发明名称 |
Methods and apparatus 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 (66) to the engine adjacent an outer surface (68) of the engine, coupling a fluid reservoir (62) 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. <IMAGE> |
申请公布号 |
ZA200304719(B) |
申请公布日期 |
2004.04.30 |
申请号 |
ZA20030004719 |
申请日期 |
2003.06.18 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
JOHN FREDERICK ACKERMAN;WILLIAM KENT WAGNER |
分类号 |
F02C7/047;F01D25/02;F02K3/02 |
主分类号 |
F02C7/047 |
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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