IP Library › Granted Patent US 8,142,126
Granted Patent B2
US 8,142,126 · App. 12/359,961 · Granted Mar 27, 2012

Multi-piece fastener with self-indexing nut

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 8,142,126
App. No.
12/359,961
Granted
Mar 27, 2012
Kind
B2
Abstract

According to a preferred embodiment, a multi-piece fastener with self-indexing nut is disclosed. The multi-piece fastener is designed for use in low clearance areas such as aircraft wing side-of-body joint locations. The multi-piece fastener comprises a stud comprising an elongated part extending between a first end face and a second end face, a threaded head fastener, a threaded tail fastener, and a wrenching feature. A self-indexing feature is provided on the stud and head fastener which allows automatic orientation of the head fastener with respect to the stud.

Claims (18)

1. A cylindrical bolt assembly comprising:

an elongated stud having a first end face, a second end face, a first threaded area spaced from said first end face and extending to an unthreaded central area, a second threaded area spaced from said second end face and extending to said unthreaded central area, and an unthreaded stop projection area extending between said second threaded area and said second end face, said unthreaded stop projection area having a stop projection;

a threaded head fastener comprising a first end and a second end and a generally cylindrical fastener body extending between said first end and said second end, said fastener body comprising an internal section of threads extending from said first end for mating with said second threaded area of said stud, and a stop indentation for receiving said stop projection;

a threaded tail fastener comprising a first end, a second end, a generally cylindrical fastener body extending between said first end and said second end, said fastener body having an internal section of threads extending from said first end, for mating with said first threaded area of said stud; and

a wrenching feature adjacent to and affixed to the first end of said stud, said wrenching feature allowing said cylindrical stud to be restrained at said threaded tail section while torque is applied to said threaded tail fastener.

2. The cylindrical bolt assembly of claim 1 , wherein:

said stop projection is movable between a depressed position and a raised position; and

said stop projection has a sloping surface permitting said threaded head fastener to move said stop projection to said depressed position while said threaded head fastener is being fastened onto said stud.

3. The cylindrical bolt assembly of claim 1 , wherein said stop projection comprises:

a ball-bearing set sufficiently deeply into the stud such that passage of the threaded head fastener over the ball-bearing is substantially hindered and such that the ball-bearing can fit into the stop indentation of the threaded head fastener.

4. The cylindrical bolt assembly of claim 1 , wherein said stop projection has a circular cross-section.

5. The cylindrical bolt assembly of claim 1 , wherein said stop projection has a rectangular cross-section.

6. The cylindrical bolt assembly of claim 1 , wherein the threaded head fastener comprises:

a circular base section with a first diameter;

a hexagonal section adjacent to said circular base section, and having a second diameter smaller than said first diameter; and

a circular stop feature section adjacent to said hexagonal section, and having a third diameter smaller than said second diameter, wherein said stop indentation is located on the stop feature section.

7. A cylindrical bolt assembly as in claim 1 , wherein said stop indentation comprises:

a notch shaped to correspond to the stop protrusion such that when the stop protrusion is caught in the notch, rotation of the threaded head fastener with respect to the stud is prevented.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2009
From: RUFIN, ANTONIO; PORTER, JOHN R.
To: THE BOEING COMPANY
Reel/Frame 022180/0073 →
Continuity (2)
Continuation In Part 11162260 · Sep 2, 2005
Related Publication 20090136294A1 · May 28, 2009