IP Library › Granted Patent US 11,885,358
Granted Patent B2
US 11,885,358 · App. 17/423,980 · Granted Jan 30, 2024

Blind fastener and method of installation thereof

Inventors: Robert B. Wilcox (McGregor, TX); James Thomas Smith (Crawford, TX); Troy Don Pierce (Hewitt, TX)
Assignee: HOWMET AEROSPACE INC.
F16B19/1054F16B19/10
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Quick Facts
Patent No.
US 11,885,358
App. No.
17/423,980
Granted
Jan 30, 2024
Kind
B2
Abstract

The present disclosure relates to a blind fastener and a method of installation thereof. The blind fastener comprises a sleeve and a mandrel. The sleeve comprises a first sleeve end, a second sleeve end, and a cavity extending from the first sleeve end to the second sleeve end. The mandrel is configured to be at least partially received by the cavity of the sleeve. The mandrel comprises a first mandrel end disposed adjacent to the first sleeve end and comprising an enlarged portion having a diameter greater than a diameter of the cavity, a second mandrel end comprising a pull region, and a shank region extending intermediate the first mandrel end and the second mandrel end. The pull region comprises an axial length no greater than four times a diameter of the shank region and is configured to be engaged by an installation tool.

Claims (42)

1. A blind fastener comprising:

a sleeve comprising

a first sleeve end,

a second sleeve end,

a cavity extending from the first sleeve end to the second sleeve end; and

a mandrel configured to be at least partially received by the cavity of the sleeve, the mandrel comprising

a first mandrel end disposed adjacent to the first sleeve end and comprising an enlarged portion having a diameter greater than a diameter of the cavity,

a second mandrel end comprising a pull region, and

a shank region extending intermediate the first mandrel end and the second mandrel end,

wherein the pull region comprises an axial length no greater than 4 times a diameter of the shank region and is configured to be engaged by an installation tool.

2. The blind fastener of claim 1 , wherein the pull region comprises an axial length no greater than 3.8 times the diameter of the shank region.

3. The blind fastener of claim 1 , wherein the pull region comprises an axial length no greater than 2 times the diameter of the shank region.

4. The blind fastener of claim 1 , wherein the pull region comprises a taper extending from the shank region.

5. The blind fastener of claim 1 , wherein the mandrel does not comprise a breakneck groove.

6. The blind fastener of claim 1 , wherein the mandrel comprises a Rockwell hardness of at least HRC 25.

7. The blind fastener of claim 1 , wherein the mandrel comprises a Rockwell hardness of at least HRC 43.

8. The blind fastener of claim 1 , wherein the shank region comprises at least one of, a threaded region, an annular shoulder, and a groove.

9. The blind fastener of claim 1 , wherein the pull region comprises at least one of a threaded region, an annular shoulder, and a groove.

10. The blind fastener of claim 1 , wherein the sleeve is generally cylindrical and the mandrel is generally cylindrical.

11. The blind fastener of claim 1 , wherein the blind fastener comprises at least one of a metal, metal alloy, and a composite material.

12. The blind fastener of claim 1 , wherein the blind fastener is adapted to be installed in a bore in a structure, the bore having a diameter greater than the diameter of the enlarged portion.

13. The blind fastener of claim 12 , wherein the sleeve further comprises a collar, the sleeve is configured to deform on a first side of the structure, and the collar is configured to swage onto the shank region on an oppositely disposed second side of the structure.

14. The blind fastener of claim 12 , wherein the structure comprises at least one of a metal, a metal alloy, and a composite material.

15. The blind fastener of claim 12 , wherein the structure is configured as at least one of an aerospace component, an automotive component, a transportation component, and a building and construction component.

16. A method for fastening, the method comprising:

inserting a first mandrel end of a blind fastener into a bore in a structure, the blind fastener comprising

a sleeve comprising

a first sleeve end,

a second sleeve end, and

a cavity extending from the first sleeve end to the second sleeve end, and

a mandrel configured to be at least partially received by the cavity of the sleeve, the mandrel comprising

a first mandrel end disposed adjacent to the first sleeve end and comprising an enlarged portion having a diameter greater than a diameter of the cavity,

a second mandrel end comprising a pull region, and

a shank region extending intermediate the first mandrel end and the second mandrel end,

wherein the pull region comprises an axial length no greater than 4 times a diameter of the shank region and is configured to be engaged by an installation tool;

engaging a collet of the installation tool with the pull region of the blind fastener;

after the inserting, forcibly contacting the second sleeve end of the blind fastener with an anvil of the installation tool and moving the pull region distal from the second sleeve end utilizing the collet of the installation tool; and

deforming the sleeve on a first side of the structure, and swaging the second sleeve end onto the shank region on an oppositely disposed second side of the structure, thereby securing at least a portion of the blind fastener in the structure.

17. The method of claim 16 , wherein the pull region comprises an axial length no greater than 3.8 times the diameter of the shank region.

18. The method of claim 16 , wherein the pull region comprises a taper or reverse taper extending from the shank region.

19. The method of claim 16 , wherein the mandrel does not comprise a breakneck groove.

20. The method of claim 16 , wherein the blind fastener comprises at least one of a metal, a metal alloy, and a composite material.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 20, 2021
From: WILCOX, ROBERT B.; SMITH, JAMES THOMAS; PIERCE, TROY DON
To: ARCONIC INC.
Reel/Frame 056911/0859 →
CHANGE OF NAME Recorded Jul 20, 2021
From: ARCONIC INC.
To: HOWMET AEROSPACE INC.
Reel/Frame 056912/0146 →
Continuity (1)
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