发明名称 COVERS FOR CAVITIES IN AIRCRAFT FAN BLADES
摘要 Hollow fan blades for gas turbine engines are disclosed. The hollow fan blades include a body having a convex side and a concave side wherein the convex side has a cavity formed therein. The cavity is covered by two covers including an inner cover that may be adhered to the body of the fan blade assembly and an outer cover that may be adhered to the inner cover and/or the body of the fan blade assembly. The covers may be made of titanium, more than two covers may be employed and more than one cavity may be employed.
申请公布号 EP2964892(A4) 申请公布日期 2016.11.09
申请号 EP20130877424 申请日期 2013.11.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 COSBY, JAMES;WEISSE, MICHAEL, A.;HUI, KWAN
分类号 F01D5/18;F04D29/38 主分类号 F01D5/18
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