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Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer

机译:用于凸点覆盖的冷却表面的增强传热表面以及增强传热的方法

摘要

An annular turbine shroud separates a hot gas path from a cooling plenum containing a cooling medium. Bumps are cast in the surface on the cooling side of the shroud. A surface coating overlies the cooling side surface of the shroud, including the bumps, and contains cooling enhancement material. The surface area ratio of the cooling side of the shroud with the bumps and coating is in excess of a surface area ratio of the cooling side surface with bumps without the coating to afford increased heat transfer across the element relative to the heat transfer across the element without the coating.
机译:环形涡轮机罩将热气路径与包含冷却介质的冷却室隔开。在护罩冷却侧的表面上铸有凹凸。表面涂层覆盖护罩的冷却侧表面(包括凸块),并包含冷却增强材料。带有凸起和涂层的护罩的冷却侧的表面积比超过了没有涂层的带有凸起的冷却侧表面的表面积比,从而提供了相对于整个元件的传热增加的整个元件的传热。没有涂层。

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