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
2017-02-14
Patent
Electronic Resource
English
Thermal management system and method for externally mounted electronics of aircraft
European Patent Office | 2024
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