IP Library › Granted Patent US 9,593,706
Granted Patent B2
US 9,593,706 · App. 13/674,055 · Granted Mar 14, 2017

Structural blind fastener and method of installation

Inventors: Jeffry G. Bickford (Federal Way, WA); Mark A. Woods (Renton, WA); Peter A. Coronado (Renton, WA); Richard Whitlock (Seattle, WA)
Assignee: The Boeing Company
F16B31/06B21J15/043B21J15/12B25B31/00F16B19/1054F16B19/1072Y10T29/49948
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Quick Facts
Patent No.
US 9,593,706
App. No.
13/674,055
Granted
Mar 14, 2017
Kind
B2
Abstract

A two-piece, one-sided-installation fastener system may have an internally-threaded sleeve having a shank and a sleeve head. The fastener system may include an externally-threaded core bolt having a frangible driving provision and a core bolt head.

Claims (22)

1. A two-piece, one-sided-installation fastener system in combination with an installation tool, comprising:

an internally-threaded sleeve having a shank and a sleeve head, the shank including a localized annealed portion extending along a portion of a sleeve length and adapted to buckle against a structure into a buckled sleeve portion;

an externally-threaded core bolt having a frangible driving provision and a core bolt head, the frangible driving provision including external annular grooves and a pair of exterior diametrical flats; and

an installation tool including a housing having a segmented collet axially slidable within the housing and configured to radially expand during axial movement over the frangible driving provision, the segmented collet having interior annular grooves engageable to the external annular grooves of the frangible driving provision after the segmented collet is axially moved over the frangible driving provision, the segmented collet configured to axially translate the core bolt relative to the sleeve independent of rotation of the core bolt to form the buckled sleeve portion, the collet including a pair of interior diametrical flats configured to engage the pair of exterior diametrical flats of the frangible driving provision and rotate the core bolt relative to the sleeve to increase a tension preload on the core bolt.

2. The system of claim 1 , wherein the buckled sleeve portion has a minimum diameter of approximately 1.2 times the sleeve outside diameter when the buckled sleeve portion is buckled against the structure.

3. The system of claim 1 , wherein the sleeve includes a locking feature restricting rotation of the core bolt relative to the sleeve.

4. The system of claim 1 , wherein the sleeve head includes an anti-rotation feature.

5. The system of claim 4 , wherein the anti-rotation feature comprises at least one of an indentation and a protrusion on the sleeve head.

6. The system of claim 4 , wherein:

the installation tool includes a sleeve engagement feature configured to engage the anti-rotation feature for preventing rotation of the sleeve relative to a hole when rotating the core bolt relative to the sleeve.

7. The system of claim 1 , wherein the frangible driving provision comprises a frangible pintail having a break groove at an interface between the frangible pintail and the core bolt head.

8. The system of claim 1 , wherein:

the installation tool includes an ejection spring configured to eject the frangible driving provision from the installation tool after the frangible driving provision fractures off of the core bolt head.

9. The system of claim 1 , wherein:

the annular grooves have ramped surfaces allowing the collet to slidably release the frangible driving provision after fracturing off of the core bolt head.

10. The system of claim 1 , wherein the core bolt and/or the sleeve are formed of at least one of:

titanium, steel, stainless steel, inconel, nickel, and cobalt.

11. A two-piece, one-sided-installation fastener system in combination with an installation tool, comprising:

an internally-threaded sleeve having a shank and a sleeve head, the shank including a localized annealed portion extending along a portion of a sleeve length and adapted to buckle against a structure into a buckled sleeve portion;

an externally-threaded core bolt having a frangible driving provision and a core bolt head, the frangible driving provision including external annular grooves and a pair of exterior diametrical flats;

an installation tool including a housing having a taper on a housing interior and having a segmented collet axially slidable within the housing and configured to radially expand during axial movement over the external annular grooves for engagement with interior annular grooves of the segmented collet, the segmented collet configured to axially translate the core bolt relative to the sleeve independent of rotation of the core bolt to form the buckled sleeve portion, the collet including a pair of interior diametrical flats configured to engage the pair of exterior diametrical flats and rotate the core bolt relative to the sleeve to increase a tension preload on the core bolt; and

an outer surface of the collet configured to bear against the taper and increase a clamping force of the collet on the frangible driving provision as the collet and core bolt are axially moved relative to the housing during forming of the buckled sleeve portion.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 11, 2012
From: BICKFORD, JEFFRY G.; WOODS, MARK A.; CORONADO, PETER A.; WHITLOCK, RICHARD
To: THE BOEING COMPANY
Reel/Frame 029276/0947 →
Continuity (1)
Related Publication 20140130335A1 · May 15, 2014