IP Library Granted Patent US 10,399,299
Granted Patent B2
US 10,399,299 · App. 14/719,568 · Granted Sep 3, 2019

Sandwich component and method for producing a sandwich component

Inventors: Jonas Gruenewald (Munich, DE); Patricia Parlevliet (Munich, DE)
Assignee: Airbus Defence and Space GmbH
B32B7/12B29B11/04B29B11/14B29C53/04B29C66/006B29C66/7254B32B3/00B32B3/12B32B5/00B32B5/02B32B5/10B32B7/00B32B7/04B32B19/02B32B19/04B32B19/048B32B25/00B32B25/02B32B25/04B32B25/16B32B27/00B32B27/06B32B27/08B32B27/12B32B27/18B32B27/28B32B27/281B32B27/285B32B27/288B32B27/30B32B27/302B32B27/32B32B27/36B32B37/144B32B37/18B32B38/0012B29K2071/00B29K2079/085B29K2671/00B29K2679/085B32B2250/05B32B2250/24B32B2250/40B32B2262/00B32B2274/00B32B2305/024B32B2305/08B32B2307/30B32B2307/50B32B2307/738B32B2371/00B32B2379/08B32B2605/00B32B2605/18Y10T156/1051Y10T428/24149Y10T428/31721
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Quick Facts
Patent No.
US 10,399,299
App. No.
14/719,568
Granted
Sep 3, 2019
Kind
B2
Abstract

A sandwich component and method of producing the sandwich component are provided wherein the sandwich component has a first cover layer, a second cover layer, and a core disposed therebetween. In the sandwich component, the cover layers are each formed from an outer layer made of a fiber-reinforced high-melting-point thermoplast material and, fused therewith, an inner layer made of a low-melting-point thermoplast material. The core has outer layers, each of which is formed from a low-melting-point thermoplast material, and an inner structure, which is formed entirely or partially from a high-melting-point thermoplast material. The inner layers of the cover layers were each fused with one of the outer layers of the core.

Claims (9)

1. A sandwich component, comprising:

a first cover layer, a second cover layer, and a core disposed therebetween, wherein

the first and second cover layers are each formed from an outer layer made of a fiber-reinforced high-melting-point thermoplast material and, fused therewith, an inner layer made of a low-melting-point thermoplast material,

the core has outer layers each of which is formed from a low-melting-point thermoplast material, and an inner structure, which is formed entirely or partially from a high-melting-point thermoplast material,

the inner layers of the cover layers are each fused with one of the outer layers of the core, and

the core is a honeycomb core, which is a folded honeycomb structure, which is provided by reshaping a film of high-melting-point thermoplast material coated with a low-melting-point thermoplast material, this coating being carried out only in regions, according to the specific shaping process, such that the low-melting-point thermoplast material is present on the finished folded honeycomb structure only in the region of the folded honeycomb structure cover layers, but not in the region of the inner structure of the folded honeycomb structure.

2. The sandwich component according to claim 1 , wherein the low-melting-point thermoplast materials are identical for an inner layer of a cover layer and the outer layer of the core fused therewith.

3. The sandwich component according to claim 2 , wherein at least one of the thermoplast materials is selected from the group comprising: ABS, PA, PBT, PC, PEEK, PEI, PES, PET, PP, PPS, PPSU, PSU.

4. The sandwich component according to claim 1 , wherein at least one of the thermoplast materials is selected from the group comprising: ABS, PA, PBT, PC, PEEK, PEI, PES, PET, PP, PPS, PPSU, PSU.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 17, 2017
From: GRUENEWALD, JONAS; PARLEVLIET, PATRICIA
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 043325/0071 →
Priority Claims (1)
DE 10 2014 007 510 · May 23, 2014 · national
Continuity (1)
Related Publication 20150336352A1 · Nov 26, 2015
Cited By (2)
US 12,246,511 US 12,611,836