Adjustable retaining structure for a cradle fixture

1. A method for aligning a plurality of sub-panels of a fuselage keel panel during an assembly of a fuselage, the method comprising:

the fuselage keel panel comprising the plurality of sub-panels;

placing a first sub-panel of the sub-panels onto a curved beam of an adjustable retaining structure of a cradle fixture comprising a base, the adjustable retaining structure configured to rotate responsive to changing loads on the fuselage assembly during the assembly of the fuselage, the cured beam comprising a shape substantially matching a curvature for a corresponding portion of an outer mold line for the fuselage and supporting the first sub-panel;

aligning the adjustable retaining structure with a curvature of the first sub-panel via the first sub-panel engaging the curved beam and passively rotating the curved beam about an X-axis, a Y-axis, and a Z-axis with respect to the base, such that the adjustable retaining structure connects to a lift configured to move along first rails parallel to the Y-axis and also move perpendicular to the Y-axis along second rails connected to a third rail transporting a utilities unit and a cable management system along the base;

placing a second sub-panel of the sub-panels onto the curved beam and engaging the first sub-panel with the second sub-panel;

aligning the adjustable retaining structure with a curvature of the second sub-panel via the second sub-panel engaging the curved beam and passively rotating the curved beam about the X-axis, the Y-axis, and the Z-axis with respect to the base; and

connecting the first sub-panel to the second sub-panel.

2. The method of claim 1 , wherein further comprising the base supporting a vertical movement system supporting a connection beam supporting an interface pivotally supporting the curved beam.

3. The method of claim 2 further comprising:

a shape of the first sub-panel and the second sub-panel temporarily connected substantially matching the curvature for the corresponding portion of the outer mold line for the fuselage; and

supporting a load of the first sub-panel and the second sub-panel using the adjustable retaining structure.

4. The method of claim 2 , further comprising:

the interface comprising a spherical interface; and

rotating the adjustable retaining structure about the spherical interface in response to the adjustable retaining structure impinging on the first sub-panel.

5. The method of claim 4 , wherein rotating the adjustable retaining structure comprises:

rotating the adjustable retaining structure about the spherical interface in response to a loading of the adjustable retaining structure when the adjustable retaining structure impinges on the first sub-panel.

6. The method of claim 1 , further comprising impinging on the first sub-panel with the adjustable retaining structure to align the curved beam of the adjustable retaining structure with the curvature of the first sub-panel.

7. The method of claim 1 , further comprising moving the adjustable retaining structure towards the first sub-panel such that the adjustable retaining structure impinges on the first sub-panel.

8. The method of claim 7 , wherein moving the adjustable retaining structure comprises:

moving the adjustable retaining structure towards the first sub-panel using at least one scissor lift mechanism.

9. The method of claim 7 , wherein moving the adjustable retaining structure comprises:

applying a force against the first sub-panel with the adjustable retaining structure as the adjustable retaining structure is moved in a direction towards the first sub-panel.

10. The method of claim 7 , wherein moving the adjustable retaining structure comprises:

translating the adjustable retaining structure along at least one of the X-axis, the Y-axis, or the Z-axis to move the adjustable retaining structure towards the first sub-panel.

11. The method of claim 10 , wherein translating the adjustable retaining structure comprises:

translating a connection member with which the adjustable retaining structure is rotatably associated along the at least one of the X-axis, the Y-axis, or the Z-axis.

12. The method of claim 11 , wherein translating the connection member comprises:

translating the connection member autonomously along the at least one of the X-axis, the Y-axis, or the Z-axis.

13. The method of claim 1 , further comprising:

impinging on the first sub-panel with the adjustable retaining structure; and

wherein rotating the adjustable retaining structure comprises rotating the adjustable retaining structure about a spherical interface about the X-axis, the Y-axis, and the Z-axis until the curved beam of the adjustable retaining structure aligns with the curvature of the first sub-panel.

14. The method of claim 1 further comprising:

moving the adjustable retaining structure relative to the base of the cradle fixture prior to the first sub-panel being engaged with the adjustable retaining structure.

15. The method of claim 14 , wherein moving the adjustable retaining structure comprises:

translating the adjustable retaining structure along at least one of the X-axis, the Y-axis, or the Z-axis to position the adjustable retaining structure relative to the base of the cradle fixture.

16. The method of claim 15 , wherein translating the adjustable retaining structure comprises:

translating a connection member with which the adjustable retaining structure is associated along the X-axis relative to the base using a first rail system; and

translating the connection member along the Y-axis relative to the base using a second rail system.

17. The method of claim 15 , wherein translating the adjustable retaining structure comprises:

translating a connection member along the Z-axis relative to the base using at least one scissor lift mechanism.

18. The method of claim 1 further comprising:

readjusting an alignment of the adjustable retaining structure with the first sub-panel during building of the fuselage.

19. The method of claim 18 , wherein readjusting the alignment of the adjustable retaining structure comprises:

rotating, passively, the adjustable retaining structure about a spherical interface as a load being applied to the adjustable retaining structure changes during the building of the fuselage.

20. The method of claim 1 , further comprising the adjustable retaining structure comprising a number of curved beams comprising a curvature that substantially matches the curvature of the outer mold line for the keel panel of the fuselage.

21. A method for adjusting an adjustable retaining structure comprising a curved beam during assembly of a plurality of sub-panels of skin panels in a keel panel, the method comprising:

the keel panel comprising the plurality of sub-panels;

engaging a first skin panel with a second skin panel while supporting at least one of the first skin panel or the second skin panel on the adjustable retaining structure;

aligning the curved beam with a curvature of the first skin panel and the second skin panel, as at least one of the first skin panel or the second skin panel apply loads to the adjustable retaining structure, via rotating, passively, the curved beam of the adjustable retaining structure about a spherical interface about an X-axis, a Y-axis, and a Z-axis, such that the adjustable retaining structure connects to a lift configured to move along first rails parallel to the Y-axis and also move perpendicular to the Y-axis along second rails connected to a third rail transporting a utilities unit and a cable management system along a base supporting the first rails and the second rails and the adjustable retaining structure; and

connecting the first skin panel to the second skin panel.

22. The method of claim 21 further comprising:

rotating the adjustable retaining structure about the spherical interface, such that the rotating occurs passively as the adjustable retaining structure supports the first skin panel and the second skin panel and loads, the loads being transferred through the first skin panel and the second skin panel to the adjustable retaining structure change; and

a shape of the first skin panel and the second skin panel temporarily connected substantially matching a curvature for a corresponding portion of an outer mold line of a structure comprising the first skin panel and the second skin panel.

23. A system configured to align sub-panels in a keel panel in a fuselage assembly, such that the system comprises a cradle fixture, configured to support assembly of the keel panel for a curved structure, such that:

the keel panel comprises a plurality of sub-panels; and

the cradle fixture comprises:

a base; and

an adjustable retaining structure associated with the base, such that the adjustable retaining structure connects to a lift configured to move along first rails parallel to a Y-axis with respect to the base and also move perpendicular to the Y-axis along second rails connected to a third rail transporting a utilities unit and a cable management system along the base, and comprises curved beams configured to:

support the plurality of sub-panels for assembly of the keel panel of the curved structure;

responsive to engaging the plurality of sub-panels to each other on the curved beams, rotate at least one sub-panel of the plurality of sub-panels passively about an X-axis, the Y-axis, and a Z-axis with respect to the base such that the plurality of sub-panels align the curved beam of the adjustable retaining structure comprising a spherical interface with a curvature of the plurality of sub-panels substantially matching a curvature for a corresponding portion of an outer mold line for the keel panel for the curved structure; and

rotate responsive to changing loads on the curved structure during the assembly of the curved structure.

24. The system of claim 23 further comprising:

a connection member, wherein the adjustable retaining structure is rotatably associated with the connection member.

25. The system of claim 24 , wherein the adjustable retaining structure is rotatably associated with the connection member through the spherical interface.

26. The system of claim 24 further comprising:

a movement system that translates the connection member along at least one of the X-axis, the Y-axis, or the Z-axis relative to the base of the cradle fixture.

27. The system of claim 26 , wherein the movement system comprises:

a rail system.

28. The system of claim 26 , wherein the movement system comprises:

a scissor lift mechanism.

29. The system of claim 23 further comprising:

a plurality of stabilizing members associated with the base.

30. The system of claim 29 further comprising:

a tower coupling unit associated with the base;

a cradle coupling unit associated with the base; and

a robotics coupling unit associated with the base.

31. The system of claim 23 further comprising:

a set of sensors associated with the adjustable retaining structure, wherein a set of sensors aid in engaging the adjustable retaining structure with the plurality of sub-panels.

32. The system of claim 23 , wherein the cradle fixture is a drivable cradle fixture.

33. An assembly fixture for a curved structure that comprises skin panels assembled to form a keel panel, such that the assembly fixture comprises:

the keel panel comprises a plurality of sub-panels;

a number of cradle fixtures in which at least one of the number of cradle fixtures comprises:

a number of retaining structures in which at least one of the number of retaining structures comprises an adjustable retaining structure that comprises: a base, such that the adjustable retaining structure connects to a lift configured to move along first rails parallel to a Y-axis with respect to the base and also move perpendicular to the Y-axis along second rails connected to a third rail transporting a utilities unit and a cable management system along the base, and a curved beam configured to:

impinge on a first sub-panel of the plurality of sub-panels engaged with a second sub-panel of the plurality of sub-panels for an exterior of the curved structure; and

passively rotate the curved beam about an X-axis, a Y-axis, and a Z-axis with respect to the base and align the curved beam of the adjustable retaining structure with a curvature of the first sub-panel engaged with the second sub-panel, such that the curvature of the first sub-panel engaged with the second sub-panel substantially matches a curvature for a corresponding portion of an outer mold line for the curved structure.