发明名称 Transonic turbine airfoil arrangement
摘要 <p>A transonic turbine blade (60). Expansion waves (125) are generated by a lifting surface (66) on the blade (60). The expansion waves (125) extend downstream, through a shock (115) generated at the trailing edge (78) of an adjacent blade (60). The invention increases the strength of the shock (115), thereby attenuating the expansion waves (125) passing through the shock (125). One stratagem for increasing the shock (115) is to reduce the aerodynamic load of the trailing edge (78) generating the shock (115).</p>
申请公布号 EP1300547(B1) 申请公布日期 2013.04.10
申请号 EP20020256986 申请日期 2002.10.04
申请人 GENERAL ELECTRIC COMPANY 发明人 KUHNE, CRAIG MILLER
分类号 F01D5/14;F01D1/04 主分类号 F01D5/14
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