IP Library Granted Patent US 10,144,200
Granted Patent B2
US 10,144,200 · App. 14/363,488 · Granted Dec 4, 2018

Fiber-reinforced composite material with improved fire resistance, and structural component made thereof

Inventors: Hans Luinge (DW Hengelo, NL); Matthias Schuett (Ottobrunn, DE); Geoff Gibson (Newcastle upon Tyne, GB)
Assignee: Airbus Defence and Space GmbH
B32B27/08B32B3/266B32B5/26B32B5/28B32B7/02B32B27/00B32B27/12B32B27/18B32B27/281B32B27/285B32B27/286B32B2250/42B32B2260/023B32B2260/046B32B2264/02B32B2264/06B32B2264/10B32B2264/104B32B2264/108B32B2305/07B32B2305/30B32B2307/3065B32B2605/18Y10T428/269Y10T428/31511
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Quick Facts
Patent No.
US 10,144,200
App. No.
14/363,488
Granted
Dec 4, 2018
Kind
B2
Abstract

A fiber-reinforced composite material includes a bulk portion with a bulk matrix having reinforcing fibers embedded therein, and a surface portion with a plurality of laminated first layers serving as “expanding layers”, which expand and/or delaminate during fire impact. The surface portion also includes a plurality of laminated second layers different from the first layers and serving as “barrier layers”. The expanding layers and barrier layers can be arranged in an alternating sequence.

Claims (21)

1. A fiber-reinforced composite material, comprising:

a multilayer bulk portion forming a bulk of the fiber-reinforced composite material and comprising a plurality of fiber material layers embedded in a bulk matrix; and

a surface portion comprising a plurality of laminated first layers structurally configured to expand or delaminate during fire impact and a plurality of laminated second layers different from the plurality of laminated first layers, wherein the plurality of laminated first layers are arranged in an alternating sequence with the plurality of laminated second layers,

wherein at least one of the laminated first layers comprises a thermoplastic film, the thermoplastic being a polymer selected from a group consisting of Polyimide, Polyetherimide, Polyether sulfone, Polyamide, Polyamide-imide, Polysulfone, Polyphenylsulfone, Polyetherketone, Polyethylene terephthalate, Polyethylene, Polyester, Polyetherester, Polyesteramide, Polymethylmethacrylate, Polypropylene, Polystyrene, Polyvinylchloride or mixtures thereof.

2. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers comprises fibers.

3. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers comprises an intumescent modifier.

4. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers has a thickness in a range of 5 to 300 μm.

5. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers has a thickness in a range of 10 to 200 μm.

6. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers has a thickness in a range of 20 to 130 μm.

7. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated first layers has a thickness of approximately 125 μm.

8. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated second layers comprises a surface matrix with embedded reinforcing fibers.

9. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated second layers comprises a polymer.

10. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated second layers comprises a resin matrix with inorganic particles dispersed in the resin matrix.

11. The fiber-reinforced composite material of claim 1 , wherein at least one of the plurality of laminated second layers comprises a resin matrix with organic particles dispersed in the resin matrix.

12. The fiber-reinforced composite material of claim 1 , wherein the plurality of laminated first layers are configured to expand or delaminate during fire impact above 100%.

13. A structural component, comprising:

a fiber-reinforced composite material, comprising

a multilayer bulk portion forming a bulk of the fiber-reinforced composite material and comprising a plurality of fiber material layers embedded in a bulk matrix; and

a surface portion comprising a plurality of laminated first layers structurally configured to expand or delaminate during fire impact and a plurality of laminated second layers different from the plurality of laminated first layers, wherein the plurality of laminated first layers are arranged in an alternating sequence with the plurality of laminated second layers,

wherein at least one of the laminated first layers comprises a thermoplastic film, the thermoplastic being a polymer selected from a group consisting of Polyimide, Polyetherimide, Polyether sulfone, Polyamide, Polyamide-imide, Polysulfone, Polyphenylsulfone, Polyetherketone, Polyethylene terephthalate, Polyethylene, Polyester, Polyetherester, Polyesteramide, Polymethylmethacrylate, Polypropylene, Polystyrene, Polyvinylchloride or mixtures thereof, and

wherein structural component is a component of an aerial vehicle.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2018
From: THE UNIVERSITY OF NEWCASTLE UPON TYNE
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 046130/0286 →
CHANGE OF NAME Recorded Mar 9, 2018
From: EADS DEUTSCHLAND GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 045543/0523 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 26, 2014
From: LUINGE, HANS; SCHUETT, MATTHIAS; GIBSON, GEOFF
To: EADS DEUTSCHLAND GMBH; THE UNIVERSITY OF NEWCASTLE UPON TYNE
Reel/Frame 033831/0328 →
Priority Claims (1)
EP 11009717 · Dec 9, 2011 · regional
Continuity (1)
Related Publication 20150174866A1 · Jun 25, 2015
Cited By (1)
US 12,291,014