发明授权
US06379528B1 Electrochemical machining process for forming surface roughness elements on a gas turbine shroud 有权
用于在燃气轮机罩上形成表面粗糙元件的电化学加工工艺

Electrochemical machining process for forming surface roughness elements on a gas turbine shroud
摘要:
The back side recessed cooling surface of a shroud defining in part the hot gas path of a turbine is electrochemically machined to provide surface roughness elements and spaces therebetween to increase the heat transfer coefficient. To accomplish this, an electrode with insulating dielectric portions and non-insulating portions is disposed in opposition to the cooling surface. By passing an electrolyte between the cooling surface and electrode and applying an electrical current between the electrode and a shroud, roughness elements and spaces therebetween are formed in the cooling surface in opposition to the insulating and non-insulating portions of the electrode, hence increasing the surface area and heat transfer coefficient of the shroud.
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