发明名称 Composite fan blade dovetail root
摘要 A composite fan blade (32) having an airfoil (36) with a leading edge (38) and a trailing edge (40) and a dovetail root (44) includes a first pressure face (50) and second pressure face (50), a lower horizontal face (54) connecting the pressure faces at the bottom of the dovetail and a first and a second dovetail runout fillet (52) connecting the pressure faces to the airfoil. The pressure faces are each angled outward at about 65 degrees to about 75 degrees from horizontal.
申请公布号 EP2372096(B1) 申请公布日期 2016.09.28
申请号 EP20110250280 申请日期 2011.03.10
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KLINETOB, CARL BRIAN;REINHARDT, GREGORY E.;HUTH, BRIAN P.
分类号 F01D5/28;F01D5/02;F01D5/30 主分类号 F01D5/28
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