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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0332319 (1981-12-18) |
발명자 / 주소 |
|
인용정보 | 피인용 횟수 : 10 인용 특허 : 0 |
An aircraft containing aerodynamic and gyroscopic stability that has a high angle of take-off and landing capabilities, with high speed horizontal powered flight, but is also able to sustain power-off flight with auto-rotation of its multiple extending airfoils. The fuselage has the shape of an inve
A fuselage body adapted for powered flight and sustained power-off flight with auto-rotation means, said fuselage body having the general shape of an aerodynamic inverted saucer, in which a continuous circular track is mounted at the periphery of said fuselage body, and mounted to and riding on bear
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