Patent Application
20130180093
The present invention relates to a fueldraulic actuator installation and removal tool. More specifically, but without limitation, the present invention is for use when performing maintenance on the F-35 fighter, specifically when removing and replacing the fueldraulic actuator.
A fueldraulic actuator is an apparatus in a jet engine which uses pressurized fuel to move the main thrust vectoring nozzle. In the F-35 military jet fighter, in order to replace the actuator an engine roll back must first be performed. This is due to the tight clearances inside the engine bay. An engine roll back requires parts of the engine and other related parts to be removed from the engine bay. This creates a long cycle time for replacing an actuator.
For the foregoing reasons, there is a need for a fueldraulic actuator installation and removal tool that allows quick and easy removal and replacement of the fuel actuator without performing an engine roll back.
The present invention is directed to a fueldraulic actuator installation and removal tool that meets the needs enumerated above and below.
The present invention is directed to a fueldraulic actuator installation and removal tool that includes a base, an actuator chassis, and at least one articulating arm. The actuator chassis is 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 is connectable to the actuator at three predetermined points on the actuator. The at least one articulating arm, which is attached to the base, communicates with the actuator chassis such that the actuator chassis can be moved forward (frontwards) and backwards, left and right, oriented at different inclines, and adjusted to allow the actuator chassis to align and interface with the jet fueldraulic actuator.
It is a feature of the present invention to provide a fueldraulic actuator installation and removal tool that allows replacement of the actuator without performing an engine rollback.
It is a feature of the present invention to provide fueldraulic actuator installation and removal tool that reduces cycle time as well as man power required to maintain and replace the fueldraulic actuator.
These and other features, aspects and advantages of the present invention will become better understood with reference to the following description and appended claims, and accompanying drawings wherein:
The preferred embodiments of the present invention are illustrated by way of example below and in
The base 100 is attachable to a universal jack 600 such that the tool 10 can be positioned by the universal jack 600. The universal jack 600 primarily moves the actuator chassis 200, as well as the tool 10, in an up and down motion.
As seen in
In the preferred embodiment, the tool 10 includes a bushing-jack screw system 700 wherein the inclined plane section 300, the first articulating arm 400 and the second articulating arm 500 communicate with the bushing-jack screw system 700 such that locations of the first articulating arm 400 and the second articulating arm 500 can be moved such that the actuator chassis 200 location can be adjusted.
The preferred embodiment of the bushing-jack screw system 700 is described herein. The inclined plane section 300 has a inclined plane section pivot bushing system 305, the first articulating arm 400 has two first articulating arm pivot bushing systems 405, the second articulating arm 500 has a second articulating arm pivot bushing system 505. The tool further includes two adjustment jack screws—a first adjustment jack screw 705 and a second adjustment jack screw 706. The first adjustment jack screw 705 communicates with the inclined plane section pivot bushing system 305 and one of the first articulating arm pivot bushing systems 405 such that the actuator chassis 200 can be moved from left to right by manipulating the first adjustment jack screw 705. In the preferred embodiment, the inclined section pivot bushing system 405 is also pivotally attached to the first articulating arm 400 via a first pivot bolt 410. The second adjustment jack screw 706 communicates with other first articulating arm pivot bushing system 405 and the second articulating arm pivot bushing system 505 such that the actuator chassis 200 can be moved from front to back (frontwards and backwards) by manipulating the second adjustment jack screw 706. In the preferred embodiment, the other first articulating arm pivot bushing system 405 (the system communicating with the second articulating arm pivot bushing system 505) is also pivotally attached to the second articulating arm 500 via a second pivot bolt 510.
In the preferred embodiment, each pivot bushing system (305, 405, 505) includes a pair of corresponding rounded parallel bushing projections 420 with an arbor 425. Within each bushing system, the arbor 425 axially extends across from one corresponding bushing projection 420 to the other corresponding bushing projection 420, with each of the bushing projections 420 holding the arbor 425. The arbors 425 are cylindrical in shape with a threaded arbor hole 426. The arbor hole 426 is perpendicular to the cylindrical axis of the arbor 425. Each screw jack 705, 706 has two corresponding arbors 425 disposed within the communicating pivot bushing systems. For instance, the first adjustment jack screw 705 corresponds to the arbor 425 in the inclined plane section pivot bushing system 305 and the arbor 425 in one of the first articulating arm pivot bushing systems 405. The second adjustment jack screw 706 corresponds to the arbor 425 in the other first articulating arm pivot bushing system 405 and the arbor 425 in the second articulating arm pivot bushing system 505. For each jack screw, one arbor 425 in each corresponding arbor pair has a right hand threaded hole, the opposing arbor 425 has a reverse or left handed threaded hole. The cylindrical shape of the arbor 425 corresponds to a hole 421 that is bored in the corresponding bushing projections 420. Each screw jack 705, 706 has a middle section 707 with a hexagonal cross section shape. Axially extending from the middle section 707 are two partially threaded fingers 708 disposed on opposite ends of the middle section 707. All three are axially aligned (all three axis lined up form a straight line). One finger 708 has a right handed thread and the other finger 708 has a left handed, or reverse thread. The fingers 708 are thread into the correspondingly threaded arbors holes 426. (Each finger 708 is threaded to a corresponding arbor 425.) When an adjustment jack screw 706, 707 is turned the pivot bushings systems are either pushed further apart or pulled closer together due to the interaction of the threads. This causes the actuator chassis 200 to move correspondingly.
As seen in
When introducing elements of the present invention or the preferred embodiment(s) thereof, the articles “a,” “an,” “the,” and “said” are intended to mean there are one or more of the elements. The terms “comprising,” “including,” and “having” are intended to be inclusive and mean that there may be additional elements other than the listed elements.
Although the present invention has been described in considerable detail with reference to certain preferred embodiments thereof, other embodiments are possible. Therefore, the spirit and scope of the appended claims should not be limited to the description of the preferred embodiment(s) contained herein.
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without payment of any royalties thereon or therefor.
