IP Library Patent Application 18356719
Patent Application
App. No. 18/356,719

INDEXING BOLT FOR JOINING COMPOSITE FORM PIECES TOGETHER

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Quick Facts
Patent No.
US None
App. No.
18/356,719
Abstract

A connection between form assemblies of a form for a composite part is disclosed. The connection includes an indexing bolt for connecting first and second form assemblies of a form for a composite part to one another. The indexing bolt includes a head and a shank extending from the head. The shank has a first barrel portion, a second barrel portion spaced apart from the first barrel portion, and an indexing section extending between the first barrel portion and the second barrel portion. The indexing section includes a tapered portion that is receivable within the tapered opening of the alignment plate of the second form assembly. The first barrel portion has a first diameter and the second barrel portion has a second diameter. The first diameter is different than the second diameter. The first and second barrel assemblies each include external threading.

Claims (28)

1 . An indexing bolt for connecting first and second form assemblies of a form for a composite part to one another, the second form assembly including an alignment plate having a tapered opening, the bolt comprising:

a head; and

a shank attached to the head and extending therefrom, the shank having a first barrel portion, a second barrel portion spaced apart from the first barrel portion, and an indexing section extending between the first barrel portion and the second barrel portion, the indexing section including a tapered portion that is receivable within the tapered opening of the alignment plate of the second form assembly, the first barrel portion having a first diameter and the second barrel portion having a second diameter, the first diameter being different than the second diameter, and the first and second barrel portions each including external threading.

2 . The indexing bolt of claim 1 , wherein the second diameter is less than the first diameter.

3 . The indexing bolt of claim 1 , wherein the indexing section includes a cylindrical portion attached to the tapered portion, the cylindrical portion being disposed between the first barrel portion and the tapered portion.

4 . The indexing bolt of claim 3 , wherein the cylindrical portion is free of threading.

5 . The indexing bolt of claim 3 , wherein the cylindrical portion has a third diameter, the third diameter being different than the first and second diameters.

6 . The indexing bolt of claim 1 , wherein the shank is a single, unitary piece of material.

7 . The indexing bolt of claim 1 , wherein the shank includes a recess formed therein, the recess is arranged to enable the shank to be broken in response to the application of a shearing torque on the shank.

8 . The indexing bolt of claim 7 , wherein the recess is disposed at an intersection of the tapered portion and the second barrel portion.

9 . The indexing bolt of claim 1 , in combination with a retainer threadably coupled to the first barrel portion.

10 . An indexing bolt assembly for connecting first and second form assemblies of a form for a composite part to one another, the bolt assembly comprising:

a shank having a first barrel portion, a second barrel portion, and an indexing section between the first barrel portion and the second barrel portion, the second barrel portion configured to be fastened to the second form portion, the indexing section being non-threaded and configured to seat within an indexing opening of the second form assembly for indexing the second form assemblies in relation to the first form assembly; and

an adjustable retainer movably connected to the first barrel portion of the shank, the adjustable retainer having an engagement surface spaced apart from the indexing section by an adjustable length, the adjustable retainer being movable for adjusting the adjustable length, wherein the adjustable retainer is configured to clamp the first and second form assemblies together by moving the adjustable retainer so that the adjustable length corresponds to a fixed critical length between an outer surface of the first form assembly and the indexing opening of the second form assembly whereby the adjustable retainer can be field-adjusted to accommodate variance in the fixed critical length.

11 . The indexing bolt assembly of claim 10 , wherein the adjustable length is the distance between the engagement surface and a proximal end of the tapered portion, the tapered portion including a distal end opposite the proximal end, the proximal end of the tapered portion being closer to the first barrel portion than the distal end of the tapered portion.

12 . The indexing bolt assembly of claim 10 , wherein the adjustable retainer is configured to be adjustable along the first barrel portion through a range of motion that extends from a first clamping position to a second clamping position, wherein the adjustable retainer defines a maximum adjustable length in the second clamping position and a minimum adjustable length in the first clamping position, and wherein a difference between the maximum adjustable length and the minimum adjustable length is in an inclusive range of from 0.1 inches to 2.0 inches.

13 . The indexing bolt assembly of claim 10 , wherein the adjustable retainer comprises a flange nut.

14 . The indexing bolt assembly of claim 10 , wherein the adjustable retainer is threadably coupled to the first barrel portion.

15 . A form for a composite part, the form comprising:

a first form assembly having a first form surface arranged to engage composite materials forming the composite part, the first form assembly including a first alignment plate having a first opening;

a second form assembly having a second form surface arranged to engage the composite materials forming the composite part, the second form assembly including a second alignment plate having a second opening that is tapered;

an indexing bolt joining the first and second form assemblies to one another, the indexing bolt having a shank extending through the first opening and the second opening, the shank having a tapered portion seated against the second alignment plate in the second opening; and

a retainer mounted to the indexing bolt, the retainer being engaged with the first form assembly and pushing the first form assembly into engagement with the second form assembly.

16 . The form of claim 15 , wherein the shank includes first threading and wherein the retainer is threadably coupled to the first threading.

17 . The form of claim 16 , wherein the retainer comprises a flange nut.

18 . The form of claim 16 , wherein the shank is attached to the second form assembly.

19 . The form of claim 18 , wherein the shank includes second threading threadably coupled to the second form assembly.

20 . The form of claim 19 , wherein a diameter of the second threading is less than a diameter of the first threading.

Assignments (7)
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073914/0067 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY INTEREST Recorded Mar 17, 2025
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 070527/0785 →
SECURITY INTEREST Recorded Mar 17, 2025
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 070527/0731 →
SECURITY AGREEMENT (TERM LOAN B) Recorded Mar 13, 2025
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 070497/0728 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 23, 2023
From: HEARNEN, JACK O.; MANNION, ALEX W.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 064676/0114 →