Method of joining of polymeric composites

Patent metadata

Field	Value
Publication number	US-10864682-B2
Application number	US-201815911683-A
Country	US
Kind code	B2
Filing date	Mar 5, 2018
Priority date	Mar 5, 2018
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

A method of joining first and second layers of polymeric composite material includes disposing a portion of a molded insert having a bottom end into a top surface of a first layer of material and then applying a layer of adhesive between the top surface of the first layer and a bottom surface of a second layer of material to create a bond-line thickness. Next, a top surface of the second layer is pierced with a headless end of a fastener and interlocked into the molded insert. A layer of protective coating is then applied to the top surface of the second layer of material to cover the interlocked fastener.

First claim

What is claimed is:

1. A method of joining first and second layers of material, the method comprising:
disposing a portion of a molded insert having a bottom end into a top surface of a first layer of material;
applying a layer of adhesive between the top surface of the first layer and a bottom surface of a second layer of material to create a bond-line thickness;
piercing through a top surface of the second layer of material with a headless end of a fastener;
interlocking the headless end of the fastener into the molded insert; and
applying a layer of protective coating to the top surface of the second layer of material to cover the interlocked fastener.

2. The method of claim 1 wherein the fastener is a flow screw.

3. The method of claim 2 further comprising positioning the first and second layers on a fastener insertion machine after applying the adhesive layer between the first and second layers and before piercing the second layer of material with the headless end of the flow screw.

4. The method of claim 3 further comprising interlocking the flow screw until the headless end pierces the bottom end of the molded insert.

5. The method of claim 1 wherein the first and second layers each include a carbon fiber composite material.

6. The method of claim 1 wherein the bond line thickness is in a range of 0.1 mm to 1.5 mm.

7. The method of claim 1 further comprising allowing a top end of the molded insert to protrude above the top surface of the first layer of material a predetermined distance equal to the bond-line thickness.

8. The method of claim 1 further comprising allowing the adhesive layer to at least partially cure.

9. The method of claim 8 further comprising piercing through a top surface of the second layer of material with a headless end of the fastener after the adhesive layer is at least partially cured.

10. A method of joining first and second layers of material, the method comprising:
disposing a portion of a molded insert having a bottom end into a top surface of a first layer of material;
applying a layer of adhesive between the top surface of the first layer and a bottom surface of a second layer of material to create a bond-line thickness;
piercing through a top surface of the second layer of material with a headless end of a flow screw;
interlocking the headless end of the flow screw into the molded insert; and
applying a layer of protective coating to the top surface of the second layer of material to cover the interlocked flow screw.

11. The method of claim 10 further comprising positioning the first and second layers on a fastener insertion machine after applying the adhesive layer between the first and second layers and before piercing the second layer of material with the headless end of the flow screw.

12. The method of claim 11 further comprising interlocking the flow screw until the headless end pierces the bottom end of the molded insert.

13. The method of claim 10 wherein the first and second layers each include a carbon fiber composite material.

14. The method of claim 10 wherein the bond line thickness is in a range of 0.1 mm to 1.5 mm.

15. The method of claim 10 further comprising allowing a top end of the molded insert to protrude above the top surface of the first layer of material a predetermined distance equal to the bond-line thickness.

16. The method of claim 10 further comprising allowing the adhesive layer to at least partially cure.

17. The method of claim 16 further comprising piercing through a top surface of the second layer of material with a headless end of a flow screw after the adhesive layer is at least partially cured.

18. A method of joining first and second layers of material, the method comprising:
disposing a portion of a solid molded insert having a bottom end into a top surface of a first layer of material;
applying a layer of adhesive between the top surface of the first layer and a bottom surface of a second layer of material to create a bond-line thickness;
piercing through a top surface of the second layer of material and the molded insert with a headless end of a fastener;
interlocking the headless end of the fastener into the molded insert; and
after the step of interlocking, applying a layer of protective coating to the entire top surface of the second layer of material to cover the interlocked fastener.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Cipriano Steven
• Blaski Bradley J
• Janis Richard C
• Wang Pei-Chung

Classifications

• B29C66/30321

  making use of protrusions belonging to at least one of the parts to be joined · CPC title

• B29K2705/00

  Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts · 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

• B29C65/561 Primary

  using screw-threads being integral at least to one of the parts to be joined · CPC title

• B29C65/48

  using adhesives {, i.e. using supplementary joining material; solvent bonding} · CPC title