Component Performance and System Payoff for Advanced Internal Power Generation Unit 751114
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.
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. Download Citation
Author(s):
F. J. Suriano
Affiliated:
AiResearch Manufacturing Co. of Arizona, div., Garrett Corp.
Pages: 12
Event:
Aerospace Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Gas turbines
Aircraft
SAE MOBILUS
Subscribers can view annotate, and download all of SAE's content.
Learn More »
