Method of making an integrally stiffened article

• US 5,632,940 A
• Filed: 03/29/1994
• Issued: 05/27/1997
• Est. Priority Date: 03/29/1994
• Status: Expired due to Fees

• Current Assignee: Composite Works, LLC
• Original Assignee: Bradford L. Whatley
• Inventors: Whatley, Bradford L.
• Primary Examiner(s): Vargot, Mathieu D.
• Application Number:
  US08/219,647
• Time in Patent Office: 1,155 Days
• Field of Search: 156/190, 156/191, 156/192, 156/193, 156/189, 156/285, 156/182, 156/173, 156/175, 156/245, 264/157, 264/257, 264/258, 264/510, 264/571, 264/46.4, 264/46.7
• US Class Current: 264/46.4
• CPC Class Codes: B29C 70/342 using isostatic pressure
• CPC Class Codes: B29C 70/72 Encapsulating inserts having non-encapsulated projections, e.g. extremities or terminal portions of electrical components B29C70/742 takes precedence
• CPC Class Codes: B29C 70/86 Incorporated in coherent impregnated reinforcing layers, e.g. by winding
• CPC Class Codes: B62K 19/16 the material being wholly or mainly of plastics
• CPC Class Codes: B62M 3/00 Construction of cranks operated by hand or foot

Abstract

A method of making an article from a fiber reinforced polymer composite material including the steps of providing at least two mandrels, wrapping at least one of the mandrels with a first layer of a fiber reinforced polymer composite material, disposing the at least two mandrels in a predetermined orientation, wrapping a second layer of a fiber reinforced polymer composite material around the mandrels, and curing the wrapped assembly.

Claims

1. A method of making an integrally stiffened article, comprising the steps of:

providing at least two elongated mandrels;

individually wrapping each of said at least two mandrels with a first layer of a reinforced polymer composite material extending at least once around each of said at least two mandrels;

disposing said at least two mandrels in a predetermined adjacent orientation;

overwrapping a second layer of a reinforced polymer composite material at least once around said at least two mandrels to form a subassembly;

providing at least one additional elongated mandrel;

individually wrapping said at least one additional mandrel with a first layer of a reinforced polymer composite material extending at least once around said at least one additional mandrel;

disposing said at least one additional mandrel in adjacent relation with said subassembly;

overwrapping a third layer of reinforced polymer composite material around said subassembly and said at least one additional mandrel to form an assembly; and

curing said assembly to form an article having a plurality of internal integral stiffeners having common fiber reinforcement, with each of said internal integral stiffeners having fiber reinforcement common to said third layer of reinforced polymer composite material.

2. The method of claim 1, wherein said first layer comprises a plurality of plies of reinforced polymer composite material.

3. The method of claim 1, wherein said second layer comprises a plurality of plies of reinforced polymer composite material.

4. The method of claim 1, wherein said third layer comprises a plurality of plies of reinforced polymer composite material.

5. The method of claim 1, wherein each of said first, second, and third layers comprise a plurality of plies of reinforced polymer composite material.

6. The method of claim 1, wherein said first layer comprises a plurality of plies of reinforced polymer composite material having various different predetermined fiber orientations with respect to a longitudinal axis of said article.

7. The method of claim 1, wherein said second layer comprises a plurality of plies of reinforced polymer composite material having various different predetermined fiber orientations with respect to a longitudinal axis of said article.

8. The method of claim 1, wherein said third layer comprises a plurality of plies of reinforced polymer composite material having various different predetermined fiber orientations with respect to a longitudinal axis of said article.

9. The method of claim 1, wherein said each of said first, second, and third layers comprises a plurality of plies of reinforced polymer composite material having various different predetermined fiber orientations with respect to a longitudinal axis of said article.

10. The method of claim 1, wherein said first layer comprises seven plies of reinforced polymer composite material having respective predetermined fiber orientations with respect to a longitudinal axis of said article of 0 degrees.

11. The method of claim 1, wherein said second layer comprises seven plies of reinforced polymer composite material having respective predetermined fiber orientations with respect to a longitudinal axis of said article of 0 degrees.

12. The method of claim 1, further comprising the step of removing at least one of said mandrels from said assembly after curing.

13. The method of claim 12, further comprising the step of slicing said assembly after said step of removing at least one of said mandrels to form a plurality of articles.

14. The method of claim 1, further comprising the step of slicing said assembly after curing to form a plurality of articles.

15. The method of claim 1, wherein at least a portion of at least one of said mandrels forms a permanent part of said article.

16. The method of claim 1, wherein at least one of said mandrels has a triangular transverse cross-sectional shape.

17. The method of claim 1, wherein at least one of said mandrels has a hexagonal transverse cross-sectional shape.

18. The method of claim 1, wherein at least two of said mandrels have different transverse cross-sectional shapes.

19. The method of claim 1, further comprising the step of removing at least one of said mandrels after said step of curing and filling the resulting void with a foam material.

20. The method of claim 1, further comprising the step of applying a torsional overwrap of a reinforced polymer composite material around said article after said step of curing, and recuring said article.

21. The method of claim 1, wherein at least one of said mandrels comprises aluminum.

22. The method of claim 1, wherein each of said internal stiffeners comprise a multi-ply construction.

23. The method of claim 1, further comprising the step of disposing said assembly in a jig fixture prior to said step of curing, said jig fixture having a free floating construction which permits movement of said mandrels together, but restrains movement of said mandrels apart.

24. The method of claim 23, further comprising the step of curing said assembly in a said jig fixture under increased pressure and heat conditions.

25. The method of claim 1, wherein said step of providing at least one additional elongated mandrel comprises providing at least two additional elongated mandrels.

26. A method of making an integrally stiffened article, comprising the steps of:

providing at least two elongated mandrels;

individually wrapping each of said at least two mandrels with a first layer of a reinforced polymer composite material extending at least once around each of said at least two mandrels;

disposing said at least two mandrels in a predetermined orientation;

overwrapping a second layer of a reinforced polymer composite material at least once around said at least two mandrels to form a subassembly including a concave portion;

providing at least one additional elongated mandrel;

individually wrapping said at least one additional mandrel with a first layer of a reinforced polymer composite material extending at least once around said at least one additional mandrel;

disposing said at least one additional mandrel in adjacent abutting relation with said each of said at least two mandrels, said at least one additional mandrel nested within said concave portion of said subassembly;

overwrapping a third layer of reinforced polymer composite material around said subassembly and said at least one additional mandrel to form an assembly; and

curing said assembly to form an article having a plurality of internal integral stiffeners having common fiber reinforcement, with each of said internal integral stiffeners having fiber reinforcement common to said third layer of reinforced polymer composite material.

27. The method of claim 26, wherein said each of said first, second, and third layers comprises a plurality of plies of reinforced polymer composite material having various different predetermined fiber orientations with respect to a longitudinal axis of said article.

28. The method of claim 26, further comprising the step of applying a torsional overwrap of a reinforced polymer composite material around said article after said step of curing, and recuring said article.

29. The method of claim 26, further comprising the step of removing at least one of said mandrels after said step of curing and filling the resulting void with a foam material.

30. The method of claim 26, further comprising the step of disposing said assembly in a jig fixture prior to said step of curing, said jig fixture having a free floating construction which permits movement of said mandrels together, but restrains movement of said mandrels apart.