Methods of manufacture of spin-forming blanks, particularly for fabrication of rocket domes

• US 6,660,106 B1
• Filed: 08/22/2001
• Issued: 12/09/2003
• Est. Priority Date: 08/22/2001
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Bozich, William F., Babel, Henry W., de Jesus, Ronaldo Reyes, Waldron, Douglas J.
• Primary Examiner(s): WYSZOMIERSKI, GEORGE P
• Application Number:
  US09/935,271
• Time in Patent Office: 839 Days
• Field of Search: 294/28, 148/527, 148/535, 228/112.1, 228/114
• US Class Current: 148/527
• 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

Large diameter dome tanks made of a plurality of plates friction stir welded together to form a blank and spun and/or stretched into form. The dome tanks may be for holding liquid rocket fuel. Methods of forming include friction stir welding two or more flat blanks together and spinning the combined workpiece into a hemisphere. The blanks may be sufficiently thick to enable stretching as well as spinning. Aluminum alloys may be used, and filler material may be included in thee friction stir welds to reduce grain growth and problems associated therewith in the spinning process.

Claims

1. A method of spin-forming a dome shaped article, comprising:

providing at least two substantially planar pieces of material having abutting edges;

friction stir welding said material pieces together along said abutting edges to form a blank suitable for spin-forming; and

spin-forming the blank into a desired article.

2. The method as recited in claim 1, wherein said article comprises a dome for an aerospace application.

3. The method as recited in claim 1, wherein said article comprises a dome for a rocket.

4. The method as recited in claim 1, wherein there are four of said substantially planar pieces of material which are friction stir welded together to form said blank.

5. The method as recited in claim 1, wherein said two material pieces are rectilinear, and said method further comprises cutting said blank into a circular shape prior to performing said spin-forming step.

6. The method as recited in claim 1, wherein said material comprises an aluminum alloy.

7. The method as recited in claim 1, and further comprising stretching the blank during the spin-forming step.

8. The method as recited in claim 1, and further comprising heating the blank during the spin-forming step.

9. The method as recited in claim 1, and further comprising annealing the blank prior to the spin-forming step.

10. The method as recited in claim 9, and further comprising solution heat treating the article.

11. A method of fabricating hemispheric domes, comprising:

providing at least two portions of material having abutting edges;

friction stir welding the two material portions together along the abutting edges to form a blank; and

spin-forming said blank into a dome.

12. The method as recited in claim 11, wherein said two material portions are rectilinear, and said method further comprises cutting said blank into a circular shape prior to performing said spin-forming step.

13. The method as recited in claim 11, wherein said material comprises an aluminum alloy.

14. The method as recited in claim 11, and further comprising stretching the blank during the spin-forming step.

15. The method as recited in claim 11, and further comprising heating the blank during the spin-forming step.

16. The method as recited in claim 11, and farther comprising annealing the blank prior to the spin-forming step.

17. The method as recited in claim 16, and further comprising solution heat treating the dome.