基于实测值的舰载机着舰下沉速度影响性分析

doi:10.7527/S1000-6893.2015.0097

固体力学与飞行器总体设计

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

基于实测值的舰载机着舰下沉速度影响性分析

冯蕴雯¹, 刘思宏¹, 薛小锋¹, 崔帅², 潘文廷³

1. 西北工业大学航空学院, 西安 710072;
2. 中国科学院上海微小卫星工程中心, 上海 200050;
3. 中国航空工业集团公司第一飞机设计研究院, 西安 710089

收稿日期:2014-12-02 修回日期:2015-04-02 出版日期:2015-11-15 发布日期:2015-04-27
通讯作者: 冯蕴雯,Tel.:029-88460383,E-mail:fengyunwen@nwpu.edu.cn E-mail:fengyunwen@nwpu.edu.cn
作者简介:冯蕴雯,女,博士,教授。主要研究方向:飞行器设计与可靠性设计。Tel:029-88460383,E-mail:fengyunwen@nwpu.edu.cn;刘思宏,女,硕士研究生。主要研究方向:飞行器结构设计。Tel:029-88492045,E-mail:shlove123@nwpu.edu.cn;薛小锋,男,博士,讲师。主要研究方向:飞行器设计与可靠性设计。Tel:029-88460383,E-mail:xuexiaofeng@mail.nwpu.edu.cn;崔帅,男,硕士,高级工程师。主要研究方向:飞行器可靠性。Tel:029-88460383,E-mail:cshuai@eyou.com;潘文廷,男,硕士,高级工程师。主要研究方向:飞机起落架强度。Tel:029-88460383,E-mail:panwenting@nwpu.edu.cn
基金资助:
国家自然科学基金(10577015);航空科学基金(2008ZA53006,2006ZD53050)

Sinking velocity impact analysis of carrier-based aircraft based on test data

FENG Yunwen¹, LIU Sihong¹, XUE Xiaofeng¹, CUI Shuai², PAN Wenting³

1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. Shanghai Engineering Center for Microsatellites, Chinese Academy of Sciences, Shanghai 200050, China;
3. The First Aircraft Institute, AVIC, Xi'an 710089, China

Received:2014-12-02 Revised:2015-04-02 Online:2015-11-15 Published:2015-04-27
Supported by:
National Natural Science Foundation of China (10577015);Aeronautical Science Foundation of China (2008ZA53006, 2006ZD53050)

摘要/Abstract

摘要：

舰载机的着舰下沉速度是起落架设计的重要输入,对起落架和机体的结构重量有很大影响。为了探索舰载机使用环境下各相关参数对下沉速度的影响,基于E-2C的实测着舰数据,将多元统计学的相关分析方法应用到舰载机着舰参数影响性分析,分析了17个着舰参数与着舰下沉速度的相关性。结果表明飞机下滑角、甲板俯仰角与下沉速度呈高度相关,舰上接合速度与下沉速度呈中度相关,这三者对下沉速度有很大影响;并进一步对这4个着舰参数进行非线性回归分析,拟合了E-2C着舰下沉速度的计算式,所得回归模型决定系数为0.991,平均绝对误差为1.66%,拟合效果很好。

关键词: 舰载机, 着舰, 起落架, 下沉速度, 影响性分析

Abstract:

The sinking velocity of carrier-based aircraft is an important input for landing gear design and has a great influence on the weight of the landing gear and airframe structure. Aimed at exploring the effect of the various related landing parameters on sinking velocity for carrier-based aircraft in the actual service environment and based on E-2C measured landing data, correlation analysis of multivariate statistics is applied to the impact analysis of landing parameters on sinking velocity. Seventeen landing parameters are analyzed in the compaction-analysis and the results show that aircraft glide path angle and deck pitch angle are highly correlated with sinking velocity; engaging velocity is moderately correlated with sinking velocity. These three parameters have a great influence on sinking velocity. Nonlinear regression analysis is carried out on the four landing parameters and a fitting equation of E-2C sinking velocity is obtained. The coefficient of determination of the regression model is 0.991 and the mean absolute error is 1.66%, thus the model provides a preferable fitting effect.

Key words: carrier-based aircraft, landing, landing gear, sinking velocity, impact analysis

中图分类号:

V214.1⁺3

冯蕴雯, 刘思宏, 薛小锋, 崔帅, 潘文廷. 基于实测值的舰载机着舰下沉速度影响性分析[J]. 航空学报, 2015, 36(11): 3578-3585.

FENG Yunwen, LIU Sihong, XUE Xiaofeng, CUI Shuai, PAN Wenting. Sinking velocity impact analysis of carrier-based aircraft based on test data[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(11): 3578-3585.

参考文献

[1] Duan P P. Analysis for carrier-based aircraft during landing process[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012(in Chinese).段萍萍.舰载飞机着舰过程动力学性能分析[D].南京:南京航空航天大学, 2012.
[2] Naval Air Systems Command. MIL-A-8863C(AS) Airplane strength and rigidity, ground loads for navy acquired airplanes[S]. Patuxent River, MD:Naval Air Systems Command, 1993.
[3] Naval Air Systems Command. JSSG-2006 Aircraft structures[S]. Patuxent River, MD:Naval Air Systems Command, 1998.
[4] Micklos R P. Carrier landing parameters from survey 45, fleet and training command aircraft landing aboard USS, Enterprise CVN-65(Appendices B through R)[R]. Warminster, PA:Naval Air Development Center, Warminster PA Air Vehicle and Crew Systems Technology Department, 1991.
[5] Geng J Z, Yao H L, Duan Z Y. Determining the approach speed envelope of carrier aircraft[J]. Engineering Sciences, 2013, 11(6):19-23.
[6] Lawrence J T, Draper-Donley M G. A review of min-imum control airspeed test methodologies for carrier-based aircraft[C]//2005 AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston:American Institute of Aeronautics and Astronautics Inc., 2005, 1:333-357.
[7] Wang Z Q, Sun X Y, Zhou S, et al. Dynamics analysis of aircraft landing on the pitching deck[J]. Key Engineering Materials, 2011, 467-469:579-582.
[8] Zhu Q D, Meng X, Zhang Z. Simulation research on motion law of arresting hook during landing[J]. Applied Mechanics and Materials, 2013, 300-301:997-1002.
[9] Lv K D, Zhu Q D, Li X F. Modeling and simulation for arrested landing of carrier-based aircraft[C]//2011 International Conference on Mechatronics and Automation (ICMA). Washington, D.C.:IEEE Computer Society, 2011:1928-1933.
[10] Wang Q S. A preliminary research of sinking velocity for carrier-based aircraft[J]. Aircraft Design, 2007, 27(3):1-6(in Chinese).王钱生.关于舰载机着舰下沉速度的初步研究[J].飞机设计, 2007, 27(3):1-6.
[11] Nie H, Peng Y M, Wei X H, et al. Overview of carrier-based aircraft arrested deck-landing dynamics[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1):1-12(in Chinese).聂宏,彭一明,魏小辉,等.舰载飞机着舰拦阻动力学研究综述[J].航空学报, 2014, 35(1):1-12.
[12] Yao N K, Sui F C, Wang C B. Free flight engagement condition of carrier-based aircraft[J]. Aircraft Design, 2011, 31(6):10-15(in Chinese).姚念奎,隋福成,王成波.舰载机的自由飞行钩住情况[J].飞机设计, 2011, 31(6):10-15.
[13] Xu D S, Wang L X, Jia Z R. Parameter matching characteristics of carrier-based aircraft during deck landing process[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(2):199-207(in Chinese).许东松,王立新,贾重任.舰载飞机着舰过程的参数适配特性[J].航空学报, 2012, 33(2):199-207.
[14] Li Q M, Feng Y W, Yu L M. Kinetics analysis and simulation of aircraft arrested shore-landing[J]. Computer Simulation, 2010, 27(1):27-31(in Chinese).李启明,冯蕴雯,于立明.飞机拦阻着陆动力学分析与仿真[J].计算机仿真, 2010, 27(1):27-31.
[15] Luo Q, Feng Y W, Feng Y S. Dynamic analysis and simulation of carrier aircraft arrested deck-landing based on kink-wave[J]. Journal of Mechanical Strength, 2009, 31(4):543-547(in Chinese).罗青,冯蕴雯,冯元生.基于弯折波的舰载机拦阻着舰动力学分析及仿真研究[J].机械强度, 2009, 31(4):543-547.
[16] Cui J H, Nie H, Zhang M, et al. Design optimization on shock absorbing performance of carrier-based aircraft landing gear[J]. Computer Aided Engineering, 2011, 20(1):88-93(in Chinese).崔俊华,聂宏,张明,等.舰载机起落架缓冲性能设计优化[J].计算机辅助工程, 2011, 20(1):88-93.
[17] Wei X H, Nie H. Study on landing impact force of carrier-based aircraft landing gears[J]. China Mechanical Engineering, 2007, 18(5):520-523(in Chinese).魏小辉,聂宏.舰载机起落架落震性能动力学仿真分析[J].中国机械工程, 2007, 18(5):520-523.
[18] Zhou S M. Simulation analysis on influence of carrier deck motion on carrier-based aircraft landing[J]. Aircraft Design, 2012, 32(6):28-32(in Chinese).周胜明.航母甲板运动对舰载机着舰影响仿真分析[J].飞机设计, 2012, 32(6):28-32.
[19] Xu D S, Liu X Y, Wang L X. Influence of carrier motion on landing safety for carrier-based airplanes[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(3):289-294(in Chinese).许东松,刘星宇,王立新.航母运动对舰载飞机着舰安全性的影[J].北京航空航天大学学报, 2011, 37(3):289-294.
[20] Li J M, Qi X E. Principle of statics[M]. Shanghai:Fudan University Press, 2014:333-341(in Chinese).李洁明,祁新娥.统计学原理[M].上海:复旦大学出版社, 2014:333-341.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

基于实测值的舰载机着舰下沉速度影响性分析

Sinking velocity impact analysis of carrier-based aircraft based on test data

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	胡伟, 万文章, 陈谋. 基于神经网络和干扰观测器的UAV自动着舰控制[J]. 航空学报, 2022, 43(S1): 726963-726963.
[2]	赵鲲, 梁俊彪, Ivan BELYAEV, Victor KOPIEV, Gareth BENNETT. 民用飞机起落架噪声及其控制技术研究进展[J]. 航空学报, 2022, 43(8): 26996-026996.
[3]	李跃明, 李晓云, 柴怡君, 杨雄伟. 飞机新牵引滑出方式下前起落架动响应分析[J]. 航空学报, 2022, 43(6): 526915-526915.
[4]	刘小川, 刘冲冲, 牟让科. 飞机起落架系统摆振动力学研究进展[J]. 航空学报, 2022, 43(6): 527063-527063.
[5]	李跃明, 李晓云, 柴怡君, 杨雄伟. 飞机新牵引滑出方式下前起落架动响应分析[J]. 航空学报, 2022, 43(6): 526915-526915.
[6]	杜晓琼, 李斌, 罗琳胤. 水陆两栖飞机高支柱起落架的刹车振动行为[J]. 航空学报, 2022, 43(6): 526199-526199.
[7]	万兵, 苏析超, 郭放, 韩维, 梁勇. 不确定性工时下甲板作业的前摄性鲁棒调度[J]. 航空学报, 2022, 43(12): 325971-325971.
[8]	鄢荣, 何逸文, 李凯翔, 李鹏, 牟让科, 史爱明. 起落架开舱构型自激振荡预测公式改进与分析[J]. 航空学报, 2022, 43(12): 226140-226140.
[9]	王霄, 程健慧, 沈天荣, 许保成, 孟轩. 舰面飞机尾喷流对进气道温度场影响的仿真分析[J]. 航空学报, 2021, 42(8): 525795-525795.
[10]	陈跃良, 陈亮, 卞贵学, 杨翔宁, 管宇, 张勇, 何刚. 先进舰载战斗机腐蚀防护控制与日历寿命设计[J]. 航空学报, 2021, 42(8): 525786-525786.
[11]	刘东, 吴家仁, 周一舟, 刘振祥, 李瑜, 王铭泽. 舰载机综合保障技术实践及发展展望[J]. 航空学报, 2021, 42(8): 525802-525802.
[12]	王永庆. 固定翼舰载战斗机关键技术与未来发展[J]. 航空学报, 2021, 42(8): 525859-525859.
[13]	梁磊, 肖静, 詹光, 苏大林. 考虑杆臂效应与挠曲变形的全自动着舰技术[J]. 航空学报, 2021, 42(8): 525841-525841.
[14]	王永庆, 于浩, 施岩. 舰载机滑跃起飞动力学与运动学特性[J]. 航空学报, 2021, 42(8): 525853-525853.
[15]	张志冰, 张秀林, 王家兴, 史静平. 一种基于多操纵面控制分配的IDLC人工着舰精确控制方法[J]. 航空学报, 2021, 42(8): 525840-525840.