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Influence of pavement unidirectional constraint on aircraft vibration response |
Dao-sheng LING1,2( ),Wen-jun SHENG1,Bo HUANG1,*( ),Yun ZHAO3 |
1. Institute of Geotechnical Engineering, Key Laboratory of Soft Soils and Geoenvironmental Engineering, Ministry of Education, Zhejiang University, Hangzhou 310058, China 2. School of Civil Engineering and Architecture, NingboTech University, Ningbo 315100, China 3. College of Civil Engineering and Architecture, Henan University of Technology, Zhengzhou 450001, China |
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Abstract A six-degree-of-freedom model of the aircraft with unidirectional constraint on pavement was established based on the B737-800 aircraft. The simulation calculation of aircraft taxiing were carried out on the pavement with single and stochastic uneven excitation respectively. Results show that, under the single uneven excitation input, the vibration response of the aircraft no longer changes monotonously with the wavelength and amplitude of the pavement deformation and the aircraft taxiing speed but the deformation model of the pavement, which is significantly different from that without considering the unidirectional constraint of pavement. The sensitive band of different taxiing speed is not the same. Under the stochastic uneven excitation input, the time when the wheels disengage from the pavement increases with the deterioration of pavement roughness. When the international roughness index of pavement is 3 m/km and the aircraft taxis at a speed of more than 70 m/s, and the taxing distance of the wheel separated from the pavement accounts for more than 1/4. The main frequency of the aircraft vibration response becomes lower, and the high-frequency vibration is greatly attenuated, and the vibration energy is concentrated to lower frequency. Between the two indexes for evaluating the roughness of pavement, the vertical maximum acceleration of the aircraft’s center of mass increases compared with that without considering the unidirectional constraint, while the root mean square of the vertical acceleration decreases because the downward acceleration response is weakened by the departure of the wheels from the pavement.
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Received: 25 September 2020
Published: 20 October 2021
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Fund: 国家重点基础研究发展计划资助项目(2014CB047005);国家自然科学基金资助项目 (51988101) |
Corresponding Authors:
Bo HUANG
E-mail: dsling@zju.edu.cn;cehuangbo@zju.edu.cn
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道面单向约束作用对飞机振动响应的影响
基于B737-800机型,建立道面单向约束的飞机六自由度模型,分别进行单个和随机不平整激励道面上飞机滑跑仿真计算. 结果表明:单个不平整激励输入下,机体振动响应与道面变形模式相关,不再随道面变形波长、幅值及飞机滑跑速度单调变化,与不考虑道面单向约束作用时有显著差异,且不同滑跑速度的敏感波段不相同. 在随机不平整激励输入下,机轮脱离道面时间随道面平整度劣化而增加. 当跑道国际平整指数为3 m/km时,飞机以超过70 m/s的速度滑跑,机轮可能脱离道面的滑跑距离占比超过1/4. 飞机振动响应主频变低、高频振动大幅衰减,振动能量向更低频集中. 在评价机场跑道平整度的2个指标中,机体质心竖向最大加速度相较于不考虑单向约束作用时有所增大,竖向加速度均方根因机轮脱离道面削弱负向加速度响应有所减小.
关键词:
机场道面,
单向约束作用,
动力响应分析,
平整度,
竖向加速度
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