|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/225 ; 244/088 ; 244/090R|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 8 인용 특허 : 0|
The present invention discloses an aircraft control system having simultaneously controllable rear aileron/elevators and a retractable body flap for longitudinal stabilization. The aileron/elevators are airfoils comprising the complete horizontal tail plane. Control arms for the rear aileron/elevators are capable of pivotal movement about the longitudinal axis of the aircraft while the aileron/elevators are secured to the control arms by axles pivotal about the lateral axis of the airfoil, for directional control. With two degrees of rotational movement,...
[ I claim:] [1.] An aircraft control system comprising:a pair of rear aileron/elevators simultaneously operable from a neutral angle of attack to a positive or negative angle of attack, both in the same or in opposite directions, and including a control arm associated with each aileron/elevator for providing simultaneous pivotal movement of the aileron/elevators about the longitudinal axis of the aircraft; anda longitudinal stabilizer means comprising a body flap hingedly mounted at a leading edge to an upper surface of the aircraft proximate the rear ai...