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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0801546 (1977-05-31) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 13 인용 특허 : 1 |
An aircraft engine installation is disclosed wherein a gas turbine engine is supported within the interior of a tubular cowling that is affixed to the aircraft and all other components of the engine installation such as an air inlet and exhaust system structurally depend from the cowling rather than
In a jet propelled aircraft wherein ambient air is supplied to a gas turbine engine by air inlet means extending forwardly of said gas turbine engine, said gas turbine engine supplying exhaust gasses to exhaust system means extending rearwardly of said gas turbine engine for discharging said engine
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