1. Introduction
Twisting an optical fiber can offer new opportunities for light controlling and shaping. It is shown that circular birefringence and single mode transmission with a large normalized frequency can be achieved by using a twisted fiber with a helical off-center core, which was fabricated by rotating during the fiber drawing process, in 1987 [
1]. Afterwards, studies on the couplings between core and cladding modes in helical fibers drew much attention. Based on the mode couplings, researchers found that the fibers can be used in various applications, such as polarizers, couplers, and sensors [
2,
3,
4,
5,
6]. Further, studies were also conducted on the helical fibers with rotational symmetric noncircular fiber core owing to the rotational symmetry of the core, which can affect the couplings between core and cladding modes greatly. More recently, the fiber processing method developed along with the progress in microfabrication, a helically twisted photonic crystal fiber (PCF), has been reported by Shin et al. [
7] and in 2012, a detailed interpretation from the terms of mode couplings was given by Wong et al. [
8]. Later, in 2013, it was shown that the helically twisted PCFs can be used for twist and strain sensing [
9]. In 2014, Xi et al. presented a helically twisted three-fold symmetry Y-shaped core PCF, showing that helical Bloch modes carrying orbital angular momentum (OAM) can be well-preserved in the fiber, and demonstrated the stable transmission of first-order OAM modes in experiments [
10]. In 2016, it was shown that helically twisted PCFs also can serve as current sensors due to their circular birefringence [
11]. Meanwhile, new guidance mechanism was discovered in a coreless photonic crystal fiber. It was demonstrated that the light can be robustly confined in such fibers without any cores and the guided modes can be controlled by changing the twist rate [
12]. In 2019, light guiding in a microstructured optical fiber with a partially open ring of holes was reported by Napiorkowski et al., and the experimental study showed that the fiber could be used for displacement sensing [
13]. To date, the potential of helically twisted PCFs has been broadened to many applications, such as circular polarizers [
14], vortex generators [
15,
16] and fiber lasers [
17,
18]. Particularly, the expansion of sensing applications can benefit greatly from the studies on the light guidance mechanism in helical microstructured optical fibers [
12,
13,
19].
In this paper, we propose a helical broken-circular-symmetry core microstructured optical fiber for refractive index sensing. It is made of pure silica with a compact structure, and a broken air ring forms an incomplete barriered core. The fiber is twisted along the propagation axis. Modal characteristics relative to the twist rate are investigated in detail. The numerical results show that for the broken air ring located in the fiber center, the fundamental core modes exhibit increasing overall confinement loss with twist rate since the helical structure cannot provide any additional confinement for the light guiding in this case. However, for the broken air ring placed a distance away from the fiber center, the confinement of the modes at the center of the ring will be enhanced due to the twist-induced light guidance mechanism, showing a decrease in the loss spectrum. Moreover, we first observe the couplings between the core modes and the leaky modes generated by the helical microstructure appeared at some twist rates. We have also studied the variations in the loss spectra by changing the refractive index of analyte filled in the air ring. The variation of modal loss shows a high linearity to the changing of refractive index of analyte and the maximum amplitude sensitivity shown in this paper can reach over 300 RIU−1. The obtained results indicate that the proposed fiber has great potential in sensing applications.
4. Results and Discussions
First, we have calculated the effective indices and the loss spectra of the HE
11 fundamental modes in the proposed fibers without any analyte filled in at five different core offsets, including the one located at the fiber center. Meanwhile, the ratio R
2/R
1 changes from 1.5 to 2.0. In
Figure 2a, we present the effective index
neff’ versus the twist rate
A, and the obvious changes in leakage loss with respect to the twist rate
A are given in
Figure 2b–g. Here,
A is the twist rate
α in a reduced form, expressed as
A = α/(2π).
As shown in
Figure 2a, the effective indices of fundamental modes increase sharply with twist rate, and for larger core offsets, the rises become more dramatic in the effective index, while for the ring located at the fiber center, the effective index basically stays the same. This is because the light is forced to travel a longer helical path when a normal fiber turns into a twisted one, leading to an increase in the effective index. Note that the effective indices presented in
Figure 2a are with R
2 = 1.5R
1 since the change in the air ring ratio has a very minor effect on the effective indices. The effective index of core modes with sufficiently large core offsets in helical-core fibers can be approximated by the following equation [
24]:
where
ρ is distance between the core and fiber center,
m is the azimuthal order relative to the total angular momentum and, for fundamental core modes, takes the value ±1 representing two opposite handedness based on the circular polarization. One can see from Equation (5) that the elongation of the optical path mainly depends on the product factor
αρ, and therefore, it is understandable for the broken air ring located at the fiber center (
ρ = 0 μm) that the effective index remains unchanged.
Figure 2b shows the variation in confinement loss with twist rate for
ρ = 0 μm. It is quite clear that the overall loss increases with twist rate, though the core modes are already at a high leakage loss when the fiber untwisted. This is because the fiber twist enhances the mode leakage through the gap in the broken air ring. However, in the case of
ρ = 5 μm, one can see that the loss decreases with twist rate, showing loss characteristics contrary to those in the case of
ρ = 0 μm. For sufficiently large core offsets, mode deformations will arise owing to the fiber twist of the helical core fibers. Specifically, they mainly manifest themselves as the mode field moving outwards with respect to the fiber center. In the case of the proposed fiber here, the fiber twist reduces the leakage from the gap greatly, and the broken air ring serves as a refractive index barrier preventing the light from leaking out in other directions. Hence, the broken air ring plays a role in reducing the confinement loss in this case. The trend of curves presented in
Figure 2d is basically the same as that in
Figure 2c, apart from the slight distortions that appear in the twist rate range from 15 cm
−1 to 20 cm
−1. By analysis, together with
Figure 2d–f, we have confirmed that the distortions/peaks that occurred in the loss spectra are due to the couplings between the core modes and the highly leaky mode created by the helical structure. With R
2 increasing, one can see that the confinement loss decreases significantly but the trends of the curves are basically the same since the increase in the proportion of air mainly enhances the confinement of mode fields.
As shown in
Figure 3a, away from the loss peak, one can see that the light can be well-confined by the broken air ring with a large
αρ factor.
Figure 3b–d show the transverse electric field distributions corresponding to the significant loss peaks
a,
b, and
c marked in
Figure 2e,f. Compared to the field distribution shown in
Figure 3a, one can clearly see the interactions between the core modes and the highly leaky modes outside. Moreover, with the increasing
αρ, the resonant peaks tend to increase and shift to the shorter twist rate. Note that the two core modes with opposite handedness appear to have the same behaviors in the curves, indicating that the optical phenomena occurring here are basically polarization-insensitive.
Next, we perform a simulation of the fibers with analyte filled in the broken air ring. The refractive index of analyte changes from 1.33 to 1.40. Here, as a contrast to
Figure 2, we begin with showing the effective indices and loss spectra of the fundamental modes with core offset changing from 0 to 20 μm and R
2/R
1 varying from 1.5 to 2.0.
As shown in
Figure 4a, the trends in effective indices are basically the same as that in
Figure 2a, except the overall magnitude increased in this case due to the analyte of refractive index filled in the air ring. The overall confinement loss illustrated in
Figure 4b–f is apparently much higher than that in
Figure 2b–f. This is owing to the rise of refractive index in the air ring causing the broadening of the mode field, leading to the increase in loss spectra. The trends of curves in loss spectra also do not change too much compared to the curves in
Figure 2b–f. However, for
Figure 4e,f one can see that the loss gradually increases again at some twist rates under the coupling conditions. Specifically, in
Figure 4e, for twist rate
A larger than 15 cm
−1 approximately, the curves begin to rise. The same case occurs in
Figure 4f for twist rate
A larger than 13 cm
−1 approximately. The same trend also appears in
Figure 2f, which is not as significant as that shown in
Figure 4e,f. The increases in the loss spectra in these cases can be attributed to the modal displacement towards the outside, which means the modal fields tend to leak into the air ring. This can be regarded as a loss amplification effect due to the fiber twist. The mode profiles are given in
Figure 5, demonstrating the evolution of mode profiles with changing twist rate.
To study the effect of changes in the refractive index of analyte
na on the core modes, we select the fiber structural parameters with R
2 = 2R
1,
ρ = 15 μm for the following sections unless specified, and with
na varying from 1.33 to 1.40 for some fixed twist rates. As shown in
Figure 6a, for twist rate
A = 5 cm
−1, one can see that the losses gradually increase with wavelength due to the fiber twist. More importantly, for a fixed wavelength, the confinement loss increases significantly with
na changing from 1.33 to 1.40 in the wavelength range from 1.5 to 1.6 μm, showing that the light confined by the ring is sensitive to the changes in refractive index of the surroundings. It is not difficult to find that the increases in the loss spectra are nonlinear with
na changing from 1.33 to 1.40. However, we have found that the loss spectra might show good linearity in the log scale. The linearity and a sensitivity of curve slope correlation for selected wavelength 1.55 μm are shown in
Figure 6b. By linear fitting, the sensitivity can be obtained from the slope of the fitting curve, which is 9.49 RIU
−1 in the log scale, and the R square can reach 0.9759, showing a satisfactory linear response to
na in the range from 1.33 to 1.40.
For twist rate
A = 12.1 cm
−1 where significant couplings occur with
na = 1.33 corresponding to the blue curve in
Figure 4e, the wavelength-dependent loss spectra near wavelength 1.55 μm are also calculated, as shown in
Figure 7. In the vicinity of the resonant coupling conditions, we can see a series of loss peaks appeared in the loss spectra for different
na. Initially, one can see that the loss peaks increase and shift towards longer wavelengths with rising
na. However, for a relatively high refractive index
na, such as
na = 1.40, the overall loss is higher than the resonant peaks corresponding to
na = 1.33 and 1.34 in the wavelength range shown in
Figure 7. This indicates that for increments of the refractive index
na taking 0.01, the increase in and movement of the loss peaks are mainly nonlinear and irregular in this case. Hence, we calculate the loss spectra with
na changing from 1.33 to1.34 by taking 0.001 as an increment in the refractive index this time.
As shown in
Figure 8a, for a fixed wavelength, the confinement loss increases in a relatively regular magnitude with
na changing from 1.330 to 1.340.
Figure 8b shows the linear fitting of loss versus refractive index
na for selected wavelength λ = 1.589 μm. One can see that the sensitivity corresponding to the slope of the fitting curve can reach a relatively high value of 1844.85 dB/(m·RIU), showing that the core modes are sensitive to small changes in the refractive index of the surroundings, and the obtained R squared value 0.9975 shows that the result has a considerably high linearity.
For the twist rates away from the coupling conditions, the loss spectra and linear fittings are shown in
Figure 9. Compared to the results in
Figure 6, the confinement losses calculated here for chosen twist rate
A = 20 and 25 cm
−1 increase much more rapidly due to the fiber twist. As shown in
Figure 9a,c, the curves may look identical to each other, but for a higher twist rate
A, the overall loss is also higher, which agrees with the blue curve in the twist rate range from 20 to 25 cm
−1 in
Figure 4e. The linear fittings for selected wavelength λ = 1.55 μm are shown in
Figure 9b,d. Analogous to the results shown in
Figure 6, it is obvious the increases in loss with
na are nonlinear, and thus, the fitting of loss versus refractive index of analyte
na is presented in the log scale, which seems to show better linearity. For the two chosen twist rates, the increases in loss versus refractive index
na show good linearity with R squared values 0.9929 and 0.9924. The obtained sensitivities are 39.02 and 40.42 RIU
−1 in the log scale, respectively. In this case, one can notice that the increase in twist rate enhances the sensitivities of the fiber. In fact, though the broken air ring plays a role in reducing the confinement loss, the modal fields tend to move outwards with the increasing twist rate. Thus, with a high twist rate and refractive index growing in the broken air ring, more of the mode field will leak into the analyte, resulting in the amplification of confinement loss, improving the response to the changes in the refractive index of the analyte.
Figure 10 shows the wavelength-dependent amplitude sensitivities of the proposed fiber with the same twist rates selected in
Figure 6 to
Figure 9. The amplitude sensitivity can be calculated based on the amplitude interrogation method [
25] and it is mostly used for evaluating the sensing performance of plasmonic photonic crystal fibers [
26]. Here we also apply the method to the proposed fiber to show the sensing performance accordingly.
As shown in
Figure 10a, the sensitivity increases greatly with the refractive index of analyte
na and the changes in the curves are smooth and stable. One can see the maximum sensitivity of 61.72 RIU
−1 is achieved at 1.6 μm with
na = 1.40. In
Figure 10b, for twist rate
A = 12.1 cm
−1 in the vicinity of the couplings the sensitivities vary dramatically and a maximum value of sensitivity which can be found at 1.567 μm is 289.69 RIU
−1. For the high twist rates
A = 20 and 25 cm
−1 the sensitivities also rise with the refractive index of analyte
na as shown in
Figure 10c,d. However, one can obtain higher sensitivities in both cases compared to
Figure 10a and the maxima of sensitivity can reach 299.3 and 321.99 RIU
−1, respectively. Moreover, the sensitivities decrease with wavelength in both cases in contrast to the lower twist rate case and this can be attributed to the increase in the overall loss caused by the fiber twist. Furthermore, it is not difficult to find the variation of amplitude sensitivity shown here is also agreed with the analysis for the linear fittings.