发明名称 Gas turbine blade has leading edge with radial smooth-outline cross section
摘要 <p>The blade has a compression-side wall (2), an induction-side wall (4) and a leading edge (6) with a cavity (5) for coolant. The leading edge has a smooth outline with curved and straight parts (10, 11, 12, 13) to provide a uniform flow of coolant about the leading edge and inside the apex cavity (9). The outlet channels (14, 16) are at an angle to the radial direction.</p>
申请公布号 CH695703(A5) 申请公布日期 2006.07.31
申请号 CH20020000056 申请日期 2002.01.15
申请人 ALSTOM TECHNOLOGY LTD 发明人 LIANG GEORGE
分类号 F01D5/20;F01D5/18 主分类号 F01D5/20
代理机构 代理人
主权项
地址