Methods and systems for shape memory alloy structures

Patent metadata

Field	Value
Publication number	US-9631268-B2
Application number	US-201313778093-A
Country	US
Kind code	B2
Filing date	Feb 26, 2013
Priority date	Feb 26, 2013
Publication date	Apr 25, 2017
Grant date	Apr 25, 2017

Abstract

There is provided a method of training a shape memory alloy (SMA) workpiece. The method includes applying a force couple to a shape memory alloy (SMA) workpiece to impart a generally planar transformational behavior to the SMA workpiece to obtain a trained shape memory alloy (SMA) workpiece.

First claim

What is claimed is:

1. A method of training a shape memory alloy (SMA) workpiece, the method comprising:
applying a force couple to the shape memory alloy (SMA) workpiece to impart a generally planar transformational behavior to the SMA workpiece to obtain a trained shape memory alloy (SMA) workpiece, the force couple comprising applying opposing forces such that edge-wise racking loads are applied to the SMA workpiece.

2. The method of claim 1 wherein applying the opposing forces comprises applying an applied force and a reactive force to the SMA workpiece.

3. The method of claim 1 wherein applying the force couple comprises applying opposing forces such that a wave-like deformation is produced in the SMA workpiece.

4. The method of claim 1 wherein applying the force couple comprises applying opposing forces that impart a non-wavy to wavy transformational behavior to change a shape of the SMA workpiece from a non-wavy shape to a wavy shape.

5. The method of claim 1 further comprising:
applying thermal cycles to the SMA workpiece; and,
applying the force couple in a cyclic manner thereby imparting substantially planar strain cycles to the SMA workpiece to cause the SMA workpiece to have the generally planar transformational behavior.

6. The method of claim 5 wherein applying the thermal cycles comprises applying heat to the SMA workpiece to produce a racking motion that changes a shape of the SMA workpiece from a substantially rectangle shape to a substantially parallelogram shape.

7. The method of claim 1 further comprising joining the trained SMA workpiece to one or more structures.

8. The method of claim 7 wherein the one or more structures are capable of changing shape in response to a change in temperature of the trained SMA workpiece.

9. The method of claim 1 further comprising integrating the trained SMA workpiece into an SMA actuator and embedding the SMA actuator in a structural spar of an air vehicle to influence a shape of the structural spar.

10. A method of training a shape memory alloy (SMA) actuator, the method comprising:
applying a force couple in a cyclic manner to the shape memory alloy (SMA) actuator to impart substantially planar strain cycles to the SMA actuator, to cause the SMA actuator to have a generally planar transformational behavior;
applying thermal cycles to the SMA actuator, wherein applying the thermal cycles comprises applying heat to the SMA actuator to produce a racking motion that changes a shape of the SMA actuator from a substantially rectangle shape to a substantially parallelogram shape; and
obtaining a trained shape memory alloy (SMA) actuator.

11. The method of claim 10 wherein applying the force couple comprises applying opposing forces such that a wave-like deformation is produced in the SMA actuator.

12. The method of claim 10 wherein applying the force couple comprises applying opposing forces that impart a non-wavy to wavy transformational behavior to change a shape of the SMA actuator from a non-wavy shape to a wavy shape.

13. The method of claim 10 further comprising joining the trained SMA actuator to one or more structures.

14. The method of claim 13 wherein the one or more structures are capable of changing shape in response to a change in temperature of the trained SMA actuator.

15. The method of claim 13 wherein the one or more structures comprise one or more structural spars used in an aircraft or a rotorcraft.

16. The method of claim 10 wherein applying the force couple in a cyclic manner comprises applying a predetermined stress level in a range of 25 ksi (one thousand pounds per square inch) to 35 ksi, and wherein applying the thermal cycles comprises repeatedly heating the SMA actuator for at least 500 cycles to 1000 cycles.

17. A method of training a shape memory alloy (SMA) actuator, the method comprising:
applying a force couple in a cyclic manner to the shape memory alloy (SMA) actuator to impart substantially planar strain cycles to the SMA actuator, to cause the SMA actuator to have a generally planar transformational behavior;
applying thermal cycles to the SMA actuator, wherein applying the thermal cycles comprises applying heat to the SMA actuator to produce a racking motion that changes a shape of the SMA actuator from a substantially square shape to a substantially rhombus shape; and
obtaining a trained shape memory alloy (SMA) actuator.

18. The method of claim 17 further comprising joining the trained SMA actuator to one or more structures.

19. The method of claim 18 wherein the one or more structures are capable of changing shape in response to a change in temperature of the trained SMA actuator.

20. The method of claim 18 wherein the one or more structures comprise one or more structural spars used in an aircraft or a rotorcraft.

Assignees

• Boeing Co

Inventors

• Brown Jonathan K
• Bushnell Glenn Scott
• Clingman Dan J

Classifications

• B64C2001/0081

  from metallic materials · CPC title

• B64C3/44

  Varying camber · CPC title

• B64C2027/7211

  without flaps · CPC title

• B64C27/72

  Means acting on blades · CPC title

• B21C37/045

  Manufacture of wire or rods with particular section or properties · CPC title