Ring laser gyroscope with ion migration field reducer shield

Patent metadata

Field	Value
Publication number	US-10330477-B2
Application number	US-201715452961-A
Country	US
Kind code	B2
Filing date	Mar 8, 2017
Priority date	Mar 8, 2017
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A ring laser gyroscope comprises a laser block that includes a resonant internal cavity defined by a plurality of surfaces of an optical closed loop pathway, and a plurality of electrodes coupled to the laser block. The electrodes are configured to generate a pair of counter-propagating laser beams from a lasing gas in the optical closed loop pathway. The ring laser gyroscope also includes a field reducer shield comprising an electrically conductive material, with the field reducer shield located completely within the laser block. The field reducer shield is configured to modify an electric field generated by the plurality of electrodes to substantially prevent ions in the laser block from migrating toward the plurality of surfaces of the optical closed loop pathway.

First claim

What is claimed is:

1. A ring laser gyroscope, comprising:
a laser block that includes a resonant internal cavity defined by a plurality of surfaces of an optical closed loop pathway;
a plurality of electrodes coupled to the laser block, the electrodes configured to generate a pair of counter-propagating laser beams from a lasing gas in the optical closed loop pathway, wherein the plurality of electrodes include a cathode mounted on a first side of the laser block, a first anode mounted on a second side of the laser block, and a second anode mounted on a third side of the laser block, wherein the anodes have a first negative electric potential, and the cathode has a second negative electric potential that is less than the first negative electric potential; and
a field reducer shield comprising an electrically conductive material, the field reducer shield located completely within the laser block, wherein the field reducer shield has an intermediate electric potential that is between the first negative electric potential and the second negative electric potential;
wherein the field reducer shield is configured to modify an electric field generated by the plurality of electrodes to substantially prevent ions in the laser block from migrating toward the plurality of surfaces of the optical closed loop pathway.

2. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises a unitary conductive segment having a curved, semi-circular shape.

3. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises a unitary conductive segment having a straight configuration.

4. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises a unitary conductive segment having an angled configuration.

5. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises multiple conductive pins each separately located in the laser block in a substantially straight line configuration.

6. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises multiple conductive pins each separately located in the laser block in a curved configuration.

7. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises a metal or metal alloy material.

8. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises a conductive film.

9. The ring laser gyroscope of claim 1 , wherein the field reducer shield comprises copper, aluminum, a nickel-iron alloy, or combinations thereof.

10. The ring laser gyroscope of claim 1 , wherein the laser block comprises a glass ceramic material.

11. The ring laser gyroscope of claim 10 , wherein the glass ceramic material comprises lithium aluminosilicate.

12. The ring laser gyroscope of claim 11 , wherein the field reducer shield reduces migration of lithium ions in the laser block.

13. The ring laser gyroscope of claim 1 , further comprising a dither motor operatively coupled with the laser block in a central area of the laser block.

14. The ring laser gyroscope of claim 13 , wherein the dither motor has a ground electric potential.

15. The ring laser gyroscope of claim 14 , wherein the field reducer shield is located between the dither motor and the cathode, such that the field reducer shield modifies an electrical gradient between the dither motor and the cathode.

16. A ring laser gyroscope, comprising:
a laser block that includes a resonant internal cavity defined by a plurality of surfaces of an optical closed loop pathway, the optical closed loop pathway configured to contain a lasing gas, wherein the laser block comprises a glass ceramic material;
a plurality of electrodes coupled to the laser block, the electrodes configured to apply an electric potential through the lasing gas to create a gas plasma discharge region in the optical closed loop pathway to generate a pair of counter-propagating laser beams, wherein the plurality of electrodes include a cathode mounted on a first side of the laser block, a first anode mounted on a second side of the laser block, and a second anode mounted on a third side of the laser block, wherein the anodes have a first negative electric potential, and the cathode has a second negative electric potential that is less than the first negative electric potential;
a dither motor operatively coupled with the laser block in a central area of the laser block, wherein the dither motor has a ground electric potential; and
a field reducer shield comprising an electrically conductive material, the field reducer shield located completely within the laser block and adjacent to the dither motor, wherein the field reducer shield has an intermediate electric potential that is between the first negative electric potential and the second negative electric potential;
wherein the field reducer shield is located between the dither motor and the cathode, such that the field reducer shield modifies an electrical gradient between the dither motor and the cathode, to substantially prevent ions in the laser block from migrating toward the plurality of surfaces of the optical closed loop pathway.

17. The ring laser gyroscope of claim 16 , wherein the field reducer shield comprises a unitary conductive segment having a curved, semi-circular shape.

18. The ring laser gyroscope of claim 16 , wherein the field reducer shield comprises a unitary conductive segment having a straight configuration.

19. The ring laser gyroscope of claim 16 , wherein the field reducer shield comprises a unitary conductive segment having an angled configuration.

20. The ring laser gyroscope of claim 16 , wherein the field reducer shield comprises multiple conductive pins each separately located in the laser block in a substantially straight line configuration or in a curved configuration.

Assignees

• Honeywell Int Inc

Inventors

• Baker Stephen Matthew
• Johnson Dean Eivind
• Clark Matthew

Classifications

• G01C19/661 Primary

  details · CPC title

• H01S3/0835

  Gas ring lasers · CPC title

• H01S3/2222

  Neon, e.g. in helium-neon (He-Ne) systems · CPC title

• H01S3/038

  Electrodes, e.g. special shape, configuration or composition · CPC title

• H01S3/03

  of gas laser discharge tubes · CPC title