基于多相机系统的大型飞机机翼结构静力测试非接触式整体三维变形测量

IF 3.8 2区 工程技术 Q1 ENGINEERING, MECHANICAL
Bingwei Zhu  (, ), Yan Liu  (, ), Zongyuan Lian  (, ), Yiqiu Cai  (, ), Hewei Zhu  (, ), Liqiang Gao  (, ), Qifeng Yu  (, )
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引用次数: 0

摘要

为了获得适航证书,必须进行全尺寸飞机静力试验。在此类测试中,准确、全面的机翼变形测量对于评估其强度、刚度和承载能力至关重要。本文提出了一种新颖、经济的视频测量方法,利用多相机系统实现了大型机翼结构整体静态变形的非接触、高精度、三维测量。为克服大视场摄像机在制作、携带和使用大型二维或三维目标标定时遇到的困难,提出了一种结合一维目标和极极几何的柔性立体摄像机标定方法。采用全站仪辅助的全局定标方法,统一各双目分系统的三维数据。利用10米长的大型机翼进行了一系列静载荷试验,以验证所提出的系统和方法。并将该方法应用于全尺寸民用飞机静态试验中翼展为33.6 m的两翼的实际机翼变形测量。该方法可以准确地获得被测机翼在各种载荷作用下的整体三维轮廓和位移数据。在所有负载情况下,在35m测量范围内,距离和位移测量的最大误差小于4.5 mm。结果表明,该方法实现了有效、高精度、现场化和可视化的机翼变形测量,为全尺寸飞机机翼静力测试提供了一种很有前景的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Non-contact overall 3D deformation measurement based on a multi-camera system for static testing of large aircraft wing structure

To obtain the certificate of airworthiness, it is essential to conduct a full-scale aircraft static test. During such test, accurate and comprehensive wing deformation measurement is crucial for assessing its strength, stiffness, and bearing capability. This paper proposes a novel and cost-effective videogrammetric method using multi-camera system to achieve the non-contact, high-precision, and 3D measurement of overall static deformation for the large-scale wing structure. To overcome the difficulties of making, carrying, and employing the large 2D or 3D target for calibrating the cameras with large field of view, a flexible stereo cameras calibration method combining 1D target and epipolar geometry is proposed. The global calibration method, aided by a total station, is employed to unify the 3D data obtained from various binocular subsystems. A series of static load tests using a 10-meter-long large-scale wing have been conducted to validate the proposed system and methods. Furthermore, the proposed method was applied to the practical wing deformation measurement of both wings with a wingspan of 33.6 m in the full-size civil aircraft static test. The overall 3D profile and displacement data of the tested wing under various loads can be accurately obtained. The maximum error of distance and displacement measurement is less than 4.5 mm within the measurement range of 35 m in all load cases. These results demonstrate that the proposed method achieves effective, high-accuracy, on-site, and visualized wing deformation measurement, making it a promising approach for full-scale aircraft wing static test.

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来源期刊
Acta Mechanica Sinica
Acta Mechanica Sinica 物理-工程:机械
CiteScore
5.60
自引率
20.00%
发文量
1807
审稿时长
4 months
期刊介绍: Acta Mechanica Sinica, sponsored by the Chinese Society of Theoretical and Applied Mechanics, promotes scientific exchanges and collaboration among Chinese scientists in China and abroad. It features high quality, original papers in all aspects of mechanics and mechanical sciences. Not only does the journal explore the classical subdivisions of theoretical and applied mechanics such as solid and fluid mechanics, it also explores recently emerging areas such as biomechanics and nanomechanics. In addition, the journal investigates analytical, computational, and experimental progresses in all areas of mechanics. Lastly, it encourages research in interdisciplinary subjects, serving as a bridge between mechanics and other branches of engineering and the sciences. In addition to research papers, Acta Mechanica Sinica publishes reviews, notes, experimental techniques, scientific events, and other special topics of interest. Related subjects » Classical Continuum Physics - Computational Intelligence and Complexity - Mechanics
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