|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/45R ; 244/36|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 34 인용 특허 : 2|
Fore mounted aft swept and aft mounted forward swept wings extend from either side of a lifting body fuselage. Each lateral pair of the wings is joined at the tops by a wing tip vortex translating device to induce translation of the tip generated vortices along the trailing edge of the aft wings. End plates extend rearwardly from the maximum chord thickness of the fuselage to increase the effective lift of the fuselage. An elevator, mounted intermediate the rear top of the end plates, provides pitch control and structurally augments the wing root and fus...
A multiwing lifting body aircraft, said aircraft comprising in combination: a. a lifting body fuselage for generating lift; b. end plates disposed along lateral sides of said fuselage for increasing the lift generating capability of said fuselage; c. a forwardly mounted dihedralled rearwardly swept wing for generating lift, said rearwardly swept wing being secured to the lower part of said fuselage; d. a rearwardly mounted anhedralled forwardly swept wing for generating lift, said forwardly swept wing being secured to the upper part of said end plates; e...