首页> 外文会议>International Compressor Engineering Conference at Purdue >IMPROVING CENTRIFUGAL COMPRESSOR PERFORMANCE BY OPTIMIZING DIFFUSER SURGE CONTROL (VARIABLE DIFFUSER GEOMETRY) AND FLOW CONTROL (INLET GUIDE VANE) DEVICE SETTINGS
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IMPROVING CENTRIFUGAL COMPRESSOR PERFORMANCE BY OPTIMIZING DIFFUSER SURGE CONTROL (VARIABLE DIFFUSER GEOMETRY) AND FLOW CONTROL (INLET GUIDE VANE) DEVICE SETTINGS

机译:通过优化扩散器浪涌控制(可变扩散器几何形状)和流量控制(入口导向叶片)设备设置,改善离心式压缩机性能

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Surge control problems have been around as long as the centrifugal compressor itself. Many different approaches have been taken to improve operating range to surge (both in head and flow) depending on what type of surge mechanism is present in the compressor system. Compressor surge triggered by diffuser stall can be suppressed by variable diffuser geometry whereas surge from impeller stall can be eliminated by the use of variable-geometry inlet guide vanes. A given compressor duty in terms of flow and pressure ratio can be realized by an infinite number combinations of inlet guide vane / variable diffuser geometry settings. These various realizations of the same duty point have different compressor efficiencies. This paper describes a method that allows for optimal inlet guide vane/variable-geometry diffuser positioning (for a diffuser surge driven system) using two or three pressure measurements along the flow path, i.e. impeller inlet pressure, impeller exit/diffuser inlet pressure and diffuser exit pressure. Maximum obtainable diffuser pressure recovery can be used to determine the onset of surge. These maximum pressure recovery values are a function of variable-geometry diffuser setting only and are over most of the operating range independent of flow, head or inlet guide vane setting and can quickly be determined experimentally by pressure measurements. During operation, the known maximum pressure recovery value can be compared to the one determined from real time pressure measurements, and a determination as to the optimal setting of the diffuser can be made. Test data shown in this paper suggest that for the most efficient operation of a compressor, the diffuser should be positioned such that its pressure recovery value is close to its maximum. This in effect brings surge close to the operating point, but with careful control and safety factors it is surmised that stable operation is possible.
机译:只要离心式压缩机本身即可浪涌控制问题已经存在。取决于压缩机系统中存在的浪涌机构的存在,已经采取了许多不同的方法来改善浪涌(头部和流动)的操作范围。通过漫射器失速触发的压缩机浪涌可以通过可变扩散器几何形状来抑制可变扩散器几何形状,而通过使用可变几何入口导向叶片,可以消除来自叶轮失速的浪涌。在流动和压力比方面可以通过入口导向叶片/可变扩散器几何设置的无限数量组合来实现给定的压缩机义。这些相同职责的各种实现具有不同的压缩机效率。本文描述了一种方法,其允许沿着流动路径的两个或三个压力测量,即叶轮入口压力,叶轮出口/扩散器入口压力和扩散器使用两个或三个压力测量来实现最佳入口导向叶片/可变几何漫射器定位(用于扩散器浪涌驱动系统)的方法退出压力。最大可获得的扩散器压力恢复可用于确定浪涌的开始。这些最大压力恢复值是仅可变几何漫射器设置的函数,并且在大多数无关的操作范围内独立于流动,头部或入口导向叶片设置,并且可以通过压力测量实验地快速确定。在操作期间,可以将已知的最大压力恢复值与从实时压力测量确定的那个进行比较,并且可以确定漫射器的最佳设置的确定。本文中所示的测试数据表明,对于压缩机最有效的操作,扩散器应定位,使得其压力恢复值接近其最大值。这实际上使浪涌靠近操作点,但是通过仔细的控制和安全因素,它被抑制了稳定的操作。

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