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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0134602 (1987-12-14) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 5 인용 특허 : 0 |
An aircraft has two vectorable front nozzles each mounted in a bearing located within the fuselage near an adjacent wing. Each nozzle is rotatable from a first position in which exhaust air is directed downwards to a second position in which the exhaust air is directed rearwards. In the first positi
An aircraft comprising: structure including a fuselage and wings, a gas turbine engine located in the fuselage, a stowable exhaust nozzle mounted in a bearing and protruding from the bearing through a cut-out section of the fuselage for rotation from a first position in which exhaust gas issuing fro
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