运载火箭控制作动器液压管道疲劳寿命周期估计及可靠性分析

Q4 Engineering
V. Murugesan, P. Sreejith, S. B. Tiwari, K. Kumar
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引用次数: 1

摘要

运载火箭电液控制执行器的单点失效模式之一是由于严重的振动环境导致的液压管道及其接头的疲劳失效。本文介绍了扩口联轴器液压管道在高振动水平下的疲劳分析实例。通过分析和实验对系统的振动响应进行了评价。建立了管道的有限元模型,以捕捉系统的动态行为。通过使用经验证的模型进行动态应力分析来评估交变应力。基于局部峰值应力、相应的局部强度及其统计分布,通过应力寿命方法,务实地确定了接头的疲劳寿命估计和可靠性。在此基础上,提出了一种简单的设计方案,以提高运载火箭关键控制执行器的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fatigue life cycle estimation and reliability analysis of hydraulic plumbing of a launch vehicle control actuator
One of the single point failure modes identified for the electro hydraulic control actuators of launch vehicles, is the fatigue failure of the hydraulic plumbing and its joints due to severe vibration environments. This paper presents a case study of the fatigue analysis on the hydraulic plumbing with flared coupling joint, subjected to high vibration levels. An evaluation of the vibration response of the system is made through analysis and experimentation. A finite element model of the plumbing is made to capture the dynamic behaviour of the system. The alternating stresses are assessed by dynamic stress analysis using the validated model. Fatigue life cycle estimation and reliability of the joint are determined pragmatically through stress life methods, based on the local peak stress, the corresponding local strength, and their statistical distribution. Based on the study, a simple design solution is suggested to improve the robustness of the critical control actuator of the launch vehicle.
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