type on small gas-turbine combustors. Performance and pollutant emission levels are documented over a range of simulated flight conditions for a reverse-flow combustor configuration using simplex pressure-atomizing, spill-flow return, and splash cone airblast injectors. A parametric evaluation of the effect of increased combustor loading with each of the fuel injector types was obtained. Jet A and an experimental referee broad specification fuel were used to determine the effect of fuel type.
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