Stimulated Brillouin scattering (SBS) gyro with coupled resonator for frequency-dependent output coupling

Patent metadata

Field	Value
Publication number	US-9772187-B2
Application number	US-201615052490-A
Country	US
Kind code	B2
Filing date	Feb 24, 2016
Priority date	Feb 24, 2016
Publication date	Sep 26, 2017
Grant date	Sep 26, 2017

Abstract

A ring laser gyroscope (RLG) is provided. The RLG includes a primary resonator, a secondary resonator, and an optical source to provide a pump field. The pump field in the primary resonator stimulates an optical gain curve at a first stokes wave frequency. A first order SBS field stimulates a second optical gain curve at a second stokes wave frequency. The second order SBS gain gives rise to a frequency-shifted field propagating in the first direction. The fraction of the pump field that couples out of the primary resonator, through the secondary resonator, and out of the secondary resonator is larger than the fraction of: the first order SBS field that couples out of the primary resonator, through the secondary resonator, and out of the secondary resonator; and a second order SBS field that couples out of the primary resonator, through the secondary resonator, and out of the secondary resonator.

First claim

What is claimed is:

1. A ring laser gyroscope comprising:
a primary-optical-ring resonator configured to guide optical fields in a first direction and a second direction, the second direction being opposite the first direction, the primary-optical-ring resonator including at least one optical coupling region to couple optical fields into and out of the primary-optical-ring resonator;
an optical source to provide a pump field at a pump frequency that is on resonance with the primary-optical-ring resonator; and
a secondary-optical-ring resonator including at least two optical coupling regions, one of which couples optical fields into and out of the primary-optical-ring resonator, and one of which couples the pump field into and out of the secondary-optical-ring resonator,
wherein the pump field couples into the primary-optical-ring resonator from the secondary-optical-ring resonator,
wherein the pump field in the primary-optical-ring resonator stimulates a first optical gain curve at a first stokes wave frequency downshifted by a Brillouin stokes frequency from the pump frequency,
wherein the primary-optical-ring resonator has a resonator mode within a bandwidth of the first optical gain curve,
wherein the SBS gain gives rise to a frequency-shifted field propagating in the second direction,
wherein a first order SBS field 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 primary-optical-ring resonator has a resonator mode within the bandwidth of the second optical gain curve,
wherein the second order SBS gain gives rise to a frequency-shifted field propagating in the first direction,
wherein the fraction of the pump field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator is larger than:
1) the fraction of the first order SBS field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator; and
2) the fraction of a second order SBS field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator.

2. The ring laser gyroscope of claim 1 , 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 field and the second order SBS field; and
an optical clock detector to generate a reference frequency signal based on two co-propagating fields.

3. The ring laser gyroscope of claim 2 , 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.

4. The ring laser gyroscope of claim 2 , 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) field, the third stokes wave frequency being downshifted by twice the Brillouin Stokes frequency from the first stokes wave frequency.

5. The ring laser gyroscope of claim 1 , wherein the primary-optical-ring resonator and the secondary-optical-ring resonator are rigid optical waveguide resonators.

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

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

8. The ring laser gyroscope of claim 7 , 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 field and the second order SBS field; and
an optical clock detector to generate a reference frequency signal based on two co-propagating fields,
wherein the pump rejection filter is a filtering-ring resonator, the filtering-ring resonator further configured to couple the second order SBS field to co-propagate with the first order SBS field to be incident on the beat detector.

9. The ring laser gyroscope of claim 1 , further comprising:
a substrate on which the primary-optical-ring resonator is formed, on which the secondary-optical-ring resonator is formed, and on which the optical source to provide the pump field is positioned.

10. The ring laser gyroscope of claim 1 , further comprising:
a substrate on which the primary-optical-ring resonator is formed, on which the secondary-optical-ring resonator is formed, and on which the optical source to provide the pump field is positioned; and
electronics positioned on the substrate and configured to process optical fields output from the secondary-optical-ring resonator to measure rotation.

11. A ring laser gyroscope comprising:
a primary-optical-ring resonator formed on a substrate and configured to guide optical fields in a first direction and a second direction, the second direction being opposite the first direction, the primary-optical-ring resonator including at least one optical coupling region to couple optical fields into and out of the primary-optical-ring resonator;
an optical source positioned on the substrate to provide a pump field at a pump frequency that is on resonance with the primary-optical-ring resonator; and
a secondary-optical-ring resonator formed on the substrate, the secondary-optical-ring resonator including at least two optical coupling regions, one of which couples optical fields into and out of the primary-optical-ring resonator, and one of which couples the pump field into and out of the secondary-optical-ring resonator,
wherein the pump field couples into the primary-optical-ring resonator from the secondary-optical-ring resonator,
wherein the pump field in the primary-optical-ring resonator stimulates a first optical gain curve at a first stokes wave frequency downshifted by a Brillouin stokes frequency from the pump frequency,
wherein the primary-optical-ring resonator has a resonator mode within a bandwidth of the first optical gain curve,
wherein the SBS gain gives rise to a frequency-shifted field propagating in the second direction,
wherein a first order SBS field 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 primary-optical-ring resonator has a resonator mode within the bandwidth of the second optical gain curve,
wherein the second order SBS gain gives rise to a frequency-shifted field propagating in the first direction,
wherein the fraction of the pump field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator is larger than:
1) the fraction of the first order SBS field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator; and
2) the fraction of a second order SBS field that couples out of the primary-optical-ring resonator, through the secondary-optical-ring resonator, and out of the secondary-optical-ring resonator.

12. The ring laser gyroscope

Assignees

• Honeywell Int Inc

Inventors

• Salit Mary K
• Wu Jianfeng
• Qiu Tiequn

Classifications

• H01S3/1086

  using scattering effects, e.g. Raman or Brillouin effect · CPC title

• H01S3/06791

  Fibre ring lasers (fibre laser gyrometers G01C19/72) · CPC title

• G01C19/661 Primary

  details · CPC title

• H01S3/083

  Ring lasers {(fibre ring lasers H01S3/06791)} · CPC title

• H01S3/30

  using scattering effects, e.g. stimulated Brillouin or Raman effects · CPC title