COMPOSITE LAMINATE HAVING A HONEYCOMB CORE, AND METHOD FOR THE MANUFACTURE THEREOF

1 . A composite laminate having a honeycomb core, comprising in sequence:

(a) a first skin layer,

(b) a first barrier film,

(c) a first adhesive film,

(d) a honeycomb core,

(e) a second adhesive film,

(f) a second barrier film,

(g) a second skin layer,

(h) a plurality of tubular rivets,

(i) a self-expanding sealant sealed around the tubular rivets, and

(j) a matrix derived from a liquid binder,

wherein

the liquid binder is selected from the group consisting of phenolic resin, epoxy resin, unsaturated polyester resin, vinyl ester resin and combinations thereof; and has a viscosity of 100 cp to 500 cp at 25° C.;

the layers (b), (c), (d), (e) and (f) are stacked in sequence to form a preform; and

the tubular rivets are inserted through the preform and set apart from each other by a distance of 30 mm to 200 mm.

2 . The composite laminate as claimed in claim 1 , wherein

the first skin layer (a) and the second skin layer (g) are not prepregs; and each independently comprises at least one reinforcing fabric comprising glass fibers, carbon fibers, aramid fibers or combinations thereof;

each of the first barrier film (b) and the second barrier film (f) independently comprises ethylene (meth)acrylate, anhydride-modified ethylene (meth)acrylate, ethylene vinyl acetate, anhydride-modified ethylene vinyl acetate, ethylene-acid ionomer, polyamide, polyurethane, polyester, polyimide or combinations thereof;

each of the first adhesive film (c) and the second adhesive film (e) independently comprises epoxy resin, acrylate resin or polyurethane resin; and has a glass transition temperature of 60° C. to 160° C.;

the honeycomb core (d) is a board having a honeycomb structure made of thin sheets composed of aramid, polycarbonate, polypropylene, steel, aluminum, aluminum alloy or glass fiber; and the cross-sectional shape of each cell of the honeycomb board is hexagonal, overexpanded hexagonal, circular or corrugate; and

the self-expanding sealant is composed of expandable polystyrene or expandable polyurethane.

3 . The composite laminate as claimed in claim 1 , which has a total thickness of 5 mm to 300 mm, and an areal density of 0.35 Kg/m 2 to 20 Kg/m 2 .

4 . The composite laminate as claimed in claim 1 , wherein the reinforcing fabric for use as the first skin layer (a) and the second skin layer (g) each independently has an areal density of 20 g/m 2 to 660 g/m 2 and the reinforcing fabric is a woven fabric or a non-woven fabric.

5 . The composite laminate as claimed in claim 1 , wherein each of the first barrier film (b) and the second barrier film (f) independently has an areal density of 20 g/m 2 to 100 g/m 2 and a thickness of 20 mm to 100 mm.

6 . The composite laminate as claimed in claim 1 , wherein each of the first adhesive film (c) and the second adhesive film (e) independently has an areal density of 100 g/m 2 to 300 g/m 2 and a thickness of 100 mm to 300 mm.

7 . The composite laminate as claimed in claim 1 , wherein the honeycomb core (d) is a honeycomb board composed of m-aramid paper or p-aramid paper, has a thickness of 2 mm to 300 mm, a cell size of 1.6 mm to 20.0 mm, a cell wall thickness of 0.1 mm to 0.3 mm, and a density of 24 Kg/m 3 to 200 Kg/m 3 .

8 . The composite laminate as claimed in claim 1 , wherein each tubular rivet has a flat head of 1.6 mm to 20.0 mm in diameter, a nail head thickness of 0.1 mm to 1.0 mm, a hollow tubular portion with an inner diameter of 1.2 mm to 19.6 mm, and a wall thickness of 0.2 mm to 0.9 mm, and the length substantially equals the thickness of the preform; and the tubular rivet is composed of metallic and non-metal materials, the metallic materials comprise copper, nickel, aluminum, titanium, an alloy thereof or stainless steel; and the non-metal materials comprise polyamide or polyester.

9 . The composite laminate as claimed in claim 1 , wherein the amount of the matrix derived from a liquid binder resin is 40 weight % to 150 weight % of the combined weight of the first skin layer (a) and the second skin layer (g).

10 . A method for manufacturing the composite laminate as claimed in claim 1 , comprising:

i) Sequentially stacking the layers: (b) a first barrier film, (c) a first adhesive film, (d) a honeycomb core, (e) a second adhesive film and (f) a second barrier film to form a preform;

ii) inserting a plurality of tubular rivets through the preform, set apart from each other by a distance of 30 mm to 200 mm;

iii) sealing around each tubular rivet with a self-expanding sealant;

iv) laying a first skin layer and a second skin layer over the outer surfaces of the preform obtained in step (iii) respectively; and

v) curing the preform, covered with the first and second skin lays, obtained in step (iv) by a vacuum-assisted resin infusion (VARI) method.

11 . The method as claimed in claim 10 , wherein the curing step is performed at 25° C. to 120° C. under a pressure of −0.08 MPa to −0.10 MPa for 1 hour to 24 hours.

12 . Articles or parts for transportation vehicles or movable homes, the articles or parts comprising the composite laminate as claimed in claim 1 , wherein the transportation vehicles include automobiles, ships, trains, magnetically levitated trains, unmanned aerial vehicles and aircrafts, and the movable homes include cabins and mobile homes.

13 . The use of the composite laminate as claimed in claim 1 for articles or parts for transportation vehicles or movable homes, wherein the transportation vehicles include automobiles, ships, trains, magnetically levitated trains, unmanned aerial vehicles and aircrafts, and the movable homes include cabins and mobile homes.

14 . A composite laminate comprising:

a preform sandwiched between a first fibrous skin layer and a second fibrous skin layer, wherein the preform comprises in order:

a first barrier film,

a first adhesive film,

a honeycomb core,

a second adhesive film,

a second barrier film;

wherein the preform further comprises a plurality of tubular rivets inserted through the thickness of the preform and having a length substantially equal to the thickness of the preform, the rivets being set apart from each other at a distance of 30 mm to 200 mm;

wherein a self-expanding sealant is sealed around the tubular rivets within the cells of the honeycomb core; and

wherein a matrix derived from a liquid resin comprising phenolic resin, epoxy resin, unsaturated polyester resin, vinyl ester resin, or combinations thereof is infused into the first fibrous skin layer and the second fibrous skin layer.

15 . The composite laminate of claim 14 , wherein

each of the first fibrous skin layer and the second fibrous skin layer independently comprises at least one reinforcing fabric, the fabric comprising glass fibers, carbon fibers, aramid fibers, or combinations thereof;

each of the first barrier film and the second barrier film independently comprises ethylene (meth)acrylate, anhydride-modified ethylene (meth)acrylate, ethylene vinyl acetate, anhydride-modified ethylene vinyl acetate, ethylene-acid ionomer, polyamide, polyurethane, polyester, polyimide, or combinations thereof;

each of the first adhesive film and the second adhesive film independently comprises epoxy resin, acrylate resin, or polyurethane resin, the resin having a glass transition temperature of 60° C. to 160° C.;

the honeycomb core comprises aramid, polycarbonate, polypropylene, steel, aluminum, aluminum alloy, or glass fiber; and

the self-expanding sealant is of expandable polystyrene or expandable polyurethane.

16 . The composite laminate of claim 14 , having a total thickness of 5 mm to 300 mm, and an areal density of from 0.35 Kg/m 2 to 20 Kg/m 2 .

17 . The composite laminate of claim 15 , wherein each reinforcing fabric has an areal density of 20 g/m 2 to 660 g/m 2 and is a woven fabric or a unidirectional fabric or a non-woven fabric.

18 . The composite laminate of claim 14 , wherein each of the first barrier film and the second barrier film independently has an areal density of 20 g/m 2 to 100 g/m 2 and a thickness of 20 μm to 100 μm.

19 . The composite laminate of claim 15 , wherein the honeycomb core comprises m-aramid paper or p-aramid paper and has a thickness of 2 mm to 300 mm, a cell size of 3.2 mm to 9.6 mm, a cell wall thickness of 0.1 mm to 0.3 mm, and a density of 24 Kg/m 3 to 200 Kg/m 3 .

20 . The composite laminate of claim 14 , wherein the amount of infused liquid resin is from 40 weight % to 150 weight % of the weight of dry fabric of the first skin layer and the second skin layer.