舰载飞机拦阻钩载荷实测方法研究

doi:10.7527/S1000-6893.2014.0334

Abstract

Abstract:

For the purpose of complete flight test mission of a carrier-based aircraft, its arresting hook loads are measured using strain gage. A three-direction (longitudinal, lateral and vertical directions) load model of arresting hook is built through analyzing the loads in the arrest deck-landing process. Strain gages are designed and installed on the arresting hook. Ground calibration tests are implemented and load equations are constructed. Some typical loads of arresting hook in the process of carrier-based aircraft arrest deck-landing are also presented in detail, and the arresting energy and efficiency of arresting gear equipment are studied. Moreover, compared with the loads obtained by an ordinary single-direction load model, the three-direction load model is discussed. The results show that the load model and measurement methods are correct and credible, which can provide some references for the engineering practice.

Key words: flight test, flight measurement of load, carrier-based aircraft, arresting hook, arrest deck-landing, strain-gage bridge

CLC Number:

V217⁺.32

YANG Quanwei. Research on flight measurement method of a carrier-based aircraft arresting hook loads[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1162-1168.

References

[1] 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.
[2] Liu G, Nie H. Dynamics of bounce of aircraft arresting hook impacting with deck and performance of arresting hook longitudinal damper[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(11): 2093-2099 (in Chinese). 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.
[3] Gao Z J. A discussion of bounce kinematics of aircraft arresting hook and cable dynamics[J]. Acta Aeronautica et Astronautica Sinica: Series B, 1990, 11(12): B543-B546 (in Chinese). 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: B辑, 1990, 11(12): B543-B546.
[4] Dodd A. TF89 design project airbrake and arrester hook design[D]. Cranfield: Cranfield Institute of Technology, 1990: 26-29.
[5] Zhang X. Dynamic analysis and simulation of carrier aircraft arrested deck-landing[D]. Xi'an: Northwestern Polytechnical University, 2007 (in Chinese). 张鑫. 舰载机拦阻着舰动力学分析及仿真[D]. 西安: 西北工业大学, 2007.
[6] Gurney T, Morley F. F/A-18E/F initial sea trials[R]. Lancaster, CA: The Society of Experimental Test Pilots, 1997: 18-19.
[7] Jones L W. Development of curves for estimating aircraft arresting hook loads[R]. Los Angeles,CA: Edwards Air Force Base, 1982: 11-18.
[8] Webb G J. Carrier suitability testing[R]. Lancaster, CA: The Society of Experimental Test Pilots, 1997: 289-291.
[9] Navy Air Engineering Center. MIL-STD-2066 Milltary standard: catapulting and arresting gear forcing functions for aircraft structural design[S]. Patuxent River, MD: Naval Air Systems Command, 1981.
[10] MIL-A-8863C. Airplane strength and rigidity, ground loads for carrier-based aircraft[S]. Patuxent River, MD: Naval Air Systems Command, 1993.
[11] Zhang Z K, Nie H, Yu H, et al. Dynamics analysis for aircraft arresting with yawing and off-center[J]. Advances in Aeronautical Science and Engineering, 2010, 1(4): 327-332 (in Chinese). 张卓坤, 聂宏, 于浩, 等. 飞机着舰偏心偏航拦阻动力学分析[J]. 航空工程进展, 2010, 1(4): 327-332.
[12] The Committee of National Defense Science, Technology and Industry. GJB 67.4A—2008 Military airplane structural strength specification Part10: Flight tests[S]. Beijing: Department of Military Standard Press, The Commission of National Defense Science, Technology and Industry, 2008: 7-8 (in Chinese). 国防科学技术工业委员会. GJB67.4A—2008 军用飞机结构强度规范第10部分:飞行试验[S]. 北京: 国防科学技术工业委员会军标出版发行部, 2008: 7-8.
[13] The Committee of National Defense Science, Technology and Industry. GJB1015A—2008 Military airplane demonstration requirements[S]. Beijing: Department of Military Standard Press, The Commission of National Defense Science, Technology and Industry, 2008: 12-13 (in Chinese). 国防科学技术工业委员会. GJB1015A—2008 军用飞机验证要求. 北京: 国防科学技术工业委员会军标出版发行部, 2008: 12-13.
[14] Kliqko M T, Aphaytob E B. Aircraft strength flight test-static load[M]. Tang J C, translated. Xi'an: ASST System Engineering Office of Ministry of Aeronautics and Astronautics, 1992: 1-31 (in Chinese). М. Д. 克利亚奇科, Е. В. 阿尔纳乌托夫.飞机强度飞行试验-静载荷[M]. 汤吉晨,译. 西安: 航空航天部《ASST》系统工程办公室, 1992: 1-31.
[15] Skopinski T H, Aiken W S, Jr, Huston W B. Calibration of strain-gage installations in aircraft structures for the measurement of flight loads, NACA Report 1178[R]. Washington, D.C.: Langley Aeronautical Laboratory, NASA, 1953.
[16] Yang Q W, He F D, Wang W J, et al. The linear transformation and robustness in load measurement of aircraft landing gear[J]. Chinese Journal of Applied Mechanics, 2013, 30(4): 608-612 (in Chinese). 杨全伟, 何发东, 汪文君, 等. 飞机起落架载荷测量中的线性变换与鲁棒性[J]. 应用力学学报, 2013, 30(4): 608-612.
[17] Yi D H.Statistical forecast:methods and applications[M]. Beijing: China Statistics Press, 2001: 17-18 (in Chinese). 易丹辉. 统计预测-方法与应用[M]. 北京: 中国统计出版社, 2001: 17-18.
[18] Yang Y D. Review of the carrier approach criteria[M]. Beijing: National Defence Industry Press, 2006: 76-77 (in Chinese). 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.
[19] Luo Q, Feng Y W, Feng Y S, et al. Dynamic analysis and simulation of carrier aircraft arrested decked 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, 等. 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.
[20] Liang L H, Wan C, Xun P P. Study on the dynamic performance of aircraft arresting cable[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(4): 833-839 (in Chinese). 梁利华, 万晨, 荀盼盼. 飞机拦阻索动态特性研究[J]. 航空学报, 2013, 34(4): 833-839.

Research on flight measurement method of a carrier-based aircraft arresting hook loads

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Yahui SONG, Gaoyu FAN, Lixia QU, Yuelin ZHANG, Yue XU, Shuo HAN. Progress of aircraft sonic boom flight test measurement technology: Review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626186-626186.
[2]	ZHAO Kun, LIANG Junbiao, Ivan BELYAEV, Victor KOPIEV, Gareth BENNETT. Review of civil airplane landing gear noise study and its control approaches [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 26996-026996.
[3]	CEN Fei, LIU Zhitao, JIANG Yong, GUO Tianhao, ZHANG Lei, KONG Yinan. Unsteady aerodynamics modeling of civil transport configuration under extreme flight conditions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125582-125582.
[4]	ZHOU Yitao, YANG Yang, WU Zhigang, YANG Chao. Flight test for gust alleviation on a high aspect ratio UAV platform [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526126-526126.
[5]	CHEN Guangqiang, DOU Guohui, WEI Haogong, ZOU Xin, LI Qi, LIU Zhou, ZHOU Weijiang. Air data sensing technology of Mars probe [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 626619-626619.
[6]	WANG Meng, LI Yujun, ZHAO Ronghuan, ZHONG Hongjie. Transition detection technique for wide speed range by means of on-line heating coating [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526820-526820.
[7]	ZHOU Zhenyao, LYU Fei, ZHOU Bin, YANG Zhao. Verification method for natural laminar flow drag reduction and layout design of test section [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526751-526751.
[8]	WANG Hao, ZHONG Min, HUA Jun, ZHONG Hai, YANG Tihao, WANG Meng, LEI Guodong. Simulation and experiment of natural laminar flow flight test wing glove [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526785-526785.
[9]	CHEN Yifu, WANG Yiwen, DENG Yiju, WANG Bo, BAI Junqiang, LU Lei. Experiment and numerical simulation of natural laminar flow wing glove [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526793-526793.
[10]	DENG Yiju, DUAN Zhuoyi, AI Mengqi. Status and development of laminar flow wing design technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526778-526778.
[11]	YANG Chao, QIU Qisheng, ZHOU Yitao, WU Zhigang. Review of aircraft gust alleviation technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527350-527350.
[12]	FU Junquan, SHI Zhiwei, GENG Xi, ZHU Jiachen, WANG Lishuang, WU Dawei, PAN Lijun. Longitudinal stability of blended-wing-body aircraft based on experimental bifurcation analysis [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 124931-124931.
[13]	FU Jiawei, YU Jialong, LIU Chao, WANG Muguo, WANG Zizi. Key technologies of aerodynamics design of stealth carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525804-525804.
[14]	WANG Xiao, CHENG Jianhui, SHEN Tianrong, XU Baocheng, MENG Xuan. Numerical simulation research of influence of wake flow field on inlet temperature field of carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525795-525795.
[15]	CHEN Yueliang, CHEN Liang, BIAN Guixue, YANG Xiangning, GUAN Yu, ZHANG Yong, HE Gang. Corrosion protection control and calendar life design of advanced carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525786-525786.