Claims
- 1. An actuator comprising an actuator element with a strain gradient variation between a first phase and a second phase.
- 2. The actuator as set forth in claim 1, wherein said actuator element comprises a shape memory alloy.
- 3. The actuator as set forth in claim 2, wherein said shape memory alloy comprises nitinol.
- 4. The actuator as set forth in claim 2, wherein said first state is a Martensite phase of said shape memory alloy.
- 5. The actuator as set forth in claim 2, wherein said second phase is an Austenite phase of said shape memory alloy.
- 6. The actuator as set forth in claim 1, wherein said actuator element in said first phase is positioned in a curved shape with said strain gradient variation along a cross-section of said actuator element.
- 7. The actuator as set forth in claim 6, wherein said actuator element in said second phase is positioned in a different curved shape when compared to said curved shape in said first phase in a direction to minimize said strain gradient.
- 8. The actuator as set forth in claim 1, wherein said actuator element in said first phase is positioned in an irregular shape with said strain gradient variation along a cross-section of said actuator element.
- 9. The actuator as set forth in claim 8, wherein said actuator element in said second phase is positioned in a different irregular shape when compared to said irregular shape in said first phase in a direction to minimize said strain gradient.
- 10. The actuator as set forth in claim 1, wherein said actuator element in said first phase is positioned in a non-linear shape with said strain gradient variation along a cross-section of said actuator element.
- 11. The actuator as set forth in claim 10, wherein said actuator element in said second phase is positioned in a different non-linear shape when compared to said non-linear shape in said first phase in a direction to minimize said strain gradient.
- 12. The actuator as set forth in claim 1, wherein said actuator element in said second phase is positioned in a substantially linear shape.
- 13. The actuator as set forth in claim 1, further comprising an activating means for said actuator element.
- 14. The actuator as set forth in claim 13, wherein said activating means comprises a heating means.
- 15. The actuator as set forth in claim 1, wherein said actuator element generates a rotary movement when transitioning from said first phase to said second phase.
- 16. The actuator as set forth in claim 1, wherein said actuator element generates a linear movement when transitioning from said first phase to said second phase.
- 17. The actuator as set forth in claim 1, wherein said actuator element generates an expanding movement when transitioning from said first phase to said second phase.
- 18. The actuator as set forth in claim 1, wherein said actuator element generates a combined linear and rotary movement when transitioning from said first phase to said second phase.
- 19. The actuator as set forth in claim 1, wherein said actuator element generates a linear movement by combining a contraction and said strain gradient.
- 20. A method of providing an actuator, comprising the steps of:
(a) providing an actuator element; (b) providing a strain gradient variation between a first phase and a second phase of said actuator element; and (c) providing an activating means to activate said actuator element and transition said actuator element from said first phase to said second phase.
- 21. The method as set forth in claim 20, wherein said actuator element comprises a shape memory alloy.
- 22. The method as set forth in claim 21, wherein said shape memory alloy comprises nitinol.
- 23. The method as set forth in claim 21, wherein said first state is a Martensite phase of said shape memory alloy.
- 24. The method as set forth in claim 21, wherein said second phase is an Austenite phase of said shape memory alloy.
- 25. The method as set forth in claim 20, wherein said actuator element in said first phase is positioned in a curved shape with said strain gradient variation along a cross-section of said actuator element.
- 26. The method as set forth in claim 25, wherein said actuator element in said second phase is positioned in a different curved shape when compared to said curved shape in said first phase in a direction to minimize said strain gradient.
- 27. The method as set forth in claim 20, wherein said actuator element in said first phase is positioned in an irregular shape with said strain gradient variation along a cross-section of said actuator element.
- 28. The method as set forth in claim 27, wherein said actuator element in said second phase is positioned in a different irregular shape when compared to said irregular shape in said first phase in a direction to minimize said strain gradient.
- 29. The method as set forth in claim 20, wherein said actuator element in said first phase is positioned in a non-linear shape with said strain gradient variation along a cross-section of said actuator element.
- 30. The method as set forth in claim 29, wherein said actuator element in said second phase is positioned in a different non-linear shape when compared to said non-linear shape in said first phase in a direction to minimize said strain gradient.
- 31. The method as set forth in claim 20, wherein said actuator element in said second phase is positioned in a substantially linear shape.
- 32. The method as set forth in claim 20, further comprising an activating means for said actuator element.
- 33. The method as set forth in claim 32, wherein said activating means comprises a heating means.
- 34. The method as set forth in claim 20, wherein said actuator element generates a rotary movement when transitioning from said first phase to said second phase.
- 35. The method as set forth in claim 20, wherein said actuator element generates a linear movement when transitioning from said first phase to said second phase.
- 36. The method as set forth in claim 20, wherein said actuator element generates an expanding movement when transitioning from said first phase to said second phase.
- 37. The method as set forth in claim 20, wherein said actuator element generates a combined linear and rotary movement when transitioning from said first phase to said second phase.
- 38. The method as set forth in claim 20, wherein said actuator element generates a linear movement by combining a contraction and said strain gradient.
- 39. An actuator device, comprising:
(a) a first body; and (b) an actuator element with a first end attached to said first body, wherein said actuator element has a strain gradient variation between a first phase and a second phase.
- 40. The device as set forth in claim 39, further comprising a second body attached to a second end of said actuator element.
- 41. The device as set forth in claim 40, wherein said first body is movably attached to said second body by a connecting means.
- 42. The device as set forth in claim 39, further comprising a second body wherein said second body is attached to a point in between said first end and a second end of said actuator element and said second end is attached to said first body.
- 43. The device as set forth in claim 39, wherein said actuator element is embedded in said actuator device.
- 44. A method of providing an actuator device, comprising the steps of:
(a) providing a first body; (b) providing an actuator element with a first end attached to said first body; (c) providing a strain gradient variation between a first phase and a second phase of said actuator element; and (d) providing an activating means to activate said actuator element and transition said actuator element from said first phase to said second phase.
- 45. The method as set forth in claim 44, further comprising the step of providing a second body attached to a second end of said actuator element.
- 46. The method as set forth in claim 45, wherein said first body is movably attached to said second body by a connecting means.
- 47. The method as set forth in claim 44, further comprising the step of providing a second body wherein said second body is attached between said first end and a second end of said actuator element and said second end is attached to said first body.
- 48. The method as set forth in claim 44, wherein said actuator element is embedded in said actuator device.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This application is cross-referenced to and claims priority from U.S. Provisional Applications 60/260,169 filed Jan. 5, 2001 and 60/257,214 filed Dec. 20, 2000, which are both hereby incorporated by reference.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] This invention was supported in part by grant number F49620-99-1-0129 from the Air Force Office of Science Research. The U.S. government has certain rights in the invention.
Provisional Applications (2)
|
Number |
Date |
Country |
|
60260169 |
Jan 2001 |
US |
|
60257214 |
Dec 2000 |
US |