High-efficiency, large stroke electromechanical actuator

• US 5,907,211 A
• Filed: 02/28/1997
• Issued: 05/25/1999
• Est. Priority Date: 02/28/1997
• Status: Expired due to Fees

• Current Assignee: Massachusetts Institute of Technology
• Original Assignee: Massachusetts Institute of Technology
• Inventors: Hall, Steven R., Prechtl, Eric F.
• Primary Examiner(s): BUDD, MARK OSBORNE
• Assistant Examiner(s): Williams, Timothy A.
• Application Number:
  US08/808,144
• Time in Patent Office: 816 Days
• Field of Search: 310/328, 310/331, 310/330, 310/333, 310/366, 310/346, 416/4
• US Class Current: 310/328
• CPC Class Codes: B64C 2027/7277 of the magnetostrictive type
• CPC Class Codes: B64C 2027/7283 of the piezoelectric type
• CPC Class Codes: B64C 27/001 Vibration damping devices
• CPC Class Codes: B64C 27/615 including flaps mounted on blades
• CPC Class Codes: H02N 2/043 Mechanical transmission means, e.g. for stroke amplification
• CPC Class Codes: Y02T 50/30 Wing lift efficiency

Abstract

An actuator having two frames, each frame including a distal end member, a proximal pivot end member or proximal end pivot point, and at least two elongated side members connected between the distal end member and the proximal pivot end member of that frame. A flexure is disposed between an end of the pivot end member of the first frame and an end of the pivot end member of the second frame. A first longitudinal span member is disposed between the distal end member of the second frame and the pivot end member of the first frame, and a second longitudinal span member is disposed between the distal end member of the first frame and the pivot end member of the second frame. At least one of the first and second longitudinal span members is an expansive element having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus. This expansive element extends in a state of compression between the corresponding distal and proximal pivot end members, with the longitudinal axis of the element in a plane parallel to side members of the first and second frames. The one or both of the longitudinal span members that are expansive elements can be, e.g., a magnetostrictive element, an electrostrictive element, or a piezoelectric element. The actuator provides many of the characteristics required to achieve optimal mass efficiency for a given set of actuator materials; and further provides advantages of high bandwidth, linearity, and large stroke performance advantages. As a result, the actuator can be adapted to many applications and can accommodate a range of engineering constraints.

Claims

1. An actuator comprising:

a first frame comprising a distal end member, a proximal pivot end member, and at least two elongated side members connected between the distal end member and the proximal pivot end member of the first frame;

a second frame comprising a distal end member, a proximal pivot end member, and at least two elongated side members connected between the distal end member and the proximal pivot end member of the second frame;

a flexure disposed between an end of the pivot end member of the first frame and an end of the pivot end member of the second frame;

a first longitudinal span member disposed between the distal end member of the second frame and the pivot end member of the first frame; and

a second longitudinal span member disposed between the distal end member of the first frame and the pivot end member of the second frame, at least one of the first and second longitudinal span members comprising an expansive element having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive element extending in a state of compression between the corresponding distal and proximal pivot end members, with the longitudinal axis of the element in a plane parallel to side members of the first and second frames.

2. The actuator of claim 1 wherein the expansive element comprises a piezoelectric element.

3. The actuator of claim 1 wherein the expansive element comprises an electrostrictive element.

4. The actuator of claim 1 wherein the expansive element comprises a magnetostrictive element.

5. The actuator of claim 1 wherein each of the first and second longitudinal span members comprise an expansive element having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive element extending in a state of compression between the corresponding distal and proximal pivot end members, with the longitudinal axis of the element in a plane parallel to side members of the first and second frames.

6. The actuator of claim 1 wherein the first and second longitudinal span members are disposed between side members of the first and second frames.

7. The actuator of claim 6 wherein the distal and proximal pivot end members of the second frame are each characterized by a width less than a width characteristic of each of the distal and proximal pivot end members of the first frame, and wherein the side members of the second frame are disposed between the side members of the first frame.

8. The actuator of claim 6 wherein the distal end member of the first frame comprises a mounting end member adapted to be relatively fixedly mounted, and wherein the distal end member of the second frame comprises a displacement end member free to extend and retract along an actuator output stroke path.

9. The actuator of claim 8 wherein the mounting end member of the first frame is adapted to comprise an elongated actuator output stroke track having two separated side members between which is disposed the displacement end member of the second frame.

10. The actuator of claim 7 wherein a longitudinal axis of each of the side members of the second frame is at a preselected angle from the longitudinal axis of the first longitudinal span member, and wherein a longitudinal axis of each of the side members of the first frame is at the preselected angle from the longitudinal axis of the second longitudinal span member, the preselected angle corresponding to a preselected amplification factor relating expansive element stroke to transverse motion of the first frame distal end member relative to the second frame distal end member.

11. The actuator of claim 10 wherein the preselected angle is an acute angle.

12. The actuator of claim 7 wherein the flexure comprises a cylindrical pivot point at the pivot end members of the first and second frames.

13. The actuator of claim 12 wherein the cylindrical pivot point comprises a cylindrical roller pin held in a state of compression between ends of the first and second frame pivot end members.

14. The actuator of claim 7 wherein the flexure comprises a hinge connected between an end of the first frame pivot end member and an end of the second frame pivot end member.

15. The actuator of claim 7 wherein the flexure comprises a flexural support having a first support member connected to the first frame pivot end member, a second support member connected to the second frame pivot end member, a mounting plate, and a flexible strut connected between the mounting plate and each of the first and second support members through corresponding first and second flexural links.

16. The actuator of claim 7 wherein the first longitudinal span member abuts the pivot end member of the first frame with a rolling contact, and wherein the second longitudinal span member abuts the pivot end member of the second frame with a rolling contact.

17. The actuator of claim 16 wherein each rolling contact comprises a cylindrical endcap that abuts the corresponding pivot end member.

18. The actuator of claim 17 wherein the first longitudinal span member comprises an endplate that abuts the distal end member of the second frame, and wherein the second longitudinal span member comprises an endplate that abuts the distal end member of the first frame.

19. The actuator of claim 16 wherein each rolling contact comprises a spherical endcap that abuts the corresponding pivot end member.

20. The actuator of claim 19 wherein the first longitudinal span member comprises a spherical endcap that abuts the distal end member of the second frame, and wherein the second longitudinal span member comprises a spherical endcap that abuts the distal end member of the first frame.

21. The actuator of claim 7 further comprising a pre-load spring connected to bias the first and second longitudinal span members in a state of compression.

22. The actuator of claim 5 wherein each of the first and second expansive elements comprises a magnetostrictive element.

23. The actuator of claim 5 wherein each of the first and second expansive elements comprises an electrostrictive element.

24. The actuator of claim 5 wherein each of the first and second expansive elements comprises a piezoelectric element.

25. The actuator of claim 24 wherein each of the first and second piezoelectric elements comprises a stack of piezoelectric ceramic wafers.

26. The actuator of claim 7 wherein the first and second frames each comprise a frame material characterized by a specific modulus that is greater than a specific modulus characteristic of each of the first and second longitudinal span members.

27. The actuator of claim 7 wherein the first and second frames each comprise a frame material characterized by a coefficient of thermal expansion that is between about 0.5 and about 1.5 times an average of coefficients of thermal expansion characteristic of each of the first and second longitudinal span members.

28. The actuator of claim 27 wherein each of the first and second frames comprises a matrix-fiber composite frame material having a volume fraction of fiber material and a corresponding volume fraction of matrix material selected to produce a frame coefficient of thermal expansion that substantially matches the average of the coefficients of thermal expansion characteristic of each of the first and second longitudinal span members.

29. An actuator comprising:

a first frame comprising a distal end member, a proximal pivot end member, and at least two elongated side members connected between the distal end member and the proximal pivot end member of the first frame;

a second frame disposed between the side members of the first frame and comprising a distal end member, a proximal pivot end member, and at least two elongated side members connected between the distal end member and the proximal pivot end member of the second frame and having a longitudinal axis parallel to a longitudinal axis of the first frame side members;

a pivot point formed at an end of the pivot end member of the first frame and an end of the pivot end member of the second frame;

a first expansive element having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive element extending in a state of compression between the distal end member of the second frame and the proximal pivot end member of the first frame, the longitudinal axis in a plane parallel to longitudinal axes of the side members of the first and second frames; and

a second expansive element having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive element extending in a state of compression between the distal end member of the first frame and the proximal pivot end member of the second frame, the longitudinal axis in a plane parallel to longitudinal axes of the side members of the first and second frames.

30. The actuator of claim 29 wherein a longitudinal axis of the side members of the second frame is at a preselected angle from the longitudinal axis of the first expansive element, and wherein a longitudinal axis of the side members of the first frame is at the preselected angle from the longitudinal axis of the second expansive element, the preselected angle corresponding to a preselected amplification factor relating expansive element stroke to transverse motion of the first frame distal end member relative to the second frame distal end member.

31. The actuator of claim 29 wherein the distal end member of the first frame comprises a mounting end member adapted to be relatively fixedly mounted, and wherein the distal end member of the second frame comprises a displacement end member free to extend and retract along an actuator stroke path.

32. An actuator comprising:

a first frame having a distal end and a proximal end pivot point;

a second frame having a distal end and a proximal end pivot point coincident with the pivot point of the first frame; and

first and second expansive elements each having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive elements each extending in a state of compression between the first and second frames such that a stimulated change in each expansive element length reacts against a proximal end of a corresponding one of the first and second frames to induce pivoting of the first and second frames relative to each other, resulting in extension of the second frame distal end relative to the first frame distal end in a direction transverse to the longitudinal axes of the expansive elements.

33. The actuator of claim 32 wherein each of the first and second frames forms a preselected angle with respect to a corresponding one of the expansive elements, the preselected angle corresponding to a preselected amplification factor relating expansive element stroke to transverse motion of the first frame distal end member relative to the second frame distal end member.

34. The actuator of claim 32 wherein the distal end of the first frame is relatively fixedly mounted.

35. The actuator of claim 32 further comprising:

a displacement sensor connected along a path of the second frame distal end extension for sensing displacement of a load connected along the path; and

a controller connected in a feedback loop between the displacement sensor and the first and second expansive elements for controlling the stimulus applied to each of the first and second expansive elements to produce a desired displacement of the load.

36. The actuator of claim 32 further comprising:

a force sensor in communication with at least one of the first frame and the second frame for sensing force produced by extension of the second frame distal end; and

a controller connected in a feedback loop between the force sensor and the first and second expansive elements for controlling the stimulus applied to each of the first and second expansive elements to produce a second frame distal end extension having a desired force.

37. The actuator of claim 32 further comprising:

a displacement sensor connected along a path of the second frame distal end extension for sensing displacement of a load connected along the path;

a force sensor in communication with at least one of the first frame and the second frame for sensing force produced by extension of the second frame distal end; and

a controller connected in a feedback loop between the force and displacement sensors and the first and second expansive elements for controlling the stimulus applied to each of the first and second expansive elements to produce a desired second frame distal end extension stiffness.

38. An actuator for controlling a deflectable trailing edge flap of an airfoil, the actuator comprising:

a first frame having a distal end and a proximal end pivot point;

a second frame having a distal end and a proximal end pivot point coincident with the pivot point of the first frame;

a flexural support connected to each of the first and second frame pivot points and mounted to the airfoil, with the first and second frames located within the airfoil;

first and second expansive elements each having a longitudinal axis along which dimensional strain can be induced in response to an applied stimulus, the expansive elements each extending in a state of compression between the first and second frames such that a stimulated change in each expansive element length reacts against a proximal end of one of the first and second frames to induce pivoting of the first and second frames relative to each other, resulting in extension of the second frame distal end with respect to the first frame distal end in a direction transverse to the longitudinal axes of the expansive elements; and

a control rod engaged with the distal end of the second frame and extending through the airfoil to engage a lever mounted to the airfoil trailing edge flap.

39. The actuator of claim 38 further comprising a pre-load element connected to bias the first and second expansive elements in a state of compression.

40. The actuator of claim 39 wherein the pre-load element comprises a torsionally pre-stressed wire connected between the airfoil and the trailing edge flap.

41. The actuator of claim 38 wherein the flexural support comprises a centrifugal support having a first support member connected to the first frame, a second support member connected to the second frame, a mounting member, and a flexible strut connected between the mounting plate and each of the first and second support members through corresponding first and second flexural links for distributing centrifugal force equally between the first and second frames.

42. The actuator of claim 38 wherein the distal end of the first frame is adapted to comprise an elongated actuator stroke track having two separated side members between which is disposed the distal end member of the second frame.