舰船电子工程Issue(9)：51-55,5.DOI:10.3969/j.issn.1672-9730.2015.09.013
某火箭弹发射装置自适应平衡机原理方案研究
Study on Decoy Launching Device Adaptive Balancing Machine Principle Scheme
方航 1王敏毅 1黄朝学1
作者信息
- 1. 中国船舶重工集团公司第 710 研究所 宜昌 443003
- 折叠
摘要
Abstract
In order to increase the pitching angle of a certain type of rocket launchers ,the directional trunnion was de‐signed in the tail and the resulting great changes and eccentric torque was balanced by balancing machine .Heavy load torque was directly influenced by the pitching angle ,the residual amount of payload ,the species and layout position of rockets and so on .This new type of balancing machine output torque must dynamically balance quality eccentric load accurately and real‐time .The adaptive balancing machine equipped with control unit was proposed in this paper ,which can be thought as combi‐nation of mechanical and electrical technology .The moment balance was transferred into hydraulic pressure balance problem . Control system recelived the measurement parameters ,calculated the theoretical output in real time and compares with the actual load pressure ,the differential pressure constituted a negative feedback which can be used to regulate the opening of electrohydraulic servo valve until it was balanced totally .The system scheme was feasible after theoretical analysis ,the adap‐tive balancing machine can achieve quality eccentric torque dynamic balance and improve the launcher fast response perform‐ance with the help of main balancing machine .关键词
平衡机/主动双向平衡/自适应/控制系统Key words
equilibrator/active bi- balancing/adaptive/control system分类
军事科技引用本文复制引用
方航,王敏毅,黄朝学..某火箭弹发射装置自适应平衡机原理方案研究[J].舰船电子工程,2015,(9):51-55,5.
