Mechanically locking actuator
A lockable telescopic actuator arranged to be in a locked state or in an unlocked state, the lockable telescopic actuator including: a body defining a cylindrical cavity; a piston mounted to slide in the cylindrical cavity; and a locking mechanism including a first locking segment arranged to move from a locked position to an unlocked position. In the locked position the first locking segment is engaged with the piston to prevent the piston from moving. In the unlocked position the first locking segment is disengaged from the piston to allow the piston to move. A first shape memory alloy, SMA, biasing element configured to be extended or compressed such that when the first SMA biasing element is compressed the first locking element is biased into the locked position and when the first SMA bias element is extended the first locking element is biased into the unlocked position.
1. A lockable telescopic actuator arranged to be in a locked state or in an unlocked state, the lockable telescopic actuator comprising:
a body defining a cylindrical cavity;
a piston mounted to slide telescopically in the cylindrical cavity; and
a locking mechanism comprising
a first locking segment, the first locking segment arranged to be movable between a locked position and an unlocked position, wherein
in the locked position the first locking segment is engaged with the piston to prevent the piston from moving relative to the body and
in the unlocked position the first locking segment is disengaged from the piston to allow the piston to move relative to the body; and
a first shape memory alloy, SMA, biasing element configured to be selectively extended or compressed, the first SMA biasing element arranged such that when the first SMA biasing element is selectively compressed, the first locking segment is biased into the locked position and when the first SMA bias element is selectively extended, the first locking element is biased into the unlocked position,
wherein the locking mechanism is located in the cylindrical cavity and further comprises
a second locking segment, the second locking segment arranged to be movable between a locked position and an unlocked position, wherein
in the locked position the second locking segment is engaged with the piston to prevent the piston from moving relative to the body and
in the unlocked position the second locking segment is disengaged from the piston to allow the piston to move relative to the body; and wherein
the first SMA biasing element is located between the first and second locking segments and arranged such that when the first SMA biasing element is selectively compressed, the second locking element is biased into the locked position and when the first SMA bias element is selectively extended, the second locking element is biased into the unlocked position,
comprising a second SMA biasing element arranged between the body and the first locking segment and a third SMA biasing element arranged between the body and the second locking segment, the second and third SMA biasing elements configured to be selectively extended or compressed and arranged to:
compress when the first SMA biasing element extends; and
extend when the first SMA biasing element compresses.
2. A lockable telescopic actuator according to claim 1 , wherein the piston includes a recess formed therein and wherein
in the locked position the first locking segment is at least partially inserted in the recess; and
in the unlocked position the first locking segment is out of the recess.
3. A lockable telescopic actuator according to claim 1 , wherein the piston and/or the first locking segment comprises an indication switch that is:
activated when the first locking segment is engaged with the piston; and
deactivated when the first locking segment is disengaged with the piston.
4. A lockable telescopic actuator according to claim 1 , wherein the first SMA biasing element is arranged to extend when at a first predefined temperature and to compress when at a second predefined temperature.
5. A lockable telescopic actuator according to claim 1 , wherein the first SMA biasing element is electrically coupled to a current source.
6. A landing gear for an aircraft, comprising a lockable telescopic actuator according to claim 1 .
7. A lockable telescopic actuator arranged to be in a locked state or in an unlocked state, the lockable telescopic actuator comprising:
a body defining a cylindrical cavity;
a piston mounted to slide telescopically in the cylindrical cavity; and
a locking mechanism comprising
a first locking segment, the first locking segment arranged to be movable between a locked position and an unlocked position, wherein
in the locked position the first locking segment is engaged with the piston to prevent the piston from moving relative to the body and
in the unlocked position the first locking segment is disengaged from the piston to allow the piston to move relative to the body; and
a first shape memory alloy, SMA, biasing element configured to be selectively extended or compressed, the first SMA biasing element arranged such that when the first SMA biasing element is selectively extended, the first locking segment is biased into the locked position and when the first SMA bias element is selectively compressed, the first locking element is biased into the unlocked position,
wherein the locking mechanism is mounted on a housing attached on an external surface of the body, the first SMA biasing element being located between the housing and the first locking segment, wherein the first locking segment is slidably engaged with the housing, and
wherein the lockable telescopic actuator further comprised a second SMA biasing element located between the housing and the first locking segment, the second SMA biasing element configured to be selectively extended or compressed, the second SMA biasing element arranged:
to compress when the first SMA biasing element extends; and
to extend when the first SMA biasing element compresses.
8. A lockable telescopic actuator according to claim 7 ,
wherein the piston includes a recess formed therein and wherein
in the locked position the first locking segment is at least partially inserted in the recess; and
in the unlocked position the first locking segment is out of the recess.
9. A lockable telescopic actuator according to claim 7 , wherein the piston and/or the first locking segment comprises an indication switch that is:
activated when the first locking segment is engaged with the piston; and
deactivated when the first locking segment is engaged with the piston.
10. A lockable telescopic actuator according to claim 7 , wherein the first SMA biasing element is arranged to extend when at a first predefined temperature and to compress when at a second predefined temperature.
11. A lockable telescopic actuator according to claim 7 , wherein the first SMA biasing element is electrically coupled to a current source.
12. A landing gear for an aircraft, comprising a lockable telescopic actuator according to claim 7 .
13. A lockable telescopic actuator arranged to be in a locked state or in an unlocked state, the lockable telescopic actuator comprising:
a body defining a cylindrical cavity;
a piston mounted to slide telescopically in the cylindrical cavity; and
a locking mechanism comprising:
a first locking segment, the first locking segment arranged to be movable between a locked position and an unlocked position, wherein
in the locked position the first locking segment is engaged with the piston to prevent the piston from moving relative to the body and
in the unlocked position the first locking segment is disengaged from the piston to allow the piston to move relative to the body;
a first shape memory alloy, SMA, biasing element configured to be selectively extended or compressed, the first SMA biasing element arranged such that when the first SMA biasing element is selectively extended, the first locking segment is biased into the locked position and when the first SMA bias element is selectively compressed, the first locking element is biased into the unlocked position;
wherein the locking mechanism is located in the cylindrical cavity and comprises
a second locking segment, the second locking segment arranged to be movable between a locked position and an unlocked position, wherein
in the locked position the second locking segment is engaged with the piston to prevent the piston from moving relative to the body and
in the unlocked position the second locking segment is disengaged from the piston to allow the piston to move relative to the body; and
a second SMA biasing element configured to be selectively extended or compressed, the second SMA biasing element arranged such that when the first SMA biasing element is selectively extended, the second SMA biasing element is selectively extended and the second locking element is biased into the locked position and when the first SMA bias element is selectively compressed, the second SMA biasing element is selectively compressed and the second locking element is biased into the unlocked position
wherein the first SMA biasing element is between the body and the first locking segment and the second SMA biasing element is between the body and the second locking segment.
14. A lockable telescopic actuator according to claim 13 , wherein the piston includes a recess formed therein and wherein
in the locked position the first locking segment is at least partially inserted in the recess; and
in the unlocked position the first locking segment is out of the recess.
15. A lockable telescopic actuator according to claim 13 , wherein the piston and/or the first locking segment comprises an indication switch that is:
activated when the first locking segment is engaged with the piston; and
deactivated when the first locking segment is disengaged with the piston.
16. A lockable telescopic actuator according to claim 13 , wherein the first SMA biasing element is arranged to extend when at a first predefined temperature and to compress when at a second predefined temperature.
17. A lockable telescopic actuator according to claim 13 , wherein the first SMA biasing element is electrically coupled to a current source.
18. A landing gear for an aircraft, comprising a lockable telescopic actuator according to claim 13 .