发明名称 ROTOR BLADE WITH L-SHAPED FEATHER SEAL
摘要 A turbine engine assembly arranged relative to an axis includes a rotor blade and a feather seal with an L-shaped geometry. The rotor blade includes an airfoil and a base. The airfoil extends axially between an upstream leading edge and a downstream trailing edge, and radially out from the base. The base includes a neck and a pocket. The neck extends axially to a downstream surface. The pocket extends laterally into the neck. The feather seal extends laterally into the pocket, and includes a down stream leg that extends substantially along the downstream surface.
申请公布号 US2016061048(A1) 申请公布日期 2016.03.03
申请号 US201414779841 申请日期 2014.03.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Corcoran Christopher;Cherolis Anthony P.
分类号 F01D11/00;F01D5/14;F01D15/12;F01D5/02 主分类号 F01D11/00
代理机构 代理人
主权项 1. A turbine engine assembly arranged relative to an axis, the assembly comprising: a rotor blade including an airfoil and a base; the airfoil extending axially between an upstream leading edge and a downstream trailing edge, and radially out from the base; andthe base including a neck and a pocket, the neck extending axially to a downstream surface, and the pocket extending laterally into the neck; and a feather seal with an L-shaped geometry, the feather seal extending laterally into the pocket, and including a downstream leg that extends substantially along the downstream surface.
地址 Hartford CT US