发明名称 TURBINE BLADE AND ITS USE IN A GAS TURBINE SYSTEM
摘要 <p>A turbine blade (1) has a wall structure (2) around which a hot gas (18) can flow. The wall structure (2) has a cooling area (5) through which a cooling fluid (6) flows between an outer wall (3) and an inner wall (4). Each cooling area (5) has heat transfer elements (7) around which the cooling fluid (6) can flow. The heat transfer elements (7) are successively arranged in a main flow direction (12) and are thermoconductively connected to the outer wall (3).</p>
申请公布号 EP0954680(B1) 申请公布日期 2002.02.06
申请号 EP19970949947 申请日期 1997.11.18
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 HAENDLER, MICHAEL;SCHEURLEN, MICHAEL
分类号 F01D5/18;(IPC1-7):F01D5/18 主分类号 F01D5/18
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