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

一种基于螺旋桨部件特性的螺旋桨建模方法

陈怀荣 王曦

陈怀荣, 王曦. 一种基于螺旋桨部件特性的螺旋桨建模方法[J]. 航空动力学报, 2017, 32(10): 2526-2535. doi: 10.13224/j.cnki.jasp.2017.10.027
引用本文: 陈怀荣, 王曦. 一种基于螺旋桨部件特性的螺旋桨建模方法[J]. 航空动力学报, 2017, 32(10): 2526-2535. doi: 10.13224/j.cnki.jasp.2017.10.027
A modeling method of propeller based on the propeller component characteristic[J]. Journal of Aerospace Power, 2017, 32(10): 2526-2535. doi: 10.13224/j.cnki.jasp.2017.10.027
Citation: A modeling method of propeller based on the propeller component characteristic[J]. Journal of Aerospace Power, 2017, 32(10): 2526-2535. doi: 10.13224/j.cnki.jasp.2017.10.027

一种基于螺旋桨部件特性的螺旋桨建模方法

doi: 10.13224/j.cnki.jasp.2017.10.027

A modeling method of propeller based on the propeller component characteristic

  • 摘要: 通过缩比法,利用螺旋桨通用部件特性获得期望研究的螺旋桨部件特性,提出了飞行速度不为零条件下的螺旋桨数学模型建模算法,同时,借鉴缩比后螺旋桨部件特性、螺旋桨定桨叶角工作性能曲线以及螺旋桨空气动力学原理,分析了静拉力状态下的螺旋桨功率系数、拉力系数、桨叶角、螺旋桨静态推力进距比阈值以及螺旋桨几何设计参数的相互作用关系,提出了静拉力状态下的螺旋桨数学模型建模算法。所述算法与Gas Turbine Simulation Program (GSP)软件仿真数据进行了数字仿真对比验证。结果表明:所提出的螺旋桨建模算法具有有效性,在前进状态下,螺旋桨拉力相对误差最大不超过6.6059×10-6,需求功率相对误差最大不超过5.5098×10-6,效率相对误差最大不超过6.6955×10-6。

     

  • [1] 张子东.A400M战术运输机简介及设计特点分析[J].航空科学技术,2006,17(2):16-19. ZHANG Zidong.Brief introduction and design features analysis of A400M tactical transport aircraft[J].Aeronautical Science and Technology,2006,17(2):16-19.(in Chinese)
    [2] 吴涛.欧罗巴之鹰A400M大型运输机全解析[J].现代兵器,2008(10):19-30. WU Tao.Complete analysis of A400M (nickname Europa Eagle) large transport aircraft[J].Modern Weaponry,2008(10):19-30.(in Chinese)
    [3] 周辉华.国外涡桨发动机的发展[J].航空科学技术,2013,24(1):18-22. ZHOU Huihua.Development of the abroad turbine propeller engine[J].Aeronautical Science and Technology,2013,24(1):18-22.(in Chinese)
    [4] KOCH L D.Design and performance calculations of a propeller for very high altitude flight[R].NASA TM-1998-206637,1998.
    [5] WEICK F E.Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies[R].NACA-TN-350,1930.
    [6] HARTMAN E P.Working charts for the determination of propeller thrust at various air speeds[R].NACA-TN-481,1934.
    [7] HARTMAN E P.A method of calculating the performance of controllable propellers with sample computations[R].NACA-TN-484,1934.
    [8] BIEMANN D,CONWAY R N.Propeller charts for the determination of the rotational speed for the maximum ratio of the propulsive efficiency to the special fuel consumption[R].NACA-TN-749,1940.
    [9] HEIDMANN M F,NOVIK D.Control considerations for optimum power proportionment in turbinepropeller engines[R].NACA-TN-17,1948.
    [10] 周盛,顾高墀,潘元杰,等.航空螺旋桨与桨扇[M].北京:国防工业出版社,1994.
    [11] 刘沛清.空气螺旋桨理论及其应用[M].北京:北京航空航天大学出版社,2006.
    [12] BURGER C,HARTFIED R,BURKHALTER J.Performance and noise optimization of a propeller using the vortexlattice method and a genetic algorithm[R].AIAA-2007-1883,2007.
    [13] HESS J L,VALAREZOT W O.Calculation of steady flow about propellers using a surface panel method[J].Journal of Propulsion and Power,1985,1(6):470-476.
    [14] SCHULTEN J B H M.Advanced propeller performancecalculation by a lifting surface method[J].Journal of Propulsion and Power,1996,12(3):477-485.
    [15] KONG C,ROH H.Steadystate performance simulation of pt6a62 turboprop engine using SIMULINK[J].International Journal of Turbo and Jet Engines,2003,20(2):183-194.
    [16] KONG C,ROH H,LIM K.Steadystate and transient simulation of turboprop engine using Simulink model[R].ASME Paper GT2003-38181,2003.
    [17] 邓志伟,黄向华,田超.涡桨发动机螺旋桨实时建模技术[J].航空动力学报,2014,29(2):434-440. DENG Zhiwei,HUANG Xianghua,TIAN Chao.Turboprop engine propeller realtime modeling techniques[J].Journal of Aerospace Power,2014,29(2):434-440.(in Chinese)
    [18] 田超.航空涡桨发动机建模与控制的仿真研究[D].南京:南京航空航天大学,2010. TIAN Chao.Simulation study of aeronautical turboprop engine modeling and control[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2010.(in Chinese)
    [19] HUANG Jiaqin,HUANG Xianghua,ZHANG Tianhong.Research on modeling of propeller in a turboprop engine[J].International Journal of Turbo and Jet Engines,2015,32(2):223-232.
    [20] 时培燕,毛宁,杨恒辉,等.涡桨发动机螺旋桨建模与控制系统设计研究[J].计算机测量与控制,2016,24(5):103-105. SHI Peiyan,MAO Ning,YANG Henghui,et al.Research on modeling and control system designing of turboprop engine propeller[J].Computer Measurement and Control,2016,24(5):103-105.(in Chinese)
  • 加载中
计量
  • 文章访问数:  661
  • HTML浏览量:  2
  • PDF量:  417
  • 被引次数: 0
出版历程
  • 收稿日期:  2016-03-21
  • 刊出日期:  2017-10-28

目录

    /

    返回文章
    返回