Large diameter domes and methods of manufacturing same

• US 7,201,811 B2
• Filed: 09/08/2003
• Issued: 04/10/2007
• Est. Priority Date: 08/22/2001
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Waldron, Douglas J., Bozich, William F., Babel, Henry W., de Jesus, Ronaldo Reyes
• Primary Examiner(s): WYSZOMIERSKI, GEORGE P
• Application Number:
  US10/658,598
• Publication Number:
  US 20040079454A1
• Time in Patent Office: 1,310 Days
• Field of Search: 148/519, 148/521, 148/535, 228/112.1
• US Class Current: 148/535
• CPC Class Codes: B21D 22/14 Spinning
• CPC Class Codes: B23K 20/122 using a non-consumable tool, e.g. friction stir welding
• CPC Class Codes: B23K 20/128 making use of additional material

Abstract

The present invention relates to methods of making large spin blanks out of pieces of aluminum sheet or plate joined by friction stir welding to provide plate blank sizes greater than 156 inch (396 cm) in diameter. Blank sizes greater than 209 inch diameter enable manufacturing possibilities for large one-piece spun parts instead of constructing large structures from pieces. This also applies to sheet, except that the maximum width obtainable is 139 inches (353 cm). The availability of large blank sizes, particularly for sheet, permits the use of traditional spinning where bending is the predominant method of metal movement rather than stretching and spinning. As the present invention is a very cost effective approach, it provides a method for producing significantly more economical spin blanks between 156 and 209 inches in diameter than are obtainable for a single piece blank.

Claims

1. A method of making spin blanks greater than a predetermined size, comprising:

providing at least two pieces of material having abutting edges;

annealing the at least two pieces of material;

friction stir welding the at least two pieces of annealed material together along the abutting edges to form a blank; and

spin forming the blank into a desired article, including clamping the blank, applying heat thereto, and rotating the blank while applying pressure to selected regions thereof using a tool.

2. The method as recited in claim 1, wherein any number and size of material pieces are joined by friction stir welding to provide the required blank size.

3. The method as recited in claim 1, wherein the material pieces are an aluminum alloy.

4. The method as recited in claim 3, wherein the material pieces comprise sheet having a thickness of 0.030 inches (0.762 mm) or greater.

5. The method as recited in claim 3, wherein the material pieces comprise plate having a thickness of 0.250 inches or greater to a maximum thickness that can be friction stir welded.

6. The method as recited in claim 1, wherein the blank is annealed after friction stir welding, prior to the spinning spin forming step.

7. The method as recited in claim 1, wherein the material pieces are friction stir welded in any heat treat condition to form a blank having a maximum size of available annealing ovens of said maximum size will accommodate a circular blank.

8. The method as recited in claim 7 wherein the blank is annealed after friction stir welding and prior to the spinning spin forming step.

9. The method as recited in claim 1 wherein the blank includes a joint, and the spin forming step is performed blank spun with the joint in the as-welded condition.

10. The method as recited in claim 1, wherein said at least two pieces comprise plates, and said blank has a diameter greater than 209 inches.

11. The method as recited in claim 1, wherein said at least two pieces comprise sheets, and said blank has a width greater then 139 inches.

12. An economical method of making spin blanks greater than a predetermined size, comprising:

providing at least two pieces of material having abutting edges;

annealing the at least two nieces of material;

friction stir welding the at least two pieces of annealed material together along the abutting edges to form a blank;

annealing the blank; and

spin forming the blank into a desired article.

13. The method as recited in claim 12, wherein the friction stir welding step is performed with the material in a fully heat treated condition.

14. The method as recited in claim 12, wherein the friction stir welding step is performed with the material in an as-rolled condition.