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    • 21. 发明公开
    • Turbomachinery with variable angle fluid guiding devices
    • Tinkomaschine mit Leiteinrichtungen mit variablem Winkel
    • EP0686774A1
    • 1995-12-13
    • EP95107839.3
    • 1995-05-22
    • EBARA CORPORATION
    • Harada, HideomiTakei, Kazuo
    • F04D27/02F04D29/46
    • F04D29/466F04D27/0246F04D27/0284F04D29/462F05D2250/51F05D2250/52
    • A turbomachinery is presented to provide stable operation at fluid flow rates much lower than the design flow rate without introducing surge in the device. This is achieved by providing a diffuser (3) with variable angle vanes (3a). The vane angle at low flow rates is adjusted so as to minimize the diffuser loss of the exiting fluid stream from the impeller (2). Since the flow angle of the exit flow of the impeller (2) is a function only of the non-dimensional flow rates, and does not depend on the flow angle at the inlet the impeller, therefore, the vane angles can be regulated to achieve a stable operation of the impeller (2) without producing surge of the turbomachinery at flow rates lower than the design flow rate. To optimize the performance of the turbomachinery, in addition to the variable angle vanes (3a), an inlet guide vane (6) having variable vane angle is provided so that the turbomachinery can be operated at the required flow rate and head pressure. The concept is demonstrated in a turbomachinery provided with variable diffuser vanes (3a) and an inlet guide vane (6).
    • 提供了一种涡轮机构,以便在流体流动速率远低于设计流量的情况下提供稳定的操作,而不会引起装置的浪涌。 这通过提供具有可变角度叶片(3a)的扩散器(3)来实现。 调节低流速下的叶片角度,以使来自叶轮(2)的离开的流体流的扩散器损失最小化。 由于叶轮(2)的出口流的流角仅与无量纲流量有关,而不依赖于叶轮入口处的流角,因此可以调节叶片角度以达到 叶轮(2)的稳定操作,而不会以低于设计流速的流速产生涡轮机械的浪涌。 为了优化涡轮机械的性能,除了可变角度叶片(3a)之外,还提供了具有可变叶片角度的入口导流叶片(6),使得涡轮机械可以以所需的流量和压头运行。 该概念在具有可变扩散器叶片(3a)和入口引导叶片(6)的涡轮机械中得以证明。
    • 27. 发明公开
    • Method for automatically limiting one controlled variable of a multivariable system and apparatus for antisurge protection of a dynamic compressor
    • 具有一种系统,用于控制变量的自动限制方法,几个变量以及用于离心式压缩机的过载保护。
    • EP0002360A1
    • 1979-06-13
    • EP78300691.9
    • 1978-11-29
    • Compressor Controls Corporation
    • Staroselsky, Naum
    • F04D27/02G05B5/01
    • F04D27/0207F04D27/0261F04D27/0284
    • A control apparatus for antisurge protection of a dynamic compressor including a junction of a closed antisurge loop with a surge limit computing module and a two mode controller with a relay backup system with deviation alarms is characterized in operation in that during a slow disturbance, the two mode controller provides modulated antisurge protection by opening a relief valve. If the operating point of the compressor crosses the surge control line and during a dangerously fast disturbance, the relay backup system (119) provides antisurge protaction if a preestablished deviation of the operating point from the surge control line appears. The relay backup system (119) opens the relief valve (107) very quickly. When the relief valve (107) is so opened, the process of the user (106) of fluid from the compressor (101) is compensated by increasing the performance of the compressor (101) to maintain pressure or flow rate. Then the relay system (119) closes the relief valve (107) exponentially, which prevents a dangerous deviation of the operating point from the surge control line. In time, the surge limit line may change so that the surge control line is no longer correctly ( placed. If under such circumstances surge appears, then the backup relay system (119) opens the relief velve (107) very fast, closes it exponentially and changes the position of surge control line.
    • 为防浪涌保护动态压缩机包括封闭防喘振循环与喘振极限计算模块的结和与偏差报警中继备份系统的双模式控制装置的控制装置,在手术的特征在于缓慢的扰动期间那样,在两个 模式控制器通过打开泄压阀提供调制防浪涌保护。 如果压缩机的动作点横切喘振控制线和一个危险几乎干扰期间,中继备份系统(119)提供防浪涌保护如果从喘振控制线的操作点的预先建立的偏差出现。 继电器备份系统(119)打开泄压阀(107)非常快。 当释放阀(107)被设置成打开时,流体从所述压缩机(101)的用户(106)的过程是通过增加压缩机(101)的性能,以保持压力或流速补偿。 然后,中继系统(119)关闭所述释放阀(107)呈指数,这防止从喘振控制线的操作点的危险的偏差。 在时间,象喘振控制线不再正确放置的喘振极限线可能会改变。 如果被调查的情况下出现激增,那么备份中继系统(119)打开救济velve(107)速度非常快,它成倍关闭,改变喘振控制线的位置。