直齿轮和斜齿轮一级前置面修改方案的封闭形式计算

U. Weinberger, M. Otto, K. Stahl
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引用次数: 1

摘要

由于对齿轮箱的日益增长的需求,是尽可能轻量化和高效的,这是最重要的,齿轮啮合的潜力是利用以及尽可能。其中一种方法是定义一个翼面修改,使载荷在翼面得到最佳分配。定义侧面修改的最佳实践是手动检查出负载分布并定义侧面修改的值。一般来说,这是一种获得最优分配负载的迭代方法。这种方法也可以自动化。为此,计算齿轮箱(轴、轴承、齿轮啮合)的变形。在此基础上提出了修正建议,并将其应用于计算模型。一旦下一个附加修改建议的值降到某个限制之下,迭代就完成了。这种方法耗费时间和计算能力。另外,由于它是一个迭代,并不总是收敛。本文提出了一种计算待计算齿轮箱各齿轮级前置翼面修正量的新方法。该方法采用了附加自由度和附加方程,并将其集成到齿轮箱模型的线性方程组中。这些自由度和方程适用于恒荷载分布模型的边界条件。通过在方程中引入附加因素,可以计算任意载荷分布下的引线侧修正。通过对这些附加自由度和方程进行积分,只需要进行一次附加计算就可以得到修正方案。文中的算例显示了该方法的结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Closed Form Calculation of Lead Flank Modification Proposal for Spur and Helical Gear Stages
Due to the growing need for gearboxes to be as lightweight and efficient as possible, it is most important that the gear mesh’s potential is utilized as well as possible. One way of doing that is to define a flank modification that optimally distributes the load over the flank. Best practice for defining a flank modification is to manually check out the load distribution and to define a value of the flank modification. In general, this is an iterative method to get an optimally distributed load. This method can also be automated. To do this, the deformations of the gearbox (shafts, bearings, gear mesh) are calculated. With those results a modification proposal is calculated and applied to the calculation model. As soon as the values for the next additional modification proposal drop under a certain limit, the iteration is finished. This method consumes time and computing power. Additionally, since it is an iteration, does not always converge. A new method for calculating the lead flank modification for all gear stages in the gearbox to be calculated is presented in this paper. The method shown in this paper uses additional degrees of freedom and equations, which are integrated into the linear equation system of the gearbox model. Those degrees of freedom and the equations apply the boundary condition to the model of a constant load distribution. By introducing additional factors in the equations, it is possible to calculate a lead flank modification for an arbitrary load distribution. By integrating these additional degrees of freedom and the equations, only one additional calculation is needed to get a modification proposal. Examples throughout this paper show the results of this method.
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