Panel structure fabrication

• US 5,366,787 A
• Filed: 10/22/1992
• Issued: 11/22/1994
• Est. Priority Date: 06/03/1991
• Status: Expired due to Term

• Current Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Original Assignee: Mcdonnell Douglas Corporation (The Boeing Co.)
• Inventors: Pettit, Richard G., Yasui, Ken K.
• Primary Examiner(s): Loney, Donald J.
• Application Number:
  US07/964,716
• Time in Patent Office: 761 Days
• Field of Search: 428/167, 428/172, 428/178, 428/188, 428/182, 428/185, 428/174, 428/72, 428/76, 428/120, 428/179, 428/184, 181/288, 181/290, 52/785, 52/795, 52/799, 52/806, 52/811, 244/117 R, 244/119, 244/123, 228/157
• US Class Current: 428/174
• CPC Class Codes: B29C 49/0691 using sheet like material, e.g. sheet blow-moulding from joined sheets
• CPC Class Codes: B29D 22/00 Producing hollow articles tubular articles B29D23/00; pneumatic tyres B29D30/00
• CPC Class Codes: B29D 24/00 Producing articles with hollow walls B29D99/0028 takes precedence
• CPC Class Codes: B32B 3/28 characterised by a layer comprising a deformed thin sheet , i.e. the layer having its entire thickness deformed out of the plane, e.g. corrugated, crumpled B32B29/08 takes precedence
• CPC Class Codes: E04C 2/08 of metal, e.g. sheet metal E04C2/26 takes precedence
• CPC Class Codes: Y10T 428/234 including elements cooperating to form cells
• CPC Class Codes: Y10T 428/24628 Nonplanar uniform thickness material
• CPC Class Codes: Y10T 428/24661 Forming, or cooperating to form cells
• CPC Class Codes: Y10T 428/24669 Aligned or parallel nonplanarities
• CPC Class Codes: Y10T 428/24694 Parallel corrugations
• CPC Class Codes: Y10T 428/24711 Plural corrugated components
• CPC Class Codes: Y10T 428/24719 with corrugations of respective components intersecting in plane projection
• CPC Class Codes: Y10T 428/24744 Longitudinal or transverse tubular cavity or cell

Abstract

The structure and process for making a metallic panel structure from a plurality, e.g. two, core elements each comprised of a pair of sheets of superplastic material welded together along a plurality of weld lines, the weld lines of one core element being spaced differently or of different shape from the weld lines of the other core element. The core elements are joined together, with the weld lines of one core panel positioned at an angle, e.g., normal, to the weld lines of the adjacent core element. The resulting panel assembly is placed in a die. The die is heated to superplastic forming temperature, and gas pressure is applied to the spaces between the sheets of the respective core elements, causing superplastic forming and expansion of the sheets of each core panel to form a first series of bulges between weld lines of one core element, and a second series of bulges dissimilar in shape, e.g. larger, than the first series of bulges, between weld lines of the adjacent core element, the bulges expanding inwardly toward each other. The two series of bulges are orthogonally disposed, the bulges from the two core elements contacting and forming around each other. Further pressurization is applied to cause diffusion bonding at the contacting areas of the two series of bulges. The resulting structure is formed of two normally disposed series of bulges, one series larger than the other, with face sheets connected to such bulges.

Claims

1. A panel structure comprising

a first core element comprised of superplastic material, said superplastic material being a metal or a metal alloy having superplasticity characteristics, and including a plurality of successive inwardly extending superplastically formed first bulges, and

at least one other core element comprised of superplastic material adjacent said first core element, and including a plurality of successive inwardly extending superplastically formed second bulges disposed at an angle to and extending toward said first bulges, said second bulges being dissimilar to said first bulges, said second bulges being formed around and contacting said first bulges, and said first and second bulges being diffusion bonded at the contacting areas.

2. The panel structure of claim 1, the bulges of said at least one other core element being of different size from the bulges of said first core element.

3. The panel structure of claim 1, said first bulges being of substantially the same size, and said second bulges being of substantially the same size, but different in size from said first bulges.

4. The panel structure of claim 1, including first spaced weld lines defining said first bulges, said first weld lines being parallel lines, and second spaced weld lines defining said second bulges, said second weld lines being parallel lines spaced apart a distance greater than said first parallel weld lines, said second bulges being larger than said first bulges.

5. The panel structure of claim 4, said second bulges being orthogonally disposed to said first bulges.

6. The panel structure of claim 4, said second bulges being disposed at an angle other than 90°

to said first bulges.

7. The panel structure of claim 1, including first spaced weld lines defining said first bulges and second spaced weld lines defining said second bulges, at least said first weld lines or said second weld lines being non-parallel.

8. The panel structure of claim 1, including first spaced weld lines defining said first bulges and second spaced weld lines defining said second bulges, at least said first weld lines or said second weld lines being curved.

9. The panel structure of claim 1, including first spaced weld lines defining said first bulges and second spaced weld lines defining said second bulges, at least said first weld lines or said second weld lines being of sine wave shape.

10. The panel structure of claim 1, including first spaced weld lines defining said first bulges and second spaced weld lines defining said second bulges, at least said first weld lines or said second weld lines being hexagon shaped.

11. The panel structure of claim 1, including a face sheet connected to said first bulges and a face sheet connected to said second bulges.

12. The panel structure of claim 1, each of said core elements formed of a pair of superplastic metal sheets, said sheets of each core element welded together along a plurality of spaced weld lines, the weld lines of said at least one other core element being spaced apart a distance greater than the weld lines of said first core element and disposed normal to the weld lines of said first core element, the first bulges on said first core element being formed between adjacent weld lines thereof and the second bulges on said second core element being formed between adjacent weld lines thereof, said second bulges being larger than said first bulges.

13. The panel structure of claim 11, employing a pair of said core elements and forming a four-sheet panel structure.

14. The panel structure of claim 1, said at least one other core element being a second core element and including a third core element comprised of superplastic material adjacent said second core element, said third core element including a plurality of superplastically formed third bulges disposed at an angle to and extending toward said second bulges, said third bulges being similar to said first bulges and being formed around and contacting said second bulges, said first and third bulges being parallel, and said second and third bulges being diffusion bonded at the contacting areas.

15. The panel structure of claim 14, each of said core elements formed of a pair of metal sheets, each comprised of a superplastic material, said sheets of each core element being welded together along a plurality of parallel weld lines, the weld lines of said first and third core elements being parallel, and the weld lines of said second core element being spaced apart a distance greater than the weld lines of said first and third core elements, and being disposed normal to the weld lines of said first and third core elements, the first bulges on said first core element being formed between adjacent weld lines thereof, the second bulges on said second core element being formed between adjacent weld lines thereof, and the third bulges on said third core element being formed between adjacent weld lines thereof, said second bulges being larger than said first and third bulges.

16. The panel structure of claim 15, including a first face sheet forming one of the sheets of said first core element and connected to the first bulges at the weld lines on said first core element, and a second face sheet forming one of the sheets of said third core element and connected to said third bulges at the weld lines on said third core element, and forming a six-sheet panel structure.

17. The panel structure of claim 15, and including a first separate face sheet contiguous to and diffusion bonded to the first bulges on said first core element and a second separate face sheet contiguous to and diffusion bonded to the third bulges on said third core element, and forming an eight-sheet panel structure.