IP Library Granted Patent US 10,410,759
Granted Patent B2
US 10,410,759 · App. 15/527,900 · Granted Sep 10, 2019

Conductive device intended to be mounted on the surface of parts made of composite materials

Inventors: Didier Mesnage (Saint Cloud, FR); Thierry Pelegrin (Viroflay, FR)
Assignee: AIRBUS
H01B7/0009B29C70/885B32B15/088B32B15/20B64C1/06H01B7/02H01B7/04B29K2077/00B29K2105/243B29K2309/08B29L2031/3076B32B2262/101B32B2307/202B32B2605/18B64C1/00B64C2001/0072Y02T50/43
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Quick Facts
Patent No.
US 10,410,759
App. No.
15/527,900
Granted
Sep 10, 2019
Kind
B2
Abstract

A conductive device to form electrical connections on the surface of a structure made of composite material. The device includes a thin interface layer having a face via which the device is fixed to the surface of the structure made of composite material. A conductive metal element is placed on the face of the interface layer opposite the face making contact with the surface of the structure. The conductive element is configured to be able to undergo tensile and compressive stresses without damage. A protective layer is configured to protect the conductive element from attack from the environment surrounding the structure. These various elements are arranged relative to one another such that the length of the conductive element can vary as a function of temperature variations independently of the amplitude of the variations undergone by the structure on which the device is mounted.

Claims (18)

1. A conducting device to install an electrical link on a surface of a composite material structure, comprising:

an interface layer exhibiting a face by which the conductive device is fixed to the surface of the composite material structure;

a conducting metallic element located on the face of the interface layer opposite to a face in contact with the surface of the composite material structure, said conducting metallic element being configured to undergo compressive and extensile stresses without damage;

a protective layer configured to protect the conducting metallic element from attacks of an exterior medium surrounding the composite material structure;

wherein the interface layer is made of a composite material and the conducting device fabricated and mounted on the composite material structure is a semi-finished flexible product, a fabrication of the conducting device comprises a pre-polymerization operation such that a total polymerization of the conducting device is performed post-mounting of conducting device on the composite material structure; and

wherein said conducting metallic element is a metallic braid.

2. The conducting device as claimed in claim 1 , wherein the protective layer comprises an envelope covering a portion of the conducting device in contact with the exterior medium, said envelope defining with the interface layer, an internal space in which the conducting metallic element is housed.

3. The conducting device as claimed in claim 1 , wherein the protective layer is made of a composite material to exhibit a deformation visible by an observer in a zone of a low-energy impact.

4. The conducting device as claimed claim 1 , wherein the conducting element is a set of superposed leaves of foil material.

5. A conducting device to install an electrical link on a surface of a composite material structure, comprising:

an interface layer exhibiting a face by which the conductive device is fixed to the surface of the composite material structure;

a conducting metallic element located on the face of the interface layer opposite to a face in contact with the surface of the composite material structure, said conducting metallic element being configured to undergo compressive and extensile stresses without damage;

a protective layer configured to protect the conducting metallic element from attacks of an exterior medium surrounding the composite material structure;

wherein the interface layer is made of an elastomer and the conducting device fabricated and mounted on the composite material structure is a semi-finished flexible product, a fabrication of the conducting device comprises a vulcanization operation such that a total polymerization of the conducting device is performed post-mounting of conducting device on the composite material structure; and

wherein the conducting metallic element is a metallic braid.

6. The conducting device as claimed in claim 5 , wherein the protective layer comprises an envelope covering a portion of the conducting device in contact with the exterior medium, said envelope defining with the interface layer, an internal space in which the conducting metallic element is housed.

7. The conducting device as claimed in claim 5 , wherein the protective layer is made of a composite material to exhibit a deformation visible by an observer in a zone of a low-energy impact.

8. The conducting device as claimed claim 5 , wherein the conducting element is a set of superposed leaves of foil material.

Assignments (4)
CHANGE OF NAME Recorded Feb 23, 2022
From: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
To: AIRBUS GROUP SAS
Reel/Frame 059083/0609 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 23, 2022
From: PELEGRIN, THIERRY
To: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
Reel/Frame 059235/0623 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 3, 2019
From: MESNAGE, DIDIER
To: AIRBUS GROUP SAS
Reel/Frame 049353/0472 →
MERGER Recorded Jun 3, 2019
From: AIRBUS GROUP SAS
To: AIRBUS
Reel/Frame 049353/0520 →
Priority Claims (1)
FR 14 61289 · Nov 21, 2014 · national
Continuity (1)
Related Publication 20180342332A1 · Nov 29, 2018