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首页> 外文期刊>Mathematical Problems in Engineering: Theory, Methods and Applications >Load Sharing Multiobjective Optimization Design of a Split Torque Helicopter Transmission
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Load Sharing Multiobjective Optimization Design of a Split Torque Helicopter Transmission

机译:分体式扭矩直升机变速器负荷分担多目标优化设计

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Split torque designs can offer significant advantages over the traditional planetary designs for helicopter transmissions. However, it has two unique properties, gap and phase differences, which result in the risk of unequal load sharing. Various methods have been proposed to eliminate the effect of gap and promote load sharing to a certain extent. In this paper, system design parameters will be optimized to change the phase difference, thereby further improving load sharing. A nonlinear dynamic model is established to measure the load sharing with dynamic mesh forces quantitatively. Afterwards, a multiobjective optimization of a reference split torque design is conducted with the promoting of load sharing property, lightweight, and safety considered as the objectives. The load sharing property, which is measured by load sharing coefficient, is evaluated under multiple operating conditions with dynamic analysis method. To solve the multiobjective model with NSGA-II, an improvement is done to overcome the problem of time consuming. Finally, a satisfied optimal solution is picked up as the final design from the Pareto optimal front, which achieves improvements in all the three objectives compared with the reference design.
机译:与传统的直升机传动行星设计相比,扭矩分配设计具有明显的优势。但是,它具有两个独特的特性,即间隙和相位差,这会导致负载分配不均的风险。已经提出了各种方法来消除间隙的影响并在一定程度上促进负载共享。本文将优化系统设计参数以改变相位差,从而进一步改善负载分配。建立了非线性动力学模型来定量地测量与动态网格力的负载分配。然后,以提高负荷分配性能,轻便性和安全性为目标,对参考分流扭矩设计进行了多目标优化。在多种运行条件下,采用动态分析方法对通过负荷分配系数测得的负荷分配特性进行评估。为了解决NSGA-II的多目标模型,进行了改进以克服耗时的问题。最后,从帕累托最优方案中挑选出满意的最优解决方案作为最终设计,与参考设计相比,这三个目标均得到了改善。

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