Allison Model 501-A2 consists of turbine section and propeller reduction gear housing, joined together by interconnecting structure; 501 is rated statically at 2550 shp and 415 lb thrust, with equivalent shaft power at takeoff speed of 2750 hp; dry weight of engine 1225 lb; installation in Convair 240 (Turboliner).
Propeller turbines in transport aircraft
Aeronautical Eng Rev
Aeronautical Engineering Review ; 9 , n 8
1950
Aufsatz (Zeitschrift)
Englisch
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Optimum Propeller Wind Turbines
AIAA | 1983
|Small Transport Aircraft Technology Propeller Study
NTIS | 1983
|Small transport aircraft technology propeller study
NTRS | 1983
|Reheating turbines and C.P. Propeller
Engineering Index Backfile | 1966