An airplane (10) including an airframe (12) and a turboprop propulsion system (14) is disclosed. The turboprop propulsion system (14) includes a propeller (20) mounted for rotation about a propeller axis (30) and a gas turbine engine (22) coupled to the propeller (20) to drive rotation of the propeller (30). The gas turbine engine (22) rotates about an axis (32) which is offset from the propeller axis (30).
AIRPLANE WITH ANGLE-MOUNTED TURBOPROP ENGINE
FLUGZEUG MIT WINKELMONTIERTEM TURBOPROPTRIEBWERK
AVION COMPORTANT UN TURBOPROPULSEUR À MONTAGE INCLINÉ
2020-02-19
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Engineering Index Backfile | 1952
|Turboprop airplane control problems associated with engine failure considerations
Engineering Index Backfile | 1956
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