发明名称 |
Turbine blade with showerhead film cooling holes |
摘要 |
A turbine rotor blade with a showerhead arrangement of film cooling air for cooling the leading edge of the airfoil, where the film cooling holes each includes a tear drop shaped opening that extends in a radial direction of the airfoil from the film hole breakout and functions to spread out the film layer of cooling air that is ejected from the holes so that a hot streak between holes along the pressure side row and the suction side row of film holes does not occur. The tear drop shaped opening have a shallow depth and include a divider wall extend down the middle to divide the opening.
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申请公布号 |
US8087893(B1) |
申请公布日期 |
2012.01.03 |
申请号 |
US20090418459 |
申请日期 |
2009.04.03 |
申请人 |
LIANG GEORGE;FLORIDA TURBINE TECHNOLOGIES, INC. |
发明人 |
LIANG GEORGE |
分类号 |
B63H1/14;B63H7/00;B64C11/00;F01D5/08;F01D5/14;F01D5/18;F01D5/28;F03D11/02;F04D29/58 |
主分类号 |
B63H1/14 |
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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