• Photonics Research
  • Vol. 11, Issue 8, A10 (2023)
Kewei Liu1、†, Zihao Wang1、†, Shunyu Yao1, Yanan Guo2、3, Jianchang Yan2、3, Junxi Wang2、3, Changxi Yang1, and Chengying Bao1、*
Author Affiliations
  • 1State Key Laboratory of Precision Measurement Technology and Instruments, Department of Precision Instruments, Tsinghua University, Beijing 100084, China
  • 2Center for Materials Science and Optoelectronics Engineering, University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Research and Development Center for Solid State Lighting, Institute of Semiconductors, Chinese Academy of Sciences, Beijing 100083, China
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    DOI: 10.1364/PRJ.489942 Cite this Article Set citation alerts
    Kewei Liu, Zihao Wang, Shunyu Yao, Yanan Guo, Jianchang Yan, Junxi Wang, Changxi Yang, Chengying Bao. Mitigating fast thermal instability by engineered laser sweep in AlN soliton microcomb generation[J]. Photonics Research, 2023, 11(8): A10 Copy Citation Text show less

    Abstract

    Transient thermal instability represents a significant challenge in generating soliton microcombs. Fast laser sweep can be an efficient method to mitigate thermal instability, but it requires an ultrahigh laser sweep rate for crystalline microresonators with fast thermal relaxation. Here, we engineer a laser sweep waveform to generate AlN-on-sapphire soliton microcombs with an intermediate sweep speed (<30 GHz/μs). Two laser sweep methods with backward plus forward tuning or two-step backward tuning added after the fast forward laser sweep were demonstrated to stabilize solitons. Reducing the soliton number is found to be useful to stabilize solitons in fast laser sweep. The effectiveness of the methods was numerically verified. Our measurements and simulations also reveal the impacts of different thermal relaxation processes occurring at quite different time scales on thermal instability. The requirement of the laser sweep protocols is discussed.

    1. INTRODUCTION

    Coherently pumped dissipative solitons generated in high-Q microcavities constitute a major advance in integrated nonlinear photonics and frequency comb techniques in the last decade [14]. These miniaturized microcombs can revolutionize many applications including time/frequency metrology [5,6], data transmission [7,8], and spectroscopy [9,10]. However, generating solitons in microcavities still remains a technical challenge, and thermal relaxation induced transient instability is one of the main challenges [1,1113]. The abrupt intracavity power reduction in soliton formation can cause resonance shifts, pushing the pump frequency detuning outside the soliton existence range (SER). The instability can be avoided by using the self-injection-locking (SIL) approach for soliton generation [1418]. Considering the available pump power from diode lasers, SIL generally requires a relatively high Q-factor, especially for microwave rate solitons. Laser cavity soliton microcombs, generated within a microresonantor embedded in an active fiber cavity, are also robust against thermal instability, but the comb bandwidth may be limited by the active Er-gain bandwidth [19]. Reducing thermal absorption of microcavities is another option to overcome thermal instability; thus, soliton generation can become possible by simply tuning the pump from blue to red slowly (even manually) [12,13]. For microcavities with relatively strong thermal effects, experimental approaches including power kick [11,20], active capture [21], dual-pump [22,23], and fast laser frequency sweep [24,25] have been demonstrated to mitigate thermal instability for soliton generation. Typically, power kick needs complicated pump power tuning protocols, while dual-pump needs an additional auxiliary laser. As a variant of the dual-pump method, the auxiliary pump in the dual-pump can be generated by electro-optically modulated sidebands [26,27]. Although it avoids an additional laser, a higher overall pump power is needed. Another variant is generating the Brillouin–Kerr soliton by a blue-detuned pump, but it requires the cavity modes arranged appropriately and the cavity material exhibiting strong Brillouin scattering to realize red-detuned Brillouin lasing for soliton generation [28]. Pumping a resonance with a closely spaced neighbor mode, so that the pump can be coupled into the cavity via the other mode, is another feasible way to mitigate thermal instability, but it works only for some specific modes [29].

    Fast laser frequency sweeping can be a relatively efficient and simple way for high-fidelity soliton generation. Generally, the thermal effect is relatively slow, and instability can be suppressed by fast laser sweeps. A fast sweep can be implemented by a single-sideband modulator (SSBM), which can be integrated using the thin-film lithium niobate platform [30], driven by a voltage controlled oscillator (VCO) [24]. The laser scan time usually needs to be faster than the thermal relaxation time to reduce heat accumulation. For silicon nitride (SiN) microcavities with a several-million Q-factor, scanning speed of about 10s GHz/µs is typically needed [25,31]. For on-chip crystalline cavities, e.g., AlN microcavities, which have faster thermal relaxation, scanning speeds need to be as high as 100s GHz/µs [32,33]. If the scanning speed is not high enough, another power-kick step would be needed to generate AlN soliton microcombs [34]. The ultrahigh laser scan speed requires VCO with a large voltage-to-frequency slope and a large bandwidth function generator. VCO with a large slope means that the voltage fluctuations will convert into pump frequency noise stronger, while function generators with a large bandwidth will increase the system cost and are hard to integrate. Hence, it is important to investigate soliton generation with not very fast laser tuning.

    In this paper, we demonstrate soliton generation in an AlN-on-sapphire microcavity with a laser scan speed lower than 30 GHz/µs, which is attainable for distributed Bragg reflector (DBR) lasers by direct current tuning [25]. By engineering the laser sweeping waveform (adding backward plus forward tuning or a two-step backward tuning after the first fast forward tuning), thermal recoil [25] and instability can be mitigated for soliton generation. Our numerical simulation based on a generalized Lugiato–Lefever equation (LLE) [12,13,35,36] shows the importance of two relaxation processes in understanding the soliton generation dynamics. Different from previously studied soliton generation using slow laser tuning where a larger soliton number is favored to balance thermal effects [12,13], a small soliton number can reduce the thermal effects when using fast laser tuning. Our work is important to tailor soliton dynamics in microresonators with fast thermal relaxation.

    2. RESULTS

    A. Experimental Setup and AlN Microcavity Thermal Properties

    The AlN microcavity was fabricated from metal-organic chemical vapor deposition (MOCVD) AlN crystalline film deposited on a sapphire substrate. The same microcavity design as in our previous work was used [37,38]. The microcavity has a radius of 100 μm and a free spectral range (FSR) of about 227 GHz. For dissipative Kerr soliton generation, we pumped the TE10 mode around 1547.9 nm, which exhibits an anomalous dispersion D2/2π=1.95  MHz (group velocity dispersion β2=41.6  ps2/km). The loaded Q-factor and intrinsic Q-factor of this pumped mode are 1.0 million and 1.4 million, respectively. This supports an on-resonance cavity enhancement ratio B of up to 226. Figure 1(a) shows the setup of the SSBM-based fast laser sweep for soliton generation. The SSBM was driven by a VCO, which converts the time-varying waveform from an arbitrary function generator (AFG) to microwave signals with sweeping instantaneous frequency. The modulated pump laser was split by a 90/10 coupler; one was used to monitor the pump frequency sweep by a Mach–Zehnder interferometer (MZI) with an FSR of 51.7  MHz, while the other seeded an Er-doped fiber amplifier (EDFA) to pump the microcavity. The transmitted pump was suppressed by a fiber Bragg grating (FBG) so as to monitor the comb power change.

    Fast laser sweep system and thermal characterization of the AlN microcavity. (a) Schematic of the experimental setup. ECDL, external cavity diode laser; SSBM, single-sideband modulator; VCO, voltage controlled oscillator; AFG, arbitrary function generator; PC, polarization controller; MZI, Mach–Zehnder interferometer; FBG, fiber Bragg grating; PD, photodiode; OSA, optical spectrum analyzer; OSC, oscilloscope. (b) Measured frequency noise of the carrier-suppression single-sideband signals with different VCO drive voltages and the original laser. The inset shows their white noise, which increases nearly quadratically with the voltage-to-frequency slope of the VCO. (c) Thermal triangle (blue dots) and corresponding fit (red line) of the AlN microcavity with 19.2 mW on-chip pump power. The gray dashed line represents the cold resonance, and the MZI fringes were used to calibrate the frequency axis. (d) Thermal and Kerr induced resonance shift increases nearly linearly with the on-chip pump power. (e) Experimental scheme for the thermal relaxation time measurement of our AlN microcavity. IM, intensity modulator; VOA, variable optical attenuator; OC, optical coupler. (f) Measured probe laser transmission with a 200 kHz square wave applied on the IM. (g) Extracted probe transmission within the shaded box in panel (f). The two-term exponential fit (red line) gives two dominated thermal relaxation times of 96 ns and 708 ns.

    Figure 1.Fast laser sweep system and thermal characterization of the AlN microcavity. (a) Schematic of the experimental setup. ECDL, external cavity diode laser; SSBM, single-sideband modulator; VCO, voltage controlled oscillator; AFG, arbitrary function generator; PC, polarization controller; MZI, Mach–Zehnder interferometer; FBG, fiber Bragg grating; PD, photodiode; OSA, optical spectrum analyzer; OSC, oscilloscope. (b) Measured frequency noise of the carrier-suppression single-sideband signals with different VCO drive voltages and the original laser. The inset shows their white noise, which increases nearly quadratically with the voltage-to-frequency slope of the VCO. (c) Thermal triangle (blue dots) and corresponding fit (red line) of the AlN microcavity with 19.2 mW on-chip pump power. The gray dashed line represents the cold resonance, and the MZI fringes were used to calibrate the frequency axis. (d) Thermal and Kerr induced resonance shift increases nearly linearly with the on-chip pump power. (e) Experimental scheme for the thermal relaxation time measurement of our AlN microcavity. IM, intensity modulator; VOA, variable optical attenuator; OC, optical coupler. (f) Measured probe laser transmission with a 200 kHz square wave applied on the IM. (g) Extracted probe transmission within the shaded box in panel (f). The two-term exponential fit (red line) gives two dominated thermal relaxation times of 96 ns and 708 ns.

    In the experiment, the SSBM shifts the pump laser to the 1st sideband, whose frequency is ωs=ωlΩm (ωl is the laser frequency and Ωm is the modulation frequency). An extinction ratio of 18 dB was observed between the 1st sideband and the carrier. Frequency noise of Ωm can add to the noise of the shifted sideband (i.e., actual pump). We measured the frequency noise change induced by the SSBM using the delayed-heterodyne method [38]. Figure 1(b) shows the measured frequency noise of the original laser and the shifted sideband subjected to VCO drive voltages of 1 V and 5 V. The shifted sideband has higher frequency noise than the original laser, especially in the white noise regime [see inset of Fig. 1(b)]. The measured white noise was observed to increase quadratically with the voltage-to-frequency slope of the VCO (this slope is 600  MHz/V around 1 V and 250  MHz/V around 5 V; the original laser can be regarded as operating at the zero slope point). This quadratic fit (with the parabola center fixed at zero) suggests that the added frequency noise results from voltage fluctuations of the AFG. Since the 1st sideband was used, the voltage applied to the VCO should be swept from low values to high values to have ωs swept from blue to red for soliton generation. This naturally ensures the drive voltage is kept at higher values, reducing the frequency noise added to the pump wave.

    To design an optimal laser sweep function, we first measured the thermal properties of the AlN-on-sapphire microcavity. The thermal strength was measured by adiabatically sweeping the laser across a resonance from blue to red with different pump powers. Figure 1(c) shows the power transmission under 19.2 mW on-chip pump power. Due to thermal and Kerr effects, the measured resonance exhibits a triangular shape and was redshifted from cold resonance by about 1230 MHz with the frequency axis calibrated by the MZI. The transmission can be fitted by a thermal and Kerr nonlinearity broadened line shape including the Fabry–Perot transmission of the waveguide facets [39]. The transmission was measured under different pump powers, and the fitted resonance shift is plotted in Fig. 1(d). The measured resonance shift shows a good linear relationship with a slope of 108 MHz/mW. The resonance redshift δf is related to the pump power Pin by δf=vgBPin(α+γ), where α and γ are thermal and Kerr nonlinear coefficients, respectively; and vg is the group velocity in the AlN cavity. The group refractive index was calculated to be 2.07 by the mode simulation, i.e., vg=1.45×108  m/s. Taking an estimated γ of 0.64  W1m1 based on the mode simulation, α was deduced to be 2.65  W1m1.

    The thermal relaxation time of AlN microcavities has not been measured quantitatively, to our knowledge. Here, we measured this time by a pump–probe approach [40], as illustrated in Fig. 1(e). The pump laser was tuned to the blue side of the pump resonance (1547.9  nm), and then its power was modulated by an intensity modulator, driven by a 200 kHz square wave. The heated cavity resonances were actuated to the red and recovered to the blue periodically by the square wave. A probe laser with low power, blue-detuned to the neighbor resonance at 1551.5  nm, was used to detect the thermal effect induced resonance shift with the pump suppressed by a filter. The measured probe power change is shown in Fig. 1(f). We fitted the decaying tail (red shaded region) by a double-exponential function A1et/τ1+A2et/τ2; see Fig. 1(g). Here τ1 and τ2 are thermal constants of the two thermal processes, and A1 and A2 are thermal strengths. The fit gives τ1=96±1.5  ns and τ2=708±2  ns, while the relaxation time can be as large as 760 ns and 14 μs for a SiN microcavity [20] (but SiN microcavities fabricated by different groups may have different relaxation time scales [40]). There may be a slow third thermal process occurring on a time scale of hundreds of microseconds that may correspond to the cooling of the entire chip. This slow response was not observed in this measurement, but is supported by the comb generation experiment (see Fig. 2).

    Soliton generation using engineered laser sweep methods. (a) Measured comb power change when using the conventional forward only laser sweep. (b) Schematic of the laser sweep waveforms of method-1 and method-2. (c) Measured comb power change when using method-1. When including the additional stage-ii, the soliton step can be elongated but still annihilated in the end. By adding stage-iii, the solitons can be stabilized. (d) Measured comb power change for method-2. When adding stage-ii, the soliton step can be extended to millisecond scale but cannot be fully stabilized. By adding another backward tuning step, the soliton can be stabilized. (e) Soliton spectra for a two-soliton and a two-FSR soliton crystal states generated by method-1 (upper and middle panels) and a single soliton state generated by method-2 (bottom panel). The dashed lines are sech2 fits. DW, dispersive wave. (f) Soliton self-starting test using (i) method-1 and (ii), (iii) method-2. Successful soliton generation and corresponding soliton number are indicated by blue boxes and text. (g) Zoom-in of comb power change for successful generation in (f). The insets show the detailed power change within the soliton step.

    Figure 2.Soliton generation using engineered laser sweep methods. (a) Measured comb power change when using the conventional forward only laser sweep. (b) Schematic of the laser sweep waveforms of method-1 and method-2. (c) Measured comb power change when using method-1. When including the additional stage-ii, the soliton step can be elongated but still annihilated in the end. By adding stage-iii, the solitons can be stabilized. (d) Measured comb power change for method-2. When adding stage-ii, the soliton step can be extended to millisecond scale but cannot be fully stabilized. By adding another backward tuning step, the soliton can be stabilized. (e) Soliton spectra for a two-soliton and a two-FSR soliton crystal states generated by method-1 (upper and middle panels) and a single soliton state generated by method-2 (bottom panel). The dashed lines are sech2 fits. DW, dispersive wave. (f) Soliton self-starting test using (i) method-1 and (ii), (iii) method-2. Successful soliton generation and corresponding soliton number are indicated by blue boxes and text. (g) Zoom-in of comb power change for successful generation in (f). The insets show the detailed power change within the soliton step.

    B. Engineered Laser Sweep for Soliton Generation

    1. Conventional Laser Tuning

    Since microcavities take time to heat up (on the thermal relaxation time scale), the abrupt power drop during soliton formation will not disturb the solitons when initializing solitons within a time scale shorter than τ1. In other words, the abrupt intracavity power change is integrated or averaged to yield the thermal response when scanning the pump fast enough, which helps to stabilize solitons. We define the effective detuning as δωeffδω0+δωΘ, where δω0 is the laser frequency detuning relative to the cold resonance, and δωΘ is the thermal resonance shift. δωeff needs to be kept in the SER to stabilize solitons.

    We first adopted a conventional waveform that includes merely a linear ramp voltage (stage-i) to implement the fast sweep with an on-chip pump power of 400 mW, which is about 13 times that of the parametric oscillation threshold. Thus, the SER was estimated to span about six times the cavity linewidth or 1.2 GHz [41]. Restricted by the bandwidth of our AFG (80 MHz), the minimum time duration of stage-i is about 100 ns, yielding an upper limit of the frequency sweep speed 30  GHz/μs (estimated for a drive voltage of 1 V, and the voltage-to-frequency slope decreases with the drive voltage for the used VCO). The measured comb power change includes a soliton step comprising five solitons [Fig. 2(a)]. This step lasted 1.8  μs and was destabilized by the thermal recoil [25]. We believe the thermal recoil is a result of the delayed heating of the cavity and redshift of the resonance due to the second thermal relaxation process, as the soliton step already lasts much longer than τ1. The step is descending, suggesting the effective detuning δωeff is decreasing and the resonance is redshifting, in contrast to the resonance blueshift that destroys solitons in slow laser tuning. The redshifted resonance eventually pushes δωeff to exit the lower boundary of SER and enter the blue-detuned regime (a power spike arises when crossing the resonance), resulting in the observed thermal recoil. Therefore, a simple forward laser scanning is not sufficient to stabilize AlN solitons.

    2. Method-1: Laser Sweep with Added Backward plus Forward Tuning

    Since the thermal effect is an accumulating effect, reducing the soliton number and intracavity power can help reduce it. Hence, we added a backward tuning step to reduce the soliton number. A backward laser sweep was also used in Ref. [34] with the purpose to follow the resonance blueshift induced by the fast first relaxation process instead of reducing the soliton number and making the microcavity cooler. By optimizing an exponentially backward scan [stage-ii in method-1 in Fig. 2(b); the duration and frequency shift were chosen as 450 ns and 120 MHz in the experiment, respectively] right after stage-i, a two-soliton step, switched from a five-soliton state, was observed [see upper panel in Fig. 2(c)]. Note that the optimal backward tuning duration and frequency shift would vary slightly with the pump power. With the reduced soliton number, the step became longer and lasted 12  μs. Nevertheless, thermal recoil still existed in this state, resulting in soliton annihilation.

    A possible way to circumvent thermal recoil is to add another forward laser scan at the end of stage-ii; see stage-iii in Fig. 2(b). This prevents the second thermal relaxation process from catching up with the red-detuned pump laser. In experiments, we found that the optimal duration of the additional forward tuning is generally two to three times τ2. By setting the forward tuning duration as 1.5 μs and frequency shift as 900 MHz, the soliton steps can eventually be stabilized [see bottom panel in Fig. 2(c)]. The comb power shown in Fig. 2(c) indicates that the soliton number switched as 632, and the solitons were stabilized in a two-soliton state. The transition from six-soliton to three-soliton occurred due to backward tuning, as the step was descending. The soliton number switching from 32 should occur due to the mode-interaction induced dispersive wave emission [42] [see the spectrum in Fig. 2(e) and discussion on method-2], as the three-soliton step is increasing. In principle, backward tuning is not necessary or stage-iii can be followed right after stage-i (as suggested in Ref. [25]). However, if the soliton number is large, the forward tuning in stage-iii would require a large frequency shift that may exceed the tuning range of the VCO; therefore, it did not work in our experiments.

    The measured spectra of the stabilized two-soliton state are shown in Fig. 2(e). The top panel is a state with solitons spaced by 588 fs, as deduced by the sech2 fit with interference (dashed black line). The 3 dB bandwidth of a single soliton spectrum is 9.8 THz, or soliton duration τs=18  fs, i.e., a full width at half-maximum (FWHM) pulse width of 32 fs. The spectrum in the middle panel is a two-soliton crystal state with solitons spaced by half of the round trip [43,44]. Some weak lines with about 60  dBm power can be observed in the spectrum, as the soliton spacing may not be perfectly half of the round trip time. Both spectra exhibit dispersive wave emission on the long wavelength side.

    3. Method-2: Laser Sweep with Added Two-Step Backward Tuning

    As noted above, dispersive waves can also be harnessed to reduce the soliton number [42]. Hence, we increased the end detuning of stage-i to enhance the dispersive wave power and reduce the soliton number [see method-2 in Fig. 2(b)]. Another benefit of increasing the end detuning is that it can make the detuning closer to the upper boundary of the SER so that the thermal recoil induced resonance redshift cannot catch up with the pump.

    Different from method-1 where the soliton number switching mainly occurs in the backward tuning in stage-ii, the soliton number has substantially decreased due to dispersive wave emission within stage-i. As a result, the total accumulated heat and resonance induced by the second thermal process are even weaker. In method-2, we also added exponential backward tuning [stage-ii in Fig. 2(b)] after stage-i. Compared to method-1, the backward tuning lasted longer (a duration of about three to five times τ1), and it is used to chase the resonance blueshift induced by the first thermal process and the fast power drop in soliton formation (note that power drop is larger in method-2 than in method-1 as fewer solitons form in stage-i) so as to prevent soliton annihilation from a too large δωeff. When using a waveform including stage-i and stage-ii, the soliton step can be extended to millisecond scale, as shown in the upper panel of Fig. 2(d). Although the achieved soliton duration exceeds the second thermal relaxation time by far, the solitons are still annihilated in the end. However, there is no power spike at the end of the step, suggesting the pump remains red-detuned (δωeff exits the SER from the upper boundary) as opposed to crossing resonance from red-detuned to blue-detuned as in the thermal recoil shown in Figs. 2(a) and 2(c). Hence, we suspect there is a much slower thermal process on the millisecond scale (see the gradually increasing comb power within the step after the laser scan ended), which may arise from the cooling of the entire chip. In addition, the two-soliton step (3.7  ms) is longer than the single-soliton step (720  μs), because a larger soliton number resists the resonance shift induced by the possible third thermal process better.

    To stabilize the soliton, we added the second backward tuning (stage-iii) at the end of the waveform to chase the slow cooling of the chip and resonance blueshift, as shown in Figs. 2(b) and 2(d). By setting the duration to 8 ms and frequency shift to 1.3 GHz for stage-iii, we obtained a stable single-soliton state, whose comb power change is shown in the lower panel of Fig. 2(d). The soliton number decreases from two to one at around 10 µs, as the backward laser tuning in stage-iii exceeds the resonance blueshift induced by the possible chip cooling. The inset shows the observed power oscillation in the soliton number switching, which can be an indication of soliton breathing [45] when δωeff is near the lower boundary of the SER. The spectrum of the stabilized single-soliton state is shown in Fig. 2(e) and is associated with a dispersive wave emission around 1670 nm.

    4. Repeatability of Soliton Generation

    To show the repeatability of our methods, we performed iterative fast frequency sweeps by periodically triggering the AFG every 200 ms. The AFG traces (blue) and the measured comb traces (purple) in 5 s are shown in Fig. 2(f). Successful soliton triggers are highlighted by the shaded boxes. The difference between the middle and bottom panels is the backward tuning frequency amounts in stage-iii, which are 0.9 GHz for Fig. 2(f-ii) and 1.3 GHz for Fig. 2(f-iii). The larger backward tuning slope in stage-iii can result in soliton number switching when it exceeds the resonance blueshift induced by the chip cooling. Hence, these two panels stop in a two-soliton state and a single-soliton state, respectively.

    The observed success rate is not very high in the experiment. A possibility for the relatively low rate for method-1 is the soliton number after backward tuning is random. Method-2 has a relatively higher success rate, as the dispersive mediated soliton number limit is relatively deterministic [42]. Another possibility is the poor repeatability of the piezo-module in the laser. Note that we also scanned the laser wavelength by a piezo periodically in this iterative experiment, since a relatively large frequency tuning range was needed to break the obtained comb state and eliminate all the intracavity power. Thus, the AFG induced pump sweep may not start from exactly the same initial δω0 in different iteratives. Despite the relatively low success rate, automatic soliton generation can be reached within seconds.

    The experiment also enabled measurement of the soliton power change over several milliseconds. For instance, the power of the soliton generated by method-1 increases for milliseconds until reaching an equilibrium state [Fig. 2(g-i)]. This also supports the possible cavity cooling (resonance blueshift) in this time scale. But this resonance blueshift will not cause soliton annihilation, as the δωeff is relatively close to the lower boundary of SER in method-1. Due to the second backward tuning in method-2, the resonance blueshift is resisted, and the soliton power is observed to increase and then decrease within the step [Figs. 2(g-ii) and 2(g-iii)]. The used frequency shift and duration in each step in the above examples can be used as a general reference, but fine adjustment is needed for different samples to get optimal results.

    3. NUMERICAL SIMULATION

    A. Simulation Model

    To understand how the engineered laser sweep mitigates thermal instability, we numerically investigated the soliton generation using the generalized LLE augmented by thermal effects as [12,13,35,36] dAdt=i(δω0+δωΘ)Aκ2Aiβ2L2TR2Aτ2+κexTREi+iγLTR|A|2A+iγRLTR[AτhR(ττ)|A|2dτ],where A is the envelope of the intracavity field, Ei is the pump amplitude, t and τ are fast and slow times, respectively, δω0 and δωΘ have the same definition as in the experiment section, κ is the total loss rate including the external coupling rate κex and intrinsic loss rate κ0, β2 is the group velocity dispersion, γ is the Kerr nonlinearity coefficient, and L and TR are the cavity length and round trip time, respectively. The Raman effect is also included in Eq. (1) since the intrapulse stimulated Raman scattering in AlN microresonators cannot be neglected [37]. γR is the Raman gain coefficient, and hR is the Raman response function. For simplicity, the Raman response was solved in the frequency domain with a single Lorentzian gain center at 19.7 THz, and a bandwidth of 138 GHz with γR=0.0079  W1m1. The motion equation for thermal detuning δωΘ can be written as [13] dδωΘ1,2dt=δωΘ1,2τ1,2+ξ1,2P,where δωΘ=δωΘ1+δωΘ2 includes two thermal relaxation processes with relaxation time τ1,2 and strength of ξ1,2, and P is the average intracavity power. ξ1,2 is related to α1,2 by ξ1,2=vgTRα1,2/τ1,2 (where α=α1+α2). In the simulation, we used parameters as L=628  μm, TR=4.34  ps, γ=0.64  W1m1, |Ei|2=400  mW, κ0/2π=137  MHz, κex/2π=60  MHz, and β2=41.6  ps2/km. The thermal strength was selected as ξ1=2×104  W1s1 and ξ2=7.1×103  W1s1 with relaxation times of τ1=100  ns and τ2=750  ns. To include the dispersive wave emission that contributes to soliton number control, we introduced an additional phase perturbation per round trip in the frequency domain as ϕ(ω)=Γ/(ωω1) [42], where Γ stands for mode-coupling strength and ω1 is the coupling center frequency. Both affect the absolute dispersive wave power and impact the soliton number control and thermal effects; they were chosen as Γ=2π×1.0  GHz and ω1=2π×3.5  THz in the simulation.

    B. Thermal Mitigation in Simulations

    We first simulated the thermal recoil effect in Figs. 3(a)–3(c). We used a conventional forward only scanning (with δω0 increasing from 2.5κ to 11κ in 100 ns) in the simulation. The corresponding intracavity field evolution is shown in Fig. 3(a). A five-soliton state was generated after the laser sweep ended, but they annihilated at about 750 ns. The resulting changes of intracavity power and δωeff are plotted in Fig. 3(b). Due to the delayed thermal accumulation, δωΘ becomes more negative within the soliton step. Due to decreasing δωeff, solitons started to breathe [dashed line in Fig. 3(b)]. Then, δωeff exited the lower boundary of the SER, and the pump crossed the effective resonance and became blue-detuned. A power spike and exponential power decay are observed in this process as in experiments. When further analyzing the change of δωΘ, we found that the second thermal relaxation process contributed to the observed thermal recoil. δωΘ2 becomes more negative within hundreds of nanoseconds, which leads to annihilation of the solitons; see the arrow in Fig. 3(c).

    Simulations of soliton generation dynamics with two thermal relaxation processes. (a) Intracavity field dynamics when sweeping the laser in a conventional way. (b) Corresponding changes of intracavity power and effective detuning δωeff. (c) Analysis of the resonance shift induced by two thermal relaxation processes shows that the thermal recoil is induced by the second thermal process. (d) Intracavity field dynamics when using method-1 for laser sweep. (e) Simulated change of intracavity power and δωeff. (f) Change of the thermally induced resonance shift in laser sweep. (g) Intracavity field dynamics when using method-2 for laser sweep. (h) Simulated change of intracavity power and δωeff for method-2. (i) Thermally induced resonance shift in generation for method-2.

    Figure 3.Simulations of soliton generation dynamics with two thermal relaxation processes. (a) Intracavity field dynamics when sweeping the laser in a conventional way. (b) Corresponding changes of intracavity power and effective detuning δωeff. (c) Analysis of the resonance shift induced by two thermal relaxation processes shows that the thermal recoil is induced by the second thermal process. (d) Intracavity field dynamics when using method-1 for laser sweep. (e) Simulated change of intracavity power and δωeff. (f) Change of the thermally induced resonance shift in laser sweep. (g) Intracavity field dynamics when using method-2 for laser sweep. (h) Simulated change of intracavity power and δωeff for method-2. (i) Thermally induced resonance shift in generation for method-2.

    To mitigate the thermal recoil, method-1 can be used [see Figs. 3(d)–3(f)]. The laser was first forward tuned from κ to 10κ in 100 ns. Although we used exponential backward and forward tuning in the experiment, the simulations show that linear backward plus forward tuning can also be effective. The soliton generation dynamics is shown in Fig. 3(d). With the added backward tuning, the pulse number decreased to three [Fig. 3(e)]. Thus, |δωΘ2| is smaller in Fig. 3(f) than in Fig. 3(c). In other words, the backward tuning and reduced soliton number help to mitigate the second thermal relaxation process. However, δωΘ2 can still push δωeff out of the SER [see red curve around 600 µs in Fig. 3(e)]. The added forward tuning balances the descending δωΘ2 [see arrow in Fig. 3(f)]; thus, δωeff is pulled back to the SER and the solitons are stabilized. In this process, the enhanced dispersive wave emission causes annihilation for one of the solitons to reach a two-soliton state. As an aside, soliton annihilation in backward tuning is usually associated with breather collision, while there is no such collision in dispersive wave mediated soliton annihilation.

    The effectiveness of method-2 is validated in Figs. 3(g)–3(i). In this method, the first forward tuning ended at 12κ, a larger δω0 than that of method-1. Due to the larger ending δω0, dispersive wave emission is enhanced and reduces the soliton number to two within forward tuning [Figs. 3(g) and 3(h)]. As the soliton number is smaller, a power drop in soliton formation is larger. As a result, δωΘ1 becomes less negative upon the formation of solitons. Therefore, the first backward tuning is used to resist the increasing tendency of δωeff to prevent increasing δωΘ1 from pushing δωeff outside the SER from the upper boundary [see arrow in Fig. 3(i); note that δωΘ2 is negligible within this fast time scale]. The two-soliton step can be elongated and stabilized by this backward tuning alone in simulations for the two thermal relaxation processes considered in Eq. (2). In experiments, the second backward tuning was used to resist the suspected chip cooling and lasted 8 ms, which is too long for the current simulation capacity. Hence, the second backward tuning was mainly added to mimic the observed soliton number switching from two to one observed during backward tuning in Fig. 2(d); see Figs. 3(g) and 3(h). When the soliton number reduces to one, both δωΘ1 and δωΘ2 become less negative and push δωeff towards the SER [red curve in Figs. 3(g)].

    Based on the above simulations, we can summarize that the backward tuning in method-1 was used to reduce the soliton number, and forward tuning balances the decreasing δωΘ2 [arrow in Fig. 3(f)]. Soliton number reduction mainly occurs due to dispersive wave emission, and the first backward tuning mainly contributes to balancing increasing δωΘ1 [arrow in Fig. 3(i)] in method-2. The choice of method-1 or method-2 depends on the microresonator characteristics. Method-1 works better for microresonators with relatively weak dispersion waves. Since soliton number reduction in backward tuning is random, whether solitons can be stabilized is also random. If there are strong dispersive wave emissions, method-2 may be used and is more deterministic.

    C. Requirement on Laser Sweep Speed

    A key parameter is the minimum laser sweep speed needed to stabilize soliton microcombs. In general, a lower laser sweep speed relaxes the hardware burden, reduces noise transduction from VCO, and is favored. Here, our analysis assumed a loaded Q-factor of about 1 million (same parameters as in Sections 3.A and 3.B except that Γ is set as 2π×2.2  GHz to better induce a two-soliton state), and the needed laser sweep speed can be lower for higher-Q-factor (narrower cavity linewidth) cases. Simulations show that our methods remain effective for microcavities with lower Q-factors, but the actual laser sweep waveform needs to be optimized.

    To investigate the low sweep speed limit, we first simulated the sweep rate needed in stage-i to initiate solitons. We started the linear forward sweep from 2.5κ and stopped at different δω0 to see if transient solitons were generated. The minimum and maximum ends δω0 that can support a transient two-soliton state under different scan times are shown in Fig. 4(a). After considering thermal effects, δω0 needs to be larger than the case without considering thermal effects. The range for δω0 to support solitons becomes narrower when sweep times become longer.

    Requirement of laser sweep speed for mitigating thermal instability. (a) Simulated upper and lower limits of laser end detuning versus the stage-i scan time. The shaded region is the SER without considering thermal effects. (b) Minimum laser scan speed for stage-i and backward tuning stage-ii versus the stage-i scan time. The intersect can be regarded as the minimum scan speed. (c) Calculated minimum laser scan speed versus thermal relaxation time with different thermal strengths.

    Figure 4.Requirement of laser sweep speed for mitigating thermal instability. (a) Simulated upper and lower limits of laser end detuning versus the stage-i scan time. The shaded region is the SER without considering thermal effects. (b) Minimum laser scan speed for stage-i and backward tuning stage-ii versus the stage-i scan time. The intersect can be regarded as the minimum scan speed. (c) Calculated minimum laser scan speed versus thermal relaxation time with different thermal strengths.

    The minimum forward sweep speed required in stage-i can be determined by the minimum end δω0 and the corresponding sweep time [green dots in Fig. 4(b)]. After obtaining this sweep speed requirement, we studied the lowest backward tuning speed needed to stabilize the solitons. Since we have assumed to reach a two-soliton state in stage-i, one-step backward tuning is sufficient to stabilize solitons in the simulation [see Section 3.B and Figs. 3(g)–3(i)]. This limit was determined by finding the minimum sweep that can prevent δωeff from exiting the SER from the upper boundary in simulations [see inset of Fig. 4(b) for an example]. The needed backward tuning speed increases when the sweep time (speed) for stage-i increases (decreases). Thus, the intersect of these two curves can be regarded as the minimum sweep speed needed. For ξ1,2 and τ1,2 used in Section 3.B, the theoretical minimum sweep speed is 5.2 GHz/µs. It is also interesting to note that backward tuning is not needed when the stage-i scan time is 100 ns and scan speed is 30 GHz/µs in Fig. 4(b), while such a speed still needs an engineered sweep in the experiment. A possible reason is that δωeff needs to be swept close to the upper boundary of the SER to enable soliton number reduction via dispersive waves in the experiment, and backward tuning is needed to pull δωeff towards the SER. In the simulation, we assumed a relatively strong dispersive wave, and δωeff is close to the lower boundary of the SER in the analysis; thus, backward tuning is not needed.

    This minimum laser sweep speed mainly depends on the first thermal relaxation process, i.e., α1(ξ1) and τ1. We varied the relaxation time τ1 and α1 to obtain the required laser sweep speed in soliton generation as shown in Fig. 4(c). The minimum sweep speed decreases with longer thermal relaxation times and decreasing α1. The discussion in Fig. 4 focuses on method-2, and the second thermal relaxation process does not impact the soliton generation dynamics much. The used α1 is close to or higher than the measured α. For a relaxation time τ1100  ns, about 10 GHz/µs is enough to stabilize solitons in simulations, consistent with the experimentally used <30  GHz/μs. The added backward plus forward tuning stages in method-1 would require lower scan rates, as they mitigate the second thermal process much slower than the first thermal process dealt with in method-2.

    4. CONCLUSION

    We have demonstrated two methods to mitigate the thermal instability in soliton microcomb generation in AlN microresonators. By adding tuning steps after the first fast laser sweep stage, solitons can be stabilized with intermediate sweep speeds. AlN is promising for visible photonics, and the demonstrated methods may be used for visible soliton generation. The engineered laser sweep protocol relaxes the requirement of laser sweep speed; thus, lower bandwidth function generators or even field programmable gate arrays (FPGAs) can be used to drive the SSBM module, which would greatly benefit system miniaturization. It can also reduce the noise transduction from the drive to the pump frequency noise via the VCO. Our experiment and simulation also reveal how thermal relaxation processes occurring on different time scales impact the soliton generation dynamics. Our work focused on soliton generation in microresonators with fast thermal relaxation, and the methods should also work for materials with strong thermal strength such as AlGaAs and Si microresonators.

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    Kewei Liu, Zihao Wang, Shunyu Yao, Yanan Guo, Jianchang Yan, Junxi Wang, Changxi Yang, Chengying Bao. Mitigating fast thermal instability by engineered laser sweep in AlN soliton microcomb generation[J]. Photonics Research, 2023, 11(8): A10
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