舰载机全机落震试验方法
收稿日期: 2016-05-10
修回日期: 2016-11-09
网络出版日期: 2016-11-30
基金资助
国家级项目
Test method for full scale drop of carrier-based aircraft
Received date: 2016-05-10
Revised date: 2016-11-09
Online published: 2016-11-30
Supported by
National Level Project
豆清波 , 杨智春 , 刘小川 , 牟让科 , 杨海 . 舰载机全机落震试验方法[J]. 航空学报, 2017 , 38(3) : 220421 -220421 . DOI: 10.7527/S1000-6893.2016.0294
Full scale aircraft drop test provides an important tool for testing the dynamic load and dynamic response of the aircraft structure and studying the function reliability under impact situation in a laboratory environment. An approach for full scale aircraft drop test is proposed in this paper. Solutions to critical technique issues arising in the testing process such as wing lift simulation, aircraft sinking speed control, aircraft horizontal velocity simulation and aircraft dynamic load testing are also derived. The feasibility and effectiveness of the test method is verified by the full scale aircraft drop test system. The test method proposed can be used for testing the dynamic load and response of carrier-based aircraft landing vibration, providing reliable test data for the design of carrier-based aircraft.
Key words： carrier-based aircraft; test; full scale aircraft; loads; dynamics
[1] 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. 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).
[2] 魏小辉, 聂宏. 舰载机着舰减震新技术研究[J]. 航空学报, 2007, 28(2):324-327. WEI X H, NIE H. New method of attenuating landing impact force on carrier-based aircraft landing gear[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(2):324-327(in Chinese).
[3] YACKLE A R. STOVL aircraft for shipboard operation:AIAA-1992-4215[R]. Reston:AIAA, 1992.
[4] RYBERG E S. The influence of ship configuration on the design of the joint strike fighter:ADA399988[R]. Arlington, VA:Joint Strike Fighter Program Office, 2002.
[5] 刘锐琛, 苏开鑫, 邵永起, 等.飞机起落架强度设计指南[M]. 成都:四川科学技术出版社, 1989:781-795. LIU R C, SU K X, SHAO Y Q, et al. Strength design guide of aircraft landing gear[M]. Chengdu:Sichuan Science and Technology Press, 1989:781-795(in Chinese).
[6] 飞机设计手册总编委会. 飞机设计手册14:起飞着陆系统设计[M]. 北京:航空工业出版社, 2002:95-102. Committee of Aircraft Design Manual. Aircraft design manual Book 14:Taking-off and landing devices design[M]. Beijing:Aviation Industry Press, 2002:95-102(in Chinese).
[7] 王钱生.舰载机总体设计主要关键技术概述[J]. 飞机设计, 2005(2):6-10. WANG Q S. Critical technologies in carrier-based aircraft design and development[J]. Aircraft Design, 2005(2):6-10(in Chinese).
[8] 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:B辑, 1990, 11(12):B534-B542. JIN C J, HONG G X. Dynamic problems of carrier aircraft catapult launching and arresting landing[J]. Acta Aeronautica et Astronautica Sinica:Series B, 1990, 11(12):B534-B542(in Chinese).
[9] 姚念奎, 隋福成, 王成波. 舰载机的自由飞行勾住情况[J]. 飞机设计, 2011, 31(6):10-15. 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).
[10] Naval Air Systems Command. Airplane strength and rigidity, general specification for:MIL-A-8860[S]. Patuxent River, MD:Naval Air Systems Command, 1987.
[11] Naval Air Systems Command.Airplane strength and rigidity, ground loads for carrier-based aircraft:MIL-A-8863(ASG)[S]. Patuxent River, MD:Naval Air Systems Command, 1960.
[12] Naval Air Systems Command. Airplane structures:JSSG-2006[S]. Patuxent River, MD:Naval Air Systems Command, 1998.
[13] 杨一栋. 舰载机进场着舰规范评估[M]. 北京:国防工业出版社, 2006:76-77. YANG Y D. Review of the carrier approach criteria[M]. Beijing:National Defense Industry Press, 2006:76-77(in Chinese).
[14] 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, 2012:16-25. DUAN P P. Investigation on dynamic performance analysis for carrier-based aircraft during landing process[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012:16-25(in Chinese).
[15] 魏小辉, 聂宏. 基于降落区概念的飞机起落架着陆动力学分析[J]. 航空学报, 2005, 26(1):8-12. WEI X H, NIE H. Analysis of landing impact force of aircraft landing gears based on the conception of landing area[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(1):8-12(in Chinese).
[16] 魏榕祥, 陈国平, 何欢, 等.轻型飞机全机水平撞击试验装置设计研究[J]. 机械科学与技术, 2012, 31(2):219-223. WEI R X, CHEN G P, HE H, et al. Horizontal crash testing facility design of light aircraft[J]. Mechanical Science and Technology for Aerospace Engineering, 2012, 31(2):219-223(in Chinese).
[17] 豆清波, 杨武刚, 牟让科, 等. 无人机全机着陆试验系统设计及应用[J]. 机械科学与技术, 2014, 33(1):146-150. DOU Q B, YANG W G, MU R K, et al. The design and application of UAV landing test system[J]. Mechanical Science and Technology for Aerospace Engineering, 2014, 33(1):146-150(in Chinese).
[18] 齐丕骞, 牟让科. 飞机起落架缓冲性能分析、试验、设计一体化技术[J]. 航空学报, 1998, 19(3):332-334. QI P Q, MU R K. Integration of shock absorber performance analysis test and design of aircraft landing gears[J]. Acta Aeronautica et Astronautica Sinica, 1998, 19(3):332-334(in Chinese).
[19] 史海文. 摇臂式、支柱式起落架缓冲参数的研究[J]. 航空学报, 1987, 8(12):B625-B629. SHI H W. A research in shock parameters of rock arm landing gear and telescopic landing gear[J]. Acta Aeronautica et Astronautica Sinica, 1987, 8(12):B625-B629(in Chinese).
[20] 史海文, 张大千, 杨树勋. 摇臂式、支柱式起落架起转、回弹载荷系数的落震试验研究[J]. 飞机设计, 2000(1):40-44. SHI H W, ZHANG D Q, YANG S X. A research in spin-up and spring back drag loads coefficient of rock arm landing gear and telescopic landing gear on drop test[J]. Aircraft Design, 2000(1):40-44(in Chinese).
[21] 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. WANG Q S. A preliminary research of sinking velocity for carrier-based aircraft[J]. Aircraft Design, 2007, 27(3):1-6(in Chinese).
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