曲柄滑块拦阻器设计与动力学仿真

PDF(1404 KB)

振动与冲击 ›› 2020, Vol. 39 ›› Issue (22) : 243-247.

论文

曲柄滑块拦阻器设计与动力学仿真

史炎1，史天成2

作者信息 +

Design and simulation of crank slider arresters

SHI Yan1， SHI Tiancheng2

Author information +

文章历史 +

摘要

介绍了一种新型液压缓冲拦阻器原理，制造工艺与活塞发动机一样，拦阻距离不受限。按照流体力学理论建立了拦阻力、空气阻力、飞机升力数学模型，利用SIMPACK软件建立了统一的动力学模型。根据国内文献对MK7-3型拦阻器性能的研究成果，对比分析了舰载机以不同重量、速度着舰的拦阻动力学过程，仿真结果表明：所设计的曲柄滑块拦阻器动力学性能良好，既能进行定长拦阻也能进行自由拦阻。

Abstract

The principle of a new type hydraulic arresting gear was introduced, which has the same manufacturing process as the piston engine while its arresting distance is not limited.The mathematical models for the arresting force, air resistance and aircraft lift were established according to the theory of fluid mechanics, and then a unified dynamic model was established by SIMPACK software.According to the domestic literature about the MK7-3 type arresting gear performance research results, a comparative analysis of arresting kinetic processes under different aircraft weight and landing velocity was carried out.The simulation results show that the crank slider damper has good dynamic performance, which is able to perform both the fixed-length arresting and the free arresting.

导出引用

史炎1，史天成2. 曲柄滑块拦阻器设计与动力学仿真[J]. 振动与冲击, 2020, 39(22): 243-247

SHI Yan1， SHI Tiancheng2. Design and simulation of crank slider arresters[J]. Journal of Vibration and Shock, 2020, 39(22): 243-247

参考文献

[1] 柳刚,聂宏,任志勇,贾锦,任国贤. 舰载型拦阻装置拦阻性能分析[J]. 中国机械工程,2014,25(09):1244-1249+1255.
LIU G, NIE H, Ren Z Y, et al. Analysis on Arresting Performance of Carrier-based Arresting Device [J]. China Mechanical Engineering,2014,25(09):1244-1249+1255(in Chinese).
[2] 杨茂胜,毕玉泉,陈跃良, 等. 简析阻拦索装置定长冲跑控制阀[J]. 海军航空工程学院学报,2012,27(02):223-227.
YANG M S, BI Y Q, CHEN Y L, et al. Research on Working Principle and Familiar Trouble of the Constant Runout Valve for the Arresting Gear[J].Journal of Naval Aeronautical Engineering Institute,2012,27(02):223-227 (in Chinese).
[3] 吴建斌. 液压减振器结构参数对性能的影响[D].西南交通大学,2015.
Wu J B. The nfluence of hydraulic damper’s structure parameters on its perforance [D]. Southwest Jiaotong University, 2015(in Chinese).
[4] 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.
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).
[5] 王玮, 郭慧杰, 孟跃. 卫星/伪卫星/惯性组合着舰导引算法[J]. 系统工程与电子技术, 2017, 39(2):391-397.
WANG W, GUO H J, MENG Y .Satellite/pseudolite/INS integrated navigation algorithm[J].Systems Engineering and Electronics, 2017, 39(2):391-397(in Chinese).
[6] 姚海林, 耿建中, 赵一飞. 舰载飞机拦阻着舰建模与仿真研究[J]. 系统仿真技术, 2016, 12(1):18-23.
YAO H L, GENG J Z, ZHAO Y F .Carrier-based Airplane Landing Modeling and Simulation Research [J].System Simulation Technology, 2016, 12(1):18-23(in Chinese).
[7] 高俊东,崔帅,冯蕴雯,薛小峰. 舰载机蒸汽弹射器热力学仿真分析[J]. 机械科学与技术,2013,32(07):963-967.
GAO J D, CUI S , FENG Y W, et al. Simulation and Analysis of Thermodynamics for Carrier-based Aircraft Steam Catapult[J]. Mechanical Science and Technology,2013,32(07):963-967 (in Chinese).
[8] 张明晖, 袁理, 洪冠新. 航空母舰液压拦阻系统拦阻力建模与仿真[J]. 北京航空航天大学学报, 2010, 36(1):100-103.
ZHANG M H, YUAN L, HONG G X. Aircraft carrier hydraulic arresting gear arresting force modeling and simulation [J]. Journal of Beijing University of Aeronautics and Astronautics,2010,36（1）：100-103(in Chinese).
[9] 朱齐丹, 闻子侠, 张智. 阻拦系统动力学建模与仿真[J]. 航空学报, 2012, 33(3):520-529.
ZHU Q D, WEN Z X, ZHANG Z. Kinetic Modeling and Simulation of Shipboard Arresting System[J]. Acta Aeronautica ET Astronautica Sinica, 2012, 33(3):520-529 (in Chinese).