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Sliding-vane rotary compressor with specific cylinder bore profile

机译:具有特定缸孔轮廓的滑片式旋转压缩机

摘要

A multiple-vane rotary compressor having a cylinder bore profile especially designed to reduce the fluctuation in the overall drive torque applied to the rotor shaft. The cylinder bore profile is configured and designed so that the individual drive torque applied to an individual vane during the compression and delivery strokes varies along a drive torque-vane angle curve which approximates an isosceles triangle having a lower side corresponding to a range of angle of 180°. The cylinder bore profile includes, for a profile section extending through an angle of 180°, a first region (i) in which the amount of vane projection is held substantially constant at a maximum value (D), a second region (ii) in which the amount of vane projection decreases at a higher rate, and a third region (iii) in which the amount of vane projection decreases to zero at a lower rate, the imaginary transitional point (A.sub.3) between the second and third regions being located at an angular position of 90°.
机译:一种具有叶片孔轮廓的多叶片旋转式压缩机,其设计旨在减少施加在转子轴上的总驱动扭矩的波动。气缸孔轮廓的配置和设计使得在压缩和输送冲程期间施加到单个叶片的单个驱动扭矩沿驱动扭矩-叶片角度曲线变化,该曲线近似于等腰三角形,该等腰三角形的下侧对应于一个角度范围。 180°。对于延伸通过180°角的轮廓段,气缸孔轮廓包括第一区域(i)和第二区域(ii),在第一区域中叶片突出量基本恒定地保持在最大值(D)。其中叶片投影的量以较高的速率减小,并且第三区域(iii)的叶片的投影量以较低的速率减小到零,第二和第三之间的虚构过渡点(A.sub.3)区域位于90°的角位置。

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