• Advanced Photonics Nexus
  • Vol. 3, Issue 5, 056011 (2024)
Merve Gokce1,†, Eilam Smolinsky1, Louis Alexandre van der Elst1, Jillian Noblet2..., Creasy Clauser Huntsman2 and Alexander Gumennik1,*|Show fewer author(s)
Author Affiliations
  • 1Indiana University, Luddy School of Informatics, Computing, and Engineering, Fibers and Additive Manufacturing Enabled Systems Laboratory, Department of Intelligent Systems Engineering, Bloomington, Indiana, United States
  • 2Cook Medical Technologies, Bloomington, Indiana, United States
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    DOI: 10.1117/1.APN.3.5.056011 Cite this Article Set citation alerts
    Merve Gokce, Eilam Smolinsky, Louis Alexandre van der Elst, Jillian Noblet, Creasy Clauser Huntsman, Alexander Gumennik, "Multimodal fiber antenna for proximity and stress sensing," Adv. Photon. Nexus 3, 056011 (2024) Copy Citation Text show less
    Application areas of multimodal fiber antenna sensor including environmental monitoring, biomedical applications, human–robot interactions, and cyber–physical systems. Figure created with permission from Ref. 17.
    Fig. 1. Application areas of multimodal fiber antenna sensor including environmental monitoring, biomedical applications, human–robot interactions, and cyber–physical systems. Figure created with permission from Ref. 17.
    (a) Thermal drawing of the multimodal fiber antenna sensor. (b) The preform fabrication steps. (c)-i. Cross-sectional image of the fiber sensor under an optical microscope (4× magnification, scale bar=500 μm). (c)-ii. SEM image of the fiber sensor (FEI Quanta 600, scale bar=500 μm). (c)-iii. Close-up illustration capturing the drawn fiber, showcasing its maintained cross-sectional geometry and enclosed parallel copper wires. (c)-iv. Photo displaying 600-μm diameter, and 65 m of drawn fiber coiled around a hand. 2.42 cm quarter coin shows the scale of the coiled fiber (scale bar = 5 cm).
    Fig. 2. (a) Thermal drawing of the multimodal fiber antenna sensor. (b) The preform fabrication steps. (c)-i. Cross-sectional image of the fiber sensor under an optical microscope (4× magnification, scale bar=500  μm). (c)-ii. SEM image of the fiber sensor (FEI Quanta 600, scale bar=500  μm). (c)-iii. Close-up illustration capturing the drawn fiber, showcasing its maintained cross-sectional geometry and enclosed parallel copper wires. (c)-iv. Photo displaying 600-μm diameter, and 65 m of drawn fiber coiled around a hand. 2.42 cm quarter coin shows the scale of the coiled fiber (scale bar = 5 cm).
    (a) Electromagnetic coupling scheme of multimodal fiber antenna sensor and TDR. (b) Principle of pressure sensing of fiber sensor by change in the capacitance due to change in the distance between metal wires. (c). Principle of proximity sensing of fiber sensor by change in the dielectric environment of the fiber.
    Fig. 3. (a) Electromagnetic coupling scheme of multimodal fiber antenna sensor and TDR. (b) Principle of pressure sensing of fiber sensor by change in the capacitance due to change in the distance between metal wires. (c). Principle of proximity sensing of fiber sensor by change in the dielectric environment of the fiber.
    Electromagnetic field FEM simulation using COMSOL Multiphysics. (a)-i. Field surrounding the fiber sensor at fiber mode 0 (symmetric). (a)-ii. Field surrounding the fiber sensor at fiber mode 1 (antisymmetric). (b)-i. Field surrounding the fiber sensor at fiber mode 0 with the presence of a foreign object within the fiber’s diffraction limit. (b)-ii. Field surrounding the fiber sensor at fiber mode 1 with a foreign object within the fiber’s diffraction limit. The simulations are conducted at a frequency of 18 GHz, a characteristic median frequency for pulses generated by electronics operating in a frequency band of up to 35 GHz. The fiber device cladding has a filleted-corner square cross section with a side of 600 μm. The dielectric constant is 2 for both the SEBS fiber cladding and the foreign object brought into the fiber proximity.
    Fig. 4. Electromagnetic field FEM simulation using COMSOL Multiphysics. (a)-i. Field surrounding the fiber sensor at fiber mode 0 (symmetric). (a)-ii. Field surrounding the fiber sensor at fiber mode 1 (antisymmetric). (b)-i. Field surrounding the fiber sensor at fiber mode 0 with the presence of a foreign object within the fiber’s diffraction limit. (b)-ii. Field surrounding the fiber sensor at fiber mode 1 with a foreign object within the fiber’s diffraction limit. The simulations are conducted at a frequency of 18 GHz, a characteristic median frequency for pulses generated by electronics operating in a frequency band of up to 35 GHz. The fiber device cladding has a filleted-corner square cross section with a side of 600  μm. The dielectric constant is 2 for both the SEBS fiber cladding and the foreign object brought into the fiber proximity.
    TDR measurements of the multimodal fiber antenna under different configurations. (a) The sensitivity curve when the metal wires are placed horizontally (horizontal configuration). Inset, an example of a measurement with 100 gr. (b) The sensitivity curve when the metal wires are placed vertically (vertical configuration). Inset, an example of a measurement with 50 gr. (c) Sensitivity measurements in the vertical configuration, using light weights of 1, 2, and 5 gr. (d) Spatial resolution in the vertical configuration. (e) Distributed pressure measurement using 50 gr at 9.5, 17, 27.5, 37.5, and 47 cm in the vertical configuration. (f) Proximity measurement without the plastic pedestal used in the pressure measurements. The weights used in this case have a footprint diameter of 7 and 18 mm for the 2 and 50 gr weights, respectively. In addition, an index finger with a width of ∼13 mm is used in the measurements.
    Fig. 5. TDR measurements of the multimodal fiber antenna under different configurations. (a) The sensitivity curve when the metal wires are placed horizontally (horizontal configuration). Inset, an example of a measurement with 100 gr. (b) The sensitivity curve when the metal wires are placed vertically (vertical configuration). Inset, an example of a measurement with 50 gr. (c) Sensitivity measurements in the vertical configuration, using light weights of 1, 2, and 5 gr. (d) Spatial resolution in the vertical configuration. (e) Distributed pressure measurement using 50 gr at 9.5, 17, 27.5, 37.5, and 47 cm in the vertical configuration. (f) Proximity measurement without the plastic pedestal used in the pressure measurements. The weights used in this case have a footprint diameter of 7 and 18 mm for the 2 and 50 gr weights, respectively. In addition, an index finger with a width of 13  mm is used in the measurements.
    Signal analysis of fiber antenna evaluating dispersion and sensitivity. (a) The refractive indices of the fiber at antisymmetric and symmetric modes are simulated at the frequency range of 0.8 to 35 GHz by COMSOL Multiphysics simulations. 0.8 and 1 GHz results of mode refractive index have error bars indicating increasing sensitivity to the mesh fineness. (b) Signal-to-noise graphic of the fiber antenna with vertical wire configuration using 1 to 50 gr weights indicates an increase in noise relevant to an increase in signal. The power function fitting shows the sensitivity limit of the fiber antenna as 0.26 kPa.
    Fig. 6. Signal analysis of fiber antenna evaluating dispersion and sensitivity. (a) The refractive indices of the fiber at antisymmetric and symmetric modes are simulated at the frequency range of 0.8 to 35 GHz by COMSOL Multiphysics simulations. 0.8 and 1 GHz results of mode refractive index have error bars indicating increasing sensitivity to the mesh fineness. (b) Signal-to-noise graphic of the fiber antenna with vertical wire configuration using 1 to 50 gr weights indicates an increase in noise relevant to an increase in signal. The power function fitting shows the sensitivity limit of the fiber antenna as 0.26 kPa.
    Change in refractive index (Δn)Change in impedance (ΔZ)
    Mode 0 (%)Mode 1 (%)Mode 0Mode 1
    2% deformation0.1770.078O (106  Ω)2.23 Ω (1.551%)
    Foreign object at 0.4 mm away1.0450.021O (106  Ω)0.39 Ω (0.27%)
    Table 1. Changes in the fiber sensor’s refractive index and impedance at mode 0 (symmetric mode) and mode 1 (antisymmetric mode) for deformation and proximity studies. Notations: O (10x) is “order of 10x.”
    Merve Gokce, Eilam Smolinsky, Louis Alexandre van der Elst, Jillian Noblet, Creasy Clauser Huntsman, Alexander Gumennik, "Multimodal fiber antenna for proximity and stress sensing," Adv. Photon. Nexus 3, 056011 (2024)
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