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Bimaterial Thermal Compensators for WGM Resonators
 Created: Wednesday, 01 October 2008
Net thermal drifts of spectra would be cancelled to first order.
Bimaterial thermal compensators have been proposed as inexpensive means of preventing (to first order) or reducing temperaturerelated changes in the resonance frequencies of whisperinggallery mode (WGM) optical resonators. A bimaterial compensator would apply, to a WGM resonator, a pressure that would slightly change the shape of the resonator and thereby change its resonance frequencies. Through suitable choice of the compensator dimensions and materials, it should be possible to make the temperature dependence of the pressureinduced frequency shift equal in magnitude and opposite in sign to the temperature dependence of the frequency shift of the uncompensated resonator so that, to first order, a change in temperature would cause zero net change in frequency.
dƒ/dT ≈ δƒ/δT + (δƒ/δF)S_{2}E_{2}(α_{2}α_{1})
where ƒ is the resonance frequency, T is temperature, δƒ/δT is the rate of change of frequency as a function of temperature of the uncompensated resonator, δƒ/δF is the rate of change of frequency as a function of applied force F at constant temperature, S_{2} is the effective crosssectional area of the spacer, and E_{2} is the modulus of elasticity of the spacer.
Through appropriate choice of materials and geometry, one could obtain temperature compensation — that is, one could make δƒ/δT ≈ 0. For example, the effective spacer crosssectional area for temperature compensation is given by
S_{2} ≈ (δƒ/δT)/[(δƒ/δF)E_{2}(α_{1}α_{2})].
Because it would be exceedingly difficult to fabricate the spacer to the precise required cross section, the spacer would have a wedge total cross section extending beyond the disk diameter, so that the effective cross section could be varied by moving the spacer. As part of the process of fabricating the temperaturecompensated WGM resonator, the resonatorandcompensator assembly would be installed on a thermoelectric cooler, which would be used to impose an oscillating temperature on the resonator. The resulting synchronous oscillation of the optical spectrum of the resonator would be monitored on an oscilloscope. The position of the spacer would be shifted in small increments until the synchronous oscillations of the spectrum were reduced to zero.
This work was done by Anatoliy Savchenkov, Nan Yu, Lute Maleki, Vladimir Iltchenko, Andrey Matsko, and Dmitry Strekalov of Caltech for NASA’s Jet Propulsion Laboratory. For more information, contact This email address is being protected from spambots. You need JavaScript enabled to view it.. NPO44441
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