4.7 Article

Transfer printed laser induced graphene strain gauges for embedded sensing in fiberglass composites

Journal

COMPOSITES PART B-ENGINEERING
Volume 219, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compositesb.2021.108932

Keywords

Laser induced graphene; Multifunctional composites; Strain sensor; Fiber-reinforced composites; In-situ sensing

Funding

  1. National Science Foundation Graduate Research Fellowship Program [DGE 1256260]
  2. National Science Foundation [CMMI-1762369, EFRI1935216]
  3. Air Force Office of Scientific Research [FA9550-16-1-0087]

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This study utilizes transfer printing of laser induced graphene (LIG) strain gauges onto commercial fiberglass prepreg for in situ self-sensing of strain in fiber-reinforced composites, eliminating the need for external sensor bonding. The embedded strain sensor is fully integrated within the final composite material, reducing weight and offering customization options. The LIG strain gauge can effectively track static and dynamic strain variations in the composite material, providing valuable information for structural health monitoring.
The continuous monitoring of strain in fiber-reinforced composites while in service typically requires bonding a network of sensors to the surface of the composite structure. To eliminate such needs, and to reduce bulk and limit additional weight, this work utilizes the transfer printing of laser induced graphene (LIG) strain gauges onto the surface of commercial fiberglass prepreg for the in situ self-sensing of strain. The resultant embedded strain sensor is entirely integrated within the final composite material, therefore reducing weight and eliminating limitations due to external bonding compared to current alternatives. Additionally, the simple printing process used here allows for the customization of the size and sensing requirements for various applications. The LIG strain sensor is shown to be capable of tracking monotonic cyclic strain as shown during tensile loading and unloading of the host composite, while also proving capable of tracking the dynamic motion of the composite which is characterized via frequency response and sinusoidal base excitation. The LIG strain gauge in this work can thus be used for tracking either quasi-static or dynamic variations in strain for the determination of the deformation experienced by the material, as well as the frequency content of the material for structural health monitoring purposes.

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