发明名称 |
Turbine rotor blade with serpentine cooling |
摘要 |
A turbine rotor blade has a number of serpentine flow cooling circuits to provide cooling to forward and aft sections of the airfoil and to upper span and lower span sections of the airfoil in order to provide specific cooling to directed sections of the airfoil. A common cooling air supply channel extends the entire spanwise length of the airfoil and supplies cooling air to each of the serpentine flow cooling circuits. |
申请公布号 |
US8628298(B1) |
申请公布日期 |
2014.01.14 |
申请号 |
US201113189075 |
申请日期 |
2011.07.22 |
申请人 |
LIANG GEORGE;FLORIDA TURBINE TECHNOLOGIES, INC. |
发明人 |
LIANG GEORGE |
分类号 |
F01D5/08 |
主分类号 |
F01D5/08 |
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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