Acoustic and Vibration Environment Prediction Technology of Instrument Cabin Based on Multi-Source Data

Noise characteristic is one of the important factors to be considered during the design of a launch vehicle system.In this paper,the acceptance conditions for the external noise environment of the instrument cabin are given based on multi-source data,including the measured data of the launch vehicle lift-off noise,the mechanical environment of the launch vehicle equipment,and the external noise environment of the instrument cabin deduced from empirical formula.Then an acoustic and vibration transfer model is established based on the response data of the instrument equipment used to conduct measurements in the noise test reverberation room.By using an external noise environment and a transfer model,the response of the instrument and equipment for the acceptance condition can be obtained.The acoustic and vibration prediction technology introduced in this paper can provide technical support in the environmental prediction analysis of heavy launch vehicles for the future.

航天飞行器管路结构的动力学强度分析与试验

航天飞行器管路呈现结构轻薄、力学环境恶劣、使用应力大、易产生低周疲劳的特点,曾多次发生飞行故障.随着航天飞行器向着轻质化、可重复使用、高可靠性的发展,对管路结构提出了由环境适应性定性考核向动力学强度定量评估转变的迫切要求.本文首先对基于Miles公式、模态均方根值等国内外管路结构动力学载荷分析方法的基本原理及其应用进行了介绍,用其指导管路结构动力学设计.其次结合工程实际,对管路结构动力学强度分析中常用的Steinberg快速评估、基于统计模型的频域疲劳分析等理论方法及技术要点进行了总结.最后结合航天领域管路结构动力学强度设计、分析与试验的研究现状,对有待于进一步开展研究的工程和科学问题进行了展望.