The utility model discloses an eVTOL
airplane aileron structure, including
aileron framework and the
aileron skin that wraps in aileron framework outside.
Aileron framework includes the beam of exhibition, chord rib,
rudder angle and a plurality of suspension joint, and the beam of exhibition is composed of web and the edge strip of web upper and lower two sides.
Rudder angle is composed of connecting portion and ear piece, and the web inside surface of beam of exhibition is fixed with suspension joint, and a plurality of suspension joint symmetrical setting is in the two sides of
rudder angle, and the through -hole is set up on suspension joint. Chord rib includes two end ribs, a plurality of ordinary ribs and a plurality of
leading edge ribs, and the aileron
skin is composed of upper
skin, lower skin and three connecting band plate. In the utility model aileron structure, the main body structure of
rudder angle is connected in the inside of aileron, only the connecting ear piece of rudder angle is exposed in the air, and the wind area is very small, and the
aerodynamic drag is small. Meanwhile, the other side of the beam of exhibition is designed with reinforcing joint in the position corresponding with rudder angle, and the reinforcing joint and rudder angle are connected together by
fastener through the web of beam, and the connecting strength is high.