The invention relates to an aircraft propulsion assembly (10) comprising a hinge (20) for articulating a first panel and a second panel, the hinge (20) comprising a yoke (22) rigidly connected to the first panel (16) and a counter yoke (24) rigidly connected to the second panel (18), the counter yoke being received between two lugs (28) of the yoke (22), the yoke (22) and the counter yoke (24) are penetrated by a hinge pin (26), the hinge pin being movable between an extended position between the ears (28) of the yoke (26) and a retracted position outside the yoke (26), characterized in that the hinge comprises bayonet mounting means (30) inserted between the pin (26) and the yoke (22).
本发明涉及一种飞行器推进组件(10),该飞行器推进组件包括用于对第一面板和第二面板进行铰接的铰链(20),铰链(20)包括被刚性地连接到第一面板(16)的轭部(22)和被刚性地连接到第二面板(18)的反向轭部(24),反向轭部被接纳在轭部(22)的两个凸耳(28)之间,轭部(22)和反向轭部(24)被铰链销(26)穿过,铰链销能够在轭部(26)的耳部(28)之间的延伸位置和轭部(26)外部的缩回位置之间移动,其特征在于,铰链包括被插入在销(26)和轭部(22)之间的卡口安装装置(30)。
Hinge for articulating two panels of aircraft propulsion assembly
用于对飞行器推进组件的两个面板进行铰接的铰链
2022-12-16
Patent
Elektronische Ressource
Chinesisch
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