A New Method for Determining the Aerodynamic Forces Arising in Turbine Seals

IF 0.9 Q4 ENERGY & FUELS Thermal Engineering Pub Date : 2023-09-05 DOI:10.1134/S0040601523090033
S. S. Dmitriev, B. N. Petrunin, V. V. Naumov, I. A. Nikitin
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Abstract

The article presents an aerodynamic force calculation method that was developed and tested at the National Research University Moscow Power Engineering Institute’s (NRU MPEI) Department of Steam and Gas Turbines. By using the proposed method, it is possible to quickly estimate, as a first approximation, the nonconservative component of the aerodynamic force arising in turbine seals proceeding from the aerodynamic force value measured under steady-state conditions without resorting to conventional costly research methods. The possibility to calculate the aerodynamic force nonconservative component at any rotor rotation frequency under steady-state conditions is substantiated. The values of the aerodynamic force nonconservative component in the seal obtained using the new method according to the calculation expression proposed by A.G. Kostyuk were compared with the results of measuring this force for similar seal models carried out previously using the conventional methods: by means of a strain-gauge balance and from the readings in seal chamber drains. The new method for determining aerodynamic forces was then applied for estimating the blade row forces, which depend on the leak uniformity through the shroud seal and act on the R-26-17A annular turbine rotor cascade. The obtained values were compared with the data of studies carried out on the IT-1 experimental setup using the conventional method by means of strain-gauge measurements, and the comparison results have shown good agreement of the data. The proposed method makes it possible to obtain qualitatively and quantitatively valid results and can be used for comparing the seals having different configurations with respect to the nonconservative force component arising in them that can give rise to self-vibration of turbine machinery shaft lines. For perfecting the method, it is possible to use the models of rotor parts that do not need balancing and that are manufactured using inexpensive materials.

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一种测定涡轮密封气动力的新方法
本文介绍了莫斯科国立研究大学动力工程学院(NRU MPEI)蒸汽和燃气轮机系开发和测试的一种气动力计算方法。采用该方法,无需采用昂贵的常规研究方法,即可从稳态条件下测量的气动力值快速估计出涡轮密封中产生的气动力的非保守分量,作为第一个近似。证明了在稳态条件下计算任意转子旋转频率下气动力非保守分量的可能性。根据A.G. Kostyuk提出的计算表达式,用新方法得到了密封中气动力非保守分量的值,并与以前用传统方法测量类似密封模型的气动力非保守分量的结果进行了比较:用应变计平衡法测量该力,并从密封室排水口的读数中测量该力。然后,将新的气动力确定方法应用于估算叶片排力,该排力依赖于通过叶冠密封的泄漏均匀性,并作用于R-26-17A环形涡轮转子叶栅。将所得值与在IT-1型试验装置上采用常规方法进行的试验数据进行了应变片测量比较,结果表明两者吻合较好。所提出的方法可以获得定性和定量的有效结果,并可用于比较具有不同结构的密封件中产生的引起涡轮机械轴系自振动的非保守力分量。为了完善该方法,可以使用不需要平衡且使用廉价材料制造的转子部件的模型。
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来源期刊
CiteScore
1.30
自引率
20.00%
发文量
94
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