发明授权
US08360726B1 Turbine blade with chordwise cooling channels 有权
涡轮叶片带有和弦冷却通道

Turbine blade with chordwise cooling channels
摘要:
A turbine rotor blade with near wall cooling that provides full coverage film cooling for the leading and trailing edges. A first layer of chordwise extending cooling channels are formed on a spar, and a second layer of chordwise extending cooling channels are formed over the first layer to provide near wall cooling. Open ends of the two layers of channels on both pressure and suction side walls of the blade open into a leading edge slot and the trailing edge wall sides to discharge film cooling air.
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