Indexing for airframes undergoing pulsed-line assembly

Patent metadata

Field	Value
Publication number	US-12509247-B2
Application number	US-202418417819-A
Country	US
Kind code	B2
Filing date	Jan 19, 2024
Priority date	Nov 18, 2020
Publication date	Dec 30, 2025
Grant date	Dec 30, 2025

Abstract

Systems and methods are provided for assembling a structure. The systems and method including micro pulsing a structure along a track in a process direction by less than a length of the structure. The structure is indexed to one or more work stations by mating indexing features in a manufacturing excess of the structure to complementary features at the work stations. The work stations would the perform work on the structure at the work stations while the structure is indexed to the work stations. Iteratively repeating the micro pulsing and indexing and working upon the structure until it is ready to advance to the next assembly process.

First claim

What is claimed is:

1 . A system for assembling structures, the system comprising:
a track that transports structures comprising indexing features, the indexing features in a manufacturing excess of the structures; an array of work stations disposed along the track configured to perform work on the structures and that are separated from each other in a process direction by less than a length of each of the structures; and indexing units that are disposed relative to the work stations along the track at known offsets from corresponding work stations in the array, and that comprise complementary indexing features that are located relative to the track, the complementary indexing features being dimensioned to mate with the indexing features; wherein the array of work stations are configured to remove the manufacturing excess.

2 . The system of claim 1 comprising:
the indexing features configured to convey a 3D characterization and/or Inner Mold Line (IML) loft and/or Outer Mold Line (OML) loft of the structure within a purview of the array of work stations to the array of work stations.

3 . The system of claim 1 wherein:
the indexing features configured to convey a digitization of the structure within a purview of the array of work stations to the array of work stations.

4 . The system of claim 1 wherein:
the indexing features configured to convey assembly instructions for the structure within a purview of the array of work stations to the array of work stations.

5 . The system of claim 1 wherein:
the track comprises a series of stanchions that include rollers at predefined locations for receiving the structures.

6 . The system of claim 1 wherein:
the indexing features are selected from the group consisting of: through-holes, blind holes, slots, pin, RFID tags and/or bar codes that have been coupled to the structure at predefined intervals.

7 . The system of claim 1 wherein:
each work station of the array of work stations performs is configured to perform a type of work selected from the group consisting of: installing frames, installing stringers, installing door surrounds, installing window surrounds, cutting window holes, and cutting door holes.

8 . The system of claim 1 wherein:
different messages are configured to be conveyed to the array of work stations based upon at least a shape or location of the indexing features.

9 . The system of claim 1 wherein:
each work station of the array of work stations performs is configured to perform work on the structure at the same time.

10 . The system of claim 1 wherein:
the structures are separated by gaps that each comprise a multiple of a micro pulse length.

11 . The system of claim 1 wherein:
the structures are configured to be micro pulsed a distance equal to a multiple of a frame pitch distance.

12 . An apparatus for assembling structures, the apparatus comprising:
a track that advances a structure in a process direction; indexing features in a manufacturing excess of the structure; at least one work station disposed along the track, the at least one work station configured to perform work on the structure; and indexing units that are disposed relative to the at least one work station, the indexing units including complementary indexing features that are located relative to the track, the complementary indexing features being dimensioned to mate with the indexing features; wherein the at least one work station is configured to remove the manufacturing excess.

13 . The apparatus of claim 12 wherein:
the indexing units are disposed at offsets from a corresponding at least one work station.

14 . The apparatus of claim 12 wherein:
the at least one work station comprises multiple work stations and the multiple work stations are arrayed serially along the structure that progresses along the track.

15 . A system for assembling a structure the system comprising:
a track that transports structures; indexing features in a manufacturing excess of the structures; an array of work stations disposed along the track, the array of work stations configured to perform work on the structures according to a common takt time; and indexing units that are disposed relative to the array of work stations along the track at known offsets from corresponding work stations in the array; wherein the structures are separated by gaps that each comprise a multiple of a micro pulse length.

16 . The system of claim 15 wherein:
the takt time is equal to a length of time during which the structures are paused between micro pulses plus a length of time during which the structures are advanced between micro pulses.

17 . The system of claim 15 wherein:
the takt time is based upon a number of aircraft fabricated per month and a number of assemblies needed per aircraft.

18 . The system of claim 15 further comprising:
feeder lines configured to feed into the track based on the takt time.

19 . The system of claim 15 wherein:
the array of work stations configured to perform work based upon instructions conveyed by the indexing features at the structures.

20 . A system for assembling structures, the system comprising:
a track; an array of work stations disposed along the track that index to indexing features in manufacturing excesses of structures arranged along the track and configured to perform work on the structures according to a takt time, and that are separated from each other in a process direction by less than a length of each of the structures; and feeder lines configured to supply material to the array of work stations; wherein the track is configured to drive the structures along a series of rollers mounted to stanchions.

21 . The system of claim 20 further comprising:
an outflow line that is configured to remove scrap.

22 . The system of claim 21 wherein:
the outflow line is configured to operate according to the takt time of a half barrel assembly line and the takt time of the outflow line.

23 . The system of claim 22 wherein:
the feeder lines are configured to supply material to the half barrel assembly line.

24 . The system of claim 23 wherein:
the feeder lines are configured to progress according to the takt time of the half barrel assembly line and the takt time of the feeder lines.

25 . The system of claim 20 wherein:
the array of work stations is configured to perform work on the structure during pauses between micro pulses.

26 . The system of claim 20 wherein:
the array of work stations is configured to perform work on the structure during micro pulses between pauses.

27 . The system of claim 20 wherein:
the takt time is equal to a length of time during which the structures are paused between micro pulses plus a micro pulse duration.

28 . The system of claim 20 wherein:
the feeder lines are configured to supply material to the array of work stations in a Just In Time (JIT) manner.

29 . The system of claim 20 wherein:
the feeder lines are configured to provide components selected from the group consisting of: frames, stringers, sections of fuselage, and door surrounds.

30 . The system of claim 20 further comprising:
an outflow line configured to feed chutes that remove scrap material from the array of work stations.

Assignees

• Boeing Co

Inventors

• Smith Daniel R
• Jones Darrell D
• Swanstrom Frederick M

Classifications

• B64C1/068

  Fuselage sections · CPC title

• B23P21/004 Primary

  the units passing two or more work-stations whilst being composed · CPC title

• B23P2700/01

  Aircraft parts · CPC title

• B64F5/50

  Handling or transporting aircraft components · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title