发明名称 TURBINE AIRFOIL TIP SHELF AND SQUEALER POCKET COOLING
摘要 <p>An airfoil comprises leading and trailing edges with pressure and suction surfaces defining a chord length therebetween. The pressure and suction surfaces extend from a root section of the airfoil to a tip section. A tip shelf is formed along the tip section between the pressure surface and a tip shelf wall spaced between the pressure surface and the suction surface. A squealer pocket is formed along the tip section between the tip shelf wall and a squealer tip wall extending from the suction surface. The tip shelf extends from within 10% of the cord length measured from the leading edge to within 10% of the chord length measured from the trailing edge. The squealer pocket extends from within 10% of the chord length measured from the leading edge to terminate between 10% and 25% of the chord length measured from the trailing edge.</p>
申请公布号 WO2013158194(A1) 申请公布日期 2013.10.24
申请号 WO2013US23847 申请日期 2013.01.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MONGILLO, DOMINIC J.;GAUTSCHI, STEVEN;QUACH, SAN
分类号 F01D5/18 主分类号 F01D5/18
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