Invention Grant
US07690893B2 Leading edge cooling with microcircuit anti-coriolis device 有权
用微电路反科里奥利装置进行前沿冷却

Leading edge cooling with microcircuit anti-coriolis device
Abstract:
A turbine engine component, such as a high pressure turbine blade, has an airfoil portion having a pressure side, a suction side, and a leading edge. A cooling system is provided within the leading edge. The cooling system includes at least one peripheral leading edge cooling channel for creating anti-Coriolis forces in the leading edge of the airfoil portion.
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