发明名称 CENTRIFUGAL GAS COMPRESSOR METHOD AND SYSTEM
摘要 The compressor compresses gas in capillaries leading to a radially distant annular container space. Centrifugal force acts on gas bubbles entrained between liquid slugs moving radially outward through the capillaries which may be radial, tangential or continuously curved. Compressed gas is collected in the annular space. A gas-liquid emulsion is fed to the capillaries by an inboard emulsification device. The emulsification may include a vortex generator, an ejector or a venturi injector, all feeding the gas-liquid mixture into the inboard ends of the capillaries. The capillaries are formed in a series of discs, coaxially stacked with outer disc ends open to the annular space. Capillary inlets may be perpendicular, tangential or may define a venturi jet.
申请公布号 SG11201600123S(A) 申请公布日期 2016.02.26
申请号 SG11201600123S 申请日期 2014.07.09
申请人 ROTATIONAL TROMPE COMPRESSORS, LLC 发明人 CHERRY, MARK A.;ALDERMAN, ROBERT A.;SHILLING, D. HANS
分类号 B04B5/08;F25B11/02;F25B11/04 主分类号 B04B5/08
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