STATOR VANE SEGMENT
卷宗概要
发明人
Dennis VON BRAUNECK; Franz-Josef ERTL; Kaspar WOLF
IPC 分类
CPC 分类
A stator vane segment for a gas turbine, in particular an aircraft engine, including a plurality of stator vanes, a radially outer shroud connecting the plurality of stator vanes, with stiffening elements integral to the shroud or integrated into the shroud being disposed on a radially outer side of the shroud. The stiffening elements form an extension of the stator vanes in the radial direction, and/or that a contour of the stiffening elements on the outer side of the shroud lies within an outer contour formed by a band around a projection of contours of the stator vane at a radially inner side onto the outer side of the shroud, a width of the band in the circumferential direction around the projection relating to no more than 20% of the thickness of the projection.
原文（中文）
A stator vane segment for a gas turbine, in particular an aircraft engine, including a plurality of stator vanes, a radially outer shroud connecting the plurality of stator vanes, with stiffening elements integral to the shroud or integrated into the shroud being disposed on a radially outer side of the shroud. The stiffening elements form an extension of the stator vanes in the radial direction, and/or that a contour of the stiffening elements on the outer side of the shroud lies within an outer contour formed by a band around a projection of contours of the stator vane at a radially inner side onto the outer side of the shroud, a width of the band in the circumferential direction around the projection relating to no more than 20% of the thickness of the projection.