IP Library › Granted Patent US 12,036,749
Granted Patent B2
US 12,036,749 · App. 17/167,659 · Granted Jul 16, 2024

Metal composite joints for composite rods

Inventor: Mark R. Gurvich (Middletown, CT)
Assignee: B/E Aerospace, Inc.
B29C66/742B21D39/048B29C57/10B29C65/568B29C65/64B29C66/5221B29C66/5344
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Quick Facts
Patent No.
US 12,036,749
App. No.
17/167,659
Granted
Jul 16, 2024
Kind
B2
Abstract

A method for joining composite rods with tubular shape includes internal and external collars applied to the ends of the composite rod and deformed via unidirectional compressive load applied by a clamp in the radial direction of the composite rod cross-section. The resulting plastic deformation of the metal collars and composite rod interlock those components to support both compressive and tensile loads.

Claims (22)

1. A method for securing joint components to a composite rod comprising:

inserting an internal collar into an end of the composite rod;

placing an external collar over the end of the composite rod;

placing a clamp device around the end of the composite rod over the external collar; and

plastically deforming the internal collar, the external collar, and the end of the composite rod via applying unidirectional compressive load in a radial direction to the clamp device.

2. The method of claim 1 , further comprising:

heating the end of the composite rod to a predetermined deformation temperature before deformation; and

cooling the end of the composite rod after deformation,

wherein the composite rod comprises a thermoplastic composite.

3. The method of claim 1 , further comprising:

partially curing the end of the composite rod before deformation; and

curing the end of the composite rod after deformation.

4. The method of claim 1 , further comprising machining a deformed portion of the external collar and internal collar to facilitate interconnection to external parts or structures.

5. The method of claim 1 , wherein the clamp device defines a deformation profile.

6. The method of claim 5 , wherein the deformation profile defines a stepped profile.

7. The method of claim 5 , wherein the deformation profile defines a constant radius curve.

8. The method of claim 1 , further comprising:

inserting a second internal collar into an end of a second composite rod;

placing the external collar over the end of the second composite rod;

placing the clamp device around the end of the second composite rod over the external collar; and

deforming the second internal collar, the external collar, and the end of the second composite rod via applying unidirectional compressive load in the radial direction to the clamp device,

wherein the external collar is configured to receive the composite rod in a first end and the second composite rod in a second end.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 4, 2021
From: GURVICH, MARK R.
To: B/E AEROSPACE, INC.
Reel/Frame 055150/0807 →
Continuity (1)
Related Publication 20220243750A1 · Aug 4, 2022
Cited By (1)
US 12,649,579