Multilayer composite and method for producing same

Patent metadata

Field	Value
Publication number	US-11370195-B2
Application number	US-201916661044-A
Country	US
Kind code	B2
Filing date	Oct 23, 2019
Priority date	Apr 28, 2017
Publication date	Jun 28, 2022
Grant date	Jun 28, 2022

Abstract

Provided is a multilayer composite that has flame retardancy and low smoking property as well as has high physical characteristics. The multilayer composite has a multilayer structure and includes at least one core layer and at least one skin layer, wherein the multilayer composite satisfies all the following conditions (A) to (D): (A) the core layer is a composite including discontinuous reinforcing fibers and a first thermoplastic resin, in which the discontinuous reinforcing fibers are randomly dispersed and bonded with the first thermoplastic resin at least at intersections of the discontinuous reinforcing fibers; (B) the skin layer is a composite including continuous reinforcing fibers and a second thermoplastic resin, in which the continuous reinforcing fibers are impregnated with the second thermoplastic resin; (C) each of the first and the second thermoplastic resins has a limiting oxygen index of 30 or higher; and (D) the first and the second thermoplastic resins are miscible with each other.

First claim

What is claimed is:

1. A multilayer composite having a multilayer structure and comprising at least one core layer and at least one skin layer, wherein the multilayer composite satisfies all the following conditions (A) to (D):
(A) the core layer is a composite comprising discontinuous reinforcing fibers, a first thermoplastic resin, and a polymer binder which is different from the first thermoplastic resin, in which the discontinuous reinforcing fibers are randomly dispersed and bonded with the first thermoplastic resin at least at intersections of the discontinuous reinforcing fibers;
(B) the skin layer is a composite comprising continuous reinforcing fibers and a second thermoplastic resin, in which the continuous reinforcing fibers are impregnated with the second thermoplastic resin;
(C) each of the first and the second thermoplastic resins has a limiting oxygen index of 30 or higher; and
(D) the first and the second thermoplastic resins are miscible with each other and are mutually solubilized in one another.

2. The multilayer composite according to claim 1 , wherein the continuous reinforcing fibers constituting the skin layer are carbon fibers.

3. The multilayer composite according to claim 1 , wherein each of the first and the second thermoplastic resins is at least one resin selected from the group consisting of a polyetherimide resin, a polyether ether ketone resin, a polyether ketone ketone resin, a poivethersulfone resin, a thermoplastic polyimide resin, a flame-retardant-containing polycarbonate resin, and a flame-retardant-containing polyester resin.

4. The multilayer composite according to claim 1 , wherein the first and the second thermoplastic resins are identical.

5. The multilayer composite according to claim 1 , wherein the multilayer composite has a void content in a range from 20 to 80%.

6. The multilayer composite according to claim 1 , wherein the core layer has a void content twice or more as high as that of the skin layer.

7. The multilayer composite according to claim 1 , wherein the discontinuous reinforcing fibers in the core layer have a bending shape and are used to expand the multilayer composite.

8. A method for producing the multilayer composite according to claim 1 , the method comprising:
overlaying the at least one core layer material and the at least one skin layer material to form a multilayer stack, and
heat-compressing the multilayer stack and then cooling so as to integrate the multilayer stack, wherein
in the formation of the multilayer stack,
the core layer material is a nonwoven fabric that is formed of the discontinuous reinforcing fibers, the first thermoplastic resin and the polymer binder which is different from the first thermoplastic resin in a fibrous form and/or a particulate form, both the discontinuous reinforcing fibers and the first thermoplastic resin being randomly dispersed in the nonwoven fabric,
the skin layer material is formed of a fabric made of the continuous reinforcing fibers and the second thermoplastic resin to be impregnated in the fabric
in the integration of the multilayer stack, and
heating-compressing is carried out to mutually solubilize the first thermoplastic resin and the second thermoplastic resin and to bend the discontinuous reinforcing fibers.

9. The method for producing a multilayer composite according to claim 8 , further comprising heating the multilayer composite obtained after the integration to release bending stress of the discontinuous reinforcing fibers so as to expand the multilayer composite.

10. The method according to claim 9 , wherein in the expansion of the multilayer composite, the multilayer composite having a void content in a range from 0 to 20% is heated such that the multilayer composite is expanded to have a higher void content after heating than the void content before heating.

11. The method according to claim 10 , wherein the void content of the multilayer composite after heating is in a range from 20 to 80%.

12. The method according to claim 9 , wherein the heating of the multilayer composite comprises form-molding.

13. The multilayer composite according to claim 1 , wherein a difference in solubility parameter between the first thermoplastic resin and the second thermoplastic resin Δδ(J/cm 3 ) 1/2 determined in accordance with the method described in Polymer Handbook Fourth .Edition Volume 2 (A John Wiley & Sons, Inc., Publication) J. BRANDRUP, E. H. IMMERGUT, and E. A. GRULKE, (1999) pp.675-714 is from 0 to 4.

14. The multilayer composite according to claim 1 , wherein a weight ratio of a total amount of the first thermoplastic resin and the discontinuous reinforcing fibers to the polymer binder in the core layer is from 85/15 to 99/1.

Assignees

• Kuraray Co

Inventors

• Katsuya Satoshi
• Washitake Yosuke
• Endo Ryokei

Classifications

• B64C1/00

  Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like · CPC title

• B32B2260/021

  Fibrous or filamentary layer · CPC title

• B32B2260/046

  Synthetic resin · CPC title

• B32B2262/106

  Carbon fibres, e.g. graphite fibres · CPC title

• B61D17/00

  Construction details of vehicle bodies (for tank wagons B61D5/00; for hopper cars B61D7/00; body details specially adapted for tipping wagons B61D9/06; for mine cars B61D11/00) · CPC title