Semiconductor Optoelectronics, Volume. 43, Issue 1, 182(2022)

Research on Load Testing Technology of Aircraft Landing Gear Based on FBG

CHU Yuanyuan1...2, WU Yue3, HUANG Pengyu1,2, CHEN Shi1,2 and YAN Guang3 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(6)

    [2] [2] ukasz S′wich. Calibration of a load measurement system for an unmanned aircraft composite wing based on fibre Bragg gratings and electrical strain gauges[J]. Aerospace, 2020, 7(3): 7030027.

    [3] [3] Raffaella D S. Fiber optic sensors for structural health monitoring of aircraft composite structures: Recent advances and applications[J]. Sensors, 2015, 15(8): 18666-18713.

    [4] [4] Daichi W, Hirotaka I, Masato T, et al. Flight demonstration of aircraft fuselage and bulkhead monitoring using optical fiber distributed sensing system[J]. Smart Materials and Structures, 2018, 27(2): 055007.

    [5] [5] Iele M, Leone M, Consales G V, et al. Load monitoring of aircraft landing gears using fiber optic sensors[J]. Sensors and Actuators A: Physical, 2018, 281: 31-41.

    [6] [6] Iadicicco A, Natale D, Di P P, et al. Strain monitoring of a composite drag strut in aircraft landing gear by fiber Bragg grating sensors[J]. Sensors (Basel, Switzerland), 2019, 19(10): 31096575.

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    CHU Yuanyuan, WU Yue, HUANG Pengyu, CHEN Shi, YAN Guang. Research on Load Testing Technology of Aircraft Landing Gear Based on FBG[J]. Semiconductor Optoelectronics, 2022, 43(1): 182

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    Paper Information

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    Received: Aug. 25, 2021

    Accepted: --

    Published Online: Mar. 24, 2022

    The Author Email:

    DOI:10.16818/j.issn1001-5868.2021082502

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