Forward looking turret

Patent metadata

Field	Value
Publication number	US-9718561-B2
Application number	US-201414502358-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Sep 30, 2014
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A gimbal mechanism for a turret includes a support member and a pair of opposing yoke arms extending from the support member. The pair of opposing yoke arms define a first axis. A sphere is rotatably mounted between the opposing yoke arms for rotation about the first axis. A disk is rotatably mounted within the sphere for rotation about a second axis perpendicular to the first axis. The disk is sized for rotation within the sphere. The second axis may be offset from the first axis. An aperture is provided in the disk. The sphere includes a slot within which the aperture is moveable in response to rotation of the disk about the second axis. The aperture is movable to define a field of coverage in response to rotation of the sphere about the first axis and the disk about the second axis.

First claim

What is claimed is:

1. A gimbal mechanism for a turret, comprising:
a support member;
a pair of opposing yoke arms extending from the support member, the pair of opposing yoke arms defining a first axis;
a sphere rotatably mounted between the opposing yoke arms for rotation about the first axis;
a disk rotatably mounted within the sphere for rotation about a second axis perpendicular to the first axis, the disk including a diameter slightly smaller than the sphere that permits rotation of the disk within the sphere, wherein the second axis is offset from the first axis;
an aperture provided in the disk, wherein the sphere comprises a slot within which the aperture is moveable between a position proximate each of the pair of opposing yoke arms in response to rotation of the disk about the second axis, the aperture being movable to define a field of coverage in response to rotation of the sphere about the first axis and the disk about the second axis;
an optical system, wherein the disk comprises at least an element of the optical system housed within the disk, the optical system being configured for transmitting and receiving optical signals via the aperture; and
an optical path for transmitting optical signals from an optical signal transmitter to the optical system.

2. The gimbal mechanism of claim 1 , wherein the support member comprises a pod mountable to an aircraft, wherein the sphere is mounted by the opposing yoke arms extending partially from an open circular end of the pod, the sphere and open circular end of the pod being configured to substantially prevent drag and allow rotation of the sphere within the pod.

3. The gimbal mechanism of claim 1 , further comprising a bearing interface associated with each yoke arm that rotatably connects the sphere to each opposing yoke arm for rotation of the sphere about the first axis.

4. The gimbal mechanism of claim 3 , further comprising:
a bulkhead disposed behind the sphere within an open end of the support member between the pair of opposing yoke arms; and
a drive mechanism mounted to the bulkhead that rotates the sphere about the first axis.

5. The gimbal mechanism of claim 4 , wherein the drive mechanism comprises dual opposing drive assemblies that contact the sphere and rotate the sphere about the first axis, the dual opposing drive assemblies work against one another to prevent backlash, rotation of the sphere in one direction or in an opposite direction is caused by generating a different torque in each dual opposing drive assembly so that the torque in one dual opposing drive assembly overcomes the torque in the other dual opposing drive assembly to rotate the sphere.

6. The gimbal mechanism of claim 4 , further comprising:
an encoder scale provided on the sphere; and
an encoder reader mounted on the bulkhead to read the encoder scale and detect a position of the aperture about the first axis.

7. The gimbal mechanism of claim 1 , wherein the optical path comprises a coudé optical path for transmitting the optical signals from the optical signal transmitter to the optical system.

8. The gimbal mechanism of claim 7 , further comprising a roller bearing on each side of the disk to rotatably couple the disk to an interior bulkhead of the sphere, wherein each roller bearing comprises a toroid shape with an opening for the coudé optical path.

9. The gimbal mechanism of claim 8 , wherein the disk comprises a truncated sphere with a semi spherical portion on opposite sides removed.

10. The gimbal mechanism of claim 9 , further comprising an electrical drive motor associated with at least one of the roller bearings for rotating the disk about the second axis.

11. A forward looking turret, comprising:
a pod;
a pair of opposing yoke arms extending from the pod, the pair of opposing yoke arms defining a first axis;
a sphere rotatably mounted between the opposing yoke arms for rotation about the first axis, the sphere extending partially from an open circular end of the pod, the sphere and open circular end of the pod being configured to substantially prevent drag and allow rotation of the sphere within the pod;
a bulkhead disposed behind the sphere within the pod;
a drive mechanism mounted to the bulkhead that rotates the sphere about the first axis;
a disk rotatably mounted within the sphere for rotation about a second axis perpendicular to the first axis, the disk including a diameter slightly smaller than the sphere that permits rotation of the disk within the sphere, wherein the second axis is offset from the first axis;
an aperture provided in the disk, wherein the sphere comprises a slot within which the aperture is moveable between a position proximate each of the pair of opposing yoke arms in response to rotation of the disk about the second axis, the aperture being movable to define a field of coverage in response to rotation of the sphere about the first axis and the disk about the second axis;
an optical system, wherein the disk comprises at least an element of the optical system housed within the disk, the optical system being configured for transmitting and receiving optical signals via the aperture; and
an optical path for transmitting optical signals from an optical signal transmitter to the optical system.

12. The forward looking turret of claim 11 further comprising a bearing interface associated with each yoke arm that rotatably connects the sphere to each opposing yoke arm, wherein the drive mechanism comprises dual opposing drive assemblies that contact the sphere and rotate the sphere about the first axis, the dual opposing drive assemblies work against one another to prevent backlash, rotation of the sphere in one direction or in an opposite direction is caused by generating a different torque in each dual opposing drive assembly so that the torque in one dual opposing drive assembly overcomes the torque in the other dual opposing drive assembly to rotate the sphere.

13. The forward looking turret of claim 12 , further comprising:
an encoder scale provided on the sphere; and
an encoder reader mounted on the bulkhead to read the encoder scale and detect a position of the aperture about the first axis.

14. The forward looking turret of claim 12 ,
wherein the optical path comprises a coudé optical path for transmitting optical signals from an optical signal transmitter to the optical system.

15. The forward looking turret of claim 14 , further comprising a roller bearing on each side of the disk to rotatably couple the disk to an interior bulkhead of the sphere, wherein each roller bearing comprises a toroid shape with an opening for the coudé optical path.

16. The forward looking turret of claim 15 , further comprising an electrical drive motor associated with at least one of the roller bearings for rotating the disk about the second axis.

17. A method for providing a forward looking turret, comprising:
providing a pod including a pair of opposing yoke arms extending from the pod, the pair of opposing yoke arms defining a first axis;
rotatably mounting a sphere between the opposing yoke arms for rotation about the first axis, the sphere extending partially from an open circular end of the pod, the sphere and open circular end of the pod being configured to substantially prevent drag and allow rotation of the sphere within the pod;
providing a bulkhead disposed behind the sphere within the pod;
providing a drive mechanism mounted to the bulkhead, the drive mechanism being configured to rotate the sphere about the first axis;
rotatably mounting a disk within the sphere for rotation

Assignees

• Boeing Co

Inventors

• Blackburn John P
• Sparks Ryan D

Classifications

• G08B13/19619

  Details of casing · CPC title

• F16M11/10

  around a horizontal axis {(F16M11/12 takes precedence)} · CPC title

• B64D47/08 Primary

  Arrangements of cameras · CPC title

• F16M11/18

  with mechanism for moving the apparatus relatively to the stand · CPC title

• G08B13/19632

  Camera support structures, e.g. attachment means, poles · CPC title