Machine Gun Finite Element Model Amending Based on Frequency Response Functions of Vibration

Article Preview

Abstract:

Correction machine gun finite element model to predict dynamic characteristics is very important. Through theoretical calculations and experimental test structure to obtain guns frequency response function, given the sensitivity of both the correlation function and expression, introduced a model correction method, and laid the theoretical foundation for a certain type of machine gun finite element model updating. Build a certain type of machine guns and modal testing and analysis system was carried out to test the vibration frequency response function. Boundary condition parameters of the machine gun was amended, and modal test results were compared to prove the validity of the model correction method.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

349-352

Citation:

Online since:

August 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] LIU Guangpu,PAN Hongxia. Research on Optimization of Structural Dynamic Characteristics for Machine Gun Based on Sensitivity Analysis, JOURNAL OF NORTH CHINA INSTITUTE OF TECHNOLOGY, 1999, Vol20, No. 2: 162-165.

Google Scholar

[2] WANG Mao-long, LIU Ming, CAO Shuang-yin. Modifying the dynamic characteristic of an undamped structure by mass and stiffness addition technique, ENGINEERING MECHANICS, 2004, Vol. 21, No. 5: 178-182.

Google Scholar

[3] WANG Rui-lin, LI Yong-jian, ZHANG Jun-nuo. Design of a Machine Gun Mount with Buffer-type Spade. ACTA ARMAMENTARⅡ, 2007, Vol. 28, No 2: 144-147.

Google Scholar

[4] ZHANG Ping, CHEN Kuifu. The Method for Improving Precision of Estimating Modal Parameter, Journal of China Agricultural University, 2002, Vol. 7 No. 6: 5-9.

Google Scholar

[5] Cauberghe, B, Guillaume, P, Dierckx, B, et al. Identification of modal parameters from inconsistent data, Proc. of the 20th IMAC, 2002: 809~815.

Google Scholar

[6] Andrea Cusano, Patrizio Capoluongo. Experimental Modal Analysis of an Aircraft Model Wing by Embeded Fiber Bragg Grating Sensors [J]. IEEE Sensors Journal, 2006, 6 (1): 67-77.

DOI: 10.1109/jsen.2005.854152

Google Scholar

[7] LIU Bing. Application of LMS Modal Analysis Software in Modal Test of Gear Assembly, Gas Turbine Experiment and Research, 2003, Vol. 16 No. 2: 43-45.

Google Scholar

[8] YUN Chao,SONG Liangliang,Li Ran,ZHOU Zhenggan,LIU Xiaoping. Experimental modal analysis of 120kg spot welding robots, chinese journal of mechanical engineering, 2001, Vol. 37 No. 6: 38-42.

DOI: 10.3901/jme.2001.06.038

Google Scholar