发明名称 Rotor blade for gas turbine stage, has whirling effect producing structures, which are formed as elevated sections on inner wall surfaces of coolant duct and enclose narrow gap, where duct is defined by side walls of blade sheet
摘要 <p>The blade has a sheet with a front edge at which two side walls (7, 8), defining a coolant duct, are connected. The side walls converge in a radially extending end region and enclose a gap between two end regions. The gap serves as a flow outlet (10) for a coolant flowing via the duct. Whirling effect producing structures are formed as elevated sections (16, 17) on inner wall surfaces of the duct and enclose a narrow gap (15).</p>
申请公布号 DE102005012803(A1) 申请公布日期 2006.09.21
申请号 DE20051012803 申请日期 2005.03.19
申请人 ALSTOM TECHNOLOGY LTD. 发明人 BATTESON, MARTIN;BENEDETTI, BRUNO;HAEHNLE, HARTMUT
分类号 F01D5/18;F15D1/00 主分类号 F01D5/18
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