Pressure exchanging compressor-expander and methods of use

作者: Charles Alexander Garris

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摘要: A novel pressure-exchange compressor-expander is disclosed whereby a high energy primary fluid compresses lower secondary through direct fluid-fluid momentum exchange. The utilizes non-steady flow principles and supersonic to obtain an ejector-compressor which can attain adiabatic efficiencies while having simplicity of construction, small size weight, the low manufacturing cost. This disclosure includes fuel-cell pressurization system humidity control utilizing compressor-expander. turbo-charger for internal combustion engines incorporating exhaust gas recirculation capabilities. Further, air-cycle heat pump suitable aircraft applications

参考文章(27)
Joseph V. Foa, Flow induction device ,(1988)
Joseph V. Foa, Core-flow rotary jet ,(1979)
James N. Anno, Sherwood L. Fawcett, Turbocharger for internal combustion engines ,(1981)
Duane E. Evans, William L. Brown, Roger W. Johnson, Exhaust gas recirculation system for turbo charged engines ,(1978)
Max Berchtold, Abrams Sidney H, Wide speed range pressure exchanger supercharger ,(1959)
Gary D. Vrbas, Don Steven Arnold, Low speed high pressure ratio turbocharger ,(1999)
Dorothy D. McDaniel, Darryl M. Nielsen, Jet pump with rotatable venturi cartridge ,(1991)
Nathan R. Long, Howard L. Anderson, Eductor pump and process ,(1982)
Daniel E. Paxson, System and method for cancelling expansion waves in a wave rotor National Aeronautics and Space Administration Report. ,(1992)