发明名称 |
Titanium sheath and airfoil assembly |
摘要 |
An airfoil assembly (20) includes an airfoil body (22) extending between a leading edge (24), a trailing edge (26), a suction side (28), and a pressure side (30). A first sheath (34) having an outer side (36) and an inner side (38) forms a cavity (40) for receiving at least a portion of the airfoil body (20) and is bonded on the inner side (38) to the leading edge (24) of the airfoil body (22). The first sheath (34) is formed of a titanium-based metallic material. A second sheath (60) is bonded to the outer side (36) of the first sheath (34). |
申请公布号 |
EP2281746(A3) |
申请公布日期 |
2013.04.17 |
申请号 |
EP20100251261 |
申请日期 |
2010.07.14 |
申请人 |
HAMILTON SUNDSTRAND CORPORATION |
发明人 |
HUTH, BRIAN P.;CARVALHO, PAUL A. |
分类号 |
B64C11/20 |
主分类号 |
B64C11/20 |
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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