Flange-bonded loopback for fiber-optic gyroscope (FOG)

Patent metadata

Field	Value
Publication number	US-11047688-B2
Application number	US-201715783299-A
Country	US
Kind code	B2
Filing date	Oct 13, 2017
Priority date	Oct 13, 2017
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

One example includes fiber optic gyroscope (FOG) assembly. The FOG assembly includes a spool comprising a flange. The FOG assembly also includes an optical fiber comprising an optical fiber coil portion that is counter-wound in a first orientation and a second orientation opposite the first orientation. The optical fiber portion can be coupled to the flange. The optical fiber further includes a loopback portion with respect to the first orientation that is secured to the flange.

First claim

What is claimed is:

1. A fiber optic gyroscope (FOG) assembly comprising:
a spool comprising a flange; and
an optical fiber comprising an optical fiber coil portion that is counter-wound in a first orientation and a second orientation opposite the first orientation, the optical fiber portion being coupled to the flange, the optical fiber further comprising a loopback portion with respect to the first orientation that is secured to the flange.

2. The FOG assembly of claim 1 , wherein the optical fiber coil is coupled to a first surface of the flange, and wherein the flange further comprises a second surface opposite the first surface, wherein the loopback portion is coupled to the second surface of the flange.

3. The FOG assembly of claim 2 , wherein the optical fiber further comprises a first transition portion associated with the first orientation, a second transition portion associated with the second orientation, and a longitudinal coupling portion that are secured to the second surface of the flange, wherein the first and second transition portions of the optical fiber are secured to the second surface of the flange and are arranged to be approximately symmetrically arranged with each other on the flange.

4. The FOG assembly of claim 3 , wherein the flange further comprises:
a first notch arranged at a periphery of the flange and being configured to receive the first transition portion of the optical fiber extending from the optical fiber coil portion from the first surface of the flange to the second surface of the flange; and
a second notch arranged at the periphery of the flange and being configured to receive the second transition portion of the optical fiber extending from the optical fiber coil portion from the first surface of the flange to the second surface of the flange.

5. The FOG assembly of claim 3 , wherein the loopback portion comprises at least a portion of the first transition portion and the longitudinal coupling portion.

6. The FOG assembly of claim 1 , wherein the flange comprises a groove preform configured to receive and secure the optical fiber along a length of the groove preform with respect to at least the loopback portion.

7. The FOG assembly of claim 6 , further comprising a buffer material layer disposed on the flange, wherein the groove preform is formed in the buffer material layer to receive the optical fiber for securing the optical fiber comprising the loopback portion to the flange.

8. The FOG assembly of claim 1 , wherein the optical fiber further comprises a first transition portion associated with the first orientation, a second transition portion associated with the second orientation, and a longitudinal coupling portion that are secured to the second surface of the flange, wherein the first and second transition portions of the optical fiber are arranged to be approximately symmetrically arranged with each other on the flange.

9. The FOG assembly of claim 1 , further comprising an optical transceiver configured to generate an optical signal that is provided to each end of the optical fiber, wherein signal paths of the optical signal from each end of the optical fiber to a portion of the optical fiber in which a winding of the spool of the optical fiber reverses orientation is approximately equal.

10. A method of fabricating a fiber optic gyroscope (FOG) assembly, the method comprising:
forming a spool that includes a flange;
forming an optical fiber into an optical fiber coil portion comprising a first orientation of the optical fiber and a second orientation of the optical fiber opposite the first orientation, the optical fiber further comprising a first transition portion extending from the optical fiber coil portion and being associated with the first orientation and a second transition portion extending from the optical fiber coil portion and being associated with the second orientation;
coupling the optical fiber coil portion to the spool; and
securing the first transition portion, the second transition portion, and a loopback portion of the optical fiber to the flange.

11. The method of claim 10 , wherein forming the spool comprises forming the spool and the flange to be integral with respect to a fabrication material associated with each of the spool and the flange.

12. The method of claim 10 , wherein coupling the optical fiber coil portion to a first surface of the flange, and wherein securing the first and second transition portions and the loopback portion of the optical fiber coil comprises securing the first transition portion, the second transition portion, and the loopback portion to a second surface of the flange opposite the first surface of the flange.

13. The method of claim 12 , further comprising:
forming a first notch in a periphery of the flange, wherein securing the first transition portion to the second surface of the flange comprises extending the first transition portion from the optical fiber coil portion on the first surface of the flange to the second surface of the flange via the first notch; and
forming a second notch in the periphery of the flange, wherein securing the second transition portion to the second surface of the flange comprises extending the second transition portion from the optical fiber coil portion on the first surface of the flange to the second surface of the flange via the second notch.

14. The method of claim 10 , wherein the securing the first and second transition portions and the loopback portion of the optical fiber coil comprises securing the first and second transition portions such that the first and second transition portions of the optical fiber are arranged to be approximately symmetrically arranged with respect to each other on the flange between the optical coil portion and a longitudinal coupling portion of the optical fiber.

15. The method of claim 10 , further comprising:
depositing a buffer material on the flange; and
forming a groove preform in the buffer material, wherein securing the first and second transition portions and the loopback portion of the optical fiber coil comprises securing the first transition portion, the second transition portion, and the loopback portion of the optical fiber to the flange in the groove preform.

16. A fiber optic gyroscope (FOG) assembly comprising:
a spool comprising a flange;
a buffer material coupled to the flange, the buffer material comprising a groove preform patterned into the buffer material; and
an optical fiber comprising an optical fiber coil portion that is counter-wound in a first orientation and a second orientation opposite the first orientation, the optical fiber portion being coupled to the flange, the optical fiber further comprising a loopback portion with respect to the first orientation that is secured to the flange via the groove preform.

17. The FOG assembly of claim 16 , wherein the optical fiber coil is coupled to a first surface of the flange, and wherein the flange further comprises a second surface opposite the first surface, wherein the loopback portion is coupled to the second surface of the flange.

18. The FOG assembly of claim 17 , wherein the optical fiber further comprises a first transition portion associated with the first orientation, a second transition portion associated with the second orientation, and a longitudinal coupling portion that are secured to the second surface of the flange, wherein the first and second transition portions of the optical fiber are secured to the second surface of the flange and are arranged to be approximately symmetrically arranged wi

Assignees

• Kim Steven M
• Lovstedt Stephan P
• Zimmerman Gregory A
• Snow Wesley A
• Saxena Ragini
• Rosete Ricardo A
• Northrop Grumman Systems Corp

Inventors

• Kim Steven M
• Lovstedt Stephan P
• Zimmerman Gregory A
• Snow Wesley A
• Saxena Ragini
• Rosete Ricardo A

Classifications

• G01C19/722 Primary

  of the mechanical construction · CPC title

• G01C19/726 Primary

  Phase nulling gyrometers, i.e. compensating the Sagnac phase shift in a closed loop system · CPC title