汽轮机叶片强度及振动参数响应面测定

Oleksiy Vodka, K. Potopalska
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引用次数: 0

摘要

研究了给定外载荷下汽轮机叶片几何参数极限函数的定义。为此,建立了汽轮机叶片的几何模型,该模型由叶片体、叶柄和叶冠组成。可变参数为叶片中部相对于质心的旋转角度(从87°到92°不等)和叶片长度(从495 mm到525 mm不等)。在下一阶段,创建了一个有限元网格。对于所构建的模型,在叶片区域建立有序有限元网格。确定叶片在工作模式下的应力-应变状态。在进行静力分析时,以50 Hz的转速作为载荷,在盘在杆的附着点处,采用各方向的固定位移。得到了等效的von Mises应力和位移。最大应力区位于刀刃附着于刀柄处,但不超过极限。为确定汽轮机叶片的振动特性,考虑静载荷作用下的预应力状态,对汽轮机叶片进行了模态分析。在给定的初始条件下,得到了汽轮机叶片的前六个本征模态。第一种形式对应的本征频率与旋转速度重合(等于49 Hz),随后的本征频率分别对应于多重度。在下一阶段,进行一系列计算以确定给定参数下的响应面。确定了最大von Mises应力和自振前4阶振型的响应面。根据对不同输入参数下叶片振动和变形状态的研究结果,可以得到求解优化问题的约束条件。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Determination of the response surface by strength and vibration parameters of the steam turbine blade
The work is devoted the definition of the function of limiting the geometric parameters of the steam turbine blade at given external loads. For this, a geometric model of a steam turbine blade was created, consisting of a blade body, a shank, and a shroud. The variable parameters were the angle of rotation of the middle section relative to the center of mass (which varied from 87 degrees to 92 degrees), as well as the length of the blade (varied from 495 mm to 525 mm). At the next stage, a finite element mesh was created. For the constructed model, an ordered finite element mesh was created in the area of the blade. Determined the stress-strain state of the blade during the operating mode. When carrying out the static analysis, an rotation velocity of 50 Hz was used as a load, and at the point of attachment of the disk in the shank, fixed displacement of all directions were used. The equivalent von Mises stresses and displacement in the structure are obtained. The zone of maximum stresses is located at the point where the blade is attached to the shank, but they do not exceed the limits. To determine the vibration characteristics of a steam turbine blade, its modal analysis was carried out taking into account the prestressed state from the action of static loads. The first six eigen modes of a steam turbine blade are obtained under the indicated initial conditions. The eigen frequency corresponding to the first form coincides with the rotational velocity (equal to 49 Hz), and the subsequent ones correspond to the multiplicities, respectively. At the next stage, a series of calculations was carried out to determine the response surface for the given parameters. The response surface for the maximum von Mises stresses and the first 4 modes of natural vibrations are determined. On the basis of the obtained results of studies of oscillations and deformed state of the blades with varying input parameters, it is possible to obtain a constraint for solving the optimization problem.
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