Single pump cascaded stimulated Brillouin scattering (SBS) ring laser gyro

Patent metadata

Field	Value
Publication number	US-9733084-B2
Application number	US-201514882101-A
Country	US
Kind code	B2
Filing date	Oct 13, 2015
Priority date	Sep 9, 2015
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A ring laser gyroscope is provided. The ring laser gyroscope includes an optical ring resonator, an optical source to provide a pump beam at a pump frequency, a beat detector, and an optical clock detector. The pump beam is coupled to the optical ring resonator in the first direction and stimulates a first optical gain curve at a first stokes wave frequency downshifted by a Brillouin stokes frequency from the pump frequency. A first order stimulated Brillouin scattering (SBS) beam propagates in the second direction and a second order SBS beam propagates in the first direction. The beat detector produces an optical beat signal that varies as a function of a frequency difference between the first order SBS beam and the second order SBS beam. The optical clock detector generates a reference frequency signal based on two co-propagating beams.

First claim

What is claimed is:

1. A ring laser gyroscope comprising:
an optical ring resonator configured to propagate optical beams in a first direction and a second direction, the second direction being opposite the first direction, the optical ring resonator including at least one optical coupling region to couple optical beams into and out of the optical ring resonator; and
an optical source to provide a pump beam at a pump frequency, the pump beam being optically coupled to the optical ring resonator in the first direction;
wherein the pump beam stimulates a first optical gain curve at a first stokes wave frequency downshifted by a Brillouin stokes frequency from the pump frequency,
wherein the optical ring resonator has a resonator mode within a bandwidth of the first optical gain curve,
wherein the resonator round-trip loss is less than the first optical gain, so that a first order stimulated Brillouin scattering (SBS) beam propagates in the second direction,
wherein the first order SBS beam stimulates a second optical gain curve at a second stokes wave frequency downshifted by twice the Brillouin Stokes frequency from the pump frequency,
wherein the optical ring resonator has a resonator mode within the bandwidth of the second optical gain curve,
wherein the resonator round-trip loss is less than a second optical gain, so that a second order SBS beam propagates in the first direction; and
the ring laser gyroscope further comprising:
a beat detector configured to produce an optical beat signal that varies as a function of a frequency difference between the first order SBS beam and the second order SBS beam; and
an optical clock detector to generate a reference frequency signal based on two co-propagating beams.

2. The ring laser gyroscope of claim 1 , wherein the optical clock detector is configured to generate the reference frequency signal based on a beat signal between the pump frequency and the second stokes wave frequency, which is downshifted by twice the Brillouin Stokes frequency from the pump frequency.

3. The ring laser gyroscope of claim 1 , wherein the optical clock detector is configured to generate the reference frequency signal based on a beat signal between the first order SBS frequency and a third stokes wave frequency of a third order stimulated Brillouin scattering (SBS) beam, the third stokes wave frequency being downshifted by twice the Brillouin Stokes frequency from the first stokes wave frequency.

4. The ring laser gyroscope of claim 1 , wherein the optical ring resonator is a rigid optical waveguide resonator.

5. The ring laser gyroscope of claim 1 , wherein the optical ring resonator is an N-turn waveguide loop with N−1 single-layer crossovers, where N is a positive integer greater than 1.

6. The ring laser gyroscope of claim 1 , further comprising:
a pump rejection filter configured to reject the pump beam after the co-propagating pump beam and the second order SBS beam are output from the optical ring resonator.

7. The ring laser gyroscope of claim 6 , wherein the pump rejection filter is a filtering-ring resonator, the filtering-ring resonator further configured to couple the second order SBS beam to co-propagate with the first order SBS beam to be incident on the beat detector.

8. The ring laser gyroscope of claim 1 , further comprising:
a substrate on which the optical ring resonator is formed and on which the optical source to provide the pump beam is positioned.

9. The ring laser gyroscope of claim 1 , further comprising:
a substrate on which the optical ring resonator is formed and on which the optical source to provide the pump beam is positioned; and
electronics positioned on the substrate and configured to process optical beams output from the optical ring resonator to measure rotation.

10. A ring laser gyroscope comprising:
an optical ring resonator formed on a substrate and configured to propagate optical beams in a first direction and a second direction, the second direction being opposite the first direction, the optical ring resonator having at least one optical coupling region to couple optical beams into and out of the optical ring resonator;
an optical source positioned on the substrate, the optical source configured to optically couple a pump beam at a pump frequency into the optical ring resonator to propagate in the first direction,
wherein the pump beam stimulates a first optical gain curve at a first stokes wave frequency downshifted by a Brillouin stokes frequency from the pump frequency,
wherein the optical ring resonator has a resonator mode within a bandwidth of the first optical gain curve,
wherein the resonator round-trip loss is less than the first optical gain, so that a first order stimulated Brillouin scattering (SBS) beam propagates in the second direction,
wherein the first order SBS beam stimulates a second optical gain curve at a second stokes wave frequency downshifted by twice the Brillouin Stokes frequency from the pump frequency,
wherein the optical ring resonator has a resonator mode within the bandwidth of the second optical gain curve,
wherein the resonator round-trip loss is less than a second optical gain, so that a second order SBS beam propagates in the first direction; and
the ring laser gyroscope further comprising:
a beat detector positioned on the substrate and configured to produce an optical beat signal that varies as a function of a frequency difference between the first order SBS beam and the second order SBS beam;
an optical clock detector positioned on the substrate, the optical clock configured to generate a reference frequency signal based on two co-propagating beams; and
a pump rejection filter to reject the pump beam from the second order SBS beam after the pump beam and the second order SBS beam propagating in the first direction are output from the optical ring resonator.

11. The ring laser gyroscope of claim 10 , wherein the optical clock detector is configured to generate the reference frequency signal based on a beat signal between the pump frequency and the second stokes wave frequency, which is downshifted by twice the Brillouin Stokes frequency from the pump frequency.

12. The ring laser gyroscope of claim 10 , wherein the optical clock detector is configured to generate the reference frequency signal based on a beat signal between the first order SBS frequency and a third stokes wave frequency of a third order stimulated Brillouin scattering (SBS) beam, the third stokes wave frequency being downshifted by twice the Brillouin Stokes frequency from the first stokes wave frequency.

13. The ring laser gyroscope of claim 10 , wherein the optical ring resonator is an N-turn waveguide loop with N−1 single-layer crossovers, where N is a positive integer greater than 1.

14. The ring laser gyroscope of claim 10 , wherein the pump rejection filter is a filtering-ring resonator, which is formed in the substrate and is further configured to couple the second order SBS beam to co-propagate with the first order SBS beam to be incident on the beat detector.

15. The ring laser gyroscope of claim 14 , wherein the optical ring resonator is a rigid optical waveguide resonator and the filtering-ring resonator is a rigid optical waveguide resonator.

16. The ring laser gyroscope of claim 10 , wherein the optical ring resonator is a rigid optical waveguide resonator.

17. A method for measuring rotation, the method comprising:
propagating the optical pump beam through an optical ring resonator in a first direction;
stimulating, from the optical pump beam, a first order stimulate

Assignees

• Honeywell Int Inc

Inventors

• Salit Mary K
• Wu Jianfeng
• Qiu Tiequn

Classifications

• G01C19/66 Primary

  Ring laser gyrometers · CPC title

• G01C19/661 Primary

  details · CPC title

• G01C19/727 Primary

  using a passive ring resonator · CPC title