Multi-arm gimbal system

• US 9,534,730 B2
• Filed: 08/25/2011
• Issued: 01/03/2017
• Est. Priority Date: 08/26/2010
• Status: Active Grant

• Current Assignee: Garrett W. Brown
• Original Assignee: Garrett W. Brown
• Inventors: Black, Micah, Sacksteder, Anthony D.
• Primary Examiner(s): WOOD, KIMBERLY T
• Application Number:
  US13/217,772
• Publication Number:
  US 20120049035A1
• Time in Patent Office: 1,958 Days
• Field of Search: 248/122.1, 248/123.11, 248/636, 248/288.11, 248/292.11, 248/292.13, 248/278.1, 248/279.1, 248/287.1, 248/660, 248/661, 248/662, 248/664, 248/667, 384/513, 295/250.1
• US Class Current: 1/1
• CPC Class Codes: F16M 11/10 around a horizontal axis F16M11/12 takes precedence
• CPC Class Codes: F16M 11/2071 for panning and rolling F16M11/2078 takes precedence
• CPC Class Codes: F16M 2200/041 for balancing rotational movement of the head
• CPC Class Codes: Y10T 29/49826 Assembling or joining

Abstract

The invention provides a gimbal support apparatus to support tools or other payloads for use during performance of tasks using those payloads. The payload can be selectively biased to achieve an optimum position for performance of the task. The gimbal support apparatus comprises rotationally connected gimbal arms that can be adjusted with respect to one another and to an equipoising support arm to attain the selected payload bias.

Claims

1. A gimbal support apparatus comprising:

a gimbal having;

a first gimbal arm rotationally connected to a payload support about a first axis via a first rotation connection device;

a second gimbal arm having a first end and a second end, the second gimbal arm rotationally connected to the first gimbal arm about a second axis via a second rotation connection device at the first end of the second gimbal arm;

the second gimbal arm configured at the second end to be rotationally connected about a third axis to an equipoising support arm via a third rotation connection device; and

an adjustment system to selectively bias a hanging resting position of a payload supported by the payload support;

wherein the adjustment system comprises components to adjust the positions of the first axis, second axis and the third axis each with respect to one another including;

the first rotation connection device adjustably attached to the first gimbal arm along at least a portion of a length of the first gimbal arm, wherein a direction of adjustment of the first rotation connection device is not coincident with the first axis of rotation;

the second rotation connection device adjustably attached to the first gimbal arm along at least a portion of the length of the first gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the first gimbal arm is not coincident with the second axis of rotation;

the second rotation connection device further adjustably attached to the second gimbal arm along at least a portion of a length of the second gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the second gimbal arm is not coincident with the second axis of rotation; and

the third rotation connection device adjustably attached to the second gimbal arm along at least a portion of the length of the second gimbal arm, wherein a direction of adjustment of the third rotation connection device is not coincident with the third axis of rotation.

2. The gimbal support apparatus of claim 1 wherein the first, second and third axes are adapted to be adjustable to converge at the center of gravity of the payload.

3. The gimbal support apparatus of claim 1 further comprising a pinch protection component.

4. The gimbal support apparatus of claim 3 wherein the pinch protection component comprises a disk disposed between two bearings.

5. The gimbal support apparatus of claim 1 wherein friction of at least one rotation connection device of the first, second and third rotation connection devices can be adjusted to control a response across the at least one rotation connection device.

6. The gimbal support apparatus of claim 1 wherein at least one of the first or second gimbal arms has a plurality of rotation connection devices attached thereto, and for the at least one of the first or second gimbal arms with a plurality of rotation connection devices attached thereto, the plurality of rotation connection devices are mounted on the same side of the at least one of the first or second gimbal arms.

7. The gimbal support apparatus of claim 1 wherein at least one of the first gimbal arm and second gimbal arm has a bend.

8. The gimbal support apparatus of claim 7 wherein a normal to a linear surface of each of the first gimbal arm, second gimbal arm and the first axis intersects.

9. The gimbal support apparatus of claim 7 wherein at least one of the first gimbal arm and second gimbal arm has a substantially right angle.

10. The gimbal support apparatus of claim 7 wherein at least one of the first gimbal arm and second gimbal arm has a double bend wherein two outer portions of the at least one of the first gimbal arm and second gimbal arm form a substantially right angle at a virtual intersection of the two outer portions.

11. The gimbal support apparatus of claim 7 wherein at least one of the first gimbal arm and second gimbal arm has a radius in a range of about 1.6 inches to about 3.0 inches.

12. The gimbal support apparatus of claim 7 wherein at least one of the first gimbal arm and second gimbal arm has a radius in a range of about 1.65 inches to about 1.70 inches.

13. The gimbal support apparatus of claim 7 wherein at least one of the first gimbal arm and second gimbal arm has a radius in a range of about 1.9 inches to about 3.0 inches.

14. The gimbal support apparatus of claim 1 wherein at least one of the first gimbal arm and the second gimbal arm has at least one flat side and an associated rotational connection device has a complimentary flat surface.

15. The gimbal support apparatus of claim 1 further comprising a payload gripping bracket attached to the payload support.

16. The gimbal support apparatus of claim 1 wherein the payload support is universal to accommodate a plurality of different payloads.

17. The gimbal support apparatus of claim 1 wherein a net moment of force is less than about 225 in-lbs force.

18. The gimbal support apparatus of claim 1 wherein a net moment of force is less than about 200 in-lbs force.

19. The gimbal support apparatus of claim 1 wherein a length of the first gimbal arm and a length of the second gimbal arm are each less than about 15 inches.

20. A method of supporting a payload comprising:

providing a gimbal support apparatus according to claim 1;

selectively biasing the resting position of the payload supported by the gimbal support apparatus by;

selecting a location on or within the payload for securing the payload to the gimbal support apparatus;

selecting an orientation of the first axis with respect to the payload; and

selecting an orientation of the third axis with respect to the equipoising support arm.

21. The method of claim 20 further comprising:

adjusting the first and second gimbal arms with respect to one another thereby selectively biasing the resting position of the payload supported by the gimbal support apparatus.

22. The gimbal support apparatus of claim 1 wherein:

the first, second, and third axes are selectively adjustable to a position wherein the first, second and third axes of rotation to converge at the center of gravity of the payload and positions wherein the first, second and third axes converge other than at the center of gravity of the payload.

23. The gimbal support apparatus of claim 1 wherein:

the first, second, and third axes are selectively adjustable to position the first, second and third axes of rotation to all intersect at a common point and all not intersect at a common point.

24. A gimbal support apparatus comprising:

a first gimbal arm rotationally connected to a payload support about a first axis via a first rotation connection device;

a second gimbal arm having a first end and a second end, the second gimbal arm rotationally connected to the first gimbal arm about a second axis via a second rotation connection device at the first end of the second gimbal arm;

the second gimbal arm configured at the second end to be rotationally connected about a third axis to an equipoising support arm via a third rotation connection device; and

an adjustment system to selectively bias a resting position of a payload supported by the payload support;

wherein the adjustment system comprises components to adjust positions of the first axis, second axis and the third axis each with respect to one another including;

the first rotation connection device adjustably attached to the first gimbal arm along at least a portion of a length of the first gimbal arm, wherein a direction of adjustment of the first rotation connection device is not coincident with the first axis of rotation;

the second rotation connection device adjustably attached to the first gimbal arm along at least a portion of the length of the first gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the first gimbal arm is not coincident with the second axis of rotation;

the second rotation connection device further adjustably attached to the second gimbal arm along at least a portion of a length of the second gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the second gimbal arm is not coincident with the second axis of rotation;

the third rotation connection device adjustably attached to the second gimbal arm along at least a portion of the length of the second gimbal arm, wherein a direction of adjustment of the third rotation connection device is not coincident with the third axis of rotation; and

at least one rotation limiting device that is a rotational motion inhibitor comprising at least one torsion spring disposed at at least one rotational intersection of the first or second gimbal arm configured to provide a balancing torsion force.

25. A gimbal support apparatus comprising:

a first gimbal arm rotationally connected to a payload support about a first axis via a first rotation connection device;

a second gimbal arm having a first end and a second end, the second gimbal arm rotationally connected to the first gimbal arm about a second axis via a second rotation connection device at the first end of the second gimbal arm;

the second gimbal arm configured at the second end to be rotationally connected about a third axis to an equipoising support arm via a third rotation connection device; and

an adjustment system to selectively bias a resting position of a payload supported by the payload support;

wherein the adjustment system comprises components to adjust the positions of the first axis, second axis and the third axis each with respect to one another including;

the first rotation connection device adjustably attached to the first gimbal arm along at least a portion of a length of the first gimbal arm, wherein a direction of adjustment of the first rotation connection device is not coincident with the first axis of rotation;

the second rotation connection device adjustably attached to the first gimbal arm along at least a portion of the length of the first gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the first gimbal arm is not coincident with the second axis of rotation;

the second rotation connection device further adjustably attached to the second gimbal arm along at least a portion of a length of the second gimbal arm, wherein a direction of adjustment of the second rotation connection device relative to the second gimbal arm is not coincident with the second axis of rotation;

the third rotation connection device adjustably attached to the second gimbal arm along at least a portion of the length of the second gimbal arm, wherein a direction of adjustment of the third rotation connection device is not coincident with the third axis of rotation; and

wherein at least one of the first gimbal arm and the second gimbal arm has at least one flat side and an associated rotational connection device has a complimentary flat surface.