Flexure assembly
A flexure assembly includes a first spiral flexure, a second spiral flexure, and a spacing element. The spacing element is positioned between the first spiral flexure and the second spiral flexure. The flexure assembly also includes a plurality of fasteners that collectively extend circumferentially around an axis defined by the flexure assembly. Each of the plurality of fasteners extends through the first spiral flexure and the second spiral flexure.
1. A flexure assembly that defines an axis, wherein the axis defines an axial direction, a circumferential direction, and a radial direction, the flexure assembly comprising:
a first spiral flexure that comprises an annular body comprising a central opening coaxial with the axis and a plurality of slots circumferentially-spaced about the axis and axially-extending therethrough;
a second spiral flexure that comprises an annular body comprising a central opening coaxial with the axis and a plurality of slots circumferentially-spaced about the axis and axially-extending therethrough;
a first spacing element positioned between the first spiral flexure and the second spiral flexure;
a second spacing element positioned between the first spiral flexure and the second spiral flexure;
a first plurality of fasteners circumferentially-spaced around the axis, wherein each of the first plurality of fasteners axially extends through radially inner portions of the first spiral flexure, the first spacing element, and radially inner portions of the second spiral flexure;
a second plurality of fasteners circumferentially-spaced around the axis, wherein each of the second plurality of fasteners axially extends through radially outer portions of the first spiral flexure, the second spacing element, and radially outer portions of the second spiral flexure;
a first plate; and
a second plate,
wherein the first spiral flexure, the first spacing element, the second spacing element, and the second spiral flexure are each positioned between the first plate and the second plate, and
wherein each of the first plurality of fasteners extends through either the first plate or the second plate, but not both, and each of the second plurality of fasteners extends through the other of the first plate or the second plate, but not both.
2. The flexure assembly of claim 1 , wherein the first spiral flexure and the second spiral flexure are oriented within the flexure assembly such that they are counterposed.
3. The flexure assembly of claim 1 , wherein the first plate is configured to move in the axial direction relative to the second plate.
4. The flexure assembly of claim 1 , wherein the first spacing element is positioned between the radially inner portions of the first spiral flexure and the radially inner portions of the second spiral flexure, wherein the second spacing element is positioned between the radially outer portions of the first spiral flexure and the radially outer portions of the second spiral flexure, wherein the first spacing element is configured to move relative to the second spacing element.
5. The flexure assembly of claim 1 , wherein each of the plurality of slots of the first spiral flexure and the second spiral flexure are nonlinear.
6. The flexure assembly of claim 5 , wherein each of the plurality of slots of the first spiral flexure and the second spiral flexure are arc shaped.
7. The flexure assembly of claim 1 , wherein each of the plurality of slots have a tilted configuration relative to the radial direction.
8. The flexure assembly of claim 1 , wherein the first spiral flexure defines a radius that extends from the axis to an outer rim of the first spiral flexure, wherein each of the plurality of slots of the first spiral flexure define a width, wherein a ratio (R:W) between the radius of the first spiral flexure and the width is at least 5:1 and up to 14:1.
9. The flexure assembly of claim 1 , wherein the first spiral flexure and the second spiral flexure each have a thickness that is less than 0.1 inch.
10. A gimbal assembly comprising:
a yoke assembly;
a payload assembly that is rotatably coupled to the yoke assembly; and
a flexure assembly positioned between the payload assembly and the yoke assembly, wherein the flexure assembly defines an axis, wherein the axis defines an axial direction, a circumferential direction, and a radial direction, the flexure assembly comprising:
a first spiral flexure that comprises an annular body comprising a central opening coaxial with the axis and a plurality of slots circumferentially-spaced about the axis and axially-extending therethrough;
a second spiral flexure that comprises an annular body comprising a central opening coaxial with the axis and a plurality of slots circumferentially-spaced about the axis and axially-extending therethrough;
a first spacing element positioned between the first spiral flexure and the second spiral flexure;
a second spacing element positioned between the first spiral flexure and the second spiral flexure;
a first plurality of fasteners circumferentially-spaced around the axis, wherein each of the first plurality of fasteners axially extends through radially inner portions of the first spiral flexure, the first spacing element, and radially inner portions of the second spiral flexure;
a second plurality of fasteners circumferentially-spaced around the axis, wherein each of the second plurality of fasteners axially extends through radially outer portions of the first spiral flexure, the second spacing element, and radially outer portions of the second spiral flexure;
a first plate; and
a second plate,
wherein the first spiral flexure, the first spacing element, the second spacing element, and the second spiral flexure are each positioned between the first plate and the second plate, and
wherein each of the first plurality of fasteners extends through either the first plate or the second plate, but not both, and each of the second plurality of fasteners extends through the other of the first plate or the second plate, but not both.
11. The gimbal assembly of claim 10 , wherein the first spiral flexure and the second spiral flexure are oriented within the flexure assembly such that they are counterposed.
12. The gimbal assembly of claim 10 , wherein the first plate is configured to move in the axial direction relative to the second plate.
13. The gimbal assembly of claim 10 , wherein the first spacing element is positioned between the radially inner portions of the first spiral flexure and the radially inner portions of the second spiral flexure, wherein the second spacing element is positioned between the radially outer portions of the first spiral flexure and the radially outer portions of the second spiral flexure, wherein the first spacing element is configured to move relative to the second spacing element.
14. The gimbal assembly of claim 10 , wherein each of the plurality of slots of the first spiral flexure and the second spiral flexure are nonlinear.
15. The gimbal assembly of claim 14 , wherein each of the plurality of slots of the first spiral flexure and the second spiral flexure are arc shaped.
16. The gimbal assembly of claim 10 , wherein each of the plurality of slots have a tilted configuration relative to the radial direction.
17. The gimbal assembly of claim 10 , wherein the first spiral flexure defines a radius that extends from the axis to an outer rim of the first spiral flexure, wherein each of the plurality of slots of the first spiral flexure define a width, wherein a ratio (R:W) between the radius of the first spiral flexure and the width is at least 5:1 and up to 14:1.
18. The gimbal assembly of claim 10 , wherein the first spiral flexure and the second spiral flexure each have a thickness that is less than 0.1 inch.