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Component Performance and System Payoff for Advanced Internal Power Generation Unit
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English
Abstract
The overall growth in aircraft internal power system requirements has dictated that a key part of that system, the small gas turbine internal power engine, become a high performance engine in terms of horsepower per engine cubic foot and pound. These performance levels must be met while facing unique problems attendant with internal power applications. Some of these problems are demonstrated by examining the engine performance influence coefficients of a USAF advanced internal power generation engine and comparing with those of a larger propulsion engine.
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Citation
Suriano, F., "Component Performance and System Payoff for Advanced Internal Power Generation Unit," SAE Technical Paper 751114, 1975, https://doi.org/10.4271/751114.Also In
References
- Private communication USAF Aero Propulsion Laboratory June 1975
- Tanemura K. T. Hainline B. C. “The Role of the Auxiliary Power Unit in Future Airplane Secondary Power Systems,” SAE Paper 730381 , presented at the Air Transportation Meeting Miami, Florida April 24-26 1973
- Schnell E. “Auxiliary Power Units for Secondary Power Systems,” Reference 18, AGARD Conference Proceedings No. 104 December 1972
- “Advanced Auxiliary Power Unit,” Final Report to Contract F33615-72-C-1936 July 1975