Process for joining fiber composite materials using self-piercing rivets

Patent metadata

Field	Value
Publication number	US-10704584-B2
Application number	US-201715658029-A
Country	US
Kind code	B2
Filing date	Jul 24, 2017
Priority date	Apr 10, 2014
Publication date	Jul 7, 2020
Grant date	Jul 7, 2020

Abstract

A process for joining fiber composite materials using self-piercing rivets. The process includes contacting first and second panels. The second panel is a fiber composite material. The process further includes elevating a temperature of only a fastening portion of the second panel. The process also includes placing the first and second panels on a die and joining the first and second panels with one or more rivets while the fastening portion is at an elevated temperature.

First claim

What is claimed is:

1. A method comprising:
contacting first and second panels, the second panel being a fiber composite material, the first panel having first and second surfaces, the second panel having first and second surfaces, the second surface of the first panel contacting the first surface of the second panel;
while the first and second panels are contacting each other, elevating a temperature of a fastening portion of the second panel from a heat source spaced apart from the second panel, the second surface of the second panel positioned adjacent to the heat source; and
while the fastening portion is at the elevated temperature and the first and second panels are contacting each other, placing the first and second panels on a die and joining the first and second panels with one or more rivets.

2. The method of claim 1 , wherein the elevating step includes applying radiant heat from the heat source.

3. The method of claim 1 , wherein the elevating step includes applying convective heat from the heat source.

4. The method of claim 1 , wherein the fiber composite material includes a thermoset composite material.

5. The method of claim 4 , wherein the thermoset composite material is an epoxy-based material.

6. The method of claim 1 , wherein the fiber composite material is a carbon or glass fiber material including glass or carbon aligned fibers.

7. A method comprising:
contacting first and second panels, the second panel being a fiber composite material, the first panel having first and second surfaces, the second panel having first and second surfaces, the second surface of the first panel contacting the first surface of the second panel;
while the first and second panels are contacting each other, elevating a temperature of a fastening portion of the second panel from a heat source spaced apart from the second panel, the second surface of the second panel positioned adjacent to the heat source; and
after the elevating step, placing the first and second panels on a die and joining the first and second panels with one or more rivets.

8. The method of claim 7 , wherein the elevating step includes applying radiant heat from the heat source.

9. The method of claim 7 , wherein the elevating step includes applying convective heat from the heat source.

10. The method of claim 7 , wherein the fiber composite material includes a thermoset composite material.

11. The method of claim 10 , wherein the thermoset composite material is an epoxy-based material.

12. The method of claim 7 , wherein the placing step occurs while the fastening portion is at an elevated temperature.

13. The method of claim 7 , wherein the fiber composite material is a carbon or glass fiber material including glass or carbon aligned fibers.

14. A method comprising:
contacting first and second panels, the second panel being a carbon or glass fiber composite material, the first panel having first and second surfaces, the second panel having first and second surfaces, the second surface of the first panel contacting the first surface of the second panel;
while the first and second panels are contacting each other, elevating a temperature of a fastening portion of the second panel from a heat source spaced apart from the second panel, the second surface of the second panel positioned adjacent to the heat source; and
while the fastening portion is at the elevated temperature and the first and second panels are contacted, placing the first and second panels on a die and joining the first and second panels with one or more rivets.

15. The method of claim 14 , wherein the carbon or glass fiber composite material includes a carbon fiber material and a polymeric material.

16. The method of claim 14 , wherein the carbon or glass fiber composite material includes a thermoset composite material.

17. The method of claim 14 , wherein the elevating step includes applying radiant heat from the heat source.

18. The method of claim 14 , wherein the elevating step includes applying convective heat from the heat source.

19. The method of claim 14 , wherein the elevated temperature is ±30% of a glass transition temperature in Kelvin of the fiber composite material.

20. The method of claim 14 , wherein the carbon or glass fiber composite material is a carbon or glass fiber material including glass or carbon aligned fibers.

Assignees

• Ford Global Tech Llc

Inventors

• Campbell Aindrea Mckelvey
• Huff Garret Sankey
• Freis Amanda Kay

Classifications

• B29C66/73117

  Tg, i.e. glass transition temperature · CPC title

• B21J15/025

  Setting self-piercing rivets · CPC title

• B29C65/02

  by heating, with or without pressure · CPC title

• B32B2037/0092

  in which absence of adhesives is explicitly presented as an advantage · CPC title

• B29C66/74283

  Iron or alloys of iron, e.g. steel · CPC title