摘要
针对目前民用水下智能装备稀缺且价格昂贵的现状,提出并设计一种气控式水下滑翔机,该设备以自带的压缩空气作为动力源,结构简单,成本低廉。对滑翔机的结构进行介绍,并设计整体气动系统,使用AMESim软件对气动系统进行仿真分析,得到的结论验证了该气动系统具有良好的稳定性。
In view of the current civil underwater intelligent equipment was scarce and expensive,a pneumatic underwater glider was designed. With compressed air as the power source,the equipment was simple structure and low cost. The structure of the glider was introduced,and the whole pneumatic system was designed. The AMESim software was used to analyze the pneumatic system. The conclusion verifies that the pneumatic system has good stability.
引文
[1]杨燕,孙秀军,王延辉.浅海型水下滑翔机技术研究现状的分析[J].海洋技术学报,2015,34(4):7-14.YANG Y,SUN X J,WANG Y H.Analysis on the State-ofthe-art Shallow Water Underwater Gliders[J].Journal of Ocean Technology,2015,34(4):7-14.
[2]温浩然,魏纳新,刘飞.水下滑翔机的研究现状与面临的挑战[J].船舶工程,2015(1):1-6.
[3]STONE L D,KELLER C M,KRATZKE T M,et al.Search for the Wreckage of Air France Flight AF 447[J].Statistical Science,2014,29(1):69-80.
[4]蒋新松,封锡盛,王棣棠.水下机器人[M].沈阳:辽宁科技出版社,2000:86-95.
[5]JIN Y Z,WANG Z W,BAO G.Condensation During Discharging of Pneumatic System[J].Bio-medical Materials and Engineering,2015,26(S1):1871-1881.
[6]曲文新.载人潜水器耐压壳结构设计与分析[D].哈尔滨:哈尔滨工程大学,2013.
[7]赵彤.气动技术的发展及在新领域中的应用[J].液压气动与密封,2004(2):1-5.ZHAO T.The Development of Pneumatic and Its Application in the New Area[J].Hydraulics Pneumatics&Seals,2004(2):1-5.
[8]金英子,朱祖超,杨庆俊,等.气动系统充放气过程中气体状态多变指数的简化与确定[J].机械工程学报,2005,41(6):76-80.JIN Y Z,ZHU Z C,YANG Q J,et al.Simplification and Determination of Polytropic Exponent of Thermodynamic Process in the Filling and Exhausting Process in a Pneumatic System[J].Journal of Mechanical Engineering,2005,41(6):76-80.
[9]莫秋云.流体传动与控制[M].西安:西安电子科技大学出版社,2013.
[10]梁全,苏齐莹.液压系统AMESim计算机仿真指南[M].北京:机械工业出版社,2014.
[11]付永领,祁晓野.LMS Imagine.Lab AMESim系统建模和仿真参考手册[M].北京:北京航空航天大学出版社,2011.