IP Library Granted Patent US 9,371,855
Granted Patent B2
US 9,371,855 · App. 11/860,830 · Granted Jun 21, 2016

Flexure based linear and rotary bearings

Inventor: George M. Voellmer (Takoma Park, MD)
Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
F16C32/02Y10T403/45
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Quick Facts
Patent No.
US 9,371,855
App. No.
11/860,830
Granted
Jun 21, 2016
Kind
B2
Abstract

A flexure based linear bearing includes top and bottom parallel rigid plates; first and second flexures connecting the top and bottom plates and constraining exactly four degrees of freedom of relative motion of the plates, the four degrees of freedom being X and Y axis translation and rotation about the X and Y axes; and a strut connecting the top and bottom plates and further constraining exactly one degree of freedom of the plates, the one degree of freedom being one of Z axis translation and rotation about the Z axis.

Claims (20)

1. A bearing, consisting essentially of:

a rigid top plate positioned above and parallel to a fixed rigid bottom plate;

first and second flexures disposed between and connecting aid rigid top plate and said bottom plate, said flexures together constraining relative motion of said top plate relative to said bottom plate in exactly four degrees of freedom, the four degrees of freedom being X and Y axis translation and rotation about the X and Y axes; a mechanical stop connected to the top and bottom plates for limiting Z axis translation of one plate relative to another plate; and

a strut connecting the top and bottom plates and further constraining exactly one additional degree of freedom of the plates, the one degree of freedom being rotation about the Z axis.

2. The bearing of claim 1 wherein a plane defined by the X and Y translational constraint axes of the first flexure is parallel to a plane defined by the X and Y translational constraint axes of the second flexure.

3. The bearing of claim 2 wherein at least one of the flexures is substantially planar and notched between said top and bottom parallel rigid plates.

4. The bearing of claim 3 wherein the substantially planar notched flexure is generally hour-glass shaped between said top and bottom parallel rigid plates.

5. The bearing of claim 3 wherein the notched flexure is generally X-shaped.

6. The bearing of claim 2 wherein centers of rotation of the first and second flexures define a line that is perpendicular to the parallel planes of constraint.

7. The bearing of claim 6 wherein the line defined by the centers of rotation of the first and second flexures does not intersect a center of the strut.

8. The bearing of claim 7 wherein the strut lies in one of the parallel planes of constraint of the first and second flexures.

9. The bearing of claim 7 wherein the strut comprises end portions and a midsection, the midsection having an X axis width that is greater than an X axis width of the end portions.

10. A bearing, comprising;

A rigid top plate positioned above and parallel to a fixed rigid bottom plate;

first and second flexures disposed between and connecting said rigid top plate and said fixed rigid bottom plate, said flexures together constraining relative motion of said top plate relative to said bottom plate in exactly four degrees of freedom, the four degrees of freedom being x and y axis translation and rotation about the x and y axes; and

a strut connecting the top and bottom plates and further constraining exactly one additional degree of freedom of the plates, the one degree of freedom being rotation about the Z axis; wherein at least one of the flexures is a substantially planar notched plate and is hour-glass shaped between said rigid top plate and said fixed rigid bottom plate.

11. A bearing, consisting of:

a rigid top plate positioned above and parallel to a fixed rigid bottom plate;

first and second flexures disposed between and connecting said rigid top plate and said fixed rigid bottom plate, said flexures being substantially planar and notched each having a generally hour glass shape and together constraining relative motion of said top plate relative to said bottom plate in exactly four degrees of freedom, the four degrees of freedom being X and Y axis translation and rotation about the X and Y axes; and

a strut connecting the top and bottom plates and further constraining exactly one additional degree of freedom of the plates, the one degree of freedom being rotation about the Z axis; wherein at least one of the flexures is a substantially planar notched plate and is hour-glass shaped between said rigid top plate and said fixed rigid bottom plate.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2007
From: VOELLMER, GEORGE M., MR.
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Reel/Frame 020205/0085 →
Continuity (2)
Provisional Application 60939146 · May 21, 2007
Related Publication 20080292392A1 · Nov 27, 2008