Bi-directional rotary shape memory alloy element actuator assemblies, and systems and methods including the same

Patent metadata

Field	Value
Publication number	US-10364805-B2
Application number	US-201715832252-A
Country	US
Kind code	B2
Filing date	Dec 5, 2017
Priority date	May 24, 2016
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

Rotary actuator assemblies, wind tunnels including the same, and associated methods are disclosed. A rotary actuator assembly includes a rotary element and a rotary actuator with a shape memory alloy element. The rotary actuator is configured to generate a first torque and a second torque in opposing rotary directions to rotate the rotary element. A rotary actuator assembly further includes an assist magnetic element and a receiver magnetic element configured to generate a magnetic force therebetween. Wind tunnels include an aerodynamic model with a rotary actuator assembly to rotate a portion of the aerodynamic model with respect to an airstream in a chamber. A method of rotating a rotary element includes modulating a temperature of a shape memory alloy element and applying a supplemental torque to the rotary element with an assist magnetic element and a receiver magnetic element.

First claim

The invention claimed is:

1. A bi-directional rotary shape memory alloy element actuator assembly, the actuator assembly comprising:
a rotary actuator configured to generate a first torque in a first rotary direction and a second torque in a second rotary direction;
a rotary element coupled to the rotary actuator, wherein the rotary element has an angular position in an angular range of motion, and further wherein the rotary element is configured to:
(i) rotate in the first rotary direction responsive to receipt of the first torque from the rotary actuator; and
(ii) rotate in the second rotary direction responsive to receipt of the second torque from the rotary actuator;
an assist magnetic element; and
a receiver magnetic element mounted on the rotary element;
wherein the rotary actuator includes a shape memory alloy element configured to generate the first torque and the second torque; and wherein the assist magnetic element and the receiver magnetic element are configured to generate a magnetic force therebetween when the angular position of the rotary element is in a magnetic assist portion of the angular range of motion.

2. The actuator assembly of claim 1 , wherein the shape memory alloy element is configured to transform from a martensite state to an austenite state responsive to a temperature of the shape memory alloy element increasing, wherein the shape memory alloy element is configured to transform from the austenite state to the martensite state responsive to the temperature of the shape memory alloy element decreasing, wherein the rotary actuator is configured to apply the first torque to the rotary element in the first rotary direction when the shape memory alloy element transforms from the martensite state to the austenite state, wherein the rotary actuator is configured to apply the second torque to the rotary element in the second rotary direction when the shape memory alloy element transforms from the austenite state to the martensite state, wherein the magnetic force is configured to apply a supplemental torque to the rotary element in the second rotary direction, and wherein the supplemental torque is applied to the rotary element when the angular position of the rotary element is in the magnetic assist portion of the angular range of motion.

3. The actuator assembly of claim 1 , wherein the rotary actuator includes a shape memory alloy torque tube.

4. The actuator assembly of claim 1 , wherein the magnetic assist portion is a subset of the angular range of motion and includes at least 5% and at most 35% of the angular range of motion.

5. The actuator assembly of claim 1 , wherein the magnetic force between the assist magnetic element and the receiver magnetic element is less than a threshold magnetic force when the angular position of the rotary element is outside the magnetic assist portion, wherein the magnetic force between the assist magnetic element and the receiver magnetic element is a maximum magnetic force when the angular position of the rotary element minimizes a separation distance between the assist magnetic element and the receiver magnetic element, and further wherein a magnitude of the threshold magnetic force is at most 5% of a magnitude of the maximum magnetic force.

6. The actuator assembly of claim 1 , wherein the assist magnetic element includes at least one of an assist permanent magnet, an assist rare earth magnet, an assist electromagnet, and an assist ferromagnetic material, and wherein the receiver magnetic element includes at least one of a receiver permanent magnet, a receiver rare earth magnet, a receiver electromagnet, and a receiver ferromagnetic material.

7. The actuator assembly of claim 1 , wherein the assist magnetic element has an assist magnetic moment, wherein the receiver magnetic element has a receiver magnetic moment, and wherein the assist magnetic element and the receiver magnetic element are configured such that the assist magnetic moment and the receiver magnetic moment are generally parallel when the angular position of the rotary element is within the magnetic assist portion, and such that the assist magnetic moment and the receiver magnetic moment are generally misaligned when the angular position of the rotary element is outside the magnetic assist portion.

8. The actuator assembly of claim 7 , wherein the assist magnetic element has an assist element surface with an assist element normal direction, wherein the receiver magnetic element has a receiver element surface with a receiver element normal direction, wherein the assist element normal direction and the receiver element normal direction are separated by a magnet offset angle, wherein the magnet offset angle is less than a threshold magnet offset angle when the angular position of the rotary element is in the magnetic assist portion of the angular range of motion, and wherein the magnet offset angle is greater than the threshold magnet offset angle when the angular position of the rotary element is not in the magnetic assist portion of the angular range of motion.

9. The actuator assembly of claim 8 , wherein the threshold magnet offset angle is at least 5 degrees and less than 90 degrees.

10. The actuator assembly of claim 1 , wherein the actuator assembly further includes a status signal generator configured to generate and transmit a status signal, wherein the status signal includes information regarding at least one of a temperature of the shape memory alloy element, a load force applied to the rotary element, the angular position of the rotary element, the angular position of the rotary element, a load direction applied to the rotary element, a load magnitude applied to the rotary element, and a magnitude of the magnetic force generated between the assist magnetic element and the receiver magnetic element.

11. The actuator assembly of claim 10 , wherein at least one of the assist magnetic element and the receiver magnetic element includes an electromagnet, wherein the actuator assembly further includes an electromagnet control unit configured to modulate a variable magnetic field generated by the electromagnet.

12. The actuator assembly of claim 1 , wherein the actuator assembly further includes an actuator mount; wherein the rotary actuator is coupled to the actuator mount; and wherein the rotary element is configured to:
(i) rotate with respect to the rotary mount in the first rotary direction responsive to receipt of the first torque from the rotary actuator; and
(ii) rotate with respect to the rotary mount in the second rotary direction responsive to receipt of the second torque from the rotary actuator.

13. The actuator assembly of claim 12 , wherein the assist magnetic element is mounted to the actuator mount.

14. The actuator assembly of claim 1 , wherein the actuator assembly further includes a thermal control unit configured to regulate a temperature of at least a portion of the rotary actuator.

15. A method of rotating the rotary element of claim 1 in two rotary directions through the angular range of motion, the method comprising:
increasing a temperature of the shape memory alloy element to rotate the rotary element in the first rotary direction;
decreasing the temperature of the shape memory alloy element to rotate the rotary element in the second rotary direction; and
applying a supplemental torque to the rotary element with the assist magnetic element and the receiver magnetic element when the angular position of the rotary element is in the magnetic assist portion of the angular range of motion.

16. A wind tunnel for testing an aerodynamic model, the wind

Assignees

• Boeing Co

Inventors

• Nicholson Douglas E
• Bass Micheal
• Mabe James Henry

Classifications

• G01M9/062

  Wind tunnel balances; Holding devices combined with measuring arrangements · CPC title

• G01M9/08

  Aerodynamic models · CPC title

• G01M9/02

  Wind tunnels · CPC title

• F03G7/065 Primary

  using a shape memory element · CPC title

• F03G7/06146

  Torque tubes or torsion bars · CPC title