发明名称 GAS TURBINE ROTARY BLADE WITH TIP INSERT
摘要 A rotary blade is provided that includes a root, an airfoil, and a tip insert. The airfoil is attached to the root, and has a suction side surface, a pressure side surface, a leading edge, a trailing edge, a tip, and a slot disposed within the tip. The slot extends in a chordwise direction between the leading edge and trailing edge. The tip insert has a base end and a rub end. The base end of the tip insert is disposed within the slot. The rub end of the tip insert extends radially outward from the airfoil tip.
申请公布号 EP2809885(A4) 申请公布日期 2015.11.04
申请号 EP20130743738 申请日期 2013.01.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HILDEBRAND, GREGORY, C.;HANSEN, JAMES O.;PARKOS, JR., JOSEPH;WEISSE, MICHAEL A.;HERTEL, CHRISTOPHER A.;MEYER, JESSE
分类号 F01D11/12;F01D5/20 主分类号 F01D11/12
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