Unitized composite structure manufacturing system

1. A composite structure manufacturing system comprising:

a heating system comprising one or more heating elements configured to generate heat, wherein the one or more heating elements have a first end and a second end;

a frame comprising a first rack that holds the first end and the second end of the one or more heating elements; and

one or more smart bladders that encompasses the heating system in which the heating system and one or more smart bladders form a curing tool defining a volume for a composite structure when one or more smart bladders in the one or more smart bladders are in a rigid state.

2. The composite structure manufacturing system of claim 1 , wherein the one or more smart bladders and the heating system are configured for positioning uncured composite components around the one or more smart bladders to form an uncured composite structure and the heating system is configured to generate heat with a thermal profile for curing the uncured composite structure during a curing operation to form the composite structure.

3. The composite structure manufacturing system of claim 2 , wherein the thermal profile for the heat causes the uncured composite components for the composite structure to have one or more temperatures selected to cure the uncured composite structure.

4. The composite structure manufacturing system of claim 2 , wherein the heating system comprises:

a heat distribution system that distributes the heat with the thermal profile.

5. The composite structure manufacturing system of claim 4 , wherein the heating system further comprises:

a temperature controller connected to at least one of the one or more heating elements or the heat distribution system.

6. The composite structure manufacturing system of claim 2 , further comprising:

a slip sheet located between a first portion of the uncured composite components and a second portion of the uncured composite components in the uncured composite structure such that the first portion of the uncured composite components and the second portion of the uncured composite components are co-cured without being attached to each other in forming the composite structure.

7. The composite structure manufacturing system of claim 2 , wherein the curing tool is an inner mold line tool further comprising:

a shell that is configured to receive the uncured composite components and the curing tool, wherein the shell is an outer mold line tool.

8. The composite structure manufacturing system of claim 7 , wherein a pressure is applied to the uncured composite components within the shell.

9. The composite structure manufacturing system of claim 1 , wherein the first rack holding the one or more heating elements is located within an interior of a shell.

10. The composite structure manufacturing system of claim 1 , further comprising:

the frame configured to hold the heating system.

11. The composite structure manufacturing system of claim 10 , wherein the frame comprises:

the first rack configured to hold the one or more heating elements within the interior of a shell; and

a second rack connected to the shell that holds the first rack within the interior of the shell.

12. The composite structure manufacturing system of claim 1 , wherein the composite structure is selected from a group consisting essentially of a united composite structure, a wing, a horizontal stabilizer, a vertical stabilizer, an engine housing, a wing box, a control surface, and a fuselage section.

13. A composite structure manufacturing system comprising:

a shell that is configured to receive uncured composite components and a curing tool, wherein the shell is an outer mold line tool;

one or more smart bladders in which the uncured composite components are positioned around the one or more smart bladders;

a heating system in which the heating system comprises:

one or more heating elements configured to generate heat;

a heat distribution system that distributes the heat with a thermal profile, wherein the thermal profile varies depending on the uncured composite components present in an uncured composite structure; and

a temperature controller connected to at least one of the one or more heating elements or the heat distribution system in which the heating system is configured to generate the heat with the thermal profile for curing the uncured composite structure during a curing operation while the one or more smart bladders are in a rigid state to form a composite structure in which the thermal profile for the heat causes the uncured composite components for the composite structure to have one or more temperatures selected to cure the uncured composite structure;

a frame configured to hold the heating system in which the frame comprises:

a first rack that holds a first end and a second end of the one or more heating elements within an interior of the shell; and

a second rack connected to the shell that holds the first rack within an interior of the shell, wherein:

the one or more smart bladders encompass the heating system in which the one or more smart bladders and the frame with the heating system are configured to be received within the interior of the uncured composite structure; and

the curing tool is formed by the heating system, the frame, and the one or more smart bladders, wherein the curing tool is an inner mold line tool that defines a volume for the composite structure in a rigid state of the one or more smart bladders;

one or more of the uncured composite components;

a first portion of the one or more of the uncured composite components;

a second portion of the one or more of the uncured composite components; and

a slip sheet located between the first portion and the second portion, such that the first portion and the second portion are co-cured without being attached to each other in forming the composite structure, and in which a pressure is applied to the uncured composite components within the shell.

14. The composite structure manufacturing system of claim 13 , wherein the composite structure is selected from a group consisting essentially of a united composite structure, a wing, a horizontal stabilizer, a vertical stabilizer, an engine housing, a wing box, a control surface, and a fuselage section.

15. The composite structure manufacturing system of claim 13 , wherein:

the thermal profile is configured to generate heat such that the uncured composite components have multiple temperatures selected to cure the uncured composite structure in a desired manner to form the composite structure with desired characteristics.

16. A composite structure manufacturing system comprising:

a heating system;

one or more smart bladders that encompasses the heating system, wherein:

the heating system and one or more smart bladders form a curing tool;

the curing tool defines a volume for a composite structure;

the volume is defined by a rigid state of the one or more smart bladders;

the heating system comprises one or more heating elements configured to generate heat; and

the one or more heating elements have a first end and a second end; and

a frame comprising a first rack that holds the first end and the second end of the one or more heating elements, wherein the first rack holds the one or more heating elements disposed within an interior of a shell.

17. The composite structure manufacturing system of claim 16 , wherein:

the frame is configured to hold the heating system.

18. The composite structure manufacturing system of claim 16 , wherein the frame comprises:

the first rack configured to hold the one or more heating elements disposed within the interior of the shell.

19. The composite structure manufacturing system of claim 16 , wherein the frame further comprises:

a second rack connected to the shell that holds the first rack within the interior of the shell.

20. The composite structure manufacturing system of claim 19 , wherein:

the one or more smart bladders and the heating system are configured for positioning uncured composite components around the one or more smart bladders to form an uncured composite structure.

21. The composite structure manufacturing system of claim 20 , wherein:

the heating system is configured to generate heat with a thermal profile for curing the uncured composite structure during a curing operation to form the composite structure.

22. The composite structure manufacturing system of claim 20 further comprising:

a slip sheet located between a first portion of the uncured composite components and a second portion of the uncured composite components in the uncured composite structure such that the first portion of the uncured composite components and the second portion of the uncured composite components are co-cured without being attached to each other in forming the composite structure.

23. The composite structure manufacturing system of claim 20 , wherein the curing tool is an inner mold line tool.

24. The composite structure manufacturing system of claim 23 , wherein:

the shell is configured to receive the uncured composite components and the curing tool.

25. The composite structure manufacturing system of claim 24 , wherein the shell is an outer mold line tool.

26. The composite structure manufacturing system of claim 20 , wherein a pressure is applied to the uncured composite components within the shell.

27. The composite structure manufacturing system of claim 20 , wherein the composite structure is one of a united composite structure, a wing, a horizontal stabilizer, a vertical stabilizer, an engine housing, a wing box, a control surface, or a fuselage section.

28. A composite structure manufacturing system comprising:

a heating system;

one or more smart bladders that encompasses the heating system, wherein:

the heating system and one or more smart bladders form a curing tool;

the curing tool defines a volume for a composite structure;

the volume is defined by a rigid state of the one or more smart bladders;

the heating system comprises one or more heating elements configured to generate heat; and

the one or more heating elements have a first end and a second end; and

a frame comprising a first rack that holds the first end and the second end of the one or more heating elements, wherein:

the first rack holds the one or more heating elements disposed within an interior of a shell; and

the shell is configured to receive uncured composite components and the curing tool.

29. The composite structure manufacturing system of claim 28 , wherein:

the curing tool is an inner mold line tool; and

the shell is an outer mold line tool.

30. The composite structure manufacturing system of claim 28 , wherein a pressure is applied to the uncured composite components within the shell.

31. The composite structure manufacturing system of claim 28 , wherein the composite structure is one of a united composite structure, a wing, a horizontal stabilizer, a vertical stabilizer, an engine housing, a wing box, a control surface, or a fuselage section.

32. A composite structure manufacturing system comprising:

a heating system;

one or more smart bladders that encompasses the heating system, wherein:

the heating system and one or more smart bladders form a curing tool;

the curing tool defines a volume for a composite structure;

the volume is defined by a rigid state of the one or more smart bladders;

the heating system comprises one or more heating elements configured to generate heat; and

the one or more heating elements have a first end and a second end; and

a frame comprising a first rack that holds the first end and the second end of the one or more heating elements, wherein:

the first rack holds the one or more heating elements disposed within an interior of a shell;

the shell is configured to receive uncured composite components and the curing tool; and

the shell is an outer mold line tool.

33. The composite structure manufacturing system of claim 32 , wherein the curing tool is an inner mold line tool.