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Crescent shaped Fabry-Perot fiber cavity for ultra-sensitive strain measurement

Optical Fabry-Perot interferometer sensors based on inner air-cavity is featured with compact size, good robustness and high strain sensitivity, especially when an ultra-thin air-cavity is adopted. The typical shape of Fabry-Perot inner air-cavity with reflection mode of operation is elliptic, with minor axis along with and major axis perpendicular to the fiber length. The first reflection surface is diverging whereas the second one is converging. To increase the visibility of the output interference pattern, the length of major axis should be large for a given cavity length. However, the largest value of the major axis is limited by the optical fiber diameter. If the major axis length reaches the fiber diameter, the robustness of the Fabry-Perot cavity device would be decreased. Here we demonstrate an ultra-thin crescent shaped Fabry-Perot cavity for strain sensing with ultra-high sensitivity and low temperature cross-sensitivity. The crescent-shape cavity consists of two converging reflection surfaces, which provide the advantages of enhanced strain sensitivity when compared with elliptic or D-shaped FP cavity. The device is fabricated by fusion splicing an etched multimode fiber with a single mode fiber, and hence is simple in structure and economic in cost.


Operating principle
The fiber devices with elliptic, D-and crescent shaped FP cavities respectively, are shown in Fig. 1, where L represents the cavity length, H denotes the height of the cavity and T is the thickness of the cavity wall.
In these FP cavities, the first reflection surfaces are diverging, flat and converging for the elliptic, D-and crescent shaped cavities respectively, while the second reflection surfaces are all converging.
The incident light beam traveling along the fiber core of SMF is reflected by the two surfaces of the FP cavity respectively and recombined in the fiber core, resulting in an interference fringe pattern at the output.
Assuming that the light intensities of the reflected beams by the two surfaces of the FP cavity are I 1 and I 2 , respectively, the interference signal intensity can be written as: where λ is the wavelength of the incident light, n is the refractive index (RI) of the cavity medium, L is cavity length and ϕ 0 is the initial phase of the interference. At the output fringe dip positions, the phase difference of the two reflected light beams satisfies the condition, where m is an integer, λ m is the wavelength of the m th order interference dip. Assuming that ϕ 0 = 0, when the is satisfied, the intensity dip appears at the wavelength The free spectral range in the spectrum can then be expressed as, For an air cavity, n = 1, the dip wavelength shift due to axial strain can be derived from Eq. (3) as where δL is the change of air cavity length.

Experimental Results and Discussion
The simple experimental set-up is demonstrated in Fig. 2. The incident light beam from a broadband (BBS) light source with wavelength range between 1452 to 1652 nm is launched into the fiber device via a circulator and the    output is directed to an optical spectrum analyzer (OSA) (YOKOGAWA 6390) with the resolution of 0.01 nm to record its spectrum. The microscope images of FP cavity device samples with different shapes and sizes are displayed in Fig. 3, where crescent, D-shaped and elliptic FP cavities can be clearly observed. The cavity length, height and wall thickness of the device samples are summarized in Table 1.
During the experiment implementation, the fiber device was mounted between a fixed stage and a moving stage, and the instant adhesive was used to fix the fiber. The axial strain was applied by adjusting the translation stage to introduce a displacement in the whole fiber device length, and the range of strain was between 0 and 3000 μ ε .
The reflection spectra and the output dip wavelength versus axial strain for three device samples of crescent shaped FP cavities with cavity lengths of 58, 20 and 9 μ m, respectively, are displayed in Fig. 4. The dip wavelength shift exhibits a good linear relationship with axial strain applied and the sensitivities achieved are 1.63, 6.21 and 9.67 pm/μ ε , respectively.  For comparison, the transmission spectra and the output dip wavelength shift versus axial strain for the device samples with elliptic FP cavity are shown in Fig. 6. Such samples are fabricated by fusion splicing a section of MMF etched by hydrofluoric (HF) acid with a section of SMF. In Fig. 6(a), the cavity length is ~48 μ m, and the strain sensitivity obtained is 1.61 pm/μ ε . In Fig. 6(b), the cavity length becomes ~24 μ m, and the strain sensitivity obtained is ~3.1 pm/μ ε .
It can be seen from Fig. 4 to Fig. 6 that the strain sensitivity depends on both the FP cavity length and the cavity shape. For the same cavity shape, the smaller the cavity length, the higher the strain sensitivity achieved. The D-shaped cavity exhibits the higher strain sensitivity than that of elliptic cavity, while the crescent shaped cavity possesses the highest strain sensitivity. This may be due to the fact that the crescent-shaped FP cavity has two converging reflection surfaces, compared with one flat and one converging, and one diverging and one converging reflection surfaces of D-shaped and elliptic shaped cavities, respectively. The converging, flat or diverging reflected beams not only affect the insertion loss of the device but also the variation of cavity length. The insertion loss of the crescent shaped FP cavity is also smaller than that of the other shaped cavities, and the smaller the cavity length, the lower the insertion loss. The smallest insertion loss achieved by crescent shaped cavity with cavity length of 9 μ m is ~16 dB. The visibility of the crescent shaped FP cavity also appears to be the best of the three type FP cavities. For the device samples with cavity length of ~20 μ m, the crescent shaped FP cavity has a visibility of 7 dB, compared with the results of 5 and 6.5 dB of the D-shaped and elliptic FP cavities with cavity length of ~24 μ m. It can also be noted that the thickness of cavity wall plays no clearly significant role when compared with the cavity length, being different from that of the previous work reported 20 . This is likely due to the fact that our device samples exhibit only a short length of cavity wall (at least one reflection surface is a curve) associated with a relatively large thickness.
The temperature responses of the FP cavity devices of different shapes are displayed in Fig. 7. The temperature sensitivities for a crescent shaped FP cavity with cavity length of 20 μ m, a D-shaped FP cavity with cavity length of 24 μ m, and an elliptic FP cavity with cavity length of 24 μ m, are ~15.45, ~12.41, and ~10.74 pm/°C, respectively. Considering of their strain sensitivity of ~6.21, ~3.38, and ~3.1 pm/μ ε respectively, the temperature cross-sensitivities are determined as ~2.49, ~3.67 and ~3.46 μ ε /°C respectively, which are lower than that of MZI (5.25 μ ε / °C) 21 and PCF based Sagnac loop 22 . The crescent shaped FP cavity also exhibits the lowest temperature cross-sensitivity when compared with that of D-shaped and elliptic FP cavities.

Conclusion
In conclusion we have demonstrated an ultra-thin crescent shaped FP cavity for ultra-sensitive strain measurement. The device is simply fabricated by fusion splicing an etched MMF with a section of SMF. The smallest cavity length achieved is ~9 μ m, which provides a high sensitivity of ~9.67 pm/μ m, more than 3 times that of optical fiber MZI and ~9 times that of fiber Bragg grating. The crescent shaped FP cavity is superior to other FP cavities such as elliptic and D-shaped cavities in terms of strain sensitivity, insertion loss, fringe visibility as well as temperature cross-sensitivity. Such an FP cavity device is highly compact, robust, low cost, simple in structure and easy in fabrication, and exhibits ultra-high strain sensitivity and low temperature cross-sensitivity, thus is promising in many strain sensing applications.

Methods
Device fabrication. The crescent shaped FP cavity device is fabricated by fusion splicing an etched MMF with a section of SMF. The fabrication process includes a number of steps which are illustrated in Fig. 8.  48, 24 and 12 μ m, respectively, are 3.5, 2 and 1 minute respectively, the discharge time and power employed are 300 ms and 40 bit respectively, and the overlap lengths adopted for all the three device samples are 10 μ m.
The elliptic FP cavity is fabricated by fusion splicing of etched MMF and SMF as shown in Fig. 10. The etched time for the two device samples of elliptic FP cavity with cavity lengths of 48, and 24 μ m, respectively are 5 and 2.5 minutes, respectively, the discharge time and power employed are 1000 ms and 30 bit respectively, and the overlap lengths adopted for both the device samples are 10 μ m.