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.
CHARNIERE D'ARTICULATION ENTRE DEUX PANNEAUX D'UN ENSEMBLE PROPULSIF D'AERONEF
HINGE FOR ARTICULATING TWO PANELS OF AN AIRCRAFT PROPULSION ASSEMBLY
SCHARNIER ZUR GELENKIGEN VERBINDUNG ZWEIER PLATTEN EINER FLUGZEUGANTRIEBSANORDNUNG
15.02.2023
Patent
Elektronische Ressource
Französisch
CHARNIERE D'ARTICULATION ENTRE DEUX PANNEAUX D'UN ENSEMBLE PROPULSIF D'AERONEF
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