Methods and systems for assembly and installation of airframe floor grids

Patent metadata

Field	Value
Publication number	US-12049330-B2
Application number	US-202117454291-A
Country	US
Kind code	B2
Filing date	Nov 10, 2021
Priority date	Nov 18, 2020
Publication date	Jul 30, 2024
Grant date	Jul 30, 2024

Abstract

Systems and methods are provided for assembling an aircraft. The method includes receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation; and installing a floor grid into the lower half barrel section while inverted.

First claim

What is claimed is:

1. A method for assembling an aircraft, the method comprising:
receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation;
installing a floor grid into the lower half barrel section while inverted, wherein installing the floor grid into the lower half barrel section comprises installing a cargo floor grid and then installing a cabin floor grid;
receiving floor beams from a floor beam assembly feeder line;
receiving intercostals from an intercostal feeder line;
indexing the floor beams and intercostals to a floor grid assembly station; and
assembling the floor grid from the intercostals and floor beams at the floor grid assembly station.

2. The method of claim 1 , wherein installing the floor grid comprises installing a floor grid that is substantially equal in length to the lower half barrel section of fuselage.

3. The method of claim 1 , wherein installing the floor grid into the lower half barrel section comprises installing a passenger floor grid.

4. The method of claim 1 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the cargo floor grid and then installing the cargo floor grid into the lower half barrel section.

5. The method of claim 1 , wherein installing the floor grid into the lower half barrel section comprises installing the floor grid into the lower half barrel section in a completed state.

6. The method of claim 1 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the floor grid and then installing the floor grid into the lower half barrel section.

7. A method for assembling an aircraft, the method comprising:
receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation;
installing a floor grid into the lower half barrel section while inverted, wherein installing the floor grid into the lower half barrel section comprises installing a cargo floor grid and then installing a cabin floor grid;
advancing the lower half barrel section in a process direction after the floor grid is installed; and
rotating the lower half barrel section to a keel down orientation.

8. The method of claim 7 , wherein installing the floor grid comprises installing a floor grid that is substantially equal in length to the lower half barrel section of fuselage.

9. The method of claim 7 , wherein installing the floor grid into the lower half barrel section comprises installing a passenger floor grid.

10. The method of claim 7 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the cargo floor grid and then installing the cargo floor grid into the lower half barrel section.

11. The method of claim 7 , wherein installing the floor grid into the lower half barrel section comprises installing the floor grid into the lower half barrel section in a completed state.

12. The method of claim 7 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the floor grid and then installing the floor grid into the lower half barrel section.

13. The method of claim 1 , further comprising indexing the floor grid to the floor grid assembly station.

14. A method for assembling an aircraft, the method comprising:
receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation;
installing a floor grid into the lower half barrel section while inverted, wherein installing the floor grid into the lower half barrel section comprises installing a cargo floor grid and then installing a cabin floor grid;
receiving floor beams from a floor beam assembly feeder line;
receiving intercostals from an intercostal feeder line; and
assembling the floor grid from the intercostals and floor beams at a floor grid assembly station;
pulsing the floor grid to a track installation station;
indexing the floor grid to the track installation station; and
installing tracks onto the floor grid at the track installation station.

15. The method of claim 14 , wherein installing tracks comprises installing one or more of cargo tie down tracks, cargo roller tracks, and seat tracks.

16. The method of claim 14 , wherein installing the floor grid comprises installing a floor grid that is substantially equal in length to the lower half barrel section of fuselage.

17. The method of claim 14 , wherein installing the floor grid into the lower half barrel section comprises installing a passenger floor grid.

18. The method of claim 14 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the cargo floor grid and then installing the cargo floor grid into the lower half barrel section.

19. The method of claim 14 , wherein installing the floor grid into the lower half barrel section comprises installing the floor grid into the lower half barrel section in a completed state.

20. The method of claim 14 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the floor grid and then installing the floor grid into the lower half barrel section.

21. A method for assembling an aircraft, the method comprising:
receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation;
installing a floor grid into the lower half barrel section while inverted, wherein installing the floor grid into the lower half barrel section comprises installing a cargo floor grid and then installing a cabin floor grid;
receiving floor beams from a floor beam assembly feeder line;
receiving intercostals from an intercostal feeder line; and
assembling the floor grid from the intercostals and floor beams at a floor grid assembly station;
pulsing the floor grid to an electrical equipment and plumbing installation station;
indexing the floor grid to the electrical equipment and plumbing installation station; and
installing electrical equipment and plumbing onto the floor grid at the electrical equipment and plumbing installation station.

22. The method of claim 21 , wherein installing the floor grid comprises installing a floor grid that is substantially equal in length to the lower half barrel section of fuselage.

23. The method of claim 21 , wherein installing the floor grid into the lower half barrel section comprises installing a passenger floor grid.

24. The method of claim 21 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the cargo floor grid and then installing the cargo floor grid into the lower half barrel section.

25. The method of claim 21 , wherein installing the floor grid into the lower half barrel section comprises installing the floor grid into the lower half barrel section in a completed state.

26. The method of claim 21 , wherein installing the floor grid into the lower half barrel section comprises installing floor panels into the floor grid and then installing the floor grid into the lower half barrel section.

27. A method for assembling an aircraft, the method comprising:
receiving a lower half barrel section of fuselage that is inverted to a keel-up orientation;
installing a floor grid into the lower half barrel section while inverted, wherein installing the floor grid into the lower half barrel section compr

Assignees

• Boeing Co

Inventors

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

Classifications

• B64C1/069

  Joining arrangements therefor · CPC title

• B23P19/04

  for assembling or disassembling parts · CPC title

• B23Q3/062

  adapted for holding workpieces having a special form or being made from a special material · CPC title

• B64C1/18

  Floors · CPC title

• B64F5/10 Primary

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