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 |