发明名称 Component and turbo engine with such a component
摘要 The component has a base (11) that is arranged with high temperature coating portion (2). The base is provided with structural element (1) which is connected with high temperature coating portion. The cross section of structural element is provided with three different widths (w1,w2,w3). A base width is formed at lower end of structural element. The overlying center portion width is set three times larger than base width and overlying tip portion width is set two times larger than base width. An independent claim is included for a turbomachine.
申请公布号 EP2589872(A3) 申请公布日期 2016.12.14
申请号 EP20120190796 申请日期 2012.10.31
申请人 Rolls-Royce Deutschland Ltd & Co KG;Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. 发明人 Roth-Fagaraseanu, Dan;Wunderlich, Thomas;Cadoret, Yannick;Brückner, Frank;Riede, Mirko
分类号 F23R3/00;B32B3/12;B32B3/26;F01D9/02;F02C7/00;F23M5/04 主分类号 F23R3/00
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