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
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