|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/036; 244/102SS; 244/119; 244/137.1|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 4|
A multi-wing, airfoil fuselage aircraft that is capable of flying in a ground-effect mode includes a main airfoil fuselage wing, a fin that extends vertically from this wing, a pivot mount that is affixed to the fin, an auxiliary wing that connects to the pivot mount so as to allow its angle of attack to be adjusted and changed during different flight conditions, a main landing gear, an adjustable-length, stabilizing landing gear, assorted control surfaces that are movably affixed to the auxiliary wing and fin, and a ground-effect control system that is ...
1. A multi-wing, airfoil fuselage aircraft capable of flying in a ground-effect mode, said aircraft comprising: a main, airfoil fuselage wing having a centerline and top, bottom, front, rear and wing tip surfaces and a specified span length between said wing tips and a specified chord length between said front and rear surfaces, and said top and bottom surfaces configured so as to yield a camber for said main airfoil fuselage wing, that is selected from the group consisting of symmetrical and reverse chamber,a fin that connects and extends vertically fro...