A rotary wing 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 connection 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 connection; the interface frame thereby joining the fuselage tail boom and the tail cone.
ROTARY WING AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE
2017-11-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Rotary wing aircraft with an interface frame joining the fuselage tail boom and the tail cone
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ROTARY WING AIRCRAFT WITH AN INTERFACE FRAME JOINING THE FUSELAGE TAIL BOOM AND THE TAIL CONE
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