Indexing For Airframes Undergoing Pulsed-Line Assembly
US-2022153434-A1 · May 19, 2022 · US
US11772822B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11772822-B2 |
| Application number | US-202217570217-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 6, 2022 |
| Priority date | Jan 26, 2021 |
| Publication date | Oct 3, 2023 |
| Grant date | Oct 3, 2023 |
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Disclosed herein is a system for lifting an object. The system comprises a first floor, a second floor, and an object rack supported on the second floor. The system further comprises an object advance apparatus coupled with the object rack. The object advance apparatus is configured to advance one object from the plurality of objects from an advancing position to a lifting position. The system additionally comprises a lifting cylinder that is configured to extend from a retracted position below the lifting position to an extended position above the first floor, such that the one object in the lifting position is removed from the object rack and lifted adjacent to the assembling body. The system also comprises a floor flap configured to open and close in synchronization with the extension and retraction of the lifting cylinder.
Opening claim text (preview).
What is claimed is: 1. A system for lifting an object, the system comprising: a first floor and a second floor, the first floor being directly above the second floor and securing an assembling body and the second floor; an object rack supported on the second floor, wherein the object rack is configured to support a plurality of objects, the plurality of objects configured to be attached to the assembling body; an object advance apparatus coupled with the object rack, the object advance apparatus configured to advance one object from the plurality of objects from an advancing position to a lifting position; a lifting cylinder supported by the second floor and positioned in line with the lifting position on the object rack, the lifting cylinder configured to extend from a retracted position below the lifting position on the object rack to an extended position above the first floor, such that as the lifting cylinder is extended from the retracted position the one object in the lifting position is removed from the object rack and lifted adjacent to the assembling body; and a floor flap in the first floor directly above the lifting cylinder, the floor flap configured to open and close in synchronization with the extension and retraction of the lifting cylinder such that the floor flap is opened as the lifting cylinder is extended toward the first floor and remains opened while the lifting cylinder is in the extended position and is closed when the lifting cylinder is retracted below the first floor toward the retracted position and remains closed while the lifting cylinder is in the retracted position. 2. The system of claim 1 , wherein the assembling body is an aircraft fuselage. 3. The system of claim 2 , wherein the plurality of objects is a plurality of frame sections to be attached to the aircraft fuselage. 4. The system of claim 1 , further comprising: a plurality of object racks, each object rack of the plurality of object racks is configured to support a plurality of objects; an object advance apparatus coupled with each object rack of the plurality of object racks, each one of the object advance apparatus is configured to advance one object from the plurality of objects of a corresponding one of the plurality of object racks from an advancing position to a lifting position; a plurality of lifting cylinders on the second floor, wherein a corresponding one of the plurality of lifting cylinders is positioned in line with the lifting position on each object rack of the plurality of object racks, each one of the plurality of lifting cylinders is configured to extend from the retracted position below the lifting position on the corresponding object rack to the extended position above the first floor, such that as the lifting cylinder is extended from the retracted position the one object in the lifting position is removed from the corresponding object rack and lifted adjacent to the assembling body secured to the first floor; and a plurality of floor flaps in the first floor each directly above a corresponding one of the lifting cylinders of the plurality of lifting cylinders, each floor flap configured to open and close in synchronization with the extension and retraction of the corresponding lifting cylinder, such that the floor flap is opened as the corresponding lifting cylinder is extended toward the first floor and remains opened while the corresponding lifting cylinder is in the extended position and is closed when the corresponding lifting cylinder is retracted below the first floor toward the retracted position and remains closed while the corresponding lifting cylinder is in the retracted position. 5. The system of claim 4 , wherein: the plurality of lifting cylinders is configured to automatically extend from the retracted position to the extended position and retract from the extended position to the retracted position at a specific rate; the plurality of cylinders is configured to extend and retract simultaneously; and the object advance apparatus coupled with each object rack is configured to advance one object from the plurality of objects from the advancing position to the lifting position when the lifting cylinder is in the retracted position. 6. The system of claim 4 , wherein: the plurality of lifting cylinders is configured to automatically extend from the retracted position to the extended position and retract from the extended position at a specific rate; each lifting cylinder of the plurality of lifting cylinders is configured to extend and retract consecutively with the other lifting cylinders of the plurality of lifting cylinders; and the object advance apparatus connected to each object rack is configured to advance one object from the plurality of objects from the advancing position to the lifting position when the lifting cylinder is in the retracted position. 7. The system of claim 4 , wherein: each lifting cylinder of the plurality of lifting cylinders is in electrical communication with a user device; and the user device is selectively operable by an operator to extend from the retracted position to the extended position and retract from the extended position to the retracted position at least one lifting cylinder of the plurality. 8. The system of claim 1 , further comprising a conveyor system, wherein: the assembling body is secured to the conveyor system on the first floor; and the assembling body is moved along the conveyor system at a specified pulse rate. 9. The system of claim 1 , further comprising a user device in electrical communication with the lifting cylinder, wherein the user device is selectively operable by an operator to extend and retract the lifting cylinder. 10. The system of claim 1 , wherein: the object rack has a plurality of notches; and each object of the plurality of objects is supported on the object rack in engagement with a corresponding notch of the plurality of notches. 11. A system for lifting an object, the system comprising: a first floor and a second floor, the first floor being directly above the second floor and securing an aircraft fuselage and the second floor supporting a plurality of frame racks, wherein each frame rack of the plurality is configured to support a plurality of frames, the plurality of frames configured to be attached to the aircraft fuselage; a frame advance apparatus in connection with each frame rack of the plurality, the frame advance apparatus configured to advance one frame from the plurality of frames from an advancing position on each frame rack to a lifting position on each frame rack; a plurality of lifting cylinders supported by the second floor, one lifting cylinder of the plurality positioned in line with the lifting position on a corresponding frame rack, each lifting cylinder is configured to extend from a retracted position below the lifting position on the corresponding frame rack to an extended position above the first floor, such that as each lifting cylinder is extended from the retracted position the one frame in the lifting position is removed from the corresponding frame rack and lifted adjacent to the aircraft fuselage; and a plurality of floor flaps, each one of the plurality of floor flaps in the first floor is directly above a corresponding one of the plurality of lifting cylinders, the floor flaps are configured to open and close in synchronization with the extension and retraction of the corresponding lifting cylinder, such that the floor flaps are opened as the corresponding lifting cylinder is extended toward the first floor and remains opened while the lifting cylinder is in the extended position and are closed when the corresponding lifting cylinder is retra
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