Repair pin-stud for repairing honeycomb pearls

Patent metadata

Field	Value
Publication number	US-10384287-B2
Application number	US-201715428116-A
Country	US
Kind code	B2
Filing date	Feb 8, 2017
Priority date	Mar 11, 2013
Publication date	Aug 20, 2019
Grant date	Aug 20, 2019

Abstract

A repair pin-stud used in processes for repairing panels, such as honeycomb panels. The repair pin-stud includes a cylindrical stud member, a tip on a first end of the cylindrical stud member, and an elongated installation member connected to a second end of the cylindrical stud member. The repair pin-stud further includes a tubular pin concentric with the cylindrical stud member. A first end of the tubular pin is connected to the cylindrical stud member, and a second end of the tubular pin is open and the elongated installation member extends outwardly from the second end of the tubular pin.

First claim

The invention claimed is:

1. A method of repairing damage to a panel having a core sandwiched between an inner face sheet and an outer face sheet, the method comprising:
drilling a hole through the inner face sheet of the panel;
inserting a sleeve into the hole;
inserting a repair pin-stud into the hole wherein the repair pin-stud includes a tip on a first end, and an installation member that extends from a second end that is open;
percussion welding the tip end of the repair pin-stud to an inner surface of the outer face sheet with a stud welder that grips the installation member of the repair pin-stud;
twisting off the installation member of the repair pin-stud;
fusion welding the second end of the repair pin-stud to the inner face sheet; and
welding the second end of the repair pin-stud closed using a weld filler wire.

2. The method of claim 1 further comprising:
retaining the repair pin-stud in the inner face sheet by expanding the second end of the repair pin-stud before fusion welding the repair pin-stud to the inner face sheet.

3. The method of claim 1 further comprising:
grinding the welds on the inner face sheet to be flush with the inner face sheet.

4. The method of claim 1 wherein the damage comprises a dent in the outer face sheet, the method further comprising:
straightening the dent in the outer face sheet before inserting the repair pin-stud into the hole.

5. The method of claim 4 wherein straightening the dent in the outer face sheet comprises:
inserting a solid rod into the hole; and
pressing the solid rod against the dent to return a contour of the outer face sheet to a blueprint contour.

6. The method of claim 5 wherein straightening the dent in the outer face sheet comprises:
placing a phenolic block on an outer surface of the outer face sheet when pressing the solid rod against the dent.

7. The method of claim 1 further comprising:
cutting a section from the inner face sheet;
preparing a patch for the inner face sheet; and
welding the patch to the inner face sheet.

8. The method of claim 1 further comprising:
inserting the installation member of the repair pin-stud in the stud welder.

9. A method of repairing a panel having a core sandwiched between an inner face sheet and an outer face sheet, the method comprising:
drilling a hole through the inner face sheet of the panel;
installing a repair pin-stud in a stud welder, wherein the repair pin-stud includes a cylindrical stud member having a tip at a first end and an elongated installation member at a second end, and includes a tubular pin concentric with the cylindrical stud member and having a larger diameter than the cylindrical stud member;
wherein one end of the tubular pin connects to the cylindrical stud member, and the tubular pin extends in a direction of the elongated installation member to an opposing open end;
wherein the elongated installation member is gripped by the stud welder;
inserting the repair pin-stud into the hole;
welding the repair pin-stud to the outer face sheet with the stud welder by welding the first end of the cylindrical stud member having the tip to an inner surface of the outer face sheet;
twisting off the elongated installation member of the repair pin-stud after welding the first end of the cylindrical stud member to the inner surface of the outer face sheet; and
welding the repair pin-stud to the inner face sheet by welding around a circumference of the open end of the tubular pin.

10. The method of claim 9 further comprising:
welding the open end of the tubular pin closed.

11. The method of claim 10 further comprising:
grinding welds down to be flush with a surface of the inner face sheet.

12. The method of claim 9 wherein when the open end of the tubular pin protrudes from the hole in the inner face sheet after welding the first end of the cylindrical stud member to the inner surface of the outer face sheet, the method further comprises:
retaining the repair pin-stud in the inner face sheet by expanding the open end of the tubular pin.

13. A method of repairing a honeycomb panel having a honeycomb core sandwiched between an inner face sheet and an outer face sheet, the method comprising:
drilling a hole through the inner face sheet and stopping short of the outer face sheet, wherein a diameter of the hole is larger than a diameter of a repair pin-stud used to repair the honeycomb panel;
wherein the repair pin-stud includes a cylindrical stud member having a tip at a first end and an elongated installation member at a second end, and includes a tubular pin concentric with the cylindrical stud member and having a larger diameter than the cylindrical stud member;
wherein one end of the tubular pin connects to the cylindrical stud member, and the tubular pin extends in a direction of the elongated installation member to an opposing open end;
installing the elongated installation member of the repair pin-stud in a stud welder;
inserting an insulation sleeve into the hole;
inserting the repair pin-stud into the hole where the insulation sleeve was already inserted;
welding the repair pin-stud to the outer face sheet with the stud welder by welding the first end of the cylindrical stud member having the tip to an inner surface of the outer face sheet;
twisting off the elongated installation member of the repair pin-stud after welding the first end of the cylindrical stud member to the inner surface of the outer face sheet;
and
welding the repair pin-stud to the inner face sheet by welding around a circumference of the open end of the tubular pin.

14. The method of claim 13 further comprising:
welding the open end of the tubular pin closed using a weld filler wire.

15. The method of claim 14 further comprising:
grinding welds down to be flush with a surface of the inner face sheet.

16. The method of claim 13 wherein when the open end of the tubular pin protrudes from the hole in the inner face sheet after welding the first end of the cylindrical stud member to the inner surface of the outer face sheet, the method further comprises:
retaining the repair pin-stud in the inner face sheet by expanding the open end of the tubular pin.

17. The method of claim 13 wherein to repair a dent in the outer face sheet, the step of drilling the hole through the inner face sheet comprises:
drilling the hole through the inner face sheet opposite the dent in the outer face sheet.

18. The method of claim 17 further comprising:
inserting a rod into the hole in the inner face sheet;
placing a block on an outer surface of the outer face sheet;
pressing the rod against the dent to straighten the dent; and
removing the rod from the hole.

19. The method of claim 13 wherein to repair a damaged section of the inner face sheet, the method further includes:
cutting the damaged section from the inner face sheet without damaging the honeycomb core; and
installing a patch in place of the damaged section by welding the patch to the inner face sheet;
wherein drilling the hole through the inner face sheet comprises drilling the hole through the patch in the inner face sheet.

Assignees

• Boeing Co

Inventors

• Yu Howe Hao

Classifications

• B23K9/20

  Stud welding · CPC title

• B23P6/00

  Restoring or reconditioning objects (straightening or restoring form of sheet metal, metal rods, metal tubes, metal profiles, or specific articles made therefrom B21D1/00, B21D3/00; repairing defective or damaged objects by casting techniques B22D19/10) · CPC title

• B23K2101/02

  Honeycomb structures · CPC title

• B23K9/0026 Primary

  specially adapted for particular articles or work · CPC title

• B23P2700/01

  Aircraft parts · CPC title