Composite component and process for producing a composite component

Patent metadata

Field	Value
Publication number	US-9314964-B2
Application number	US-201414301915-A
Country	US
Kind code	B2
Filing date	Jun 11, 2014
Priority date	Dec 12, 2011
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

Abstract

A process is provided for producing a composite component having a first component element and a second component element, which are connected with one another by an adhesive connection. The process includes forming an adhesive cavity by applying thermally active plastic material to an adhesive connection side of the first component element and/or to an adhesive connection side of the second component element; arranging the first component element on the second component element, wherein a gap is formed between the adhesive connection side of the first component element and the adhesive connection side of the second component element, and supplying of heat in such a manner that the thermally active plastic material expands and forms a boundary in the gap between the first component element and the second one. The process further fills the formed adhesive cavity with an adhesive for the permanent connection of the first component element with the second component element.

First claim

What is claimed is:

1. A process for producing a composite component having a first component element and a second component element, the first and second component elements being mutually connected by an adhesive connection, the process comprising the acts of:
forming a locally limited adhesive cavity having a limited axial extent relative to an axial extent of the first and second component elements by:
(i) applying a thermally active plastic material to an adhesive connection side of the first component element and/or to an adhesive connection side of the second component element, the applied thermally active plastic material being applied about a whole circumference of the adhesive connection side at two locations spaced axially apart from one another;
(ii) arranging the first component element and the second component element opposite and spaced apart from one another, wherein a gap is formed between the adhesive connection side of the first component element and the adhesive connection side of the second component element; and
(iii) supplying heat to expand the thermally active plastic material to form boundaries in the gap between the first component element and the second component element at the two locations, wherein the locally limited adhesive cavity is formed by the gap between the boundaries at the two locations such that the locally limited adhesive cavity has the limited axial extent relative to the axial extent of the first and second com onent elements; and

filling the formed locally limited adhesive cavity with adhesive to adhere the first component element with the second component element, the adhesive completely filling the gap between the boundaries.

2. The process according to claim 1 , wherein
the first component element is formed of a first material,
the second component element is formed of a second material, and
the first material and the second material have different thermal coefficients of linear expansion.

3. The process according to claim 2 , wherein the first material is a plastic material and the second material is a metallic material.

4. The process according to claim 3 , wherein the plastic material is a fiber-reinforced plastic material.

5. The process according to claim 1 , wherein
the thermally active plastic material is applied so as to form a closed boundary in the gap at least after the heat is supplied.

6. The process according to claim 1 , wherein the act of supplying heat further comprises an act of coating the composite component with a coating.

7. The process according to claim 6 , wherein during the act of coating the composite component, the process further comprises the act of drying the coating, wherein process heat for the drying of the coating supplies the heat to expand the thermally active plastic material.

8. The process according to claim 7 , wherein the act of coating is a dip painting process.

9. The process according to claim 1 , wherein the first component element is a hollow sectioned element and the second component element is a reinforcing element, the process further comprising the acts of:
arranging the reinforcing element inside the hollow section element; and
during the forming of the adhesive cavity, applying the thermally active plastic material to an exterior side of the reinforcing element and/or to an interior side of the hollow section element.

10. The process according to claim 9 , wherein the hollow section element comprises a first hollow-section component and a second hollow-section component.

11. The process according to claim 10 , wherein
during the arranging of the reinforcing element inside the hollow section element, the reinforcing element is first arranged in the first hollow-section component, and then the first hollow-section component is connected with the second hollow-section component.

12. The process according to claim 1 , wherein the composite component is a support part of a motor vehicle body.

13. The process according to claim 1 , wherein multiple locally limited adhesive cavities are formed in the gap between the first component element and the second component element, whereby multiple locally limited adhesive connections are made within the gap between the first component element and the second component element.

Assignees

• Bayerische Motoren Werke Ag

Inventors

• Brauch Michael

Classifications

• B29C65/7826

  said distance pieces being non-integral with the parts to be joined, e.g. particles · CPC title

• B29C66/1312

  Single flange to flange joints, the parts to be joined being rigid (the parts to be joined being flexible B29C66/133) · CPC title

• B29C66/004

  Preventing sticking together, e.g. of some areas of the parts to be joined · CPC title

• B29C66/547

  Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles, e.g. endless tubes · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title