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DEVELOPMENT OF NEW HIGH-PERFORMANCE LABYRINTH SEAL USING AERODYNAMIC APPROACH

机译:运用气动方法开发新型高性能拉贝林密封

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As key technologies to improve the performance of steam turbines, various types of high performance seal, such as active clearance control (ACC) seals and leaf seals, have been developed by Mitsubishi Heavy Industries, LTD (MHI). Moreover, a new seal concept has also been developed, which remarkably reduces the leakage flow through the blade tip/base clearance by using an aerodynamic approach. The main concept of this technology is to control and utilize the vortex structure in the cavities of the labyrinth seal by optimizing the cavity geometry. In the optimized geometry, locally-controlled flow on the upstream side of the fin tip causes a strong contraction of the leakage flow and reduces the discharge coefficient significantly. This concept allows for a remarkably reduced leakage flow, whilst keeping clearance at the same level as that of conventional set-up, and thus the risk of contact between rotating and stationary parts low. Therefore, this technology realizes reliable and durable seals with high performance. In addition, it is possible to keep manufacturing cost at the same level as conventional seals, since the structure of this seal is basically the same as the conventional one. In the development of this technology, a parametric study using Computational Fluid Dynamics (CFD) was carried out to optimize the cavity geometry. The verification test was carried out for the optimized geometry under the real steam conditions. From the results, we confirmed that the optimized geometry reduced the discharge coefficient by up to 30%, compared to conventional seals.
机译:作为提高汽轮机性能的关键技术,三菱重工已开发出各种类型的高性能密封件,例如主动间隙控制(ACC)密封件和叶片密封件。此外,还开发了一种新的密封概念,该密封概念通过使用空气动力学方法显着减少了通过叶片尖端/基部间隙的泄漏流量。该技术的主要概念是通过优化型腔的几何形状来控制和利用迷宫式密封的型腔中的涡流结构。在优化的几何形状中,在翅片尖端上游侧的局部控制流动会导致泄漏流的强烈收缩,并显着降低排放系数。该概念可显着减少泄漏流量,同时将间隙保持在与传统装置相同的水平,从而降低了旋转部件与固定部件之间接触的风险。因此,该技术实现了高性能的可靠耐用的密封。另外,由于该密封件的结构基本上与传统密封件相同,因此可以将制造成本保持在与传统密封件相同的水平。在这项技术的发展中,使用计算流体动力学(CFD)进行了参数研究,以优化型腔的几何形状。在真实蒸汽条件下对优化的几何形状进行了验证测试。根据结果​​,我们确认,与传统的密封件相比,优化的几何形状可将排放系数降低多达30%。

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