发明名称 AN APPARATUS FOR MIXING FLUIDS
摘要 A premixer for a combustor to entrain a selected volume of fuel in an oxidizer to be combusted to heat the oxidizer. The combustor is for a gas powered turbine which employs the hypergolic or high energy air stream which will allow a fuel to be combusted in the absence of an additional ignition source. A heat exchanger and a catalyst combusts a first portion of fuel in air without the production of undesired chemical species. The catalyst is employed to lower the combustion temperature of the fuel to substantially eliminate selected chemical species. The fuel premixed in the air then encounters the catalyst and the fuel is combusted to increase the temperature of the air to an auto-ignition temperature so that no other ignition source is needed to combust additional fuel added later.
申请公布号 WO2004085815(A3) 申请公布日期 2004.12.16
申请号 WO2004US09365 申请日期 2004.03.25
申请人 THE BOEING COMPANY 发明人 SPROUSE, KENNETH, M.;FARHANGI, SHAHRAM;MATTHEWS, DAVID, R.
分类号 F23L15/04;F23R3/00;F23R3/40 主分类号 F23L15/04
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