Multi-material joint and method of making thereof

Patent metadata

Field	Value
Publication number	US-10899109-B2
Application number	US-201916298839-A
Country	US
Kind code	B2
Filing date	Mar 11, 2019
Priority date	Mar 11, 2019
Publication date	Jan 26, 2021
Grant date	Jan 26, 2021

Abstract

A multi-material joint and a method of making thereof. The multi-material joint includes a first member comprising a first metal or metal alloy that is secured to a second member comprising a second metal or metal alloy that is different than the first metal or metal alloy. A sealant is positioned between the first member and the second member that galvanically insulates the first member from the second member. The sealant comprises a liquid elastomer and a foaming agent.

First claim

The invention claimed is:

1. A method of making a multi-material joint comprising:
applying a sealant to a first member comprising steel or a second member comprising an aluminum alloy, the sealant comprising one or more liquid elastomers in an amount of from 0.1% to 20% by pre-cure weight of the sealant, from 0.1% to less than 10% epoxy resin by pre-cure weight of the sealant, and one or more foaming agents;
attaching the first member to the second member with the sealant positioned therebetween to form the multi-material joint, wherein the sealant galvanically insulates the first member from the second member; and
curing the sealant, wherein the post-cure elongation at break of the sealant is from 80% to 120%, and the post-cure tensile shear strength of the sealant is less than 0.5 MPa.

2. The method of claim 1 , wherein a post-cure volume of the sealant is from 15% to 35% greater than a pre-cure volume of the sealant.

3. The method of claim 1 , wherein the post-cure compressive modulus of elasticity of the sealant is from 20% to 35%.

4. The method of claim 1 , further comprising:
e-coating the second member before the step of applying the sealant to the first member or the second member, wherein the step of applying the sealant to the first member or the second member includes applying the sealant to the second member; and
e-coating the multi-material joint before the step of curing the sealant, wherein the step of curing the sealant comprises heating the e-coated multi-material joint at a temperature of from 150° C. to 230° C. for a time period ranging from 5 minutes to 1 hour.

5. The method of claim 4 , wherein the second member comprises an aluminum alloy casting.

6. A method of making a multi-material joint comprising:
providing a casting comprising an aluminum alloy;
applying a sealant to the casting, the sealant comprising an epoxy resin in an amount from 0.1% to less than 10% by pre-cure weight of the sealant, one or more liquid elastomers in an amount of from 0.1% to 20% by pre-cure weight of the sealant, and one or more foaming agents;
positioning a plurality of stamped steel components along a perimeter of the casting, wherein the sealant is positioned between each of the stamped steel components and the casting to galvanically insulate the stamped steel components from the casting;
attaching the casting to the plurality of stamped steel components with the sealant positioned therebetween to form the multi-material joint; and
heating the multi-material joint to expand and cure the sealant, wherein the sealant has a post-cure elongation at break of from 80% to 120% and a post-cure tensile shear strength of less than 0.5 MPa.

7. The method of claim 6 , further comprising securing each of the stamped steel components to the casting with one or more fasteners that extends through the sealant to form the multi-material joint, and securing at least one of the stamped steel components of the multi-material joint to a side rail of a vehicle front body structure before heating the multi-material joint.

8. The method of claim 7 , further comprising e-coating the casting before applying the sealant to the casting, and e-coating the vehicle front body structure after securing the at least one of the stamped steel components to the side rail and before heating the multi-material joint.

9. The method of claim 8 , wherein the sealant has a post-cure volume that is 15-35% greater than a pre-cure volume of the sealant.

10. The method of claim 9 , wherein the sealant has a post-cure compressive modulus of elasticity of 20-35%.

11. The method of claim 6 , wherein the sealant prior to curing comprises a solid rubber.

12. The method of claim 6 wherein the multi-material joint is free of other sealants and structural adhesives.

13. A method of making a multi-material joint comprising:
providing a first member comprising steel and a second member comprising an aluminum alloy casting;
applying a sealant to the first member or the second member, the sealant comprising an epoxy resin in an amount from 0.1% to less than 10% by pre-cure weight of the sealant, one or more liquid elastomers in an amount of from 0.1% to 20% by pre-cure weight of the sealant, and one or more foaming agents;
attaching the first member to the second member with the sealant positioned therebetween to form the multi-material joint, wherein the sealant galvanically insulates the first member from the second member, wherein the sealant before curing comprises from 0.1% to 20% liquid elastomer by weight; and
curing the sealant, wherein a post cure tensile shear strength of the sealant is less than 0.5 MPa, a post cure volume of the sealant is from 15% to 35% greater than a pre-cure volume of the sealant and a post cure compressive modulus of elasticity of the sealant is from 20% to 35%.

14. The method of making a multi-material joint of claim 13 , wherein the multi-material joint is free of other sealants and structural adhesives.

Assignees

• Honda Motor Co Ltd

Inventors

• Meaige Benjamin J
• Gilsinger Negar B
• Berg Mariko Elaine
• Kauffman Jared S

Classifications

• C25D7/00

  Electroplating characterised by the article coated · CPC title

• B32B5/20

  foamed in situ · CPC title

• B32B2266/0207

  Materials belonging to B32B25/00 · CPC title

• B32B2605/00

  Vehicles · CPC title

• B32B2307/542

  Shear strength · CPC title