Superelastic Alloy Structural Geometry for Ultrahigh Mechanical Damping
US-2015337420-A1 · Nov 26, 2015 · US
US10018238B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10018238-B2 |
| Application number | US-201414527077-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 29, 2014 |
| Priority date | Nov 1, 2013 |
| Publication date | Jul 10, 2018 |
| Grant date | Jul 10, 2018 |
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An actuator includes an effective stiffness. The effective stiffness is based at least in part on non-linear deflection characteristics of buckling. A method of varying an effective stiffness of an actuator includes providing an actuator and varying an effective stiffness of the actuator based at least in part on non-linear deflection characteristics of buckling. Another method of varying an effective stiffness of an actuator includes applying a load to a member. The load causes the member to buckle, and the buckling produces non-linear deflection of the member. The method further includes varying an effective stiffness of an actuator based at least in part on the non-linear deflection of the member.
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What is claimed is: 1. A method of controlling an effective stiffness of a single actuator comprising: providing an actuator; and varying a positive effective stiffness of the actuator based at least in part on non-linear deflection characteristics of buckling that includes independently controlling a negative stiffness, wherein varying the positive effective stiffness comprises applying a load to a member to vary the stiffness of the member, wherein the load causes the member to buckle, wherein the buckling of the member defines at least in part the non-linear deflection characteristics of buckling, and wherein the member is selected from the group consisting of a beam, a shaft, a column, a rod, a spring, a plate or a shell. 2. The method of claim 1 , wherein the load is a compressive load. 3. The method of claim 1 , wherein the load is a tensile load. 4. The method of claim 1 , wherein the load is a bending load. 5. The method of claim 1 , wherein the load is a torsional load. 6. The method of claim 1 , wherein the stiffness of the member is based at least in part on the non-linear deflection characteristics of buckling, and wherein varying the stiffness of the member varies the effective stiffness of the actuator. 7. The method of claim 1 , further comprising: controlling a position of an end effector of the actuator based at least in part on a force applied to the end effector. 8. The method of claim 7 , wherein the force applied to the end effector causes a deflection of the end effector, and the method further comprises: estimating the force applied to the end effector based at least in part on the deflection of the end effector and the effective stiffness of the actuator; and controlling the position of the end effector based at least in part on the estimated force. 9. A method of varying a positive effective stiffness of an actuator comprising: applying a load to a member, wherein the load causes the member to buckle, and wherein the buckling produces non-linear deflection of the member that includes a variable negative stiffness, and varying an effective stiffness of the actuator based at least in part on controlling the variable negative stiffness. 10. The method of claim 9 , wherein a stiffness of the member is based at least in part on the non-linear deflection of the member, the method further comprising: varying the stiffness of the member, wherein varying the stiffness of the member varies the effective stiffness of the actuator. 11. The method of claim 9 , further comprising varying the effective stiffness of the actuator not based at least in part on non-linear deflection of the member. 12. An actuator comprising: a member defining at least in part a positive effective stiffness of the actuator, the member is selected from the group consisting of a beam, a shaft, a column, a rod, a spring, a plate or a shell; a loading actuator connected to the member and configured to apply a load to the member, wherein the load causes the member to buckle, wherein the buckling produces non-linear deflection of the member that includes variable negative stiffness, and wherein the effective stiffness of the actuator is based at least in part on variable negative stiffness; and a controller configured to vary a stiffness, including varying the negative stiffness, of the member, wherein varying the stiffness of the member varies the effective stiffness of the actuator. 13. The actuator of claim 12 , wherein the loading actuator is configured to apply at least one of a compressive load, a tensile load, a bending load, and a torsional load to the member. 14. The actuator of claim 12 , further comprising: an end effector connected to the member, and a positioning actuator configured to control a position of the end effector. 15. The actuator of claim 14 , wherein the positioning actuator is configured to control the position of the end effector based at least in part on a force applied to the end effector. 16. The actuator of claim 15 , wherein the force applied to the end effector causes a deflection of the end effector, wherein the controller is configured to estimate the force applied to the end effector based at least in part on the deflection of the end effector and the effective stiffness of the actuator, and wherein the positioning actuator is configured to control the position of the end effector based at least in part on the estimated force.
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