发明名称 |
Compressor blade for a gas turbine engine |
摘要 |
A blade (11) as a main body of a rotor blade has a suction side (11a) made convex and a pressure side (11b) made concave so as to have an aerofoil profile. A squealer tip (17) having a back face (17a) continuous to the suction side and a front face (17b) matching with a center plane of the blade (11) is formed as a distal end of the blade. The front face (17b) is coated with a hard coating. |
申请公布号 |
EP1930547(B1) |
申请公布日期 |
2016.03.30 |
申请号 |
EP20070254540 |
申请日期 |
2007.11.22 |
申请人 |
IHI CORPORATION |
发明人 |
OCHIAI, HIROYUKI;FURUKAWA, TAKASHI;WATANABE, MITSUTOSHI;FUJIMURA, TETSUJI |
分类号 |
F01D5/20;F01D11/12 |
主分类号 |
F01D5/20 |
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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