发明名称 Turbomachine turbine shroud sector
摘要 <p>The sector has a wall bounding an aerodynamic flowpath in which gases flow from an upstream region toward a downstream region, and a multiperforated plate (2) is situated on an opposite side of the aerodynamic flowpath with respect to the wall. The multiperforated plate comprises a bottom and side walls, where the distance between the wall and the bottom of the plate defining a gap is progressive in an axial direction. A value of the gap situated at the upstream region is below the value situated at the downstream region.</p>
申请公布号 EP1918526(A1) 申请公布日期 2008.05.07
申请号 EP20070075862 申请日期 2007.10.05
申请人 SNECMA 发明人 BOTREL, ERWAN;DORIN, CLAIRE D.
分类号 F01D11/24 主分类号 F01D11/24
代理机构 代理人
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