发明名称 PREMIXING CHAMBER FOR TURBINE COMBUSTOR
摘要 <p>A swirled diffusion dump combustor of the present invention includes a cylindrical combustor can and a fuel and air mixer attached to the upstream end of the combustor can. The mixer is generally formed by an annular chamber which is defined between annular outer and inner walls, having an annularly continuous truncated conical cross-section. The upstream end of the annular chamber is closed by a manifold ring which includes an annular fuel passage and two rows of swirled air passages. Thus, the compressor air approaching the mixer from above enters the swirled air passages, and the swirled air flow in the annular chamber shears fuel from the lips of the annular fuel passage to produce a fuel/air mixture.</p>
申请公布号 WO2003006885(A1) 申请公布日期 2003.01.23
申请号 CA2002001037 申请日期 2002.07.08
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