A nacelle for an engine has outer and inner cowl doors that are independently rotatable about offset hinge lines. A connection device is provided for selectively connecting the outer and inner cowl doors so as to cause them to open simultaneously. The inner cowl door is arranged to rotate by a greater angle than the outer cowl door so as to improve access to the engine for maintenance purposes.
NACELLE WITH HINGED COWL DOORS ENABLING ACCESS TO THE ENGINE
TRIEBWERKSGONDEL MIT VERKLEIDUNGSTÜREN MIT SCHARNIEREN FÜR DEN ZUGANG ZUM MOTOR
NACELLE DOTÉE DE PORTES DE CAPOT ARTICULÉES PERMETTANT D'ACCÉDER AU MOTEUR
2018-12-05
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
NACELLE WITH HINGED COWL DOORS ENABLING ACCESS TO THE ENGINE
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