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Involute trapped vortex combustor assembly

机译:渐象被捕获的涡旋燃烧器组件

摘要

A combustor assembly includes a volute wall extended annularly around a combustor centerline, extended at least partially as a spiral curve from a circumferential reference line around the combustor centerline, and defining a combustion chamber therewithin, an annular inner wall extended at least partially along a lengthwise direction from the volute wall, an annular outer wall extended at least partially along the lengthwise direction from the volute wall, the annular inner wall and the annular outer wall being separated along a radial direction from the combustor centerline, and a primary flow passage being defined between the annular inner wall and the annular outer wall in fluid communication with the combustion chamber, and a flow passage wall extending between a portion of the volute wall and a portion of the annular outer wall.
机译:燃烧器组件包括围绕燃烧器中心线围绕燃烧器中心线延伸的蜗壳壁,至少部分地从燃烧器中心线周围的圆周参考线延伸,并且在其中限定燃烧室,环形内壁至少部分地沿着纵向延伸从蜗壳壁的方向,环形外壁沿着从蜗壳壁,环形内壁和环形外壁沿着从燃烧器中心线径向分离的环形内壁和环形外壁,以及限定的主要流动通道在环形内壁和环形外壁与燃烧室流体连通,以及在蜗壳壁的一部分之间延伸的流动通道壁和环形外壁的一部分。

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