发明名称 |
Methods for operating gas turbine engines |
摘要 |
A method for operating an aircraft engine facilitates preventing ice accumulation on the aircraft engine. The method comprises coupling a semi-permeable membrane to the engine adjacent an outer surface of the engine, coupling a fluid reservoir to the aircraft engine in flow communication with the semi-permeable membrane, and supplying fluid from the fluid reservoir to the semi-permeable membrane to facilitate preventing ice accumulation on the aircraft engine outer surface.
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申请公布号 |
US7188464(B2) |
申请公布日期 |
2007.03.13 |
申请号 |
US20050072084 |
申请日期 |
2005.03.04 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
ACKERMAN JOHN FREDERICK;WAGNER WILLIAM KENT |
分类号 |
B64D15/08;F02C7/047;F01D25/02;F02K3/02 |
主分类号 |
B64D15/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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