High integrity linear actuator and method of operation
View Patent ↗A linear actuator for an aircraft comprising a casing comprising a first casing section and a second casing section, wherein the first casing section and the second casing section are extendible and retractable with respect to each other, and a first drive mechanism and a second drive mechanism disposed in the casing, wherein the first drive mechanism and the second drive mechanism are operable independently of each other to drive at least one transmission element connected to an interior of the casing.
1. A linear actuator for an aircraft comprising:
a casing comprising:
a first casing section and a second casing section, wherein the first casing section and the second casing section are extendible and retractable with respect to each other; and
a first drive mechanism and a second drive mechanism disposed in the casing, wherein the first drive mechanism and the second drive mechanism are operable independently of each other to drive at least one transmission element connected to an interior of the casing;
wherein the at least one transmission element comprises a screw-threaded rod that is splined to the interior of the first casing section and the interior of the second casing section.
2. The linear actuator according to claim 1 , wherein the first drive mechanism and the second drive mechanism comprise electric motors.
3. The linear actuator according to claim 1 , wherein the first casing section and the second casing section have a substantially constant cross-section.
4. The linear actuator according to claim 1 , wherein at least one of the first drive mechanism and the second drive mechanism drives the screw-threaded rod through a roller screw.
5. The linear actuator according to claim 1 , wherein at least one of the first drive mechanism and the second drive mechanism are concentric with the at least one transmission element.