Turbine engine accessory drive techniques were investigated to establish potential systems for a lightweight low profile package. The frame of reference was provided by three classes of advanced engines for the 1975 to 1980 time period: the (1) low bypass turbofan (fighter), (2) high bypass turbofan (transport), and (3) small turbofan (remote-piloted vehicle). Design study information is presented and used to establish a ranking of candidate system attractiveness against defined and weighted criteria. Conceptual design drawings, depicting a selected system for each study engine class, are provided and development recommendations are given. (Modified author abstract)
Turbine Engine Advanced Accessory Drive System Study
1973
314 pages
Report
Keine Angabe
Englisch