Two-axis motor-driven spherical orienting mechanism

Patent metadata

Field	Value
Publication number	US-12305794-B2
Application number	US-202218568889-A
Country	US
Kind code	B2
Filing date	Mar 28, 2022
Priority date	Jul 21, 2021
Publication date	May 20, 2025
Grant date	May 20, 2025

Abstract

A mechanism for orienting a payload support includes first and second transversely deployed drive assemblies, each having a motor that drives a drive arm. The payload support is directly pivotally mounted to a first drive arm. Connection between the second drive arm and the payload support is via a coupling linked to the second drive arm via a coupling rotary joint, and to the payload support via a support rotary joint. Both the first drive arm and the second drive arm are supported relative to the frame by sets of two bearing assemblies located on opposite sides of the center of rotation. Each of the bearing assemblies is preferably implemented as a loaded duplex bearing assembly, and most preferably with a back-to-back loaded duplex bearing assembly on each axis.

First claim

What is claimed is:

1. A spherical orienting mechanism for orienting a payload relative to two axes of rotation about a center of rotation, the mechanism comprising:
(a) a payload support located at the center of rotation;
(b) a frame at least partially encompassing said payload support;
(c) a first drive assembly comprising:
(i) a first motor deployed in fixed relation to said frame, and
(ii) a first drive arm deployed so as to be driven by said first motor to rotate about a first drive axis aligned with the center of rotation, said payload support being supported relative to said first drive arm by a first support rotary joint, said first support rotary joint defining a first support rotation axis that is transverse to said first drive axis and aligned with the center of rotation;

(d) a second drive assembly comprising:
(i) a second motor deployed in fixed relation to said frame, and
(ii) a second drive arm deployed so as to be driven by said second motor to rotate about a second drive axis, transverse to said first drive axis and aligned with the center of rotation, said second drive arm being linked to said payload support by a coupling linked to said second drive arm via a coupling rotary joint and to said payload support via a second support rotary joint, said coupling rotary joint defining a coupling rotation axis that is transverse to said second drive axis and aligned with the center of rotation, said second support rotary joint defining a second support rotation axis that is transverse to said coupling rotation axis and to said first support rotation axis,

wherein said first drive arm is supported relative to said frame for rotation about said first drive axis by a first set of two bearing assemblies located on opposite sides of said center of rotation,
and wherein said second drive arm is supported relative to said frame for rotation about said second drive axis by a second set of two bearing assemblies located on opposite sides of said center of rotation.

2. The mechanism of claim 1 , wherein said first frame is a closed frame encompassing said payload support.

3. The mechanism of claim 2 , wherein said bearing assemblies of said first and second sets of bearing assemblies are implemented as loaded duplex bearing assemblies.

4. The mechanism of claim 3 , wherein at least one of said first set of two bearing assemblies is a back-to-back loaded duplex bearing assembly, and at least one of said second set of two bearing assemblies is a back-to-back loaded duplex bearing assembly.

5. The mechanism of claim 3 , wherein one of said first set of two bearing assemblies is a back-to-back loaded duplex bearing assembly and another of said first set of two bearing assemblies is a face-to-face loaded duplex bearing assembly, and wherein one of said second set of two bearing assemblies is a back-to-back loaded duplex bearing assembly and another of said second set of two bearing assemblies is a face-to-face loaded duplex bearing assembly.

6. The mechanism of claim 1 , wherein said bearing assemblies of said first and second sets of bearing assemblies are implemented as loaded duplex bearing assemblies.

7. The mechanism of claim 6 , wherein at least one of said first set of two bearing assemblies is a back-to-back loaded duplex bearing assembly, and at least one of said second set of two bearing assemblies is a back-to-back loaded duplex bearing assembly.

8. The mechanism of claim 6 , wherein one of said first set of two bearing assemblies is a back-to-back loaded duplex bearing assembly and another of said first set of two bearing assemblies is a face-to-face loaded duplex bearing assembly, and wherein one of said second set of two bearing assemblies is a back-to-back loaded duplex bearing assembly and another of said second set of two bearing assemblies is a face-to-face loaded duplex bearing assembly.

9. The mechanism of claim 1 , wherein said first drive arm has a bifurcated medial portion defining a medial opening, and wherein said first support rotary joint comprises a third set of two bearing assemblies located on opposite sides of said center of rotation supporting said payload support bilaterally from said bifurcated medial portion of said first drive arm.

10. The mechanism of claim 9 , wherein said coupling extends from said second drive arm through said medial opening in said first drive arm.

11. The mechanism of claim 10 , wherein an end portion of said coupling is bifurcated, and wherein said second support rotary joint comprises a fourth set of two bearing assemblies located on opposite sides of said center of rotation supporting said payload support bilaterally from said bifurcated end portion of said coupling.

12. The mechanism of claim 11 , wherein said bearing assemblies of said third and fourth sets of bearing assemblies are implemented as loaded duplex bearing assemblies.

13. The mechanism of claim 1 , wherein said coupling rotary joint is configured to provide adjustability of an axial position of said coupling along said coupling rotation axis.

14. The mechanism of claim 9 , wherein said coupling rotary joint is configured to provide adjustability of an axial position of said coupling along said coupling rotation axis.

Assignees

• Rafael Advanced Defense Systems Ltd

Inventors

• Lahav Oded
• Shacham Omri Zvi
• Fraiman Leonid

Classifications

• G02B27/64

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• F16M11/18

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• F16C19/18

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• G02B27/644 Primary

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• F16M11/2035

  in more than one direction · CPC title