发明名称 |
AIRFOIL AND METHOD FOR PROTECTING AIRFOIL LEADING EDGE |
摘要 |
An airfoil is disclosed having a concave pressure side (70) and a convex suction side (72) defining a chord length, and a leading edge (74) and a trailing ed ge (76). A leading edge protective strip (80) is adhered by a bond layer (82) to and protectively covers the leading edge (74) and respective predetermined portions of the pressure side (70) and suction side (72) of the airfoil body from the leading edge (74) downstream towards the trailing edge (76). The predetermined portion of the suction sid e (72) covered by the leading edge protective strip (80) is less than the predetermined portion of the pressure side (70) covered by the leading edge protective strip (80). |
申请公布号 |
CA2630951(A1) |
申请公布日期 |
2009.01.23 |
申请号 |
CA20082630951 |
申请日期 |
2008.05.08 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SCHNEIDER, MICHAEL HARVEY;BAUR, ROBERT GEORGE;SCHILLING, JAN CHRISTOPHER |
分类号 |
F01D5/14;F01D5/28 |
主分类号 |
F01D5/14 |
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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