IP Library Granted Patent US 10,864,682
Granted Patent B2
US 10,864,682 · App. 15/911,683 · Granted Dec 15, 2020

Method of joining of polymeric composites

Inventors: Steven Cipriano (Chesterfield Township, MI); Bradley J. Blaski (Sterling Heights, MI); Richard C. Janis (Grosse Pointe Woods, MI); Pei-chung Wang (Troy, MI)
Assignee: GM GLOBAL TECHNOLOGY OPERATIONS LLC
B29C65/561B29C65/48B29C66/02B29C66/30321B29C66/30325B29C66/7212B29K2705/00B29K2907/04
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Quick Facts
Patent No.
US 10,864,682
App. No.
15/911,683
Granted
Dec 15, 2020
Kind
B2
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.

Claims (33)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 5, 2018
From: CIPRIANO, STEVEN; BLASKI, BRADLEY J.; JANIS, RICHARD C.; WANG, PEI-CHUNG
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 045107/0065 →
Continuity (1)
Related Publication 20190270258A1 · Sep 5, 2019
Cited By (1)
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