STRESS-STRAIN STATE AND CRITICAL ROTATIONAL VELOCITIES OF AIR BLOWER ROTOR PART OF A HIGH BOOST ENGINE

M. Tkachuk, A. Grabovskiy, O. Shut, Andrey Lipeiko, Egor Ovcharov, M. Tkachuk, Mykola Prokopenko, V. Tretyak, I. Klochkov, M. Saverska, S. Kutsenko, N. Pinchuk
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Abstract

The stress-strain state and critical rotation speeds of the air blower rotor part of highly forced engine are investigated. For this purpose, their parametric geometric and finite-element models are built. Due to the high speeds of rotation, the impeller disk acquires an umbrella-shaped deformed shape. This deformation can cause a gap to be selected between the impellers and the stator of the supercharger. In areas of abrupt change of shape on the impeller there is a concentration of stresses. In addition, the supercharger impeller is located cantilevered. This causes low critical speeds. These frequencies may fall within the operating range of angular velocities of the supercharger rotor. All these factors in the complex within a single calculation model were not previously taken into account. Instead, taking into account the dependences of stress, strain and critical velocity levels on the design parameters is of interest in the development of supercharger designs. In particular, the stiffness characteristics of the elastic rotor bearings were varied. The influence of these parameters on the critical rotation speeds of the rotor part of the air supercharger is determined. Recommendations have been developed for debugging from hazardous supercharger modes. In particular, it is proposed to reduce the radial stiffness of the shaft bearings by using elastic flexible rings. This can reduce critical rotor velocities beyond the operating range. In addition, a lighter material can be used to increase the strength of the impeller. It is also possible to limit the operating range of the angular rotational velocities of the rotor part of the investigated air blower. Analysis of the stress-strain state and the critical rotational velocities of the rotor were carried out on the basis of a unified generalized mathematical and numerical model. Keywords: rotor system, air blower, impeller, stress-strain state, critical rotation speed
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某大功率发动机鼓风机转子部件的应力应变状态及临界转速
研究了高压发动机鼓风机转子部件的应力-应变状态和临界转速。为此,建立了它们的参数化几何模型和有限元模型。由于高速旋转,叶轮盘呈伞状变形。这种变形会导致在增压器的叶轮和定子之间选择一个间隙。在叶轮形状突变的区域,应力集中。此外,增压器叶轮是悬臂式的。这将导致较低的临界速度。这些频率可能落在增压器转子角速度的操作范围内。所有这些因素在复杂的单一计算模型以前没有被考虑在内。相反,考虑到应力,应变和临界速度水平对设计参数的依赖关系是增压器设计发展的兴趣所在。特别是,弹性转子轴承的刚度特性发生了变化。确定了这些参数对空气增压器转子部分临界转速的影响。已经制定了从危险增压器模式调试的建议。特别是,建议通过使用弹性柔性环来降低轴轴承的径向刚度。这可以降低超出工作范围的临界转子速度。此外,可以使用较轻的材料来增加叶轮的强度。还可以限制所研究的鼓风机转子部分的角转速的工作范围。基于统一的广义数学和数值模型,对转子的应力-应变状态和临界转速进行了分析。关键词:转子系统,鼓风机,叶轮,应力-应变状态,临界转速
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