A two-part aircraft emergency kit storage assembly simplifies installation and enables precise rail alignment without reaching into the housing.
Overlapping upper and lower forearm supports let adjacent passengers share one armrest, easing elbow conflict without increasing seat pitch.
A hybrid battery and engine-generator reserve system adjusts aircraft flight attitude by reserve state, cutting battery reserve weight while preserving backup power.
A severable wing fixing portion lets the wing detach and absorb landing impact, reducing fuselage deformation and passenger risk.
Impact-triggered severing of the wing attachment lets wings separate during emergency landing to reduce fuselage deformation and load.
Flight parameter checks and timed prompts detect pilot incapacitation without extra hardware, then trigger an emergency protocol.
A blower-inflated vision enclosure clears smoke around critical sightlines while a compact housing expands only during deployment.
A fuse member lets the trailing arm rotate beyond its normal range under overload, enabling compact gear collapse without cabin or fuel tank intrusion.
Inflatable enclosures filter smoke to maintain pilot visibility, resolving the contradiction between reliable visual access and device complexity.
A drone featuring ducted rotors and an expandable landing mechanism for controlled descent during rotor failure.
An articulated push rod mechanism moves transverse leaves in cylindrical fuselages, maximizing travel distance while maintaining structural rigidity.
Integrating a radio antenna within the protective housing of an aircraft signaling light enables dual visual signaling and radio communication functions.
Threaded shaft mechanism deploys wing-like support cables to slow descent speed during rotor failure.
Airbag buffer deploys when battery is low or near objects, absorbing impact energy to protect the drone and ground property from crash damage.
Sensors compare cable tension and position against thresholds to trigger automatic homing, preventing component wear from system vibrations.
A deployable ramp and guide panel system extends from an overhead crew rest hatch to the main cabin floor.
Segmented hook mount and removable assembly jettison payloads via sacrificial connectors, preventing fuel tank puncture during crashes.