The power section for an advanced rotary stratified-charge general aviation engine has been designed under contract to NASA. The single-rotor research engine of 40 cubic-inches displacement (RCI-40), now being procured for test initiation this summer, is targeted for 320 T.O. horse-power in a two-rotor production engine. The research engine is designed for operating on jet-fuel, gasoline or diesel fuel and will be used to explore applicable advanced technologies and to optimize high output performance variables. Design of major components of the engine is described in this paper.
Design of a high-performance rotary stratified-charge research aircraft engine
01.06.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
Design of a high-performance rotary stratified-charge research aircraft engine
Tema Archiv | 1984
|Advanced Stratified Charge Rotary Engine Design
SAE Technical Papers | 1989
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