留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于横向二次射流的水下推力矢量方法

耿令波 胡志强 林扬 衣瑞文 杨翊

耿令波, 胡志强, 林扬, 衣瑞文, 杨翊. 基于横向二次射流的水下推力矢量方法[J]. 航空动力学报, 2017, 32(8): 1922-1932. doi: 10.13224/j.cnki.jasp.2017.08.016
引用本文: 耿令波, 胡志强, 林扬, 衣瑞文, 杨翊. 基于横向二次射流的水下推力矢量方法[J]. 航空动力学报, 2017, 32(8): 1922-1932. doi: 10.13224/j.cnki.jasp.2017.08.016
Underwater thrust vectoring method based on cross second flow[J]. Journal of Aerospace Power, 2017, 32(8): 1922-1932. doi: 10.13224/j.cnki.jasp.2017.08.016
Citation: Underwater thrust vectoring method based on cross second flow[J]. Journal of Aerospace Power, 2017, 32(8): 1922-1932. doi: 10.13224/j.cnki.jasp.2017.08.016

基于横向二次射流的水下推力矢量方法

doi: 10.13224/j.cnki.jasp.2017.08.016
基金项目: 国家重点研发计划课题(2016YFC0301601)

Underwater thrust vectoring method based on cross second flow

  • 摘要: 提出一种基于横向二次射流的水下推力矢量技术,通过二次射流的横向速度场诱导主流发生偏转,建立了推力矢量偏角与流速偏角的数学关系,证明了通过主流偏转实现推力矢量偏转的有效性。通过数值计算方法分析了不同二次射流深度、不同二次射流/主流体积比及不同二次射流/主流速度比条件下主流偏转角度变化。结果显示:随着二次射流深度的增加,主流受到壁面阻碍作用增强,因而偏转角度减小。随着二次射流/主流体积比的减小,出口负压区所占比例减小,主流偏转角度增加,且当体积比减小到一定值后,负压影响可以忽略,主流不再随体积比而变化。主流偏转角度随速度比增加而增加,且在速度比一定的条件下,速度数值的变化对主流偏转没有影响。设计了一种主流为圆形射流的水下矢量推进器,对其数值分析结果揭示:当位于射流中剖面同侧的二次射流全部作动时,主流可以取得最大的偏转角度,且主流的偏转方向可以通过使不同的二次射流组合处于作动状态进行控制。

     

  • [1] 蒋新松,封锡盛,王棣棠.水下机器人[M].沈阳:辽宁科学技术出版社,2000.
    [2] 吴宝山,潘子英,陈纪军,等.潜艇组合翼舵的水动力非线性特性研究[J].船舶力学,2008,12(1):54-58.WU Baoshan,PAN Ziying,CHEN Jijun,et al.Investigation on nonlinear characteristics of normal force on stern- plane of submarine by CFD simulation[J].Journal of Ship Mechanics,2008,12(1):54-58.(in Chinese)
    [3] 郭春雨,杨晨俊,马宁.襟翼舵的敞水及桨后水动力性能研究[J].华中科技大学学报(自然科学版),2008,36(11):108-111.GUO Chunyu,YANG Chenjun,MA Ning.Research of the hydrodynamic performance of flap rudder on open water and behind propeller[J].Journal of Huazhong University of Science and Technology(Natural Science Edition),2008,36(11):108-111.(in Chinese)
    [4] 高富东,潘存云,杨政,等.多矢量推进水下航行器6自由度非线性建模与分析[J]机械工程学报,2011,47(5):93-100.GAO Fudong,PAN Cunyun,YANG Zheng,et al.Nonlinear mathematics modeling and analysis of the vectored thruster autonomous underwater vehicle in 6-DOF motions[J].Journal of Mechanical Engineering,2011,47(5):93-100.(in Chinese)
    [5] YOERGER D R,BRADLEY A M,WALDEN B B,et al.Surveying a subsea lava flow using the autonomous benthic explorer (ABE)[J].International Journal of Systems Science,1998,29(10):1031-1044.
    [6] WANG H H,ROCK S M,LEE M J,et al.OTTER:the design and development of an intelligent underwater robot[J].Autonomous Robots,1996,3(2):297-320.
    [7] YUH J.Design and control of autonomous underwater robots:a survey[J].Autonomous Robots,2000,8(1):7-24.
    [8] 魏东杰.水下机器人并联式矢量推进器设计与研究[D].天津:天津大学,2013.WEI Dongjie.Design and research of the underwater robot vectored thruster with parallel mechanism[D].Tianjin:Tianjin University,2013.(in Chinese)
    [9] NAWROT M T.Conceptual design of a thrust-vectoring tailcone for underwater robotics[R].Boston,MA:Massachusetts Institute of Technology,2012.
    [10] CAVALLO E,MICHELINI R C,FILARETOV V F,et al.Conceptual design of an AUV equipped with a three degrees of freedom vectored thruster[J].Journal of Intelligent and Robotic Systems,2004,39(4):365-391.
    [11] BA Xin,LUO Xiaohui,SHI Zhaocun,et al.A vectored water jet propulsion method for autonomous underwater vehicles[J].Ocean Engineering,2013,74(3),133-140.
    [12] 肖中云,顾蕴松,江雄,等.一种基于引射效应的流体推力矢量新技术[J].航空学报,2012,33(11):1966-1974.XIAO Zhongyun,GU Yunsong,JIANG Xiong,et al.A new fluidic thrust vectoring technique based on ejecting mixing effects[J].Acta Aeronautica et Astronautica Sinica,2012,33(11):1966-1974.(in Chinese)
    [13] 邓雄,夏智勋,罗振兵,等.合成双射流矢量特性影响因素分析[J].推进技术,2014,35(8):1131-1138.DENG Xiong,XIA Zhixun,LUO Zhenbing,et al.Analysis of impact factors on vectoring characteristic of dual synthetic jet actuator[J].Journal of Propulsion Technology,2014,35(8):1131-1138.(in Chinese)
    [14] 曹永飞,顾蕴松,程克明.基于被动二次流的射流偏转比例控制[J].航空学报,2015,36(3):757-763.CAO Yongfei,GU Yunsong,CHENG Keming.Proportional control of jet deflection with passive secondary flow[J].Acta Aeronautica et Astronautica Sinica,2015,36(3):757-763.(in Chinese)
    [15] 吴雄,张为华.固体火箭发动机二次喷射控制矢量喷管流场仿真[J].国防科技大学学报,2006,28(2):22-25.WU Xiong,ZHANG Weihua.Simulation of the flowfield in secondary injection vector control nozzle for solid rocket motor[J].Journal of National University of Defense Technolgy,2006,28(2):22-25.(in Chinese)
    [16] 陈著,单勇,沈锡钢,等.射流控制反推力装置流场数值研究[J].推进技术,2014,35(9):1181-1187.CHEN Zhu,SHAN Yong,SHEN Xigang,et al.Numerical study on thrust reverser controlled with secondary flow[J].Journal of Propulsion Technology,2014,35(9):1181-1187.(in Chinese)
  • 加载中
计量
  • 文章访问数:  888
  • HTML浏览量:  1
  • PDF量:  611
  • 被引次数: 0
出版历程
  • 收稿日期:  2016-07-26
  • 刊出日期:  2017-08-28

目录

    /

    返回文章
    返回