|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/124 ; 244/55 ; 244/56|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 2|
A VTOL airplane having a stub wing integrating a powerplant to either side of an airplane fuselage to rotatably relate the powerplant means to the airplane fuselage for uniform rotation, allow for flexible interconnecting design and lower the use of gravitational and aerodynamic moments in assistance of rotation of this powerplant/stub wing assembly.
An airplane and powerplant combination comprising: an airplane fuselage; a stub wing mounted through said fuselage so as to be movable relative thereto; fan jet means mounted to said stub wing at least one on either side of said fuselage; an airplane wing joined to said fuselage behind said stub wing with said fan jet means extending from ahead of said stub wing, under the airplane wing to a position adjacent the trailing edge of the airplane wing; a pivot arm means fixed to said stub wing; a means to connect said pivot arm means to said fuselage so as t...