发明名称 Turbine blade with a hot gas suporting platform and a mechanical load suporting platform
摘要 <p>A hot-gas platform (12) transversely extends to a vane axis (4). The hot-gas platform and a load platform (14) are integrally formed on a profiled vane aerofoil (2) that extends along the vane axis. The vane aerofoil exclusively forms the mechanical connection between the load platform and hot-gas platform.</p>
申请公布号 EP1329593(B1) 申请公布日期 2005.03.23
申请号 EP20020001267 申请日期 2002.01.17
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 TIEMANN, PETER
分类号 F01D9/02;F01D5/14;F01D9/04;(IPC1-7):F01D9/02 主分类号 F01D9/02
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