变体飞行器柔性复合蒙皮植入式光纤形状传感

张雄雄; 宋言明; 孟凡勇; 孙广开; 祝连庆

doi:10.3788/IRLA201948.0622003

变体飞行器柔性复合蒙皮植入式光纤形状传感

doi: 10.3788/IRLA201948.0622003

1.
北京信息科技大学光电信息与仪器北京市工程研究中心,北京 100192

基金项目:

教育部“长江学者与创新团队发展计划”项目（IRT_16R07）;北京市属高等学校高层次人才引进与培养计划（IDHT20170510）

详细信息

作者简介:
张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

中图分类号: TP212;TN253

Flexible composite skin embedded optical fiber shape sensing for variant aircraft

1.
Beijing Engineering Research Center of Optoelectronic Information and Instruments,Beijing Information Science and Technology University,Beijing 100192,China

摘要: 针对变体飞行器变形机翼气动外形监测需求，提出一种植入式柔性复合蒙皮形状光纤传感方法。通过将光纤光栅传感器植入硅胶薄层，并与聚氯乙烯薄片组成复合蒙皮。建立柔性蒙皮形状传感系统，采用光纤传感解调系统，实验测得不同翼型下柔性蒙皮中光纤光栅反射谱特征及其变化规律；计算出柔性蒙皮弯曲曲率，并重建出柔性蒙皮变形三维形状；采用数字摄影测量系统完成对比测试。研究结果表明：柔性复合蒙皮变形光纤传感测量与数字摄影测试误差小于4.62%，光纤传感灵敏度达到245.5 pm/m-1。验证了植入式光纤传感方法的有效性，为变体飞行器变形机翼气动外形监测提供了参考。
- 柔性蒙皮 /
- 复合基体 /
- FBG传感 /
- 变形重构
Abstract: To meet the demand for monitoring the morphing wing aerodynamic shape of morphing aircraft, a flexible composite skin embedded optical fiber shape sensing method for variant aircraft was proposed. The fiber Bragg grating sensor was embedded into the thin layer of silicone rubber, then combining the silicone rubber layer with polyvinyl chloride sheet to form composite skin. The flexible skin shape sensing system was established, and the optical fiber sensing demodulation system was used to test the reflection spectrum characteristics of the fiber Bragg grating in the flexible skin under different airfoil. The morphing curvature of the flexible skin was calculated and the three-dimensional shape of the flexible skin was reconstructed. The contrast test was completed by the digital photogrammetry system. The results show that the measurement error of flexible composite skin deformation optical fiber sensing compared with digital photography is less than 4.62%, and the sensitivity of optical fiber sensing reaches 245.5 pm/m-1. The effectiveness of the embedded fiber sensing method is verified, which provides a reference for monitoring the morphing wing aerodynamic shape of the morphing aircraft.
- flexible skin /
- composite matrix /
- FBG sensing /
- morphing reconstruction

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变体飞行器柔性复合蒙皮植入式光纤形状传感

doi: 10.3788/IRLA201948.0622003

作者简介:
张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

Flexible composite skin embedded optical fiber shape sensing for variant aircraft

计量

变体飞行器柔性复合蒙皮植入式光纤形状传感

doi: 10.3788/IRLA201948.0622003

1. 北京信息科技大学光电信息与仪器北京市工程研究中心,北京 100192

作者简介:
张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

English Abstract

Flexible composite skin embedded optical fiber shape sensing for variant aircraft

1. Beijing Engineering Research Center of Optoelectronic Information and Instruments,Beijing Information Science and Technology University,Beijing 100192,China

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目录

留言板

变体飞行器柔性复合蒙皮植入式光纤形状传感

doi: 10.3788/IRLA201948.0622003

作者简介: 张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

Flexible composite skin embedded optical fiber shape sensing for variant aircraft

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出版历程

变体飞行器柔性复合蒙皮植入式光纤形状传感

doi: 10.3788/IRLA201948.0622003

1. 北京信息科技大学 光电信息与仪器北京市工程研究中心,北京 100192

作者简介: 张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

English Abstract

Flexible composite skin embedded optical fiber shape sensing for variant aircraft

1. Beijing Engineering Research Center of Optoelectronic Information and Instruments,Beijing Information Science and Technology University,Beijing 100192,China

全文HTML

目录

作者简介:
张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn

1. 北京信息科技大学光电信息与仪器北京市工程研究中心,北京 100192

作者简介:
张雄雄(1992-),男,硕士生,主要从事光纤传感技术等方面的研究。Email:xiongxiong_z@sina.cn