Invention Grant
US08366395B1 Turbine blade with cooling 有权
涡轮叶片冷却

Turbine blade with cooling
Abstract:
A turbine blade with individual metering and impingement cooling modules spaced around four zones of the airfoil designed to provide local blade cooling based on the heat load as well as tailoring the local pressure distribution to optimize film cooling. Each metering and impingement module is fluidly separated from others.
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