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Switching through symmetry breaking in coupled nonlinear micro-cavities

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Abstract

We describe stable symmetry-breaking states in systems with two coupled nonlinear cavities, using coupled-mode theory and rigorous simulations. Above a threshold input level the symmetric state of the passive Kerr system becomes unstable, and we show how this phenomenon can be employed for switching and flip-flop purposes, using positive pulses only. A device with compact photonic crystal microcavities is proposed by which we numerically demonstrate the principle.

©2006 Optical Society of America

1. Introduction

Symmetry-breaking is at the heart of many physical phenomena. Here, we describe the breaking of left-right symmetry in a nonlinear optical system. In linear symmetric systems the breaking is absent, as superposition of equal inputs from left and right results in equal outputs to the left and right. Here, as usual, the symmetry breakup arises from coupling and feedback between two nonlinearly adjustable modes. In the linear case both modes are excited with the same strength. In the nonlinear case this excitation shifts the resonance frequencies of the modes. Because of the coupling of intensities between the modes, it is possible that the symmetric situation is no longer stable at a certain input power. Then the system will drift to a situation where one mode is more excited than the other, and thus an asymmetric state arises.

Different nonlinearities can instigate the breaking, but we employ the instantaneous Kerr nonlinearity, where the index depends on the intensity of the local field. Previous optical settings in which the pitchfork bifurcation has been explored [1–9] include a Fabry-Pérot cavity with two inputs at an angle [5]. In [7] two coupled cavities are studied, but the nonlinearity stems from two-level atoms. Here, in contrast, we study passive cavities.

The principle can be applied to many different systems in which nonlinear coupled cavities are present. As a possible realistic implementation we study photonic crystal (PhC) defects. These structures possess practically achievable nonlinear effects such as bistability through a folding bifurcation [10, 11], which was recently demonstrated experimentally [12, 13]. Here we extend the switching capabilities by adding another cavity and using inputs from both sides. We show that this system presents a pitchfork bifurcation, that can be flipped with the use of both positive (an increase in intensity) and negative (a dip in intensity) pulses. For certain applications it is much easier to switch with positive pulses only. By use of coupled-mode theory (CMT) we give a precise and simple analytical description of the processes, that agrees well with simulations.

2. Analytical description

The structure, see Fig. 1(a), is described by [14]:

dajdt=[i(ω0+δωj)1τ]aj+dfj+dbj+1,
bj=exp(iϕ)fj+daj,
fj+1=exp(iϕ)bj+1+daj,

for j = 1,2. Here d = iexp(/2)/ √τ, where ϕ represents the phase that depends on the waveguide length and the PhC reflection properties. The nonlinear frequency shift is δωj = - |aj |/(P 0 τ 2), with P 0 the ‘characteristic nonlinear power’ of the cavity [10]. In these equations |aj |2 is the energy in the cavity mode. |fj |2 (resp. |bj |2) represents the power flowing in the (single-mode) waveguide in the forward (resp. backward) direction. Thus, |f 1|2 = PinL (resp. |b 3|2 = PinR ) is the input power from the left (resp. right), and |b 1|2 = PoutL (resp. |f 3|2 = PoutR ) is the output power to the left (resp. right).

In the following we show that asymmetric solutions can exist, even if the system is excited with equal powers from both sides. The analysis is analogous to the one in [5]. We work in the frequency domain, so d/dt becomes . Eliminating f 2 and b 2 we obtain:

[i(ω0ω+δω1)1τ]a1+κ(γa1+a2)=df1,
[i(ω0ω+δω2)1τ]a2+κ(γa2+a1)=db3,

with γ = exp() and κ = d 2/(1 - γ 2). We equate the left sides of Eqs. 4 and 5, as we assume f 1 = b 3, thus equal input power (and phase) from both sides. We take the modulus squared, and after factoring we get:

(AB)[(A2+AB+B2)+2Δ(A+B)+Δ2+14]=0,

with dimensionless cavity energies A = α|a 1|2 and B = α|a 2|2 , where α = -1/(P 0 π). Further-more, the detuning ∆′ = ∆ + tan(ϕ/2), with ∆ = τ(ω 0 - ω). From Eq. 6 we learn that there is the possibility of an asymmetric solution AB, apart from the symmetric solution A = B. The asymmetric solution appears (for certain input powers) if the detuning ∆′ is chosen correctly, and if the solution is stable.

 figure: Fig. 1.

Fig. 1. (a) Schematic of the coupled cavity structure. (b) The PhC device, with 4 periods in between the switches. An electric field distribution is superimposed to illustrate the defect modes.

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We now derive a criterion for ∆′ concerning the existence of the symmetry-breaking solution. The factor for the asymmetric solution (between square brackets in Eq. 6) can be seen as a quadratic equation in B. For the existence of real solutions its discriminant has to be positive: -3A 2 - 4∆′A - 1 > 0. It is positive if A lies between the values (2Δ±4Δ23)3. Thus the asymmetric solution exists if |∆′| > √3/2. For positive nonlinearity (α < 0) one needs A < 0 and thus ∆′ > 0, so one takes ∆′ > √3/2, and vice versa for negative nonlinearity.

Two examples of the input-output curves are shown in Fig. 2. We depict the powers instead of the mode amplitudes, as derived from Eqs. 4 and 5. Note that these curves depend both on ∆ and ϕ, instead of only on ∆′. Calculations of Eqs. 4 and 5 proof this (not shown). Above a certain input power level the symmetric solution becomes unstable, and the system switches to an asymmetric state. Linear stability analysis shows indeed that the symmetric solution destabilizes, if an asymmetric solution exists. More power exits to the left than to the right, or vice versa. It is possible to obtain high contrasts between the left and right output powers; even a zero output in one direction is attainable. At high detuning the shape of the curve becomes more complex, and the asymmetric branch shows multistability, see Fig. 2(b).

 figure: Fig. 2.

Fig. 2. Output power versus input power for (a) ∆ = 1.039, ϕ = 0.570 and (b) ∆ = 2.0, ϕ = 0.595. Stable and unstable states are shown with solid and dashed lines, respectively. Dots show rigorous simulation results.

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3. Numerical modeling

As a model system for rigorous simulations we use the 2D PhC structure depicted in Fig. 1(b). We use a square lattice with period a of squares with side length 0.4a and index 3.5 in air. The two identical defect rods have side 0.6a. The nonlinear material has a realistic nonlinear coefficient n 2 = 2.15 × 10-17m2/W. We use TM-polarization (one E-field component out-of-plane).

From linear calculations with the mode-expansion technique [15], which computes exact solutions of the vectorial Maxwell equations, we obtain that ω 0 = 0.321169(2πc/a) and 1/τ = 1.623 × 10-4(2πc/a), thus Q = ω 0 τ/2 = 990. By changing the intermediate waveguide length the phase ϕ can be varied. We used eight periods between the cavities (thus four more than depicted in Fig. 1(b)); in that case the phase can be linearly approximated by ϕ = -163.9ω/(2πc/a)+2.9.

For precise nonlinear calculations we use an iterative extension of the mode-expansion method, that uses a grid for the nonlinear sections [16]. The method allows to study the stable states in the frequency domain. Only the large defect rods are considered nonlinear, with a 12 × 8-grid. Using the horizontal symmetry plane only one upper half in Fig. 1 needs to be simulated. Furthermore, the linear sections have to be calculated once during iteration at a fixed frequency. The use of 60 eigenmodes is sufficient to obtain converged results. From single switch nonlinear calculations we get P 0 = 3.52MW/m. CMT with these parameters and the rigorous calculations with two switches agree very well, as can be seen in Fig. 2. Note that P 0 is proportional to 1/Q 2 [10], therefore high Q factors give rise to practical switching powers, as already obtained in slab structures [12, 13].

 figure: Fig. 3.

Fig. 3. Output powers versus left input power PinL at ∆ = 1.039, ϕ = 0.570 and PinR = 3.125P 0. Stable states for PoutR (resp. PoutL ) are shown with red (resp. blue) solid lines. Dashed lines indicate unstable states. Dots (resp. circles) show rigorous simulation results for PoutR (resp. PoutL ). Labels AB, CD and EF display key states.

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4. Switching

The system can be switched from one asymmetric state to the other by adding a positive or negative pulse to the side with lower output power. The switching mechanism becomes clear from Fig. 3. Here the input power from the right PinR is held constant, while the one from the left PinL is varied. Starting from state AB, in the situation where PoutR . PoutL , we follow the arrows to the right, if we increase PinL . Eventually this branch stops and we flip to state CD, with PoutR < PoutL . Decreasing PinL we again reach state AB, but now the outputs are flipped. We could also follow the arrows to the left, by decreasing PinL , starting from state AB, again with PoutR > PoutL. Then we reach the left end of the branch, and the solution jumps to the state EF, with PoutR < PoutL. Increasing PinL brings the system to the flipped state AB. Once the system is flipped, one needs to add or remove power at the other side to flip again. This corresponds to changing the left/right labels L and R in Fig. 3.

To ascertain that switching is possible by positive pulses we have performed time-domain simulations of the CMT equations. It was previously shown that these equations provide a highly accurate picture of temporal switching aspects [17]. An example of a state flip is shown in Fig. 4. The same parameters are used as in Fig. 3. At times < 0 all input powers are considered zero. In the beginning after time zero a slight perturbation of PinR brings the system into state AB with PoutR > PoutL. Then at a time 4×104 periods PinL is increased to 3.7P 0, that is able to switch the system into state CD, in agreement with Fig. 3. After a time 9 × 104 periods we equalize the input powers again, PinL = PinR = 3.125P 0, and we obtain the flipped AB state. Other switching aspects, such as flipping with negative pulses and being unable to switch with weak pulses, have also been checked.

 figure: Fig. 4.

Fig. 4. Switching of the state by adding power to the left input PinL Here ∆ = 1.039, ϕ = 0.570 and the period is 2π/ω. After an initial small perturbation of the right input power it is held constant at PinR = 3.125P 0. The dotted (dashed) line shows PinL (PinR ). The blue and red lines depict PoutL and PoutR , respectively.

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In experiments the cavities are not identical. We have checked the case where the resonance frequencies differ, say one has ω0A and ω0B. The solutions are more complex (the states become non-degenerate). However, the functionality remains the same, up until a certain resonance frequency difference. This tolerance depends upon the detuning. With the parameters of Fig. 2(b), a non-optimized value for the tolerance amounts to |ω0A - ω0B|/ωavg < 0.5/Q, with ωavg = (ω0A + ω0B)/2.

In order to separate the counter-propagating beams in the ports one could use a photonic crystal circulator [20], or adjust the design. Note that the related system with two-level atoms in thin coupled films presents a rich time-domain behavior, such as self-sustained pulsations [18]. Therefore, analogous phenomena may be observable in the structure considered here. Furthermore, many PhC-geometries have been studied thus far [19]. It is expected that the study of these elements will reveal other asymmetric states.

5. Conclusion

In conclusion, we study a new switching scheme involving symmetry breaking states in coupled nonlinear cavities. CMT provides simple analytical insight and a good agreement with rigorous simulations is observed. The use of positive pulses for flip-flop operation is described by both frequency- and time-domain results. Symmetry breaking is a powerful principle in nature, and the presented behavior should be general for many types of nonlinearities and devices.

Acknowledgments

BM and PB acknowledge postdoctoral fellowships from the Funds for Scientific Research -Flanders (FWO-Vlaanderen). We acknowledge the Belgian DWTC project IAP-Photon and the NSF MRSEC grant DMR-02-13282.

References and links

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12. M. Notomi, A. Shinya, S. Mitsugi, G. Kira, E. Kuramochi, and T. Tanabe, “Optical bistable switching action of Si high-Q photonic-crystal nanocavities,” Opt. Express 13, 2678–2687 (2005), http://www.opticsinfobase.org/abstract.cfm?URI=oe-13-7-2678. [CrossRef]   [PubMed]  

13. P.E. Barclay, K. Srinivasan, and O. Painter, “Nonlinear response of silicon photonic crystal mi-croresonators excited via an integrated waveguide and fiber taper,” Opt. Express 13, 801–820 (2005), http://www.opticsinfobase.org/abstract.cfm?URI=oe-13-3-801. [CrossRef]   [PubMed]  

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Figures (4)

Fig. 1.
Fig. 1. (a) Schematic of the coupled cavity structure. (b) The PhC device, with 4 periods in between the switches. An electric field distribution is superimposed to illustrate the defect modes.
Fig. 2.
Fig. 2. Output power versus input power for (a) ∆ = 1.039, ϕ = 0.570 and (b) ∆ = 2.0, ϕ = 0.595. Stable and unstable states are shown with solid and dashed lines, respectively. Dots show rigorous simulation results.
Fig. 3.
Fig. 3. Output powers versus left input power PinL at ∆ = 1.039, ϕ = 0.570 and PinR = 3.125P 0. Stable states for PoutR (resp. PoutL ) are shown with red (resp. blue) solid lines. Dashed lines indicate unstable states. Dots (resp. circles) show rigorous simulation results for PoutR (resp. PoutL ). Labels AB, CD and EF display key states.
Fig. 4.
Fig. 4. Switching of the state by adding power to the left input PinL Here ∆ = 1.039, ϕ = 0.570 and the period is 2π/ω. After an initial small perturbation of the right input power it is held constant at PinR = 3.125P 0. The dotted (dashed) line shows PinL (PinR ). The blue and red lines depict PoutL and PoutR , respectively.

Equations (6)

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d a j d t = [ i ( ω 0 + δ ω j ) 1 τ ] a j + d f j + d b j + 1 ,
b j = exp ( i ϕ ) f j + d a j ,
f j + 1 = exp ( i ϕ ) b j + 1 + d a j ,
[ i ( ω 0 ω + δ ω 1 ) 1 τ ] a 1 + κ ( γ a 1 + a 2 ) = d f 1 ,
[ i ( ω 0 ω + δ ω 2 ) 1 τ ] a 2 + κ ( γ a 2 + a 1 ) = d b 3 ,
( A B ) [ ( A 2 + A B + B 2 ) + 2 Δ ( A + B ) + Δ 2 + 1 4 ] = 0 ,
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