发明名称 |
Turbine airfoil including diffusing trailing edge pedestals |
摘要 |
A turbine airfoil having a cut-back trailing edge and a plurality of diffusing flow dividers upstream of the cut-back trailing edge is disclosed. Various construction details are developed which provide ejection of a diffusing film of cooling fluid over a cut-back trailing edge. In one particular embodiment, a turbine airfoil includes a plurality of radially spaced flow dividers extending between a pressure wall and a suction wall. Each flow divider includes a rounded leading edge, a pair of parallel sidewalls downstream of the leading edge, and a pair of converging sidewalls downstream of the parallel sidewalls. Adjacent sidewalls of adjacent flow dividers form flow channels having a constant area channel and a diffusing section. The diffusing section includes a covered portion upstream of the cut-back trailing edge and an uncovered portion extending over the cut-back trailing edge.
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申请公布号 |
US5368441(A) |
申请公布日期 |
1994.11.29 |
申请号 |
US19920980817 |
申请日期 |
1992.11.24 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SYLVESTRO, JOSEPH A.;LINASK, INDRIK;BEABOUT, BRIAN K. |
分类号 |
F01D5/18;(IPC1-7):F01D5/18 |
主分类号 |
F01D5/18 |
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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