An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. The central element and the two lateral extensions are configured as an integrated piece.
AIRCRAFT FUSELAGE FRAME
2016-06-02
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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