B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01) B64C 3/18 (2006.01) B64F 5/00 (2006.01)
Patent
CA 2726575
Aircraft fuselage frame in composite material with stabilising ribs which, in at least a first sector (31), comprises a frame (9) with an omega-shaped cross-section (11) formed by a top element (23), two webs (25, 25'), two feet (27, 27') which includes at least one internal rib (41) formed by a top element (43) joined to the top element (23) of the frame (9), a web (45), two flanges (49, 49') joined to the webs (25, 25') of the frame (9) and a foot (47) aligned with the feet (27, 27') of the frame (9). The invention also relates to a manufacturing procedure for the first sector (31) of the frame with stabilised web (10) comprising steps for: a) providing a frame (9) and at least one internal rib (41) with the configurations indicated; b) joining at least said internal rib (41) to the frame (9).
Arevalo Rodriguez Elena
Cruz Dominiguez Francisco Jose
Airbus Operations S.l.
Bereskin & Parr Llp/s.e.n.c.r.l.,s.r.l.
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