Shape-memory alloy power-assist apparatus
A power-assist apparatus includes a shape-memory alloy (SMA) rod, a power source, an actuator, and a differential gearbox. The SMA rod configured to rotate at an end of the SMA rod. The power source is coupled to the SMA rod. The actuator coupled to an openable apparatus. The differential gearbox is coupled between the actuator and the SMA rod. The differential gearbox converts the rotation of the SMA rod to motion of the actuator.
1. A power-assist apparatus comprising:
a shape-memory alloy (SMA) rod configured to rotate at an end of the SMA rod;
a power source coupled to the SMA rod;
an actuator coupleable to an openable apparatus; and
a differential gearbox coupled between the actuator and the SMA rod, wherein the differential gearbox converts the rotation of the SMA rod to motion of the actuator;
wherein the openable apparatus comprises an aircraft stowage bin comprising a door hingedly coupled to a cabinet.
2. The power-assist apparatus according to claim 1 , further comprising a sensor coupled to the power-assist apparatus and configured to detect an external opening or closing force on the openable apparatus.
3. The power-assist apparatus according to claim 1 , wherein the actuator is configured to reduce a minimum force necessary to open or close the openable apparatus.
4. The power-assist apparatus according to claim 1 , wherein the actuator is a ball bearing screw drive.
5. The power-assist apparatus according to claim 1 , further comprising a plurality of SMA rods each coupled to a corresponding one of a plurality of differential gearboxes, wherein each of the plurality of differential gearboxes is coupled to a corresponding one of a plurality of actuators.
6. The power-assist apparatus according to claim 1 , wherein the actuator is coupleable at one end to the door and at an opposite end to the cabinet.
7. The power-assist apparatus according to claim 1 , further comprising a rate control sensor configured to control a rate of closing or opening of the openable apparatus.
8. The power-assist apparatus according to claim 1 , wherein the SMA rod is perpendicular to the actuator.
9. The power-assist apparatus according to claim 1 , wherein the SMA rod is coupled to the differential gearbox at one end of the SMA rod and coupled to another differential gearbox at an opposite end of the SMA rod.
10. The power-assist apparatus according to claim 1 , wherein the actuator is a linear actuator.
11. A system comprising:
an openable apparatus; and
a power-assist apparatus comprising:
a shape-memory alloy (SMA) rod configured to rotate at an end of the SMA rod;
a power source coupled to the SMA rod;
an actuator coupled to the openable apparatus; and
a differential gearbox coupled between the actuator and the SMA rod, wherein the differential gearbox converts the rotation of the SMA rod to motion of the actuator and actuation of the openable apparatus;
wherein one of:
the power-assist apparatus further comprises a plurality of SMA rods each coupled to a corresponding one of a plurality of differential gearboxes, wherein each of the plurality of differential gearboxes is coupled to a corresponding one of a plurality of actuators; or
the SMA rod is coupled to the differential gearbox at one end of the SMA rod and coupled to another differential gearbox at an opposite end of the SMA rod.
12. The system according to claim 11 , wherein the power-assist apparatus further comprises the plurality of SMA rods each coupled to a corresponding one of a plurality of differential gearboxes.
13. The system according to claim 12 , wherein the openable apparatus comprises an aircraft stowage bin.
14. The system according to claim 11 , wherein the power-assist apparatus further comprises a torque limiter between the power source and the SMA rod, the torque limiter being configured to regulate electrical current supplied to the SMA rod from the power source.
15. The system according to claim 11 , further comprising a sensor coupled to the power-assist apparatus and configured to detect an external opening or closing force on the openable apparatus.
16. A method comprising:
heating to a shape-memory alloy (SMA) rod to cause the SMA rod to rotate, the SMA rod coupled to an interior part of an aircraft;
converting torque of the SMA rod to motion of an actuator, wherein the motion of the actuator applies a closing or opening force on an openable apparatus; and
sensing an external opening or closing force on the openable apparatus and adjusting a temperature of the SMA rod in response to sensing the external opening or closing force.
17. The method according to claim 16 , further comprising applying an assisting force to the openable apparatus, wherein the openable apparatus is a stowage bin.
18. The power-assist apparatus according to claim 2 , wherein the power source supplies power to the SMA rod to adjust a temperature of the SMA rod in response to detection, by the sensor, of an external opening or closing force on the openable apparatus.
19. The system according to claim 15 , wherein the power source supplies power to the SMA rod to adjust a temperature of the SMA rod in response to detection, by the sensor, of an external opening or closing force on the openable apparatus.
20. The method according to claim 16 , wherein the motion of the actuator is a linear motion.