Blow down actuator assembly having a drag brake

1. An actuator assembly, comprising:

a drive assembly comprising a drive arm assembly configured to extend and retract in order to actuate a controlled member;

the drive arm assembly comprises an actuation member;

the drive arm assembly further comprises a release member; and

a source of pressurized gas;

wherein during a normal mode of operation, the actuation member and the release member are engaged with a securing mechanism to move in unison to extend the controlled member;

wherein during an emergency mode of operation, pressurized gas automatically decouples the actuation member from the release member to move separately in order for the actuation member to extend the controlled member; and

wherein the securing mechanism is configured to lock the actuation member in a fully extended position during the emergency mode of operation.

2. The actuator assembly of claim 1 , further comprising:

a drag brake assembly configured to control movement of the actuation member as it moves past the release member during the emergency mode of operation; and

the drag brake assembly comprising at least one brake component.

3. The actuator assembly of claim 2 , wherein the at least one brake component comprises at least one brake shoe and at least one brake disk.

4. The actuator assembly of claim 3 , wherein the drag brake assembly comprises a drag brake pinion and a drag brake rack that are configured to engage one another.

5. The actuator assembly of claim 4 , wherein the drag brake pinion is configured to rotate and further configured to be braked by the at least one brake shoe and the at least one brake disk during the emergency mode of operation.

6. The actuator assembly of claim 1 , further comprising a ball screw configured with a raceway on a periphery thereof and ball nut housing bearings that ride on the raceway, a ball nut being coupled to the actuation member during the normal mode of operation such that a direction of rotation of the ball screw determines whether the actuation member extends or retracts from a housing.

7. The actuator assembly of claim 1 , wherein the securing mechanism is configured to releasably lock the actuation member to the release member during the normal mode of operation such that the actuation member and the release member are engaged to move in unison as one assembly.

8. The actuator assembly of claim 7 , further comprising a cover tube covering the actuation member, an end cap provided at an end of the cover tube and through which the actuation member extends, and a seal plug provided to close an end of the actuation member; and

the release member is configured to move toward the actuation member that is locked in the fully extended position to reset the release member with the actuation member such that the release member and the actuation member thereafter operate in the normal mode of operation.

9. The actuator assembly of claim 8 , further comprising a release piston that defines an expansion chamber between the release piston and the seal plug within the actuation member.

10. The actuator assembly of claim 9 , wherein when pressurized gas is released into the expansion chamber, the release member is driven to unlock the securing mechanism, releasing the actuation member to move past the release member.

11. An electro-mechanical actuator comprising:

an electro-mechanical drive system that comprises an actuation member and a release member; and

an integrated backup system operated by a pressurized gas;

wherein during a normal mode of operation, the actuation member and the release member are engaged with a securing mechanism to move in unison to extend a controlled member to a predetermined position; and

wherein when the integrated backup system is activated during an emergency mode of operation, the electro-mechanical drive system is decoupled such that the actuation member and the release member move separately in order for the actuation member to extend the controlled member to the predetermined position and a securing mechanism mechanically locks the controlled member in the predetermined position.

12. The electro-mechanical actuator of claim 11 , further comprising:

a drag brake assembly configured to control movement of the actuation member to move past the release member during the emergency mode of operation; and

the drag brake assembly comprising at least one brake component.

13. The electro-mechanical actuator of claim 12 , wherein the at least one brake component comprises at least one brake shoe and at least one brake disk.

14. The electro-mechanical actuator of claim 13 , wherein the drag brake assembly comprises a drag brake pinion and a drag brake rack that are configured to engage one another.

15. The electro-mechanical actuator of claim 14 , wherein the drag brake pinion is configured to rotate and further configured to be braked by the at least one brake shoe and the at least one brake disk during the emergency mode of operation.

16. The electro-mechanical actuator of claim 11 , wherein the electro-mechanical drive system includes a ball screw configured with a raceway on a periphery thereof and ball nut housing bearings that ride on the raceway, a ball nut being coupled to drive the actuation member during the normal mode of operation.

17. The electro-mechanical actuator of claim 11 , wherein the pressurized gas is pressurized nitrogen.

18. The electro-mechanical actuator of claim 11 , wherein the electro-mechanical drive system comprises a release piston that defines an expansion chamber for receiving the pressurized gas.

19. The electro-mechanical actuator of claim 11 , wherein the securing mechanism comprises an expandable retention ring biased to engage a ring groove on a drive arm of the electro-mechanical drive system.

20. A landing gear unit for an airplane including an electro-mechanical actuator according to claim 11 .