3.1. Mode Analysis
As shown later, the performance of a DFG based on a waveguide structure is closely related to the waveguiding characteristics of the mode guided, aiming to produce the TF-LN-on-sapphire rib-type waveguide depicted in
Figure 1a.
Some considerations taken into account in the input parameters are described briefly below. When the wavelength of input pump wave is fixed at 980 nm and that of input signal wave is tunable from 1340 to 1440 nm, an idler wavelength tunable from 3.0 to 3.6 μm is generated. The present mode analysis at the central wavelength λ = 3.3 μm focuses on the effects of waveguide geometries on the waveguiding characteristics.
Figure 2a–c show effective refractive indices n
eff of a few lower-order modes—TE
00, TM
00 and TE
10—calculated as a function of rib width W when the rib has three different heights—h = 0.5, 0.7 and 0.9 μm. The other input parameters are α = 78.5°, H = 1 μm and λ = 3.3 μm. Note that the value of the inclination angle α = 78.5° is taken from the earlier experimental work in Ref. [
17]. Here, we chose a thicker LN film of H = 1 μm (the most common thickness is 0.7 μm [
26]). Our reason for such a choice is that the longer the operating wavelength, the larger the waveguide cross section required to realize single-mode propagation. In order to find the waveguide dimensions where only the TE
00 mode is conductive while the TM
00 and TE
10 modes are cut off, the effective refractive indices of three low-order modes are calculated in total. It can be seen that the cutoff widths of the TE
00 mode and TM
00 mode are similar, so we can only choose the dimensions where only the TE
10 mode is cut off. One can see from
Figure 2a–c that the mode index increases with the rib width W but decreases with the increase in the mode order for a given polarization state and given W and h values. This observation is expected from the waveguide theory.
Moreover, the rib height h considerably affects the waveguiding characteristics. The increase in etching depth h is equivalent to the decrease in rib width W. As a result, the mode index decreases as the rib height h increases. The observation may also be explained on the basis of the slab waveguide thickness effect on the mode index. For a slab waveguide, the mode index increases with its thickness. The increase in the rib thickness h is equivalent to the decrease in slab thickness and, thereby, of the mode index. The considerable rib height effect on the mode index leads to a definite effect on the single-mode condition. One can see from
Figure 2a–c that the cutoff rib width of the TE
10 mode is similar—2.5, 3.25 and 3.5 μm for the rib height h = 0.5, 0.7 and 0.9 μm, respectively.
The n
eff curves at the signal and pump wavelengths are provided in
Figure 3a–f. It shows that the cutoff widths of the TE
00 and TM
00 modes of the pump light and signal light are less than 0.5 μm and that the cutoff width of the TE
10 mode of the pump light and signal light is around 1.5 μm. The influences of W and h on n
eff are the same as that mentioned in
Figure 2a–c.
We have further studied the inclination angle α effect on the mode index.
Figure 4 shows the effective refractive indices n
eff of a few lower-order modes—TE
00, TM
00 and TE
10—calculated as a function of rib width W when α = 60°, 70°, 80° and 90°. The other input parameters are H = 1 μm, h = 0.7 μm and λ = 3.3 μm. We can see that the inclination angle α has a small effect on the mode index but noticeably affects the the single-mode condition. As the inclination angle α changes from 60° to 90°, the cutoff rib width of the TE
10 mode increases from ~3.0 to ~3.5 μm.
For an optical waveguide, a confinement factor is usually considered to characterize the extent of confinement to a mode guided in it. The factor is defined as the ratio of power flux of a wave confined in the waveguide region to the total power flux on the plane normal to the waveguide axis. As shown later, the confinement factor is directly related to the nonlinear conversion efficiency of the QPM-DFG through the effective mode field area. Next, attention is paid to the confinement factor of the TF-LN-on-sapphire rib-type waveguide studied.
Figure 5a shows the confinement factor of the TE
00 mode in the rib waveguide as a function of rib width W for three different rib heights: h = 0.5, 0.7 and 0.9 μm (the other parameters are α = 78.5°, H = 1 μm and λ = 3.3 μm).
Figure 5b shows the cases for different inclination angles: α = 60°, 70°, 80° and 90° (the other input parameters are H = 1 μm, h = 0.7 μm and λ = 3.3 μm). We note that, as the rib width W is increased, the confinement factor increases strongly in the initial stage, slowly and, then, eventually saturates to a constant, which is similar and less dependent on either the rib height h or the inclination angle α, as shown in
Figure 5a,b. In contrast, in the cut-off region, the confinement factor reveals slight effects of rib height h and inclination angle α. These observations may be explained as follows: According to the definition given above, the confinement factor depends mainly on the evanescent field. For an optical waveguide with a given cross-sectional geometry, the larger the confinement factor, the smaller the waveguide loss with regard to the evanescent field and, thereby, the smaller the total waveguide loss. For a smaller W, the mode is in the cut-off state, the evanescent field is significant and the confinement factor has a small value in this case. Moreover, the evanescent field may be influenced by either the rib height h or the inclination angle α. It is thus comprehensible that the confinement factor reveals slight effects of rib height h and inclination angle α. As the W is increased, the mode is far from the cut-off state, the evanescent field decreases gradually and the confinement factor increases correspondingly. As the W is sufficiently large, the mode is well-guided, the evanescent field becomes minor and the confinement factor tends toward a constant. As the minor evanescent field is less influenced by either the rib height h or the inclination angle α, the constant remains essentially fixed for a given H and hardly depends on either the rib height h or the inclination angle α.
It can be seen that a highly slanted waveguide (alpha = 60) result in maximum confinement, which can be explained as follows: the mode field in the waveguide will leak along both lateral and longitudinal.
Figure 5 shows that, when W is large enough, the confinement factor is almost 0.75 and remains constant, indicating that there is almost no lateral leakage of the mode in the waveguide, only longitudinal leakage. However, when lateral leakage exists and W remains constant, a larger inclination angle means a larger lateral cross-sectional area of the waveguide, which can reduce lateral leakage, and thus shows a larger confinement factor.
An overall consideration for single-mode operation and mode field confinement factor allows us to give a preliminary rib width W ≈ 3.0 μm.
3.2. Nonlinear Conversion Efficiency
For a QPM-DFG having a nonlinear interaction length L, its nonlinear conversion efficiency
ηDFG is given by [
27]
where
Pi is the output power of the idler wave with a wavelength
λi,
Pp is the power of the input pump wave with a wavelength
λp and
Ps is the power of the input signal wave with a wavelength
λs. These powers are given by [
27]
where
j∈{
p,
s,
i},
is the unit vector along the waveguide axis, and
Ej and
Hj are the normalized distributions of electric and magnetic fields in the waveguide, respectively. For convenience, an
xyz Cartesian reference frame is fixed at the bottom of the silica layer, with the
x axis pointing to the width and the
y axis pointing to the depth of the rib waveguide, as shown in
Figure 1b. The integral in Equation (2) is carried out over the whole plane normal to the propagation direction z.
By solving difference-frequency coupled-mode equations under no pump depletion approximation [
27], Equation (1) can be expressed as
where
ηn is the normalized efficiency. In particular, for a waveguide structure,
ηn is given by [
27]
where
c is the light speed in free space;
Nj (
j =
p,
s,
i) is the effective refractive index of the pump, signal or idler mode; and
deff is the effective second-order nonlinear coefficient, given by [
27]
in which
m,
n,
k ∈ {
x,
y,
z}.
Ep,
Es and
Ei are the normalized electric field distributions of the pump, signal and idler waves, respectively.
dm,n,k is the second-order nonlinear tensor matrix element of a nonlinear optical material, such as the LN studied here [
27]. The integral in Equation (5) is carried out over the cross section of the related waveguide.
However, for devices using
d33, the element in summation with
d33 in Equation (3) is much bigger than the other terms in summation, which means that terms without
d33 hardly contribute to the value of
deff. So, we can simplify Equation (5) as
Furthermore, we can convert Equation (4) into
where
Aeff is the effective mode field area and
ζ is the mode overlap factor, and they are given by
Aeff and ζ are key factors influencing the nonlinear conversion efficiency. It is evident from Equations (7)−(9) that the normalized efficiency ηn decreases with the increased effective mode field area Aeff, while increases with the increase in mode overlap factor ζ. Aeff is closely related to mode confinement of the waveguide. A smaller Aeff means better mode confinement, which results in a higher nonlinear conversion efficiency. ζ represents the overlap in the mode field distribution of the three coupled beams. A larger ζ means stronger coupling of the three beams, which results in a higher nonlinear conversion efficiency.
In Equation (3), ∆
β represents the phase mismatch amount along the unit propagation distance [
27]:
where the effective refractive index
Nj (
j =
p,
s,
i) is dependent on either the wavelength
λj or the temperature
T. ∆
β = 0 means that the quasi-phase matching condition, i.e., the law of momentum conservation, is exactly satisfied.
The validity of the theoretical expressions described above should be demonstrated first. This can be carried out by comparing the calculation results with the relevant experimental data. On the basis of the experimental parameters of the mid-IR QPM-DFG based on the periodically poled LN-on-sapphire channel waveguide (H = 0.63 μm, h = 0.3 μm, W = 3 μm and α = 78.5°) reported in Ref. [
17], we have evaluated the normalized nonlinear conversion efficiency
ηn of the idler wave as a function of its wavelength. The calculated result is shown in
Figure 6 (see red balls) in comparison with the experimental data without the loss corrections (black balls) reported in Ref. [
17]. The errors are indicated for both the calculated and experimental data. Our theoretical data have an error of ±20% originating from the uncertainties of the input parameters, including ±10% uncertainty of the second-order nonlinear tensor element [
25], about ±5% uncertainty with respect to no pump depletion approximation [
27] and about ±5% uncertainty associated with the numerical method. It is unfortunate that Ref. [
17] did not specify the error of their experiment results. Here, we assume that their experimental data have a conservative error of ±10%, as indicated in
Figure 5. One can see that our theoretical result can be regarded as identical to their experimental data within the error, verifying the validity of the relevant theoretical expressions and the reliability of the theoretical results predicted and given below.
After verification of the relevant theoretical expressions, attention is paid to the key parameters influencing the nonlinear conversion efficiency.
Figure 7 shows the effective mode field area
Aeff and mode overlap factor ζ of the pump, signal and idler TE
00 waves calculated as a function of rib width W in the range of 2.4–4.0 μm for different rib heights h = 0.5, 0.7 and 0.9 μm. The other input parameters are H = 1 μm, α = 78° and λ = 3.3 μm. One can see that, while the mode overlap factor ζ is hardly influenced by either the rib width W or the rib height h, the effective mode field area
Aeff is considerably affected by both, and smaller W and larger h favor obtaining a smaller effective mode field area
Aeff. The observations are easily understood from the W and h effects on the waveguiding characteristics described above. It can be predicted from the observations that a higher nonlinear conversion efficiency is expected for smaller W and larger h, which result in a smaller effective mode field area
Aeff and hence a higher conversion efficiency.
The most remarkable feature in
Figure 7 is the appearance of the maximum
Aeff and the minimum
ζ at W = 2.944, 3.072 and 3.09 μm for the rib heights h = 0.5, 0.7 and 0.9 μm, respectively. These maximum
Aeff and minimum
ζ values yield minimum normalized efficiency values, as shown in
Figure 7a, where the normalized nonlinear conversion efficiency
ηn is plotted against the rib width W for the rib height h = 0.5, 0.7 and 0.9 μm. Next, we give a qualitative explanation for the appearance of minimum normalized nonlinear conversion efficiency
ηn at a specific rib width W for a given rib height h. It is associated with the occurrence of mode hybridization between the TE
00 and TM
30 modes. To make the argument clear, here, we exemplify the hybridization between the modes of the 980 nm pump wave.
Figure 8b–d shows the effective refractive indices n
eff of several lower-order pump modes (TE
00, TM
00, TM
10, TM
20 and TM
30) calculated as a function of rib width W in the case of rib height h = 0.5, 0.7 and 0.9 μm. The other input parameters are H = 1 μm, α = 78° and λ = 0.98 μm. The mode hybridization usually takes place in an asymmetric waveguide when the two modes involved have similar effective indices [
28,
29,
30].
Regarding the presently studied LNOI-on-sapphire rib waveguide, which is asymmetric along the vertical (y) direction, the mode hybridization between the TE
00 and TM
30 modes occurs in the region of W = 2.944, 3.072 and 3.09 μm for h = 0.5, 0.7 and 0.9 μm, respectively. It is featured by both the variational tendency of the mode index with W and the mode field distribution in that W region. One can see from
Figure 8b−d that the tendency of either the TE
00 or the TM
30 mode index is normal as W is far from the hybridization region. In the W region where the mode hybridization occurs, the two plots of the TE
00 and TM
30 mode indices are very close but do not actually intersect each other. This is clearly shown in the insets in
Figure 8b–d, where an expanded view in the hybridization region is shown. Very close mode indices provide the possibility that the two modes couple each other and that mode hybridization happens. The mode hybridization is also featured by the mode field distribution in the related rib width region. As a representative figure,
Figure 9 shows the evolution of two-dimensional distributions of electric field E and its two components E
x and E
y of the fundamental mode TE
00 with the rib width W in the range of 2.9−2.99 μm in the case of rib height h = 0.5 μm. Because the TE
00 mode occurs when the TM
30 mode is not related to the normalized efficiency
ηn, only the evolution feature of the electric field distributions with regard to the TE
00 mode is followed here. Note that mode hybridization occurs at W ≈ 2.944 μm in the case of rib height h = 0.5 μm. One can see that, in the W = 2.944 μm region where the mode hybridization occurs, the electric field distribution of the TE
00 mode is significantly different from that in the W region far from the mode hybridization zone. The significant change in mode field distribution in the mode hybridization zone makes neither the mode confinement nor the mode overlap become worse, which leads to a substantial change in the effective mode field area
Aeff and mode overlap factor ζ and, hence, the normalized efficiency
ηn, as shown in
Figure 7 and
Figure 8a. It is thus comprehensible that a minimum normalized nonlinear conversion efficiency
ηn appears at a specific rib width W for a given rib height h.
We have also studied the inclination angle α effect on the conversion efficiency.
Figure 10 shows the normalized efficiency
ηn calculated as a function of rib width W in the range of 2.5–4.0 μm for four different inclination angles: α = 60°, 70°, 80° and 90°. The other parameters are H = 1 μm and h = 0.7 μm. As expected, the larger α, the higher the efficiency
ηn. A 90° inclination angle allows for the maximum conversion efficiency to be obtained, as shown in
Figure 10. We also note that both the minimum
ηn value and its location change with α more obviously than with rib height h.
3.3. Thermal Tunability and QPM Bandwidth
It is essential to further study the thermal tunability and QPM bandwidth of the device studied. According to Equation (10), the quasi−phase matching condition is given by
The thermal tunability can be studied on the basis of Equation (11) and the law of energy conservation [
27].
From Equations (11) and (12), one can derive the expression for thermal sensitivity of the idler’s wavelength
λi or angular frequency
ωi, i.e., ∂
λi/∂T or ∂
ωi/∂T, which characterizes the thermal tunability of the idler wave.
Note that, in the derivation, the pump wavelength remains constant while the wavelengths of both signal and idler waves are variables.
Since an LNOI waveguide has a smaller cross-section geometry, a mode guided in it usually has significant waveguide dispersion. Group velocity dispersion should be considered. For the pump, signal and idler waves, their involved group mode indices, named
Njg (
j =
s,
i), are given by
where
υjg (
j =
s,
i) denotes the group velocity. Inserting Equation (15) into Equations (13) and (14), we have
where
reflects group velocity mismatch between the signal and idler waves. One can see from Equations (16) and (17) that the thermal sensitivity is determined mainly by the thermo-optic coefficient of the material, wavelengths or frequencies of the pump, signal and idler waves, as well as the GVM factor. For a given material and the given pump and signal waves, the tunability of the idler wave is controlled by the GVM.
For QPM bandwidth, we combine Equation (3) with Equation (10) and we obtain
In Equation (3),
K equals
ΔβL/2, then we differentiate both sides of Equation (3) using Equation (12), and we obtain
As for QPM bandwidth, the equation
sinc(Δ
K/2) = 1/2 needs to be ensured. In this article, the value of Δ
K is approximated to π for ease of calculation, which is an approximation with a tiny error. Finally, we substitute Equation (15) into Equation (19), and the QPM bandwidth can be expressed as
The absolute value of GVM is used in Equation (20) because the bandwidth is always positive. Equation (20) shows that the QPM bandwidth also depends on the GVM, together with the length L of a periodically poled TF-LNOI. By making use of an optical waveguide with a smaller GVM, which can be obtained by optimizing the waveguide dimensions, not only a higher thermal tunability but also a larger QPM bandwidth are expected.
To understand the GVM effect on both thermal tunability and QPM bandwidth, at the wavelengths λp = 980 nm, λs = 1390 nm and λi = 3322.4 nm, we have simulated, firstly, the waveguide properties and, then, the nonlinear frequency conversion features of three periodically poled TF-LN-on-sapphire rib waveguides with different structural parameters, as follows:
WG#1: H = 1.0 μm, h = 0.70 μm, W = 2.8 μm, α = 78°, Λ = 7.68 μm, L = 4 mm;
WG#2: H = 0.9 μm, h = 0.60 μm, W = 2.3 μm, α = 78°, Λ = 6.90 μm, L = 4 mm;
WG#3: H = 0.7 μm, h = 0.35 μm, W = 3.7 μm, α = 78°, Λ = 6.71 μm, L = 4 mm.
These structural parameters are chosen on the basis of the resultant GVM values, as given below. The simulation on the waveguide properties gives, firstly, the dispersion relation and the derivative (with regard to the wavelength) of the mode index in the proximity of the signal and idler wavelengths; then, the group mode indices
Njg (
j =
s,
i); and finally, the GVM values of the three waveguide structures studied, i.e., GVM = 69.4, −160.8 and –320.4 fs/mm for WG#1, WG#2 and WG#3, respectively. According to Equation (3), we calculated the QPM curves of the studied three waveguide structures at two different temperatures of 20 and 60 °C. The calculated results are shown in
Figure 11a–c. The black plot corresponds to the temperature at 20 °C and the red plot to that at 60 °C. For the WG1 waveguide, which has a positive GVM value 69.4 fs/mm, as the temperature is increased from 20 to 60 °C, the QPM peak blue-shifts from 3322.4 to 3234.5 nm, yielding an averaged thermal tunability of ∂
λi/∂T = −2.2 nm/°C. However, for the WG#2 and WG#3 waveguides, both of which have negative GVM values of –160.8 and –320.4 fs/mm, respectively, the QPM peak red-shifts with a rise in temperature. As the temperature is increased from 20 to 60 °C, the QPM peak red-shifts by 95.1 and 31.9 nm, yielding an averaged thermal tunability of ∂
λi/∂T = 2.4 and 0.8 nm/°C, respectively. On the other hand, we have also evaluated the thermal tunability of each waveguide by directly using Equation (16), and consistent results are obtained for each case, verifying the validity of Equation (16). This is also true for the QPM bandwidth.
Figure 11d shows a comparison of the phase matching curves of three waveguides—WG#1, WG#2 and WG#3—at 20 °C.
The three curves are taken from
Figure 11a–c. From the three curves, we have obtained the QPM bandwidths 145, 63 and 31 nm, respectively, consistent with the results evaluated from Equation (20): 133, 57 and 28 nm, respectively.
We can see that a DFG based on the WG#1 waveguide with H = 1.0 μm, h = 0.7 μm, W = 2.8 μm, α = 78°, Λ = 7.68 μm and L = 4 mm exhibits a higher thermal tunability and a larger QPM bandwidth than the other two, WG#2 and WG#3. It is essential to further study the efficiency and output power of the idler wave of the DFG device based on the WG#1 waveguide. In terms of the DFG based on the WG#1 waveguide, we have studied the wavelength dependence of normalized efficiency
ηn, as well as temperature effects on both the efficiency η
DFG and output power P
i of the idler wave when P
p = 20 dBm and P
s = 11.5 dBm, which is the most common power for commercial lasers. The results are shown in
Figure 12a–c. Similar to the feature observed in
Figure 6, the normalized efficiency is wavelength-independent and decreases remarkably with an increased wavelength of the idler wave, as shown in
Figure 12a. As the idler wavelength is increased from 3068 to 3648 nm,
ηn decreases almost linearly from 284 to 174% W
−1cm
−2.
We can see from
Figure 12b that the QPM peak blue-shifts from 3322.4 to 3104.8 nm as the temperature is increased from 20 to 120 °C, yielding an averaged thermal tunability of –2.2 nm/°C, consistent with the results obtained from
Figure 11a. We can further see from
Figure 12b that the higher the temperature, the larger the peaking η
DFG value. As the temperature goes from 20 to 120 °C, the peaking η
DFG value increases from 230 to 273.2% W
−1cm
−2 and increases by ~20%. In addition to the increase in η
DFG, operation at higher temperature also favors the suppression of detrimental photorefractive effects [
31]. The output power P
i of the idler wave shows similar temperature effects. As shown in
Figure 12c, the P
i peak blue-shifts and its peaking value increases slightly and almost linearly with a rise in operation temperature (the increase is by 0.8 dB as the temperature goes from 20 to 120 °C). The largest output power of the idler wave is similar to –2 dBm.
Figure 12d shows the temperature tuning curve of the DFG device based on the WG#1 waveguide (note that the vertical axis is broken to more clearly show the change in the signal or idler wavelength with temperature). From the tuning curve, we obtain a temperature tunability similar to –2.2 nm/°C, consistent with the result given above.
Finally, we have also comparatively studied the DFG performance of the higher-order mode TE10 of the idler wave. The results show that the normalized efficiency degrades by two more times than the case of the TE00 fundamental mode because of the quite different field distributions in the TE00 and TE10 modes.