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Weave Design Enhances Heat Transfer and Reduces Thermal Stresses in Gas Turbines
总结
A Purdue University graduate student has developed an improved cooling paradigm for the trailing edge of turbine airfoils. This weave design combines several geometrical concepts to efficiently utilize the internal flow to cool the trailing edge material effectively and uniformly. When compared to three advanced cooling strategies, the weave design provided more efficient and uniform cooling and caused less unnecessary pressure loss.
技术优势
More efficient coolingMore uniform, solid temperature Requires less coolant mass flow
技术应用
Gas Turbine Industry
详细技术说明
Purdue Aeronautics and Astronautics
国家
United States
申请号码
None
国家/地区
美国
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