Friction stir welding joins body and cover components into smooth aerodynamic surfaces, cutting aircraft weight, drag, and fastener assembly work.
Deployable aerodynamic panels stabilize a towed refueling boom, enabling precise concurrent in-flight refueling of multiple aircraft.
A forward-deploying wing section increases drag to slow descent and stabilize attitude, then retracts to limit cruise energy use.
A retractable leading edge surface replaces multiple wing control surfaces to manage lift while saving wing space, weight, and complexity.
Blade-mounted flaps add drag to decelerate and stabilize a rotor, enabling smoother air vehicle transition from rotary to winged flight.
A mechanical limiter blocks spoiler deployment until external power is disconnected, creating a safer maintenance sequence with fewer parts.
A mechanical interlock blocks spoiler deployment when external power is connected.
Dynamic spoiler adjustment resolves the contradiction between maximum fineness and high drag during rolling, enhancing takeoff efficiency.
An asymmetric flap extension disrupts symmetrical vortex formation, reducing pressure fluctuations and resonance risks while maintaining braking force.
A segmented spoiler design articulates multiple segments about a transverse axis to adjust inclination angles independently.
Controller generates optimized drag device deployment cues on a vertical situation display to prevent unstable aircraft states during approach.
A wing assembly integrates a spoiler on the upper surface and a flap on the lower surface to increase control area.
A slotted aerofoil uses a blunt leading edge and mild stall ramp to maintain lift at high angles of attack.
A torque tube drives a gearing assembly to rotate an eccentric member, translating a linear actuator.
Segmented spoiler design uses a mechanical release to disengage the aft-section during backdrive events, reducing system weight and repair costs.
Monolithic seal locking mechanism reduces aircraft weight by merging door panel, locking members, and coil spring into a single integrated assembly.
A deployable lower wing spoiler causes flow separation to reduce lift on aft-loaded aircraft wings, alleviating root bending moments during turbulence.
Hinge members rotate a bell-mouth panel from a stowed position to deployed, reducing air separation at the nozzle opening during reverse thrust operations.