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Centrifugal compressor having an asymmetric self-recirculating casing treatment

机译:具有非对称自循环壳体处理的离心压缩机

摘要

A centrifugal compressor includes an asymmetric self-recirculating casing treatment that includes, on an inner face of a casing 10, a suction ring groove 1, a ring guide channel 2 and a back-flow ring groove 3 to form a self-recirculating channel. An axial-direction position Sr from an upstream end face of the suction ring groove to an impeller full blade leading edge 4 or a width br of the suction ring groove 1 is represented as A(α·D−β·D)2+A0 and is distributed in a parabolic shape in a circumferential direction. An initial phase angle θ0 is in a range of 0≦θ0≦2π. A circumferential angle α of the casing has a definition range of θ0≦α≦θ0+2π. In the expression, A denotes a parameter of the parabola in the axial-direction position Sr or the width br, and A0 denotes an extreme of the axial-direction position Sr or the width br when corresponding circumferential angle β and the α are equal at an extreme point of distribution of the parabola.
机译:一种离心式压缩机,包括不对称的自循环壳体处理,该处理在壳体 10 的内表面上包括吸入环槽 1 ,环形引导通道 2 和回流环槽 3 形成自循环通道。从吸入环凹槽的上游端面到叶轮全叶片前缘 4 或宽度b r r 吸气环凹槽 1 的>表示为A(α·D-β·D) 2 + A 0 ,并分布在沿圆周方向呈抛物线形。初始相位角θ 0 在0≤θ 0 ≤2π的范围内。壳体的圆周角α具有θ 0 ≤α≤θ 0 +2 π的定义范围。在表达式中,A表示抛物线在轴向位置S r 或宽度b r 的参数,而A 0 表示当相应的圆周角β和α在抛物线分布的极端时相等时,轴向位置S r 或宽度b r 的极值。

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