Method of using a tower for accessing an interior of a fuselage assembly

Patent metadata

Field	Value
Publication number	US-10406593-B2
Application number	US-201414559234-A
Country	US
Kind code	B2
Filing date	Dec 3, 2014
Priority date	Jul 9, 2014
Publication date	Sep 10, 2019
Grant date	Sep 10, 2019

Abstract

A method and apparatus for accessing an interior of a fuselage assembly. A tower having a number of platform levels may be driven into a selected tower position within an assembly area. The interior of the fuselage assembly may be accessed using the number of platform levels.

First claim

What is claimed is:

1. A method for accessing an interior of a fuselage assembly, the method comprising:
driving a tower having a number of platform levels into a selected tower position within an assembly area;
coupling a number of utilities between the tower and a utility fixture at the selected tower position in the assembly area;
distributing the number of utilities from the utility fixture via the tower to an assembly fixture holding the fuselage assembly;
distributing the number of utilities from the utility fixture via the tower to an internal mobile platform located on one of the number of platform levels by carrying the number of utilities from the utility fixture in a number of utility cables from the tower to the internal mobile platform;
accessing the interior of the fuselage assembly using the number of platform levels by driving the internal mobile platform located on the one of the number of platform levels from the tower into the interior of the fuselage assembly; and
managing the number of utility cables carrying the number of utilities from the utility fixture to the internal mobile platform while driving the internal mobile platform from the tower into the fuselage assembly using a cable management system on the tower.

2. The method of claim 1 , wherein driving the tower comprises:
driving the tower autonomously into the selected tower position.

3. The method of claim 1 further comprising:
building the assembly fixture proximate to the tower.

4. The method of claim 3 further comprising:
engaging a plurality of panels with the assembly fixture to build the fuselage assembly.

5. The method of claim 3 wherein
accessing the interior of the fuselage assembly comprises driving the internal mobile platform onto at least one of a number of floors within the interior of the fuselage assembly from the one of the number of platform levels of the tower.

6. The method of claim 1 further comprising:
mating the number of platform levels of the tower to a number of floors of the fuselage assembly.

7. The method of claim 6 , wherein mating the number of platform levels of the tower to the number of floors of the fuselage assembly comprises:
aligning a ramp system associated with the one of the number of platform levels to a corresponding one of the number of floors.

8. The method of claim 6 , wherein mating the number of platform levels of the tower to the number of floors of the fuselage assembly comprises:
aligning the number of platform levels to the number of floors using a plurality of stabilizing members.

9. The method of claim 8 , wherein aligning the number of platform levels to the number of floors comprises:
aligning the number of platform levels to the number of floors autonomously using the plurality of stabilizing members.

10. The method of claim 1 , wherein coupling the number of utilities between the tower and the utility fixture comprises:
coupling a set of coupling units associated with the tower to a corresponding set of coupling units associated with the utility fixture such that the number of utilities flows from the utility fixture to the tower.

11. The method of claim 1 , wherein coupling the number of utilities between the tower and the utility fixture comprises:
coupling the tower to the utility fixture autonomously to enable the number of utilities to flow downstream from the utility fixture to the tower.

12. The method of claim 1 further comprising:
coupling the number of utilities between the tower and the assembly fixture.

13. The method of claim 1 further comprising:
coupling the assembly fixture to the tower to enable a flow of the number of utilities from the tower to the assembly fixture.

14. The method of claim 1 further comprising:
coupling the assembly fixture to the tower to form an interface; and
distributing the number of utilities from the tower to the assembly fixture across the interface.

15. The method of claim 14 , wherein coupling the assembly fixture to the tower comprises:
coupling the assembly fixture to the tower autonomously to form the interface.

16. The method of claim 14 further comprising:
driving the assembly fixture into a selected cradle position relative to the tower.

17. The method of claim 14 , wherein driving the tower comprises:
driving the tower into the selected tower position relative to the assembly fixture already located within the assembly area.

18. The method of claim 1 further comprising:
decoupling the number of utilities between the tower and the utility fixture.

19. The method of claim 18 , wherein decoupling the number of utilities comprises:
decoupling a set of coupling units associated with the tower from a corresponding set of coupling units associated with the utility fixture autonomously to stop a flow of the number of utilities from the utility fixture to the tower.

20. The method of claim 1 further comprising
accessing, by a human operator, the interior of the fuselage assembly from one of the number of platform levels.

21. The method of claim 1 , wherein managing the number of utility cables comprises:
spooling the number of utility cables using a number of cable wheels in the cable management system on the tower as the internal mobile platform moves through the interior of the fuselage assembly.

22. The method of claim 1 , wherein driving the internal mobile platform comprises:
driving the internal mobile platform autonomously onto one of a passenger floor and a cargo floor inside the fuselage assembly from a corresponding one of the number of platform levels.

23. The method of claim 1 further comprising:
driving an autonomous vehicle across a floor into a position underneath the tower; and
coupling the autonomous vehicle with the tower.

24. The method of claim 23 , wherein coupling the autonomous vehicle with the tower comprises:
transferring a load of the tower onto the autonomous vehicle.

25. The method of claim 24 , wherein transferring the load comprises:
lifting the tower vertically off of the floor using a number of lift devices associated with the autonomous vehicle.

26. The method of claim 23 , wherein driving the tower comprises:
driving the tower autonomously across the floor into the selected tower position using the autonomous vehicle with the autonomous vehicle coupled to the tower.

27. The method of claim 26 further comprising:
lowering the tower back onto the floor; and
stabilizing the tower relative to the floor using a plurality of stabilizing members.

28. The method of claim 1 , further comprising performing an assembly process on the fuselage assembly by an internal robotic device on the internal mobile platform in the interior of the fuselage assembly to assemble a portion of an aircraft.

29. The method of claim 1 , wherein managing the number of utility cables comprises keeping the number of utility cables in tension to prevent the number of utility cables from dragging on the one of the number of platform levels or a floor of the fuselage assembly.

Assignees

• Boeing Co

Inventors

• Oberoi Harinder S
• Reese Iv Richard Griffith
• Barrick Kevin Marion
• Do Quang T
• Draper Alan S
• Hu Yuanxin Charles
• Gerosa Alfredo Jose
• Kozak Michael J
• Miller Jeffrey Lawrence

Classifications

• G05B19/41865

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• B29C39/22

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• B60G2300/60

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