A rotary aircraft comprising a fuselage tail boom, a tail cone and an interface frame, the interface frame in turn having a connecting structure directly attached to the tail cone by means of a tail cone mechanical connexion and a connecting sleeve fitting axially the fuselage tail boom, the connecting sleeve and the fuselage tail boom being directly attached by means of a one boom mechanical connexion; the interface frame thereby joining the fuselage tail boom and the tail cone.
ROTARY AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE
DREHFLÜGLER MIT EINEM SCHNITTSTELLENRAHMEN, DER MIT DER HINTEREN RUMPFRÖHRE UND DEM HECKKONUS VERBUNDEN IST
AÉRONEF ROTATIF AVEC UN CADRE D'INTERFACE RATTACHANT LA POUTRE ARRIÈRE DU FUSELAGE ET LE CÔNE ARRIÈRE
2020-04-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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