发明名称 |
Method and apparatus for reducing distortion losses induced to gas turbine engine airflow |
摘要 |
A vane assembly for a gas turbine engine includes at least one vane that includes a first body, a second body, and a passageway. The first body includes a first sidewall and a second sidewall that are connected at a leading edge and a trailing edge. The passageway extends between the second body and the first body leading edge.
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申请公布号 |
US6715983(B2) |
申请公布日期 |
2004.04.06 |
申请号 |
US20010965351 |
申请日期 |
2001.09.27 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
KOSHOFFER JOHN MICHAEL;DRAKE KEVIN ROBERT |
分类号 |
F01D25/30;F01D5/14;F01D9/04;F02C7/00;F02K3/10;(IPC1-7):F01D17/16 |
主分类号 |
F01D25/30 |
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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