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http://dx.doi.org/10.5139/JKSAS.2011.39.10.966

Research Activities of Transpiration Cooling for High-Performance Flight Engines  

Hwang, Ki-Young (국방과학연구소 1본부 5부)
Kim, You-Il (국방과학연구소 1본부 5부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.39, no.10, 2011 , pp. 966-978 More about this Journal
Abstract
Transpiration cooling is the most effective cooling technique for the high-performance liquid rockets and air-breathing engines operating in aggressive environments with higher pressures and temperatures. When applying transpiration cooling, combustor liners and turbine blades/vanes are cooled by the coolant(air or fuel) passing through their porous walls and also the exit coolant acting as an insulating film. Practical implementation of the cooling technique has been hampered by the limitations of available porous materials. But advances in metal-joining techniques have led to the development of multi-laminate porous structures such as Lamilloy$^{(R)}$ fabricated from several diffusion-bonded, etched metal thin sheets. And also with the availability of lightweight, ceramic matrix composites(CMC), transpiration cooling now seems to be a promising technique for high-performance engine cooling. This paper reviews recent research activities of transpiration cooling and its applications to gas turbines, liquid rockets, and the engines for hypersonic vehicles.
Keywords
Transpiration Cooling; Lamilloy$^{(R)}$; Porous Ceramics; Liquid Rocket; Air-Breathing Engine;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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