IP Library Granted Patent US 11,747,613
Granted Patent B2
US 11,747,613 · App. 17/090,317 · Granted Sep 5, 2023

Multi-axis actuator with differential drive

Inventors: Michael E. Knotts (Milford, NH); Adam J. Marcinuk (Lyndeborough, NH); Chris L. Willis (Hollis, NH)
Assignee: BAE Systems Information and Electronic Systems Integration Inc.
G02B26/105F16H48/00F16M11/00G02B7/1821
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,747,613
App. No.
17/090,317
Granted
Sep 5, 2023
Kind
B2
Abstract

A multi-axis rotary actuator includes a payload support configured to be rotatable about a first axis, a disk surrounding at least a portion of the payload support, and an elevation wheel rotatably coupled to the payload support. The disk is configured to be rotatable about the first axis. The elevation wheel is configured to be in contact with the disk and to be rotatable about a second axis perpendicular to the first axis. The actuator can include a mirror or other device coupled to the elevation wheel. The mirror or other device is configured to be rotatable about the first axis and the second axis as the payload support and the elevation wheel rotate about the first axis and the second axis, respectively.

Claims (15)

1. A multi-axis rotary actuator, comprising:

a payload support configured to be rotatable about a first axis;

a disk surrounding at least a portion of the payload support, the disk configured to be rotatable about the first axis independently of the payload support; and

an elevation wheel rotatably coupled to the payload support, the elevation wheel configured to be in contact with the disk and to be rotatable about a second axis perpendicular to the first axis as a function of the differential angular rotations of the payload support and the disk.

2. The actuator of claim 1 , further comprising a mirror coupled to the elevation wheel and configured to be rotatable about the first axis and the second axis as the payload support and the elevation wheel rotate about the first axis and the second axis, respectively.

3. The actuator of claim 1 , further comprising at least one idler wheel coupled to the payload support and configured to be in contact with the disk.

4. The actuator of claim 3 , wherein the disk includes an integral flexure spring configured to bias the disk against the at least one idler wheel.

5. The actuator of claim 1 , further comprising a counterweight coupled to the elevation wheel or to the payload support.

6. The actuator of claim 1 , further comprising a base assembly rotatably coupled to the payload support and the disk, the base assembly comprising:

a first open bore torque motor configured to rotate the payload support about the first axis; and

a second open bore torque motor configured to rotate the disk about the first axis independently of the payload support.

7. The actuator of claim 6 , further comprising:

a first encoder sensor configured to provide first position information to first open bore torque motor; and

a second encoder sensor configured to provide second position information to the second open bore torque motor.

8. The actuator of claim 1 , wherein the disk includes at least one of a ceramic material, anodized aluminum, and/or stainless steel.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 5, 2020
From: KNOTTS, MICHAEL E.; MARCINUK, ADAM J.; WILLIS, CHRIS L.
To: BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
Reel/Frame 054287/0809 →
Continuity (1)
Related Publication 20220137401A1 · May 5, 2022