|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/012.3 ; 244/012.1 ; 244/023B|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 115 인용 특허 : 3|
A semiautonomously directed, autonomously controlled, gyroscopically stabilized, horizontal or vertical take off and landing (HOVTOL) flying apparatus employing two vertical lift devices equally and longitudinally spaced from the center of gravity of the apparatus; continuously integrated with a drive train apparatus, optional single or multiple power means; congruously connected thereto horizontal thrust devices. Integral to the vertical lift devices; pitch axis control devices situated at the exhaust orifices therein to vector said devices exhaust slip...
[ It is claimed:] [1.] An aircraft comprising: a body having a front end, a rear end, two opposite facing sides, a top end, and a bottom end, a longitudinal axis extending between said front and rear ends, front and rear openings extending through said body transverse to said longitudinal axis and between said top and bottom ends, front and rear ducts defining said front and rear openings respectively with each of said ducts having top bottom ends, front and rear propeller means located in said front and rear openings for rotation about the front and rea...