A door assembly for mounting on an aircraft includes a rail mounted exteriorly to an outer skin of the aircraft, and a door movably coupled to the rail. The door assembly also includes a motor mountable in an interior of the aircraft, and a shaft extending through a sealed shaft port in the outer skin of the aircraft. The shaft couples the motor to the door, such that the door is movable between a first position and a second position along an outer moldline of the aircraft.
Externally mounted auxiliary door for an aircraft
14.02.2017
Patent
Elektronische Ressource
Englisch
Thermal management system and method for externally mounted electronics of aircraft
Europäisches Patentamt | 2024
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