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Vibration transfer path analysis of rocket engine based on weighted regularization |
LU Guanglin 1 LUO Yajun 1 ZHANG Xinong 1 LI Luxian 1 MA Chicheng 2 |
1.State Key Lab for Mechanical Structural Strength and Vibration, School of Aerospace, Xi’an Jiaotong University, Xi’an 710049, China;
2.Department of Mechanics, Shandong University of Technology, Zibo 255000, China |
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Abstract To provide the basis for vibration control of rocket engine under multi-load, the vibration transfer path analysis (TPA) of the engine is necessary, mainly consisting of load identification and vibration contribution analysis. To identify accurately the engine multi-source excitation and provide reliable analysis results of vibration contribution, an improved TPA based on weighted regularization was proposed. Firstly, the upper bound of relative load identification error was derived and then weighted matrix and Bayesian theory were adopted to improve the accuracy of load recognition, and then the theory of the improved TPA was built. Secondly,a ground vibration testing of the rocket engine was performed to analyze its path contributions. Finally,with the response data of the reference points and the proposed theory of the load identification, the loads on the engine were identified and the vibration contributions of different loads on the target points were calculated and analyzed. The results show that, the proposed TPA is more accurate than the traditional TPA in load identification and vibration contribution analysis.
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Received: 11 December 2017
Published: 28 April 2019
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