The AiResearch TFE731-2 Turbofan Engine Control system was created out of a recognition of engine and aircraft operating requirements in which a free weighting of candidate control components and logic was made. From this free design iteration process, which considered both conventional and advanced concepts of control, the control described in this paper has evolved and has fulfilled the in-flight operating requirements of the engine.
A Control Concept Combining the Best of the Current Hydromechanical and Electronic Technologies
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1974
1974-02-01
Aufsatz (Konferenz)
Englisch
Electronic-control System of Hydromechanical Transmission
British Library Conference Proceedings | 1999
|Tema Archiv | 1975