Patent ID: 9108310
Filing Date: 2015-08-18
Classification: B25B,Y10T

Abstract:
1. A fueldraulic actuator installation and removal tool comprising: a base; an actuator chassis, the actuator chassis able to communicate with a jet fueldraulic actuator located in a jet engine bay such that the actuator can be removed from the jet engine bay, the actuator chassis connectable to the actuator at three predetermined points on the actuator, the actuator chassis includes a plate and an elbow extending from the plate, the three predetermined points being a first point, a second point and a third point, the plate having two pairs of plate projections that allow attachment to the first point and the second point to the actuator, the elbow having a first end and a second end, the first end attached to the plate, the second end having a pair of elbow projections for attachment to the third point on the actuator and, at least one articulating arm communicating with the actuator chassis such that the actuator chassis can be moved frontwards and backwards and left and right, and oriented at different inclines and adjusted to allow the actuator chassis to align and interface with the jet fueldraulic actuator, the at least one articulating arm attached to the base.