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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) |
|
출원번호 | US-0119954 (1987-11-13) |
발명자 / 주소 |
|
인용정보 | 피인용 횟수 : 4 인용 특허 : 1 |
An airplane construction is described in which the flight characteristics of the airplane, are radically changed from hypersonic capable to short take off and landing (STOL) capable by the approximate ninety degree (90) rotation of a new component of the airplane, referred to as a body spar, which f
An airplane comprising a fuselage having a nose portion a tail portion and an intermediate portion, control surfaces mounted on said tail portion, a fixed wing connected to said fuselage adjacent said tail portion and a second wing pivotally mounted to said intermediate portion, said second wing hav
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