发明名称 Ring-shaped flow channel section for a turbo engine
摘要 <p>The flow channel section (12) has a guide vane ring comprising a number of guide vanes (10) arranged adjacent to each other in circumferential direction. Shielding elements (22) are arranged on platforms (16) for creating the flow channel section while creating a gap, and impingement-cooling openings (24) are provided in the platform. A flow channel is delimited on the platform side by the shielding elements, where each of the shielding elements is provided between two airfoils (14). The airfoils project into the flow channel.</p>
申请公布号 EP2282014(A1) 申请公布日期 2011.02.09
申请号 EP20090008227 申请日期 2009.06.23
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 AHMAD, FATHI
分类号 F01D11/00;F01D9/04 主分类号 F01D11/00
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