发明名称 GAS TURBINE COMBUSTION SYSTEM
摘要 <p>A combustion system with provisions to minimize undesired exhaust products including carbon monoxide, incompletely burned fuel, and oxides of nitrogen. Air entering the combustion zone of the combustion apparatus is mixed with a relatively large amount of recirculated combustion products, preferably about twice the weight of the fresh air entering the combustion zone. The combustion products which are recirculated are cooled by heat exchange with air flowing to a dilution zone of the combustion apparatus where the combustion products and air are mixed to provide the high temperature gas output of the system which is the motive fluid of a gas turbine.</p>
申请公布号 CA963671(A) 申请公布日期 1975.03.04
申请号 CA19720155631 申请日期 1972.11.06
申请人 GENERAL MOTORS CORPORATION 发明人 STETTLER, RICHARD J.;VERDOUW, ALBERT J.
分类号 F02C3/34;F23R3/00;(IPC1-7):02C7/10 主分类号 F02C3/34
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