Composite rivet blank and installation thereof

Patent metadata

Field	Value
Publication number	US-10589468-B2
Application number	US-201515123084-A
Country	US
Kind code	B2
Filing date	Mar 6, 2015
Priority date	Mar 7, 2014
Publication date	Mar 17, 2020
Grant date	Mar 17, 2020

Abstract

Composite fasteners, associated blanks and also methods and apparatus for the installation of such fasteners are disclosed. An exemplary composite rivet ( 10 ) disclosed comprises an elongated body including braided reinforcement fibers ( 14 ) embedded inside the body and supported in a matrix material ( 16 ). Also disclosed are structural assemblies comprising composite fasteners and panels or other parts comprising composite and/or other materials.

First claim

What is claimed is:

1. A composite fastener blank comprising:
an elongated body having an axis and a length along the axis, the body comprising braided reinforcement fibers embedded inside the body and supported in a matrix material, the braided reinforcement fibers comprising a first braid and a second braid nested in the first braid, the braided reinforcement fibers forming a braid structure where a diameter of the braid structure increases upon compression of the braid structure such that the blank is installable in a hole by compression of the blank, wherein said blank is formed from at least one of a pultruded rod or a compression molded rod from which said blank is cut.

2. The blank as defined in claim 1 , wherein the braided reinforcement fibers extend the length of the body.

3. The blank as defined in claim 1 , wherein the fibers of the first braid comprise carbon.

4. The blank as defined in claim 1 , wherein at least some of the fibers are oriented at an inclination angle between 15 degrees and 30 degrees from the axis of the body.

5. The blank as defined in claim 1 , wherein at least some of the fibers are oriented at an inclination angle of about 20 degrees from the axis of the body.

6. The blank as defined in claim 1 , wherein the volume fraction of reinforcement fibers in the body is between 55% and 63%.

7. The blank as defined in claim 1 , wherein the volume fraction of reinforcement fibers in the body is about 60%.

8. The blank as defined in claim 1 , wherein the first and second braids are tubular biaxial braids.

9. A composite rivet comprising:
a body having braided reinforcement fibers embedded inside the body and supported in a matrix material, the braided reinforcement fibers comprising a first braid and a second braid nested in the first braid, the body comprising a first finished end for engaging a first part and a second finished end for engaging a second part, wherein said body is formed from at least one of a pultruded rod or a compression molded rod from which said body is cut.

10. The rivet as defined in claim 9 , wherein at least one of the finished ends comprises a fiber anchoring protrusion used to at least partially control the deformation of the fibers during finishing of the at least one of the finished ends.

11. The rivet as defined in claim 9 , wherein the fibers of the first braid comprise carbon.

12. The rivet as defined in claim 9 , wherein the first and second braids are tubular biaxial braids.

Assignees

• Bombardier Inc

Inventors

• Trudeau Paul
• Laberge Lebel Louis
• Landry Alain
• Hoste Didier

Classifications

• B29L2031/3085

  Wings · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title

• B29L2031/3002

  Superstructures characterized by combining metal and plastics, i.e. hybrid parts · CPC title

• B29C70/24

  oriented in at least three directions forming a three-dimensional [3D] structure · CPC title

• B29C66/71

  characterised by the composition of the plastics material of the parts to be joined (welding bar compositions B29C65/125) · CPC title