Patent ID: 6167694
Filing Date: 2001-01-02
Classification: F02K,F16H,Y10T

Abstract:
An aircraft engine thrust reverser utilizing one or more actuators for deploying cowls of a thrust reverser system, the actuator comprising a drive arrangement arranged to rotate a first drive member, the first member being in screw-threaded engagement with a second member, the second member being in screw-threaded engagement with a third, output member, wherein the screw-threaded engagement between the first and second members is such that, when the first member rotates at a given speed relative to the second member, the second member moves axially relative to the first member at a first speed, the screw-threaded engagement between the second and third members being such that, when the second member rotates at the said given speed relative to the third member, the third member moves axially relative to the second member at a second, higher speed; wherein said second member comprises a dual rate nut, the first and third members comprising first and second screw-threaded rods, the first rod and its corresponding part of the dual rate nut being provided with fine pitch screw threads, the second rod and its corresponding part of the dual rate nut being provided with coarser pitch threads.