Method for removing a blind rivet in a workpiece arrangement

Patent metadata

Field	Value
Publication number	US-11801549-B2
Application number	US-202117526081-A
Country	US
Kind code	B2
Filing date	Nov 15, 2021
Priority date	May 15, 2019
Publication date	Oct 31, 2023
Grant date	Oct 31, 2023

Abstract

A method for removing a blind rivet includes a workpiece arrangement having first and second surfaces and a connecting hole. A blind rivet is fixed in the hole and has a shell and screw through the shell extending coaxially along a common center axis, the shell having a shell head portion, straight portion, deformation portion and threaded portion having an internal thread. The straight portion is in the hole and the deformation portion and the threaded portion protrude out of the hole, the screw having a screw head portion and pin portion having an external thread. The screw is in the shell such that the deformation portion of the shell is deformed where the outside diameter of the deformed deformation portion is larger than the diameter of the hole. The shell is cut in the region of the thread portion and/or the deformation portion, and the blind rivet is removed from the hole.

First claim

The invention claimed is:

1. A method for removing a blind rivet in a workpiece arrangement, comprising:
providing a workpiece arrangement having a first surface and an opposite second surface and having a hole, which connects the first surface to the second surface,
wherein a blind rivet is fixed in the hole, the blind rivet having a shell and a screw extending through the shell,
wherein the shell and the screw arranged therein extend coaxially along a common center axis between a first end on a same side as the first surface and a second end on a same side as the second surface of the workpiece arrangement,
wherein the shell has a shell head portion with a diameter which is greater than a diameter of the hole in the workpiece arrangement, a straight portion, an outside diameter of which is less than or equal to the diameter of the hole, a deformation portion and a threaded portion having an internal thread, wherein the straight portion is located in the hole and the deformation portion and the threaded portion protrude from the hole on the same side as the second surface,
wherein the screw has a screw head portion with a diameter which is greater than the diameter of the hole, and a stem portion, the diameter of which is less than or equal to the inside diameter of the shell, wherein, when viewed along the center axis, at least part of the stem portion has an external thread,
wherein the screw is in the shell such that the internal thread of the shell engages in an external thread of the screw and the deformation portion of the shell is deformed, wherein the outside diameter of the deformed deformation portion is greater than the diameter of the hole,

cutting the shell in the region of the threaded portion and or of the deformation portion; and
removing the blind rivet from the hole.

2. The method of claim 1 , wherein the shell is cut with a cut parallel to the center axis.

3. The method of claim 2 , wherein the cut extends at least along the threaded portion.

4. The method of claim 2 , wherein the cutting of the shell is performed with a cutting tool, wherein the cutting tool has a blade with a straight cutting edge which is moved toward the shell in a radial direction toward the center axis while aligned parallel to the center axis.

5. The method of claim 4 , wherein the cutting tool has a supporting body with an abutment surface and a bore starting from the abutment surface and with a guide slot extending radially outward from the bore, wherein the blade is in the guide slot and movable in a guided manner such that the cutting edge extends parallel to the central axis of the bore and can be moved into the bore and toward the central axis.

6. The method of claim 5 , wherein, for cutting the shell, the cutting tool is arranged such that the abutment surface rests against the second surface of the workpiece arrangement, and the blind rivet protrudes from the hole at the second surface extends into the bore, after which the blade is moved toward the shell in a direction of the center axis in the guide slot until the cutting edge cuts the shell.

7. The method of claim 5 , wherein one or more further cutting edges are provided on the inner wall of the bore at a distance from the guide slot in a circumferential direction, the cutting edges extending parallel to the central axis and against which the threaded portion rests when the latter is located in the bore.

8. The method of claim 1 , wherein, after the cutting of the shell, the screw is removed in a direction of the first surface.

9. The method of claim 8 , wherein the removal of the screw is effected by striking a second end of the screw.

10. The method of claim 8 , wherein, after the removal of the screw, the shell head portion is drilled out from the same side as the first surface and then removed.

11. The method of claim 10 , wherein, after the removal of the shell head portion, remaining parts of the shell are removed on the same side as the second surface.

12. The method of claim 1 , wherein the shell is cut with a cut transverse to the center axis.

13. The method of claim 12 , wherein the shell is cut at a transition between the deformation portion and the straight portion.

14. The method of claim 12 , wherein the shell is cut along an extension of the second surface.

15. The method of claim 12 , wherein, during the cutting of the shell, several cuts are made from different sides of the shell.

16. The method of claim 12 , wherein the cutting of the shell is performed with a cutting tool, wherein the cutting tool has a blade with a cutting edge which is moved toward the shell in a radial direction toward the center axis while aligned perpendicularly to the center axis.

17. The method of claim 16 , wherein the cutting edge is moved between the second surface and the deformation portion in order to cut the shell.

18. The method of claim 16 , wherein several cuts are carried out in order to cut the shell, wherein the cutting tool is rotated about the center axis relative to the shell between the cuts, ensuring that the cuts are made at different angles.

19. The method of claim 16 , wherein, in order to cut the shell, the cutting edge is first moved toward the shell in the radial direction toward the center axis, and then the cutting tool is rotated about the center axis, wherein the cutting edge cuts the shell continuously in a circumferential direction.

20. The method of claim 16 , wherein the blade is concavely curved relative to the shell.

21. The method of claim 20 , wherein the cutting edge has a radius of curvature greater than or equal to the internal radius of the shell.

22. The method of claim 16 , wherein the cutting tool has two blades with opposite cutting edges, which are moved toward the shell from opposite sides in order to cut the shell.

23. The method of claim 22 , wherein the cutting tool has a supporting body with an abutment surface and an opening starting from the abutment surface and having a central axis perpendicular to the abutment surface, wherein the two blades with opposite cutting edges are in the opening and movable in a guided manner such that the cutting edges extend perpendicularly to the central axis and can be moved toward the central axis in the radial direction from opposite sides.

24. The method of claim 23 , wherein, for cutting the shell, the cutting tool is arranged on the workpiece arrangement such that the abutment surface rests against the second surface, and the blind rivet extends into the opening, wherein the center axis runs coaxially with the central axis, after which the blades are moved toward the shell from opposite sides and cut the latter.

25. The method of claim 12 , wherein, after the cutting of the shell, the threaded portion and the deformation portion are unscrewed from the external thread of the screw and removed on the same side as the second surface.

26. The method of claim 25 , wherein, after the removal of the threaded portion and of the deformation portion, the screw is removed in a direction of the first surface.

27. The method of claim 26 , wherein, after the removal of the screw or at a same time as the removal of the screw, the straight portion of the shell and the shell head portion are removed in the direction of the first surface.

28. The method of claim 12 , wherein, with the cutting of the shell, the screw extending in the shell is c

Assignees

• Airbus Operations Gmbh

Inventors

• Skirke Jörn
• Schäfer Alexander

Classifications

• B21J15/50 Primary

  Removing or cutting devices for rivets · CPC title

• B25B27/18

  withdrawing broken threaded parts or twist drills · CPC title