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Characterization and synthesis of random acceleration vibration specifications

机译:随机加速度振动规范的表征与综合

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摘要

Random acceleration vibration specifications for subsystems, i.e. instruments,udequipment, are most times based on measurement during acoustic noise tests on system level, i.e. a spacecraft and measured by accelerometers, placed in the neighborhood of the interface between spacecraft and subsystem. Tuned finite element models can be used to predict the random acceleration power spectral densities at other locations than available via the power spectral density measurements of the acceleration. The measured and predicted power spectral densities do represent the modal response characteristics of the system and show many peaks and valleys. The equivalent random acceleration vibration test specification is a smoothed, enveloped, peak-clipped version of the measured and predicted power spectral densities of the acceleration spectrum.udThe original acceleration vibration spectrum can be characterized by a different number response spectra: Shock Response Spectrum (SRS) , Extreme Response Spectrum (ERS), Vibration Response Spectrum (VRS), and Fatigue Damage Spectrum (FDS). An additional method of non-stationary random vibrations is based on the Rayleigh distribution of peaks. The response spectra represent the responses of series of SDOF systems excited at the base by random acceleration,udboth in time and frequency domain. The synthesis of equivalent random acceleration vibration specifications can be done in a very structured manner and are more suitable than equivalent random acceleration vibrationudspecifications obtained by simple enveloping. In the synthesis process Miles’ equation plays a dominant role to invert the response spectra into equivalent random acceleration vibration spectra. A procedure is proposed to reduce the number of data point in the response spectra curve by dividing the curve in a numbers of fields. The synthesis to an equivalent random acceleration spectrum is performed on a reduced selected set of data points. The recalculated responseudspectra curve envelops the original response spectra curves. A real life measured random acceleration spectrum (PSD) with quite a number of peaks andudvalleys is taken to generate, applying response spectra SRS, ERS, VRS, FDS and the Rayleigh distribution of peaks, equivalent random acceleration vibration specifications. Computations are performed both in time and frequency domain.
机译:子系统(即仪器设备)的随机加速度加速度规范通常是基于在系统水平(即航天器)的声学噪声测试期间的测量结果,并通过加速度计测量的,该加速度计位于航天器和子系统之间的界面附近。调整后的有限元模型可用于预测其他位置的随机加速度功率谱密度,而不是通过加速度的功率谱密度测量获得。测得的功率谱密度和预测的功率谱密度确实代表了系统的模态响应特性,并显示出许多峰和谷。等效的随机加速度振动测试规范是加速度频谱的测量和预测功率谱密度的平滑,包络,峰值剪切版本。 ud原始加速度振动频谱可以通过不同的数字响应谱来表征:冲击响应谱( SRS),极限响应谱(ERS),振动响应谱(VRS)和疲劳损伤谱(FDS)。非平稳随机振动的另一种方法是基于峰的瑞利分布。响应谱表示在时域和频域中由随机加速度在基点激励的一系列SDOF系统的响应。等效随机加速度振动规范的合成可以非常结构化的方式进行,比通过简单包络获得的等效随机加速度振动/规范更合适。在合成过程中,迈尔斯方程起着主导作用,将响应谱转换为等效的随机加速度振动谱。提出了一种通过将曲线划分为多个字段来减少响应光谱曲线中数据点数量的方法。对减少的选定数据点集执行等效随机加速度谱的合成。重新计算的响应 udspectra曲线包围了原始响应谱曲线。应用响应光谱SRS,ERS,VRS,FDS和峰的瑞利分布以及等效的随机加速度振动规范,来生成具有相当多的峰和 udvalley的真实测量的随机加速度谱(PSD)来生成。计算在时域和频域中进行。

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