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- W272929231 abstract "Abstract : The purpose of the program was to advance the technology of small Auxiliary power units, using the secondary power system requirements of a hypothetical fighter aircraft of mid-1970 as a goal and an auxiliary power system as a test bed for exploratory development. The APU was 10 in. in diameter by 24 in. long, and the design-point performance goal was 300 equivalent shaft horsepower at 2200F turbine inlet temperature and sea level, 130F ambient conditions. Other design-point goals included an 11:1 cycle pressure ratio, 55- lb/min bleed-air at 6:1 pressure ratio, and a total system weight under 200 lb, including the starting system. The program resulted in technological advancements in the axial-centrifugal compressor, including variable inlet guide vanes, uncooled 2200F combustion, an advanced radial in-flow cooled-turbine, uncooled columbium nozzles, and an advanced high-speed torque converter with lockup feature." @default.
- W272929231 created "2016-06-24" @default.
- W272929231 creator A5068872974 @default.
- W272929231 creator A5091014832 @default.
- W272929231 date "1972-11-30" @default.
- W272929231 modified "2023-09-27" @default.
- W272929231 title "Advanced Auxiliary Power System" @default.
- W272929231 doi "https://doi.org/10.21236/ad0754903" @default.
- W272929231 hasPublicationYear "1972" @default.
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