A joint assembly in an aircraft connecting a belly fairing to the fuselage of the aircraft. The belly fairing has a sewing angle connected to a main belly fairing section, while the fuselage has a fuselage skin with an exterior and an interior. The joint assembly includes a sewing angle with a flange connected to the fuselage skin exterior at a fixation zone of the fuselage skin, with the fixation zone being overlapped by the flange where it is connected thereto. The joint assembly further includes a stringer connected to the fuselage skin interior and overlapping the fixation zone. This joint assembly is less susceptible to vibrations. The disclosure herein also pertains to a method of providing such a joint assembly.
ENSEMBLE DE JONCTION RACCORDANT UN CARENAGE VENTRAL D'AERONEF AU FUSELAGE POURVU D'UN RAIDISSEUR EN POSITION PARTICULIERE
2017-02-10
Patent
Electronic Resource
French
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