发明名称 |
METHOD FOR OPERATING AIRCRAFT ENGINE AND ICE ACCUMULATION PREVENTING SYSTEM |
摘要 |
PURPOSE: A method for operating an aircraft engine and an ice accumulation preventing system are provided to secure high reliability for easily preventing ice accumulation along an exposed surface without the loss of engine performance. CONSTITUTION: A method for operating an aircraft engine to facilitate preventing ice accumulation on the aircraft engine comprises steps for coupling a membrane(66) to the engine adjacent to an outer surface(68) of the engine; coupling a fluid reservoir(62) to the aircraft engine in flow communication with the membrane; and supplying fluid from the fluid reservoir to the membrane to facilitate preventing ice accumulation on the outer surface of the aircraft engine. In the step for coupling the membrane to the engine has a step for coupling a distributor(80) to the engine to form a gap(82) between the membrane and the distributor.
|
申请公布号 |
KR20040004134(A) |
申请公布日期 |
2004.01.13 |
申请号 |
KR20030044628 |
申请日期 |
2003.07.02 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
ACKERMAN JOHN FREDERICK;WAGNER WILLIAM KENT |
分类号 |
F02C7/047;F01D25/02;F02K3/02;(IPC1-7):F02C7/047 |
主分类号 |
F02C7/047 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|