Multiple axis gimbal employing nested spherical shells

• US 7,905,463 B2
• Filed: 12/13/2005
• Issued: 03/15/2011
• Est. Priority Date: 12/13/2004
• Status: Expired due to Fees

• Current Assignee: Optical Alchemy, Inc.
• Original Assignee: Optical Alchemy, Inc.
• Inventors: Burnham, Heidi, Daigle, Marc
• Primary Examiner(s): King; Anita M
• Application Number:
  US11/909,129
• Publication Number:
  US 20100019120A1
• Time in Patent Office: 1,918 Days
• Field of Search: 248/177.1, 248/660, 248/550, 248/637, 248/184.1, 248/274.1, 396/12, 396/13, 348/144, 348/147, 348/211, 348/99, 74/53.4
• US Class Current: 248/550
• CPC Class Codes: F16M 11/123 the axis of rotation intersecting in a single point, e.g. by using gimbals
• CPC Class Codes: F16M 11/18 with mechanism for moving the apparatus relatively to the stand
• CPC Class Codes: F41A 27/14 Central-pivot bearings
• CPC Class Codes: F41G 3/22 for vehicle-borne armament, e.g. on aircraft
• CPC Class Codes: Y10T 74/1221 Multiple gyroscopes

Abstract

A multi-axis gimbal has each axis defined by a respective spherical shell driven by a flat, compact motor attached to the driven shell and to a next outer shell (or to an external mounting platform, in the case of the outermost shell). The shells rotate about respective axes. In one configuration, the outermost shell is referred to as the “azimuth” shell because in use it rotates about a vertical axis. The next inner shell is an elevation shell that rotates about a first horizontal axis that is orthogonal to the axis of the camera or other sensor payload. An optional third shell can be used to provide “roll” motion, such as rotating a camera about its axis to obtain a particular rotational orientation with respect to a target.

Claims

1. A gimbal for controlling the orientation of a sensor payload to be carried by the gimbal, comprising:

a substantially spherical first shell configured for rotation about a first axis; and

a payload support structure disposed within and rotatably coupled to the first shell by a direct-drive rotational motor disposed between the first shell and the payload support structure, the direct-drive rotational motor having (i) a rotor housing attached to one of the first shell and the payload support structure and (ii) a stator housing attached to the other of the first shell and the payload support structure, the payload support structure being configured for rotation about a second axis with respect to the first shell, the second axis being orthogonal to the first axis,

wherein the rotor housing and stator housing rotate with respect to each other about the second axis.

2. A gimbal according to claim 1, wherein the first shell is an outermost shell of the gimbal.

3. A gimbal according to claim 1, further comprising a second shell in which the first shell is rotatably disposed, the second shell being rotatable about a third axis orthogonal to both the first and second axes.

4. A gimbal according to claim 1, wherein the first shell includes a ribbed or pocketed structure to reduce weight and increase stiffness.

5. A gimbal according to claim 1, wherein the payload support structure is a substantially spherical second shell.

6. A gimbal according to claim 5, further comprising an air bearing and low-friction support pads between the first and second shells.

7. A gimbal according to claim 5, further comprising momentum reaction wheels to adjust gimbal attitude.

8. A gimbal according to claim 5, further comprising high-surface-tension fluid bearings between the first and second shells.

9. A gimbal according to claim 1, wherein the first shell comprises an integral wire channel to hold signal cables.

10. A gimbal according to claim 9, wherein the integral wire channel comprises a depression in the first shell.

11. A gimbal according to claim 1, further comprising a drive assembly including a rotary joint twist capsule for conduction of signals.

12. A gimbal according to claim 1, further comprising a payload operative to pass payload signals wirelessly via a transceiver across the first shell to an external electronic transceiver.

13. A gimbal according to claim 1, further comprising an inertial reference measurement unit (IRMU) on the payload support structure for inertial stabilization.

14. A gimbal according to claim 1, further comprising a slip ring between the first shell and the payload structure to pass signals therebetween.

15. A gimbal according to claim 1, further comprising components of inertial reference measurement unit distributed within the gimbal.