| 摘要 |
<p>The invention relates to a stator vane for a gas turbine engine, comprising a leading edge and a trailing edge and a vane platform extending at least between the leading edge and the trailing edge. The vane platform has first and second side walls extending substantially in the radial and axial directions of the gas turbine engine, whereby the first side wall, at least in the area of the trailing edge, is provided with a groove extending in the longitudinal direction of the vane platform for receiving a sealing plate, whereby the first side wall of the vane platform in the area of the trailing edge has a recess extending from the groove.</p> |
