IP Library › Granted Patent US 10,232,428
Granted Patent B2
US 10,232,428 · App. 15/914,155 · Granted Mar 19, 2019

Blind track bolt with higher clamp-up strength

Inventors: Scott William Gunther (Seattle, IL); Edward John Batt (Bothell, IL); Farahnaz Sisco (Mukilteo, IL)
Assignee: THE BOEING COMPANY
B21J15/043B23P25/00F16B19/1054Y10T29/49799
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Quick Facts
Patent No.
US 10,232,428
App. No.
15/914,155
Granted
Mar 19, 2019
Kind
B2
Abstract

A blind tack fastener includes a pull stem having an elongated shaft with an extended tail portion. The blind tack fastener also includes a crush-initiating washer, a crush sleeve, and a swage collar, surrounding the elongated shaft of the pull stem. The elongated shaft has a breakaway groove configured to create a predictive fracture point below the head-end surface of the swage collar, such that a hole in the swage collar serves as a centering lead-in for a drill that can be used to remove the blind tack fastener.

Claims (34)

1. A method of processing a workpiece, the method comprising:

inserting a pull stem and a crush sleeve of a blind tack fastener through a hole in the workpiece such that a swage collar of the blind tack fastener is located on a first side of the workpiece and a crush-initiating washer of the blind tack fastener is located on a second side of the workpiece;

pulling the pull stem of the blind tack fastener to form a bulb in the crush sleeve of the blind tack fastener, thereby compressing the workpiece between the swage collar and the bulb in the crush sleeve;

swaging the swage collar onto lock grooves located in an outer surface of the pull stem; and

breaking the pull stem below a head-end surface of the swage collar.

2. The method of claim 1 , further comprising:

performing one or more manufacturing operations on the workpiece; and

removing the blind tack fastener by drilling the pull stem through a hole in the head-end surface of the swage collar.

3. The method of claim 1 , further comprising centering a drill bit over the pull stem in the hole in the head-end surface of the swage collar prior to drilling the pull stem.

4. The method of claim 1 , wherein formation of the bulb is facilitated by an inward taper on a head-end surface of the crush-initiating washer and a taper on a tail-end surface of the crush sleeve.

5. The method of claim 1 , wherein the pull stem comprises aluminum or an aluminum alloy having a yield strength greater than 60 ksi and a machinability rating greater than 40%.

6. The method of claim 1 , wherein the crush-initiating washer comprises high-alloy steel having a yield strength greater than 150 ksi.

7. The method of claim 1 , wherein the crush sleeve comprises aluminum, copper or an alloy having a yield strength less than 20 ksi and a ductility greater than 15%.

8. The method of claim 1 , wherein the swage collar comprises aluminum or an aluminum alloy having a yield strength less than 20 ksi.

9. A method of processing a workpiece, the method comprising:

inserting a pull stem and a crush sleeve of a blind tack fastener through a hole in the workpiece such that a swage collar of the blind tack fastener is located on a first side of the workpiece and a crush-initiating washer of the blind tack fastener is located on a second side of the workpiece;

pulling the pull stem of the blind tack fastener to form a bulb in the crush sleeve of the blind tack fastener, thereby compressing the workpiece between the swage collar and the bulb in the crush sleeve; and

breaking the pull stem below a head-end surface of the swage collar, wherein breaking the pull stem below the head-end surface of the swage collar comprises breaking the pull stem at a breakaway groove located within an inner bore of the swage collar.

10. The method of claim 9 , further comprising swaging the swage collar onto lock grooves located in an outer surface of the pull stem.

11. The method of claim 9 , wherein formation of the bulb is facilitated by an inward taper on a head-end surface of the crush-initiating washer and a taper on the tail-end surface of the crush sleeve.

12. A method of processing a workpiece comprising a plurality of parts with a hole extending through the workpiece, the method comprising:

inserting a pull stem and a crush sleeve of a blind tack fastener through the hole in the workpiece such that a swage collar of the blind tack fastener is located on a first side of the workpiece and a crush-initiating washer of the blind tack fastener is located on a second side of the workpiece;

pulling the pull stem of the blind tack fastener to form a bulb in the crush sleeve of the blind tack fastener, thereby compressing the parts of the workpiece between the swage collar and the bulb in the crush sleeve;

breaking the pull stem below a head-end surface of the swage collar at a breakaway groove located within an inner bore of the swage collar;

performing one or more manufacturing operations on the workpiece; and

removing the blind tack fastener by drilling the pull stem through a hole in the head-end surface of the swage collar.

13. The method of claim 12 , further comprising swaging the swage collar onto lock grooves located in an outer surface of the pull stem.

14. The method of claim 12 , further comprising centering a drill bit over the pull stem in the hole in the head-end surface of the swage collar prior to drilling the pull stem.

15. The method of claim 12 , wherein formation of the bulb is facilitated by an inward taper on a head-end surface of the crush-initiating washer and a taper on a tail-end surface of the crush sleeve.

16. The method of claim 12 , wherein the workpiece comprises more than two parts.

17. The method of claim 12 , wherein the pull stem comprises aluminum or an aluminum alloy having a yield strength greater than 60 ksi and a machinability rating greater than 40%.

18. The method of claim 12 , wherein the crush-initiating washer comprises high-alloy steel having a yield strength greater than 150 ksi.

19. The method of claim 12 , wherein the crush sleeve comprises aluminum, copper or an alloy having a yield strength less than 20 ksi and a ductility greater than 15%.

20. The method of claim 12 , wherein the swage collar comprises aluminum or an aluminum alloy having a yield strength less than 20 ksi.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 7, 2018
From: GUNTHER, SCOTT W.; BATT, EDWARD J.; SISCO, FARAHNAZ
To: THE BOEING COMPANY
Reel/Frame 045130/0964 →
Continuity (3)
Division 14672794 · Mar 30, 2015
Provisional Application 61973360 · Apr 1, 2014
Related Publication 20180193900A1 · Jul 12, 2018