|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 6|
A system providing aft fuselage flight controls on forward lifting elevator aircraft. My invention relates to aft fuselage controls on a forward lifting elevator aircraft, with the main lifting wing placed aft on the fuselage, and equipped with trailing edge flaps. My embodiment includes a means for controlling a nose down pitching condition produced by lowering trailing edge flaps, using aft vertical flaps 2. The design of the aft vertical flaps 2 produces a tail-down moment to counter the main aft wing trailing edge flap action. In addition, the aft ve...
1. An aft fuselage flight control system attachment with the aft end of a fuselage of a forward lifting elevator aircraft, the aft fuselage flight control system comprising: a. at least two aft vertical flaps with each aft vertical flap including a forward edge, and an aft trailing edge; b. a means for hingedly connecting the forward edge of each of the aft vertical flaps with the aft end of the fuselage of an aircraft such that in the direction of the rear of the aircraft, the forward edge forms an acute angle with the aircraft centerline, and such ...