Flexible manufacturing for aircraft structures

Patent metadata

Field	Value
Publication number	US-10427254-B2
Application number	US-201414558867-A
Country	US
Kind code	B2
Filing date	Dec 3, 2014
Priority date	Apr 30, 2014
Publication date	Oct 1, 2019
Grant date	Oct 1, 2019

Abstract

A method and apparatus for manufacturing an aircraft structure. A drivable support may be driven from a first location to a second location to bring the drivable support together with at least one other drivable support to form a drivable support system. A structure may be held in a desired position using the drivable support system.

First claim

What is claimed is:

1. A method for manufacturing a structure, the method comprising:
independently driving each drivable support in a first plurality of drivable supports from a first location to a second location;
attaching each drivable support in the first plurality of drivable supports to a different point along a first side of the structure at the second location;
independently driving each drivable support in a second plurality of drivable supports to the second location;
attaching each drivable support in the second plurality of drivable supports to a different point along a second side of the structure at the second location, wherein the first plurality of drivable supports attached to the structure and the second plurality of drivable supports attached to the structure form a drivable support system for the structure;
holding the structure in a desired position using the drivable support system;
placing first support structures between each of the first plurality of drivable supports to create a first platform at the second location; and
placing second support structures between each of the second plurality of drivable supports to create a second platform at the second location.

2. The method of claim 1 further comprising:
driving the structure from the second location to a third location on a floor of a manufacturing environment using the drivable support system.

3. The method of claim 2 further comprising:
performing operations on the structure using a plurality of autonomous tool systems.

4. The method of claim 3 , wherein the operations are performed while the structure is at the third location.

5. The method of claim 4 further comprising:
steering the plurality of autonomous tool systems.

6. The method of claim 3 further comprising:
steering the drivable support system.

7. The method of claim 3 , wherein the operations are performed while the structure is at the second location.

8. The method of claim 3 further comprising:
determining a current position for at least one of the drivable support system, the plurality of autonomous tool systems, or the structure, in which the current position is determined using a metrology system.

9. The method of claim 8 further comprising:
controlling operation of the plurality of autonomous tool systems, the drivable support system, and the metrology system using a controller.

10. The method of claim 8 further comprising:
removing the structure from the drivable support system;
separating the plurality of drivable supports in the drivable support system from one another; and
driving at least one of the plurality of drivable supports to a fourth location.

11. The method of claim 10 , wherein the fourth location is the first location.

12. The method of claim 8 further comprising:
performing the operations on the structure using at least one of a crawler robot, a tack driller, a hexapod, a lower panel driller, or an upper panel driller.

13. The method of claim 12 further comprising:
pulsing the structure through a plurality of work cells in the manufacturing environment using the drivable support system, wherein the operations are performed on the structure at the plurality of work cells.

14. The method of claim 12 further comprising:
continuously moving the structure through the manufacturing environment using the drivable support system.

15. The method of claim 3 further comprising:
positioning the plurality of autonomous tool systems relative to the structure using commands generated by a controller.

16. The method of claim 15 further comprising:
monitoring a current position of the plurality of autonomous tool systems using a metrology system.

17. The method of claim 3 further comprising:
reconfiguring at least one of the drivable support system or the plurality of autonomous tool systems based on changes in at least one of dimensions of the manufacturing environment, a status of the structure, or a status of the at least one of the drivable support system or the plurality of autonomous tool systems.

18. The method of claim 3 further comprising:
generating commands to move the plurality of autonomous tool systems from a current position to a desired position relative to the structure, wherein the commands are generated using a controller.

19. The method of claim 18 further comprising:
assigning tasks to the plurality of autonomous tool systems in the commands generated by the controller.

20. The method of claim 19 further comprising:
monitoring a status of the tasks assigned to the plurality of autonomous tool systems;
monitoring a status of the plurality of autonomous tool systems; and
reassigning the tasks between the plurality of autonomous tool systems based on at least one of the status of the tasks or the status of the plurality of autonomous tool systems.

21. The method of claim 3 further comprising:
generating commands for the first plurality of drivable supports to drive from the first location to the second location using a controller.

22. The method of claim 21 further comprising:
assigning tasks to each drivable support in the commands generated by the controller.

23. The method of claim 22 further comprising:
monitoring a status of the tasks assigned to the plurality of drivable supports;
monitoring a status of the plurality of drivable supports; and
reassigning the tasks between the plurality of drivable supports based on at least one of the status of the tasks or the status of the plurality of drivable supports.

24. The method of claim 3 further comprising:
generating a path for a plurality of autonomous tool systems to reach the desired position relative to the structure, wherein the path is generated by a navigator.

25. The method of claim 3 further comprising:
positioning an upper skin panel relative to the structure.

26. The method of claim 25 further comprising:
performing the operations on the upper skin panel using a first portion of the plurality of autonomous tool systems.

27. The method of claim 26 further comprising:
positioning a lower skin panel relative to the structure.

28. The method of claim 27 further comprising:
performing the operations on the lower skin panel using a second portion of the plurality of autonomous tool systems.

29. The method of claim 3 further comprising:
driving the plurality of autonomous tool systems along the floor of the manufacturing environment.

30. The method of claim 29 further comprising:
driving the plurality of autonomous tool systems across the structure.

31. The method of claim 3 further comprising:
operating the plurality of autonomous tool systems simultaneously to perform the operations on the structure.

32. The method of claim 31 , wherein an operation in the operations includes at least one of a drilling operation, a fastening operation, an inspecting operation, a sealing operation, a measurement operation, a leveling operation, or a cleaning operation.

33. The method of claim 1 further comprising:
carrying the structure from the second location to a third location using the drivable support system.

34. The method of claim 1 further comprising:
carrying a portion of the structure from the first lo

Assignees

• Boeing Co

Inventors

• Day Dan Dresskell
• Munk Clayton Lynn
• Schmitt Steven John
• Reid Eric M

Classifications

• Y10T408/03

  Processes · CPC title

• Y10T408/52

  with work advancing or guiding means · CPC title

• Y10T29/50

  Convertible metal working machine · CPC title

• B23P21/004 Primary

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

• B64F5/10 Primary

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