Composite structure formed of fiber reinforced plastic sheet and metallic sheet, and manufacturing method thereof

Patent metadata

Field	Value
Publication number	US-10232560-B2
Application number	US-201414776005-A
Country	US
Kind code	B2
Filing date	Mar 12, 2014
Priority date	Mar 13, 2013
Publication date	Mar 19, 2019
Grant date	Mar 19, 2019

Abstract

A manufacturing method of a composite structure includes: (a) preparing: a metallic sheet(s) having a through-hole(s) penetrating throughout the metallic sheet(s) in its thickness direction; (b) setting a prepreg(s), constituting a fiber reinforced plastic sheet(s), and the metallic sheet in a pair of dies, which have a recess(es) arranged at a position(s) opposed to one side opening(s) of the through-hole(s), the recess(es) having a larger diameter than the one side opening; (c) closing the dies, wherein, upon closing, (ca) the prepreg(s) and the metallic sheet are molded to the predetermined shape, while surface-contacting therebetween, (cb) at least one of the prepreg(s) and a patch member(s) is extruded into the through-hole(s), so that the shaft part is molded, and (cc) the patch member(s) forms at least part of a head part(s) in the recess(es), the head part(s) integrated with the shaft part(s) and engaging on the metallic sheet(s).

First claim

The invention claimed is:

1. A method of manufacturing a composite structure formed of a fiber reinforced plastic sheet and a metallic sheet, comprising:
preparing a pair of dies for molding a composite structure of a predetermined shape;
preparing a metallic sheet(s) having at least one opening defined by a through-hole(s) penetrating the metallic sheet(s) in a thickness direction of the metallic sheet(s);
setting a patch member(s) on one of the pair of dies, the patch member(s) made of plastic and having a larger size than the opening(s);
setting a prepreg(s) to constitute a fiber reinforced plastic sheet(s) and the metallic sheet(s) in the pair of dies in a manner that the metallic sheet(s) is interposed between the prepreg(s) and the patch member(s); and
closing the pair of dies, and simultaneously, selectively applying pressure on a corresponding portion(s) located inwardly of the at least one opening so as to joint-bond the prepreg(s), the metallic sheet and the patch member(s) to each other by bonding the prepreg(s) to the patch member(s) through the at least one opening, thereby producing the composite structure molded in the predetermined shape; wherein
the one die of the pair of dies has a recess(es) receiving the patch member(s), the recess(es) open toward a removal direction of the composite structure after molded,
a shaft part(s) is molded in the through-hole(s) so that the shaft part(s) is integrated with the prepreg, and
a head or engaging part(s) is molded in the recess(es) so that the head or engaging part(s) is integrated with the shaft part(s) and has a larger diameter(s) than the opening(s).

2. The manufacturing method of the composite structure according to claim 1 , wherein
the pair of dies have a step difference profile(s) arranged on the inner surface extending in a relative movement direction of the pair of dies, and wherein
the recess(es) is defined by the step difference profile(s).

3. The manufacturing method of the composite structure according to claim 1 , wherein
the fiber reinforced plastic sheet(s) is bonded to one side surface(s) of the metallic sheet(s).

4. The manufacturing method of the composite structure according to claim 1 , wherein
the fiber reinforced plastic sheet(s) contains continuous reinforce fiber.

5. The method of manufacturing a composite structure according to claim 1 , further comprising:
as the prepreg(s), preparing a prepreg(s) having a thickening part(s) arranged at a position(s) opposed to the through-hole(s); and
extruding the thickening part(s) into the through-hole(s) so as to bond to the patch member(s) set in the pair of dies.

6. A method of manufacturing a composite structure formed of a fiber reinforced plastic sheet and a metallic sheet, comprising:
preparing a pair of dies for molding a composite structure of a predetermined shape;
preparing a metallic sheet(s) having at least one opening defined by a through-hole(s) penetrating the metallic sheet(s) in a thickness direction of the metallic sheet(s);
setting a patch member(s) on a prepreg(s) for constituting a fiber reinforced plastic sheet(s), the patch member(s) made of plastic and having a larger size than the opening(s);
setting the prepreg(s), the patch member(s) and the metallic sheet(s) in the pair of dies in a manner that the patch member(s) is interposed between the prepreg(s) and the opening(s); and
closing the pair or dies, and simultaneously, selectively applying pressure on a corresponding portion(s) located inwardly of the at least one opening so as to joint-bond the prepreg(s), the metallic sheet and the patch member(s) to each other by bonding the prepreg(s) to the patch member(s) and protruding the patch member(s) to the opposite side through the opening(s), thereby producing the composite structure molded in the predetermined shape: wherein
the one die of the pair of dies has a recess(es) receiving the patch member(s), the recess(es) open toward a removal direction of the composite structure after molded,
a shaft part(s) is molded in the through-hole(s) so that the shaft part(s) is integrated with the prepreg, and
a head or engaging part(s) is molded in the recess(es) so that the head or engaging part(s) is integrated with the shaft part(s) and has a larger diameter(s) than the opening(s).

7. A method of manufacturing a composite structure formed of a fiber reinforced plastic sheet and a metallic sheet, comprising:
preparing:
a metallic sheet(s) having a through-hole(s) penetrating the metallic sheet(s) in a thickness direction of the metallic sheet(s);
a prepreg(s) in order to constitute a fiber reinforced plastic sheet(s);
a pair of dies for molding a composite structure into a predetermined shape, wherein the pair of dies can have a recess(es) arranged at a position(s) opposed to one side opening(s) of the through-hole(s), the recess(es) having a larger diameter than the one side opening, and
a patch member(s) to be set at a position(s) opposed to the through-hole(s);

setting the prepreg(s) and the metallic sheet in the pair of dies; and
closing the pair of dies, wherein, upon closing,
the prepreg(s) and the metallic sheet are molded into the predetermined shape, while surface-contacting therebetween,
at least one of the prepreg(s) and the patch member(s) is extruded into the through-hole(s), so that the shaft part is molded, and
the patch member(s) forms at least part of a head part(s) in the recess(es), the head part(s) being integrated with the shaft part(s) and engaging on the metallic sheet(s).

8. The method of manufacturing a composite structure according to claim 7 , wherein
the patch member(s) is set in the recess(es), and thereafter, upon closing the pair of dies, the prepreg(s) is extruded into the through-hole(s) to bond to the patch member(s), thereby molding the shaft part(s) and the head part(s).

9. The method of manufacturing a composite structure according to claim 7 , wherein
the patch member(s) is set on the prepreg(s), and thereafter, upon closing the pair of dies, the patch member(s) is extruded into the through-hole(s), and further into the recess(es), thereby molding the shaft part(s) and the head part(s).

10. The method of manufacturing a composite structure according to claim 7 , wherein
a first patch member(s) as the patch member(s) is set on the prepreg(s), and a second prepreg(s) as the patch member(s) is set in the recess(es), and thereafter,
upon closing the pair of dies, the first patch member(s) is extruded into the through-hole(s) to be bonded to the second patch member(s), thereby molding the shaft part(s) and the head part(s).

Assignees

• Aisin Takaoka Ltd

Inventors

• Kondo Kiyohito
• Yamashita Yuji

Classifications

• B29C66/721

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

• B32B15/08

  of synthetic resin · CPC title

• B29C70/745

  Filling cavities in the preformed part (for joining B29C70/84) · CPC title

• B29C66/742

  to metals or their alloys · CPC title

• B29C66/843

  Machines for making separate joints at the same time in different planes; Machines for making separate joints at the same time mounted in parallel or in series · CPC title