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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0305706 (1981-09-25) |
우선권정보 | GB-0031265 (1980-09-26) |
발명자 / 주소 |
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출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 46 인용 특허 : 3 |
A fully aerobatic oil system for an aircraft gas turbine engine includes two re-circulatory oil systems the pumps for which have inlets 19 and 31a disposed at locations in the engine such that when one inlet is starved of oil, due to the aircraft attitude changing, oil will be supplied to the other
An oil supply system for use with an engine having engine bearings and subject to orientation in first and second engine positions, said oil system comprising: an oil tank configured to receive a quantity of oil; pump means, having an inlet coupled to said oil tank and an outlet, for pumping oil fro
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