Method for producing a surface structure with lightning protection, and surface structure which can be produced in this way

Patent metadata

Field	Value
Publication number	US-9623984-B2
Application number	US-201214122426-A
Country	US
Kind code	B2
Filing date	May 25, 2012
Priority date	May 27, 2011
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

A method for producing a surface structure with a lightning strike protective system involves providing a support structure based on a fiber-reinforced composite material. At least one arrangement of a lightning strike protective material made from or with a conductive material is applied onto the support structure so that the lightning strike protective material arrangement adheres to the support structure in such a way that it is held securely in its position. A cover material is applied in such a way that it embeds the at least one arrangement of a lightning strike protective material that is held securely in its position on the support structure, and the cover material is solidified.

First claim

The invention claimed is:

1. A method for producing a surface structure having a lightning strike protective system, said method comprising the steps:
a) providing a support structure of a fiber-reinforced composite material;
b) applying an arrangement of electrically conductive particles as the lightning triggering elements onto the support structure such that the electrically conductive particles adhere in a fixed position and in a particular arrangement and distribution on the support structure, thereby forming an arrangement of a lightning strike protective material;
c) applying a cover material in such a way that the applied arrangement of electrically conductive particles is embedded within the cover material and is held securely in position on the support structure; and
d) solidifying the applied cover material,
wherein the electrically conductive particles are positioned on the support structure prior to being embedded in the cover material.

2. The method of claim 1 , wherein step b) further comprises:
b 1) gluing the arrangement of the lightning strike protective material, which is formed by the particles, on the support structure using an adhesive.

3. The method of claim 2 , wherein step b1) further comprises:
b1b) applying the adhesive on the support structure in certain regions, in order to form a plurality of adhesive areas, or
b1c) applying the adhesive on the support structure at certain points.

4. The method of claim 2 , wherein the adhesive applied in step b1) is an electrically conductive adhesive.

5. The method of claim 1 , wherein the electrically conductive particles are selected from a group that includes fibers, carbon fibers, tubes, nanotubes, filaments, SIC filaments, graphite filaments, and metal pins.

6. The method of claim 1 , wherein step b) further comprises:
spraying metal pins onto the support structure.

7. The method of claim 6 , wherein the metal pins are composed of aluminum powder.

8. The method of claim 1 , wherein step a) further comprises:
producing a two-dimensional flat component substrate from a CFRP composite material.

9. The method of claim 8 , wherein the CFRP composite material is an epoxy resin reinforced with carbon fibers.

10. The method of claim 1 , wherein prior to step b) the support structure is provided on the surface, which is to be provided with the arrangement of the lightning strike protective material, with a felt made of conductive or non-conductive fibers as an intermediate layer between the fiber-reinforced composite material and the arrangement of the lightning strike protective material.

11. A method of manufacturing a component of an aircraft, the component having a surface structure with a lightning strike protective system, the method comprising the steps:
a) providing a support structure of a fiber-reinforced composite material;
b) applying an arrangement of electrically conductive particles as the lightning triggering elements onto the support structure such that the electrically conductive particles adhere in a fixed position and in a particular arrangement and distribution on the support structure, thereby forming an arrangement of a lightning strike protective material;
c) applying a cover material in such a way that the applied arrangement of electrically conductive particles is embedded within the cover material and is held securely in its position on the support structure; and
d) solidifying the applied cover material,
wherein the electrically conductive particles are positioned on the support structure prior to being embedded in the cover material, and wherein the surface structure is of the component of the aircraft.

12. An aircraft component with a surface structure having a lighting strike protective system, the surface structure comprising:
a support structure of a fiber-reinforced composite material;
an arrangement of electrically conductive particles as the lightning triggering elements applied onto the support structure such that the electrically conductive particles adhere in a fixed position and in a particular arrangement and distribution on the support structure, thereby forming an arrangement of a lightning strike protective material; and
a cover material applied to the arrangement of electrically conductive particles in such a way that the applied arrangement of electrically conductive particles is embedded within the cover material and is held securely in its position on the support structure,
wherein the cover material is solidified and wherein the electrically conductive particles are positioned on the support structure prior to being embedded in the cover material.

Assignees

• Steinwandel Juergen
• Englhart Martin
• Jonke Dietrich P
• Piringer Helmut
• Wulbrand Wilhelm
• Eads Deutschland Gmbh

Inventors

• Steinwandel Juergen
• Englhart Martin
• Jonke Dietrich P
• Piringer Helmut
• Wulbrand Wilhelm

Classifications

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• B64D45/02 Primary

  Lightning protectors; Static dischargers · CPC title

• B32B15/14

  next to a fibrous or filamentary layer · CPC title

• B29C70/885

  with incorporated metallic wires, nets, films or plates (as lost heating elements B29C35/0272, B29C61/0625) · CPC title