JOINT ASSEMBLY AND METHOD CONNECTING AN AIRCRAFT BELLY FAIRING TO THE FUSELAGE PROVIDED WITH A PARTICULARLY POSITIONED STRINGER

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 flang...

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Bibliographische Detailangaben
Hauptverfasser: ANTYPAS JÉROME, MENARD SÉBASTIEN, ROUYRE FRANÇOIS, CROS CHRISTIAN
Format: Patent
Sprache:eng
Schlagworte:
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