An aircraft propulsion assembly has a hinge for articulating a first and a second of its panels. The hinge includes a yoke rigidly connected to the first panel and a counter-yoke rigidly connected to the second panel, which is received between two lugs of the yoke. The yoke and the counter-yoke are passed through by a hinge pin that is movable between an extended position between the lugs of the yoke and a retracted position outside the yoke. The hinge further includes bayonet mounting means interposed between the pin and the yoke.
Hinge for articulating two panels of an aircraft propulsion assembly
2024-12-24
Patent
Electronic Resource
English
Hinge for articulating two panels of aircraft propulsion assembly
European Patent Office | 2022
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