以非满管代替满管进行转管炮身管寿命试验研究

doi:10.3969/j.issn.1000-1093.2017.10.004

兵工学报 ›› 2017, Vol. 38 ›› Issue (10): 1899-1908.doi: 10.3969/j.issn.1000-1093.2017.10.004

以非满管代替满管进行转管炮身管寿命试验研究

张培忠，郑建福，米中贺，陈国利，宁金贵，黄彦昌

(中国白城兵器试验中心，吉林白城 137001)

收稿日期:2017-02-14 修回日期:2017-02-14 上线日期:2017-11-22
通讯作者: 宁金贵（1981—），男，工程师，硕士 E-mail:njgnjgnjg19810118@163.com
作者简介:张培忠（1966—），男，研究员，博士。E-mail：zhangpeizhong9966@163.com
基金资助:
总装备部试验技术研究项目（2010SY4205001）

Research on Barrel Life Test of Revolving Barrel Cannon by Substituting Full Charge Loading with Non-full Charge Loading

ZHANG Pei-zhong, ZHENG Jian-fu, MI Zhong-he, CHEN Guo-li, NING Jin-gui, HUANG Yan-chang

(China Baicheng Ordnance Test Center, Baicheng 137001, Jilin, China)

Received:2017-02-14 Revised:2017-02-14 Online:2017-11-22

摘要/Abstract

摘要： 为减少转管炮身管寿命试验的用弹量，研究用非满管代替满管进行转管炮身管寿命试验的技术。建立炮口振动位移计算方程，利用高阶傅里叶级数拟合炮膛合力，获得炮膛合力的频域函数；利用模态实验获得了转管炮的模态参数，构建转管炮起落部分的频响函数；利用频响函数计算了转管炮在满管射击、非满管射击方式下的炮口振动位移。以满管射击、非满管射击方式下炮口振动位移的一致性为原则，确定身管寿命试验方案。通过试验验证了满管射击、满非管射击方式下的身管寿命试验结果具有一致性，从而获得用弹量较少的身管寿命试验方法，节省了试验的弹药消耗。

关键词: 兵器科学与技术, 火炮, 身管寿命, 试验技术

Abstract: The technology of substituting full charge loading with non-full charge loading is researched to decrease the ammunition consumption in the barrel life test of revolving barrel cannon. The computing equations of muzzle vibration displacement are established. High-order Fourier series is used to fit the resultant force in bore, and then the frequency equations of resultant force are established. The modal parameters of cannon are obtained by model measuring and analysis, and a frequency response equation of the cannon elevating part is established. The frequency response equation is used to calculate the muzzle vibration displacements in the way of non-full charge loading and full charge loading. The differences among these muzzle vibration displacements are compared. Based on the law that the muzzle vibration displacements of non-full charge loading and full charge loading are consistent, the barrel life test scheme is confirmed. In verification experiment, the barrel life’s consistency is proved. The barrel life test method of less amount ammunition is designed to decrease the ammunition consumption in test. Key

Key words: ordnancescienceandtechnology, cannon, barrellife, testtechnology

中图分类号:

TJ306⁺.1

张培忠，郑建福，米中贺，陈国利，宁金贵，黄彦昌. 以非满管代替满管进行转管炮身管寿命试验研究[J]. 兵工学报, 2017, 38(10): 1899-1908.

ZHANG Pei-zhong, ZHENG Jian-fu, MI Zhong-he, CHEN Guo-li, NING Jin-gui, HUANG Yan-chang. Research on Barrel Life Test of Revolving Barrel Cannon by Substituting Full Charge Loading with Non-full Charge Loading[J]. Acta Armamentarii, 2017, 38(10): 1899-1908.

参考文献

［1］ GJB349.23—1990常规兵器定型试验方法:高射炮和海军炮[S].北京：国防科学技术工业委员会，1990:10,21,29.
GJB349.23—1990 Conventional weapon approval test method : antiaircraft gun and navy gun[S]. Beijing: the Committee of Science, Technology and Industry for National Defense,1990: 10,21,29.(in Chinese)
[2］米中贺，王毅，李战旗，等. 转管武器炮膛合力在ADAMS中的实现方法[J].火炮发射与控制学报，2011，32(4)：46-49.
MI Zhong-he,WANG Yi, LI Zhan-qi, et al. Realization method of revolving barrels cannon resultant force based on ADAMS software [J]. Journal of Gun Launch and Control, 2011，32(4):46-49.(in Chinese)
[3］杨明华，薛静，韩小平，等.某高射速多管炮刚体动力学建模仿真[J].四川兵工学报,2011,32(12): 24-28.
YANG Ming-hua,XUE Jing, HAN Xiao-ping, et al. Dynamic simulation analyzing for high speed revolving barrels cannon[J]. Sichuan Ordnance Journal，2011，32(12) : 24-28.(in Chinese)
[4］芮筱亭，陆毓琪，王国平，等.多管火箭发射动力学仿真与试验测试方法[M].北京：国防工业出版社,2001: 188-189，217-235.
RUI Xiao-ting, LU Yu-qi, WANG Guo-ping,et al. Simulation and measurement method for multi-barrels rocket gun[M]. Beijing: National Defense Institute Press,2001:188-189，217-235.(in Chinese)
[5］廖日东.I-DEAS实例教程[M].北京：北京理工大学出版社，2003：97-100.
LIAO Ri-dong.Course of I-DEAS examples [M].Beijing: Beijing Institute of Technology Press,2003:97-100.(in Chinese)
[6］李德葆，陆秋海. 实验模态分析及其应用[M].北京：科学出版社，2001：62-66，87-91.
LI De-bao, LU Qiu-hai. Experiment model analysis and utility[M].Beijing: Science Press,2001:62-66，87-91.(in Chinese)
[7］沃德·海伦，斯蒂芬·拉门兹，波尔·萨斯.模态分析理论与试验[M].白化同，李继忠，译. 北京：北京理工大学出版社,2003: 5-6.
Heylen W, Lammens S, Szasz B. Modal analysis theory and experiment[M]. BAI Hua-tong, LI Ji-zhong, translated. Beijing:Beijing Institute of Technology Press,2003:5-6.(in Chinese)
[8］张海航，狄长安.某型多管火炮的振动模态分析[J].兵工学报,2008，29（12）: 1514-1517.
ZHANG Hai-hang, DI Chang-an. Analysis of model of a multi barrel cannon[J]. Acta Armamentarii,2008，29(12):1514-1517.(in Chinese)
[9］张学锋，马大为，乐贵高，等.对某型多管火箭武器减少试验用弹量的仿真[J].兵工学报,2006，27（5）: 792-796.
ZHANG Xue-feng, MA Da-wei, LE Gui-gao, et al. Simulation on decreasing ammunition consumption for test of some multile launch rocket system[J]. Acta Armamentarii,2006，27(5):792-796.(in Chinese)

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以非满管代替满管进行转管炮身管寿命试验研究

Research on Barrel Life Test of Revolving Barrel Cannon by Substituting Full Charge Loading with Non-full Charge Loading

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