Shape memory alloy actuators with heat transfer structures, actuated assemblies including the shape memory alloy actuators, and methods of manufacturing the same

Patent metadata

Field	Value
Publication number	US-10428805-B2
Application number	US-201615265505-A
Country	US
Kind code	B2
Filing date	Sep 14, 2016
Priority date	Sep 14, 2016
Publication date	Oct 1, 2019
Grant date	Oct 1, 2019

Abstract

Shape memory alloy actuators with heat transfer structures, actuated assemblies including the shape memory alloy actuators, and methods of manufacturing the same are disclosed herein. The shape memory alloy actuators include a shape memory alloy torque tube and a heat transfer structure. The actuated assemblies include a base structure, an attached component, and a shape memory alloy actuator that operatively attaches the attached component to the base structure. The methods include providing a shape memory alloy torque tube, providing a heat transfer structure, applying a dimension-modifying force to the heat transfer structure, combining the heat transfer structure with the shape memory alloy torque tube, and releasing the dimension-modifying force.

First claim

The invention claimed is:

1. A shape memory alloy actuator, comprising:
a shape memory alloy (SMA) torque tube having a first end, a second end, and an elongate surface extending between the first end and the second end; and
a heat transfer structure configured to increase heat transfer with the SMA torque tube to increase a rate at which the SMA torque tube transitions between a martensite state and an austenite state, wherein the heat transfer structure:
(i) is in mechanical and thermal contact with the elongate surface of the SMA torque tube;
(ii) extends at least partially between the first end and the second end of the SMA torque tube;
(iii) exerts a retention force on the SMA torque tube that retains the heat transfer structure in mechanical and thermal contact with the elongate surface of the SMA torque tube;
(iv) is shaped such that a surface of the heat transfer structure that is in mechanical and thermal contact with the elongate surface of the SMA torque tube is in at least partial face-to-face contact with the elongate surface of the SMA torque tube; and
(v) includes an elongate conductive body, wherein the elongate conductive body has a plurality of at least substantially helical regions that are in mechanical and thermal contact with the elongate surface of the SMA torque tube and a plurality of deviation regions that deviate from a helical shape and project away from the elongate surface of the SMA torque tube, wherein a corresponding deviation region of the plurality of deviation regions extends between adjacent pairs of helical regions of the plurality of helical regions.

2. The actuator of claim 1 , wherein the heat transfer structure is at least one of helically shaped, at least partially helically shaped, coil-shaped, at least partially coil-shaped, spiral-shaped, and at least partially spiral-shaped.

3. The actuator of claim 1 , wherein the heat transfer structure includes a plurality of surface-contacting regions that mechanically and thermally contacts the elongate surface of the SMA torque tube and applies the retention force to the elongate surface of the SMA torque tube, and a plurality of projecting regions that projects from the elongate surface of the SMA torque tube.

4. The actuator of claim 3 , wherein the heat transfer structure is at least partially defined by an elongate conductive body, and further wherein the elongate conductive body is shaped to define both the plurality of surface-contacting regions and the plurality of projecting regions.

5. The actuator of claim 3 , wherein the heat transfer structure is at least partially defined by an elongate conductive body, and further wherein at least a subset of the plurality of projecting regions is operatively attached to the elongate conductive body.

6. The actuator of claim 3 , wherein each of the plurality of surface-contacting regions is spaced apart from an adjacent surface-contacting region of the plurality of surface-contacting regions by a corresponding projecting region of the plurality of projecting regions.

7. The actuator of claim 1 , wherein the heat transfer structure includes an elongate conductive body, and further wherein the elongate conductive body defines a conductive heat transfer surface, which is shaped to mechanically and thermally contact the elongate surface of the SMA torque tube, and a convective heat transfer surface, which is shaped for heat transfer with a heat transfer fluid stream, wherein a transverse cross-section of the conductive heat transfer surface is at least substantially linear, and further wherein a transverse cross-section of the convective heat transfer surface is at least one of:
(i) nonlinear;
(ii) arcuate;
(iii) partially circular;
(iv) partially elliptical; and
(v) D-shaped.

8. The actuator of claim 1 , wherein the heat transfer structure is retained in mechanical and thermal contact with the elongate surface of the SMA torque tube solely by the retention force over at least a fraction of a length of the heat transfer structure.

9. The actuator of claim 1 , wherein the heat transfer structure is defined by a heat transfer material, wherein the SMA torque tube is defined by a shape memory alloy, and further wherein the heat transfer material is different from the shape memory alloy.

10. The actuator of claim 1 , wherein the SMA torque tube defines an inner surface and an outer surface, and further wherein the elongate surface of the SMA torque tube includes at least one of:
(i) the inner surface; and
(ii) the outer surface.

11. The actuator of claim 1 , wherein the shape memory alloy actuator further includes a thermal sensor configured to detect a temperature of the SMA torque tube, wherein the thermal sensor is operatively attached to the heat transfer structure, and further wherein the heat transfer structure presses the thermal sensor into mechanical and thermal contact with the elongate surface of the SMA torque tube.

12. An actuated assembly, comprising:
a base structure;
an attached component; and
the shape memory alloy actuator of claim 1 , wherein the attached component is operatively attached to the base structure via the shape memory alloy actuator such that actuation of the shape memory alloy actuator produces relative motion between the base structure and the attached component.

13. The assembly of claim 12 , wherein the actuated assembly further includes a thermal control assembly configured to regulate a temperature of the SMA torque tube.

14. The assembly of claim 13 , wherein the thermal control assembly includes a fluid propulsion system configured to direct a heat transfer fluid stream in thermal contact with the elongate surface of the SMA torque tube and with the heat transfer structure.

15. The assembly of claim 12 , wherein the base structure includes one of an aircraft, an airplane, and a helicopter.

16. The assembly of claim 12 , wherein the attached component includes one of an actuated component, a landing gear, a flap, an aileron, and a rotor.

17. A method of manufacturing a shape memory alloy actuator, the method comprising:
providing a shape memory alloy (SMA) torque tube that defines a first end, a second end, and an elongate surface extending between the first end and the second end;
providing a heat transfer structure configured to increase heat transfer with the SMA torque tube to increase a rate at which the SMA torque tube transitions between a martensite state and an austenite state;
applying a dimension-modifying force to the heat transfer structure to place the heat transfer structure in a modified-dimensional conformation such that a modified characteristic dimension of the heat transfer structure differs from a natural characteristic dimension of the heat transfer structure prior to application of the dimension-modifying force;
combining the heat transfer structure with the SMA torque tube such that the heat transfer structure extends at least partially between the first end and the second end of the SMA torque tube; and
releasing the dimension-modifying force such that the heat transfer structure transitions to an intermediate conformation in which an intermediate characteristic dimension of the heat transfer structure is between the modified characteristic dimension and the natural characteristic dimension and also such that the heat transfer structure exerts a retention force on the elongate surface of the SMA torque tube to retain the heat transfer structure in mechanical and thermal contact with the elongate surface of the SMA torque tube.

18. The method of claim

Assignees

• Boeing Co

Inventors

• Gissen Abraham Naroll
• Mabe James Henry
• Nicholson Douglas E
• Bass Micheal A

Classifications

• B21C23/002

  Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences · CPC title

• F03G7/065 Primary

  using a shape memory element · CPC title

• F03G7/06146 Primary

  Torque tubes or torsion bars · CPC title

• F03G7/062

  characterised by the activation arrangement · CPC title