发明名称 AIRCRAFT RINSE SYSTEM
摘要 A method and apparatus for separating particles and dissolved matter from a fluid stream incorporated in an aircraft rinse system. The present invention includes a first pressure source which transports collected rinse fluid into a separator annulus with a filter element disposed therein. The untreated fluid is placed under appropriate pressure sufficient to produce turbulent flow, increased particle kinetics and/or cavitation physics allowing the desired fluid to penetrate and pass into and through the filter media. The filtered fluid is then transported to a collection tank. The contaminant particulate matter retained on the exterior of the filter media may be removed by the instantenous reverse pressurization of the separator annulus by a second pressure source thereby removing the contaminant particles away from contact with the filter media, and which may then be transported to a waste collection tank or a concentrator for further treatment. The treated rinse fluid is thus recycled for use in the aircraft rinse system.
申请公布号 WO2005084189(A3) 申请公布日期 2006.10.12
申请号 WO2005US02134 申请日期 2005.01.25
申请人 LJC TECHNOLOGIES, LLC;JOHNSON, RAYMOND, FORD;JOHNSON, MARKLEY, DEAN;GRAGE, RODNEY 发明人 JOHNSON, RAYMOND, FORD;JOHNSON, MARKLEY, DEAN;GRAGE, RODNEY
分类号 B01D65/02;B01D17/02;B01D61/00;B01D61/14;B01D61/18;B01D61/20;B01D63/06;B01D65/00;B01D65/08;B64D11/00;C02F1/44;C12M1/34;F04B9/113 主分类号 B01D65/02
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