发明名称 |
Compound tip notched blade |
摘要 |
A gas turbine engine blade includes pressure and suction sidewalls extending between leading and trailing edges and from root to tip. The pressure sidewall includes an inclined tip rib offset therein by a ramp defining a tip notch having compound inclinations.
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申请公布号 |
US6790005(B2) |
申请公布日期 |
2004.09.14 |
申请号 |
US20020334091 |
申请日期 |
2002.12.30 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LEE CHING-PANG;CHERRY DAVID GLENN;PRAKASH CHANDER;WADIA ASPI RUSTOM |
分类号 |
F01D5/18;F01D5/20;(IPC1-7):F01D5/16 |
主分类号 |
F01D5/18 |
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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