发明名称 GAS­TURBINE BURNER
摘要 <p>A gas-turbine burner having a plurality of main swirl generators, each having an inlet flow opening formed by the main swirl generator edge, is provided. In order to achieve a uniform flow of combustion air through the main swirl generator, the gas-turbine burner has an inlet-flow guide means with a flow guide surface which runs from one of the inlet-flow openings to an adjacent inlet-flow opening, to which the main swirl generator edges which form the inlet-flow openings are connected, and the flow guide surface widens from there radially upwards. The main swirl generators are central-symmetrically arranged around a pilot burner and the flow guide surface runs radially outside the main swirl generators.</p>
申请公布号 KR101493256(B1) 申请公布日期 2015.02.16
申请号 KR20107002188 申请日期 2008.07.02
申请人 发明人
分类号 F23R3/14;F23R3/28;F23R3/34 主分类号 F23R3/14
代理机构 代理人
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