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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0069419 (1987-07-02) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 28 인용 특허 : 4 |
A unique anti-icing management system for a gas turbine engine is disclosed according to which, at all times, only the required amount of heat is applied to inlet surfaces of the engine to prevent the formation of ice. Heated air is bled from the compressor discharge for this purpose and the amount
In a gas turbine engine having inlet surfaces subject to the formation of ice thereon and including a source of heated air, air duct means adjacent to said surfaces for receiving the heated air to prevent the formation of ice thereon, and passage means enabling the flow of heated air from said sourc
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