Redundant hydraulic actuator, particularly for an aircraft...

Details Redundant hydraulic actuator, particularly for an aircraft... Redundant hydraulic actuator, particularly for an aircraft...

F - Mech Eng,Light,Heat,Weapons

15

B

F15B 15/14 (2006.01) B64C 13/42 (2006.01) F15B 9/12 (2006.01) F15B 18/00 (2006.01)

Patent

CA 2358218

A redundant hydraulic actuator having two hydraulic cylinders, each having a body and a rod having a piston sliding in sealed manner in the body, and wherein the bodies of the two cylinders are connected rigidly to a first connecting member of the actuator, and the rods of the cylinders are connected rigidly to a second connecting member of the actuator; the bodies of the two cylinders being coaxial with each other and inserted one inside the other.

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