Methods and systems for assembly and installation of airframe crown modules

Patent metadata

Field	Value
Publication number	US-12252271-B2
Application number	US-202117454276-A
Country	US
Kind code	B2
Filing date	Nov 10, 2021
Priority date	Nov 18, 2020
Publication date	Mar 18, 2025
Grant date	Mar 18, 2025

Abstract

Systems and methods are provided for assembling an aircraft. The method includes receiving an upper half barrel section of fuselage that is in a crown up orientation and installing a crown module into the upper half barrel section.

First claim

What is claimed is:

1. A method for assembling an aircraft, the method comprising:
receiving an upper half barrel section of a fuselage that is in a crown up orientation at a crown module attach station of a first assembly line;
advancing the upper half barrel section on a track in a process direction along the first assembly line through a line of serially arranged work stations according to a takt time;
fabricating a crown module of the aircraft in a second assembly line according to the takt time, wherein the second assembly line is a feeder line to the crown module attach station; and
installing the crown module into the upper half barrel section at the crown module attach station;
wherein the crown module and the upper half barrel section are fabricated in parallel such that the crown module and the upper half barrel section arrive at the crown module attach station just in time to install the crown module into the upper half barrel section.

2. The method of claim 1 wherein installing the crown module comprises installing a crown module that is substantially equal in length to the upper half barrel section of the fuselage.

3. The method of claim 1 wherein installing the crown module into the upper half barrel section comprises installing the crown module in a completed state into the upper half barrel section.

4. The method of claim 1 wherein fabricating the crown module comprises fabricating the crown module in the second assembly line that is full pulsed.

5. The method of claim 1 wherein fabricating the crown module comprises fabricating the crown module across work stations of the second assembly line with full pulses between each.

6. The method according to claim 1 further comprising indexing the crown module to a work station using an indexing feature associated with the crown module to an indexing component associated with the work station.

7. The method according to claim 1 wherein fabricating the crown module comprises:
assembling ceiling grid components into a ceiling grid at a crown module grid work station;
installing insulation onto the ceiling grid at an insulation attach work station;
installing stow bins onto the ceiling grid at a stow bin attach work station;
installing ceiling panels onto the ceiling grid at a ceiling panel attach work station; and
installing lighting components on to the ceiling grid at a lighting attach work station.

8. The method according to claim 1 further comprising providing components of the crown module to the line of serially arranged work stations using feeder lines.

9. The method according to claim 1 further comprising micro pulsing the crown module through a work station.

10. The method of claim 1 wherein fabricating the crown module further comprises:
advancing a ceiling grid in a process direction; and
installing insulation onto the ceiling grid.

11. The method of claim 1 wherein fabricating the crown module further comprises:
advancing a ceiling grid in a process direction; and
installing stow bins onto the ceiling grid.

12. The method of claim 1 wherein fabricating the crown module further comprises:
advancing a ceiling grid in a process direction; and
installing ceiling panels onto the ceiling grid.

13. The method of claim 1 wherein fabricating the crown module further comprises:
advancing a ceiling grid in a process direction; and
installing lighting onto the ceiling grid.

14. The method of claim 1 , further comprising:
installing crown module components onto a ceiling grid using a plurality of work stations of the second assembly line;
advancing the ceiling grid in a process direction through the work stations; and
providing a crown module component to the work stations via a feeder line associated with one of the work stations just in time for installation onto the ceiling grid.

15. The method of claim 14 , wherein:
at least one of the work stations is a crown module grid work station; and
the feeder line associated with one of the work stations provides ceiling grid components to the crown module grid work station for fabrication into the ceiling grid.

16. The method of claim 14 , wherein:
at least one of the work stations is an insulation attach work station; and
the feeder line associated with one of the work stations provides insulation to the insulation attach work station for attachment to the ceiling grid.

17. The method of claim 14 , wherein:
at least one of the work stations is a stow bin work station; and
the feeder line associated with one of the work stations provides stow bin components to the stow bin work station for attachment to the ceiling grid.

18. The method of claim 14 , wherein:
at least one of the work stations is a ceiling panel work station; and
the feeder line associated with one of the work stations provides ceiling panel components to the ceiling panel work station for attachment to the ceiling grid.

19. The method of claim 14 , wherein:
at least one of the work stations is a lighting attach work station; and
the feeder line associated with one of the work stations provides lighting components to the lighting attach work station for attachment to the ceiling grid.

20. The method of claim 14 , wherein at least two of the work stations are operable to attach the crown module components onto the ceiling grid simultaneously.

21. The method of claim 14 further comprising indexing the plurality of work stations with indexing components associated with each of the plurality of work stations, the indexing components operable to interface to an indexing feature associated with the ceiling grid to control a position of the ceiling grid with respect to a respective work station.

22. The method of claim 1 , wherein multiple work stations of the first assembly line perform work on the upper half barrel section simultaneously while the half barrel section advances on the track.

23. The method of claim 1 , further comprising:
advancing the upper half barrel section with the installed crown module along the first assembly line to a join station for attachment to a lower half barrel section.

24. The method of claim 1 , further comprising:
providing work instructions to the work stations based on feedback received from communication between indexing features located on the upper half barrel section and indexing components located on the work stations.

25. The method of claim 1 , wherein a gap is present between a first upper half barrel section and a second upper half barrel section on the first assembly line such that a work station of the line of serially arranged work stations can receive maintenance while the work station is positioned in the gap as the first upper half barrel section and the second upper half barrel section advance in the process direction.

Assignees

• Boeing Co

Inventors

• Smith Daniel R
• Jones Darrell D
• Justice Jeremy Evan

Classifications

• B64C1/068

  Fuselage sections · CPC title

• B64C1/061

  Frames · CPC title

• B23P21/004

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

• B23P2700/01

  Aircraft parts · CPC title

• B64F5/10 Primary

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