发明名称 |
Turbine stage and corresponding turbine blade having a scalloped platform |
摘要 |
A turbine stage includes a row of airfoils (14) joined to corresponding platforms (16) to define flow passages (36) therebetween. Each airfoil includes opposite pressure (20) and suction (22) sides and extends in chord between opposite leading (24) and trailing (26) edges. At least some of the platforms have a scalloped flow surface including a bulge (38) adjoining the pressure side and a bowl (40) adjoining the suction side, aft of the leading edge, of the respective airfoils. The bulge is configured having a maximum height located within its respective flow passage, and wherein the bulge decreases in height in a forward and aft direction and decreases in height laterally toward the pressure side of the airfoil and toward the bowl adjoining the suction side of a next adjacent airfoil. A corresponding turbine blade is also provided. |
申请公布号 |
EP2642075(A3) |
申请公布日期 |
2014.03.19 |
申请号 |
EP20130160022 |
申请日期 |
2013.03.19 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BARR, BRIAN CHANDLER;KEITH, BRIAN DAVID;KAJFASZ, GREGORY JOHN |
分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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