The present disclosure provides a landing gear assembly for reducing drag on an aircraft. Landing gear assembly may include a proximal joint, a movable leg extending from the proximal joint, and a base attached to a distal end of the leg. The base may be configured to support the electric aircraft on an environmental surface. The landing gear assembly may transition between a deployed landing position and a collapsed flight position when landing and taking off to provide optimal aerodynamics of the aircraft.
Landing gear assembly for reducing drag on an aircraft
2022-10-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |