Theoretical substantiation of new features of rolling bearings operation under combined loading conditions

Valeriy V. Kirilovskiy, Кириловский Валерий Владимирович, Y. Belousov, Белоусов Юрий Вениаминович
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引用次数: 1

Abstract

Rolling bearings are widely used in the products of aviation and space technology. To ensure their long-term trouble-free operation, it is necessary to have accurate and reliable information about the forces acting on the bearings. The required values of forces and, accordingly, the required durability of bearings are usually determined on the basis of the traditional design scheme of a double-support beam (smooth beam mounted on two hinged supports). The paper presents a new interpretation of the features of the operation of bearing units on ball radial single-row bearings installed according to the cross located arrangement. It is shown that under conditions of combined loading, including radial and axial forces, the generally accepted theoretical model of a doublesupport beam is not implemented. There is no single calculation model that adequately reflects the nature of the interaction of bearing parts over the entire range of external loads. In the most general case, this model can be represented by a sequence of five statically indeterminate calculation schemes, which are modified and transformed into one another. So, with an increase in the external radial force, the cantilevered beam with additional hinge support scheme is first implemented, which, then, is transformed into the double-sided jamming scheme, and that, later, is transformed into the two double hinge supports scheme. It is also possible to implement two intermediate transition schemes. A specific example shows that in the products of aviation and space technology, determining the durability of bearings based on the traditional model is not advisable, since it can give an overestimated value with an error of 28,37 to 26663,9 times.
组合载荷条件下滚动轴承运行新特征的理论证实
滚动轴承广泛应用于航空航天技术产品中。为了确保其长期无故障运行,有必要掌握作用在轴承上的力的准确可靠的信息。所需的力值以及相应的轴承所需的耐久性通常是根据双支撑梁(安装在两个铰接支撑上的光滑梁)的传统设计方案确定的。本文对按交叉定位布置安装的滚珠径向单列轴承的轴承单元的运行特点作了新的解释。结果表明,在径向力和轴向力共同作用下,普遍接受的双支撑梁理论模型并不适用。没有一个单一的计算模型能充分反映轴承部件在整个外部载荷范围内相互作用的性质。在最一般的情况下,该模型可以由五个静态不确定计算方案组成的序列来表示,这些方案可以被修改并相互转换。因此,随着外径向力的增大,悬臂梁首先采用附加铰支承方案,然后将附加铰支承方案转化为双面卡壳方案,再将附加铰支承方案转化为双铰支承方案。还可以实施两种中间过渡方案。具体实例表明,在航空航天技术产品中,基于传统模型确定轴承耐久性是不可取的,因为它可以给出高估值,误差为28,37至26663,9倍。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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