Self-forming thread blind fastener

Patent metadata

Field	Value
Publication number	US-2023250842-A1
Application number	US-202118004717-A
Country	US
Kind code	A1
Filing date	Jul 16, 2021
Priority date	Jul 24, 2020
Publication date	Aug 10, 2023
Grant date	—

Abstract

Self-forming thread blind fasteners and methods for fastening are provided. The self-forming thread blind fastener comprises a sleeve and a pin. The sleeve comprises a first sleeve end, a second sleeve end, an elongate portion, and an inner wall defining a bore. The pin is configured to be at least partially received by the bore. The pin comprises a first pin end, a second pin end, a pin head portion, an at least partially threaded portion, a shank intermediate, and a driving portion. The at least partially threaded portion is configured to form threads on at least a portion of the inner wall of the sleeve. The driving portion is configured to receive a torque to rotate the pin within the sleeve and thereby axially compress and deform the sleeve and form the threads on the at least a portion of the inner wall of the sleeve.

First claim

What is claimed is:

1 . A self-forming thread blind fastener comprising:
a sleeve comprising
a first sleeve end,
a second sleeve end,
an elongate portion extending from the first sleeve end to the second sleeve end, and
an inner wall extending longitudinally through the sleeve from the first sleeve end to the second sleeve end and the inner wall defining a bore; and
a pin configured to be at least partially received by the bore and comprising
a first pin end,
a second pin end,
a pin head portion adjacent to the second pin end and configured to inhibit traversal of the pin head portion into the bore,
an at least partially threaded portion, the at least partially threaded portion configured to form threads on at least a portion of the inner wall of the sleeve,
a shank intermediate the pin head portion and the at least partially threaded region, and
a driving portion adjacent to the first pin end, wherein the driving portion is configured to receive a torque to rotate the pin within the sleeve and thereby axially compress and deform the sleeve and form the threads on the at least a portion of the inner wall of the sleeve.

2 . The blind fastener of claim 1 , wherein the at least partially threaded portion is disposed in the bore.

3 . The blind fastener of claim 2 , wherein the inner wall comprises a narrowed region, wherein the at least partially threaded portion is configured to form threads on at least a portion of the narrowed region.

4 . The blind fastener of claim 3 , wherein the narrowed region comprises a first diameter less than a major diameter of the at least partially threaded portion.

5 . The blind fastener of claim 4 , wherein the inner wall comprises a second region configured to receive the at least partially threaded portion and wherein the second region is substantially tubular and comprises a second diameter greater than the major diameter of the at least partially thread portion.

6 . The blind fastener of claim 1 , wherein a diameter of the bore decreases along a length of the sleeve in an axial direction towards the first sleeve end.

7 . The blind fastener of claim 1 , wherein the sleeve further comprises a sleeve head portion adjacent to the first sleeve end, wherein the sleeve head portion is configured to inhibit the sleeve from passing into a bore in a structure beyond a predetermined distance.

8 . The blind fastener of claim 7 , wherein the sleeve head portion is configured to receive a torque.

9 . The blind fastener of claim 1 , wherein the elongate portion of the sleeve is configured to deform into a bulb shape responsive to the at least partially threaded region forming threads on the inner wall and compressing the elongate portion.

10 . The blind fastener of claim 1 , wherein the pin head portion is configured to compress the elongate portion responsive to the at least partially threaded region forming threads on the inner wall.

11 . The blind fastener of claim 1 , wherein the driving portion comprises at least one of a substantially flat side, a rib, a spline, an indent, a knurl, a lobe, a bore, a recessed socket, threads, and a tab.

12 . The blind fastener of claim 1 , wherein the pin comprises a first material with a first hardness, wherein the sleeve comprises a second material with a second hardness, and wherein the second hardness is less than the first hardness.

13 . The blind fastener of claim 1 , wherein the pin comprises a breakneck portion configured to fracture upon installation of the blind fastener.

14 . The blind fastener of claim 1 , wherein the driving portion is substantially cylindrical and does not comprise a breakneck portion.

15 . The blind fastener of claim 1 , further comprising a locking component attached to the sleeve head portion, the driving portion, or a combination thereof, wherein the locking component is configured to inhibit the sleeve head portion from rotating during installation of the fastener.

16 . The blind fastener of claim 15 , wherein the locking component comprises at least one of a substantially flat side, a rib, a spline, an indent, a knurl, a lobe, a bore, a recessed socket, and a tab.

17 . The blind fastener of claim 1 , wherein the blind fastener is configured to be installed in a bore in a structure configured as at least one of an aerospace part or component, an automotive part or component, a transportation part or component, and a building and construction part or component.

18 . A method for fastening, the method comprising:
inserting a second sleeve end of a sleeve of a self-forming thread blind fastener into a bore in a structure, the blind fastener comprising:
the sleeve comprising
a first sleeve end,
the second sleeve end,
an elongate portion extending from the first sleeve end to the second sleeve end, and
an inner wall extending longitudinally through the sleeve from the first sleeve end to the second sleeve end and the inner wall defining a bore; and

a pin configured to be at least partially received by the bore and comprising
a first pin end,
a second pin end,
a pin head portion adjacent to the second pin end and configured to inhibit the pin head portion from passing into the bore,
an at least partially threaded portion,
a shank intermediate the pin head portion and the at least partially threaded region, and
a driving portion adjacent to the first pin end;

forcibly contacting the at least partially threaded portion of the pin with the inner wall of the sleeve, thereby deforming the inner wall and forming threads thereon; and deforming the elongate portion of the sleeve to form a bulb thereon.

19 . The method of claim 18 , wherein forcibly contacting comprises rotating the pin and moving the pin head portion axially towards the first sleeve end.

20 . The method of claim 18 , wherein the pin further comprises a breakneck portion and the method further comprises rotating the pin until the pin fractures at the breakneck portion.

Assignees

• Howmet Aerospace Inc

Inventors

• Brennetot Thomas

Classifications

• F16B19/1072 Primary

  the pull-mandrel or the like comprising a thread and being rotated with respect to the rivet, thereby mechanically expanding and fastening the rivet (nuts fastened by riveting F16B37/067) · CPC title

• F16B19/1054 Primary

  the pull-mandrel or the like being frangible · CPC title