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 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. 本发明提供了种在飞行器(1)中的将腹部整流罩(11)连接至飞行器(1)的机身(3)的接头组件(100)。腹部整流罩(11)具有连接至主腹部整流罩部段(13)的缝合角(12)，而机身(3)具有机身蒙皮(10)，其中，机身蒙皮(10)具有外部(10A)和内部(10B)。接头组件(100)包括具有在机身蒙皮(10)的固定区(14)处连接至机身蒙皮外部(10A)的凸缘(12A)的缝合角(12)，其中，固定区被凸缘(12A)叠置，凸缘(12A)连接至固定区。接头组件(100)还包括连接至机身蒙皮内部(10B)并与所述固定区(14)叠置的桁条(15)。接头组件(100)不易受振动的影响。本发明还