基于飞行参数的舰载机拦阻力统计建模与预计

doi:10.7527/S1000-6893.2020.24030

固体力学与飞行器总体设计

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基于飞行参数的舰载机拦阻力统计建模与预计

蒋启登

中国飞行试验研究院飞机所, 西安 710089

收稿日期:2020-03-28 修回日期:2020-06-16 发布日期:2020-08-21
通讯作者: 蒋启登 E-mail:2623670635@qq.com
基金资助:
省部级项目

Statistical modeling and prediction of arresting force for carrier-based aircraft based on flight parameters

JIANG Qideng

Aircraft Flight Test Technology Institute, Chinese Flight Test Establishment, Xi'an 710089, China

Received:2020-03-28 Revised:2020-06-16 Published:2020-08-21
Supported by:
Ministry Level Project

摘要/Abstract

摘要： 拦阻钩是舰载飞机最重要的特征部件之一，对其受载进行测量、统计建模与预计具有重要的工程意义。在飞机拦阻动力学分析基础上确定了飞行数据统计建模所需的关键参数，结合某型机载荷试飞、机舰适配性试验，实测研究了飞机拦阻实际受载特点，采用线性或非线性方法统计建立了最大拦阻力与常规飞行参数之间的拟合函数关系，并得到了最大拦阻力的预计模型。建模、验模与预计结果表明，所选关键参数合理，能够充分反映拦阻钩的受载及其主要影响因素，采用纵向过载、啮合速度和发动机高压转速等参数建立的拦阻载荷统计模型可用于拦阻着陆或着舰试验时最大拦阻力的有效预测。

关键词: 舰载飞机, 拦阻钩, 舰载适应性陆上试验, 飞行实测, 拦阻力, 统计建模与预计

Abstract: Measuring, modeling and predicting the arresting hook load statistically is both important and urgent for carrier-based aircraft flight tests, such as landing gear structure verification and carrier suitability certification. After dynamics analysis of an arresting hook engaged in a cable, key flight data from the arresting hook load test and the carrier suitability test was selected and used as the input and output of our statistical modeling and prediction. The results show that the arresting hook load model based on the relative engaging speed and engine rotational speed can calculate and predict the maximum load successfully and effectively from the interaction process between the arresting hook and the cable.

Key words: carrier-based aircraft, arresting hooks, land-based carrier suitability tests, flight investigation, arresting force, statistical modeling and prediction

中图分类号:

蒋启登. 基于飞行参数的舰载机拦阻力统计建模与预计[J]. 航空学报, 2020, 41(12): 224030-224030.

JIANG Qideng. Statistical modeling and prediction of arresting force for carrier-based aircraft based on flight parameters[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 224030-224030.

参考文献

[1] 飞机设计手册总编委会. 飞机设计手册:起飞着陆系统设计[M]. 北京:航空工业出版社, 2002:271-280. The Chief Committee of Aircraft Design Manual. Aircraft design manual:Takeoff and landing system[M]. Beijing:Aviation Industry Press, 2002:271-280(in Chinese).
[2] 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):1-10. 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):1-10(in Chinese).
[3] LYLE W J. Development of curves for estimating aircraft arresting hook loads:ADA119551[R]. California:Edwards Air Force Base, 1982.
[4] HSIN C C. Arrested landing studies for stol Aircraft:AIAA-1973-51[R].Reston:AIAA,1973.
[5] BILLEC W. The effect of deck span upon arresting gear performance:AD813761[R]. New Jersey:Naval Air Test Facility, 1967.
[6] BILLEC W B, SILLEN W B. Dynamic performance of a Mark7 Mod1 arresting system using 24-inch and 28-inch PD fair-lead sheaves:0454384[R]. New Jersey:Naval Air Test Facility, 1966.
[7] WILSON T. F-35 Carrier suitability testing[C]//AIAA AVIATION Forum, Atlanta, Georgia. 2018 Aviation Technology, Integration, and Operations Conference.Reston:AIAA, 2018.
[8] Naval Air Systems Command. Catapulting and arresting gear forcing functions for aircraft structural design:MIL-STD-2066[S]. 1981.
[9] Naval Air Systems Command. Arresting hook installation-AIRCRAFT:MIL-A-18717C[S].1993.
[10] 高泽迥. 飞机拦阻钩振动运动学和拦索动力学研究[J]. 航空学报, 1990, 11(12):B543-B548. GAO Z J. A discussion of bounce kinematics of aircraft arresting hook and cable dynamics[J]. Acta Aeronautica et Astronautica Sinica, 1990, 11(12):B543-B548(in Chinese).
[11] 张萍, 金栋平. 计及弯折波的舰载机拦阻过程控制[J]. 航空学报,2011, 32(11):2008-2015. ZHANG P, JIN D P. Control of arresting process for carrier aircraft considering kink-wave[J].Acta Aeronautica et Astronautica Sinica, 2011, 32(11):2008-2015(in Chinese).
[12] 张鑫, 李玉龙, 刘元镛,等. 飞机对中和偏心拦阻钩索动力学分析[J]. 机械强度, 2008, 30(4):549-554. ZHANG X, LI Y L, LIU Y Y, et al. Arresting hook and cable dynamics of aircraft arrest landing on or off center[J]. Journal of Mechanical Strength, 2008, 30(4):549-554(in Chinese).
[13] 金长江, 洪冠新. 舰载机弹射起飞及拦阻着舰动力学问题[J]. 航空学报, 1990, 11(12):B534-B542. JIN C J, HONG G X. Dynamic problems of carrier aircraft catapult launching and arrest landing[J]. Acta Aeronautica et Astronautica Sinica, 1990, 11(12):B534-B542(in Chinese).
[14] 胡孟权, 林国华. 舰载飞机着舰拦阻动力学分析[J]. 空军工程大学学报:自然科学版, 2000, 1(5):8-11. HU M Q, LIN G H. Arresting dynamics research of carrier aircraft[J]. Journal of Air Force Engineering University:Natural Science Edition, 2000, 1(5):8-11(in Chinese).
[15] 徐东松, 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):200-205. 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):200-205(in Chinese).
[16] 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):27-29. LI Q M, FENG Y W, YU L M. Kinetics analysis simulation of aircraft arrested shore-landing[J]. Computer Simulation, 2010, 27(1):27-29(in Chinese).
[17] 徐彦军, 沈文厚, 孙岩. 舰载机拦阻着舰纵向载荷的简化算法[J]. 飞机设计, 2009, 29(13):32-33. XU Y J, SHEN W H, SUN Y. A simple calculation to carrier landing load[J]. Aircraft Design, 2009, 29(13):32-33(in Chinese).
[18] 王海东, 杨炳恒, 毕玉泉,等. MK7-3型拦阻装置缓冲系统动力学分析[J]. 舰船科学技术, 2011, 33(3):142-143. WANG H D, YANG B H, BI Y Q, et al. Analysis on dynamics of MK7-3 arresting gear's damper system[J]. Ship Science and Technology, 2011, 33(3):142-143(in Chinese).
[19] 彭一明, 聂宏, 张明,等. 偏航状态下拦阻钩挂索动力学分析[J]. 航空学报, 2015, 36(6):1876-1884. PENG Y M, NIE H, ZHANG M, et al. Dynamics analysis of arresting hook following engagement of an arresting cable in yaw condition[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(6):1876-1884(in Chinese).
[20] 张声伟, 段卓毅, 耿建中,等. 阻拦索断裂对螺旋桨舰载机着舰安全影响数值分析[J]. 航空学报, 2019, 40(4):622293. ZHANG S W, DUAN Z Y, GENG J Z, et al. Numerical analysis of the effect of block cable crack on landing safety of propeller carrier-based aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(4):622293(in Chinese).
[21] 闵强, 王斌团, 王亚芳,等. 舰载机拦阻着舰载荷谱编制技术[J]. 航空学报, 2019, 40(4):622284. MIN Q, WANG B T, WANG Y F, et al. Compiling load spectrum method for arrested deck-landing of carrier-based aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(4):622284(in Chinese).
[22] 熊文强, 张闰, 张晓晴,等. 舰载无人机拦阻着舰中机身冲击响应分析[J]. 航空学报, 2019, 40(12):222892. XIONG W Q, ZHANG R, ZHANG X Q, et al. Analysis of impact response of mid-fuselage ground arresting in a carrier-based UAV[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(12):222892(in Chinese).
[23] 杨全伟. 舰载飞机拦阻钩载荷实测方法研究[J]. 航空学报, 2015, 36(4):1162-1168. YANG Q W. Research on flight measuremen method of a carrier-based aircraft arresting hook loads[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(4):1162-1168(in Chinese).
[24] WATTERS K C, ATCLIFFE P. Calibration of mirage main undercarriage to determine wheel loads from measured strains:ARL-STRUC-TECH-MEMO-300[R]. Commonwealth of Australia, 1979.
[25] RICHARD D L, IWAN P. Stepwise regression analysis of MDOE balance calibration data acquired at DNW:AIAA-2007-144[R].Reston:AIAA,2007.

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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

基于飞行参数的舰载机拦阻力统计建模与预计

Statistical modeling and prediction of arresting force for carrier-based aircraft based on flight parameters

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[8]	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.
[9]	叶舸, 田兆锋, 闫楚良. 基于OpenGL的飞机飞行实测数据可视化研究[J]. 航空学报, 2011, 32(6): 1050-1057.
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[11]	柳刚;聂宏. 拦阻钩初次碰撞道面反弹动力学[J]. 航空学报, 2009, 30(9): 1672-1677.
[12]	柳刚;聂宏. 飞机拦阻钩碰撞动力学和拦阻钩纵向阻尼器性能[J]. 航空学报, 2009, 30(11): 2093-2099.
[13]	余勇;杨一栋. 侧向甲板运动补偿技术研究[J]. 航空学报, 2003, 24(1): 69-71.
[14]	高泽迥. 飞机拦阻钩振动运动学和拦索动力学研究[J]. 航空学报, 1990, 11(12): 543-548.