Hybrid components containing reactive hotmelt adhesives
View Patent ↗Reactive hotmelt adhesives based on copolyamide can be used in hybrid components. These hybrid components find application in, for example, vehicle construction and aircraft construction.
1. A hybrid component comprising:
a metal bound to a polymer with a laurolactam-based copolyamide hotmelt adhesive that comprises 2.5% to 15% of blocked isocyanate and 2.5% to 10% of epoxide, and
a cathodic electrocoating (EC) over the surface of the metal bound to the polymer which is distinct from the hotmelt adhesive.
2. The hybrid component of claim 1 that is made by a process comprising:
binding a metal to a polymer with said laurolactam-based copolyamide hotmelt adhesive, and
applying a cathodic electrocoating, which is distinct from the laurolactam-based polyamide hotmelt adhesive, over the surface of the metal bound to the polymer.
3. The hybrid component according to claim 2 , wherein said process further comprises
coating said metal over its full area with said hotmelt adhesive using an electrostatic spray gun or a suitable coating system, and
sintering incipiently at 150° C. 120 to 300 seconds.
4. The hybrid component according to claim 2 , wherein said process further comprises
partially coating said metal with said hotmelt adhesive using an electrostatic spray gun or a suitable coating system, and
sintering incipiently at 150° C. 120 to 300 seconds.
5. The hybrid component according to claim 2 , wherein said process further comprises passing said hybrid component through an EC oven for coating.
6. The hybrid component according to claim 2 , wherein said process further comprises degreasing of said metal.
7. The hybrid component according to claim 2 , wherein said process further comprises preheating of the metal to 60 to 80° C.
8. The hybrid component according to claim 2 , wherein said process further comprises exposing said hybrid to a temperature of 150° C. to 190° C. for a period of 10 to 30 minutes in a cathodic electrocoating oven.
9. The hybrid component of claim 1 that is made by a process comprising:
coating a metal with said hotmelt adhesive using a electrostatic spray gun to obtain a coated metal.
10. The hybrid component according to claim 1 that is made by a process comprising:
coating said metal over its full area with said hotmelt adhesive using an electrostatic spray gun or a suitable coating system, and
sintering incipiently at 150° C. 120 to 300 seconds.
11. The hybrid component according to claim 1 that is made by a process that comprises:
partially coating said metal with said hotmelt adhesive using an electrostatic spray gun or a suitable coating system, and
sintering incipiently at 150° C. 120 to 300 seconds.
12. The hybrid component according to claim 1 , that is made by a process that comprises passing said hybrid component through an EC oven for coating.
13. The hybrid component according to claim 1 , that is made by a process that comprises degreasing of said metal.
14. The hybrid component according to claim 1 , that is made by a process that comprises preheating the metal to 60 to 80° C.
15. The hybrid component according to claim 1 , that is made by a process that comprises exposing said hybrid component to a temperature of 150° C. to 190° C. for a period of 10 to 30 minutes in a cathodic electrocoating oven.
16. The hybrid component according to claim 1 , that is made by a process comprising:
coating a metal with said hotmelt adhesive using an electrostatic spray gun to obtain a coated metal; and
binding the coated metal to a polymer;
wherein said coated metal is heated at about 150° C. over a time of approximately 120to 300 seconds in order to cause incipient melting of the adhesive; and
wherein said polymer is introduced by injection moulding, to obtain a structure-forming component which then passes through an EC oven for coating a temperature of 150° C. to 190° C. for a period of 10 to 30 minutes.
17. A vehicle construction comprising the hybrid component of claim 1 .
18. A rail construction comprising the hybrid component of claim 1 .
19. An aircraft construction comprising the hybrid component of claim 1 .
20. A bumper comprising the hybrid component of claim 1 .