Rotary wing aircraft with a structural arrangement that comprises an electrically conductive connection

Patent metadata

Field	Value
Publication number	US-10507491-B2
Application number	US-201715716635-A
Country	US
Kind code	B2
Filing date	Sep 27, 2017
Priority date	Sep 27, 2016
Publication date	Dec 17, 2019
Grant date	Dec 17, 2019

Abstract

A rotary wing aircraft that comprises a structural arrangement with at least one first fiber reinforced polymer component and at least one second fiber reinforced polymer component that are spaced apart from each other by an interspace and that are rigidly attached to an associated structural component, wherein the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component are at least partly interconnected by means of an electrically conductive connection, and wherein the electrically conductive connection comprises at least one sprayed layer of electrically conductive particles, the at least one sprayed layer of electrically conductive particles being provided in the interspace.

First claim

What is claimed is:

1. A structural arrangement with at least one first fiber reinforced polymer component and at least one second fiber reinforced polymer component that are spaced apart from each other by an interspace and that are rigidly attached to an associated structural component, wherein the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component are at least partly interconnected by means of an electrically conductive connection,
wherein the electrically conductive connection comprises at least one sprayed layer formed by spraying of electrically conductive particles, the at least one sprayed layer of electrically conductive particles being provided in the interspace, the at least one first fiber reinforced polymer component is electro-conductively connected to a first electrically conductive foil and the at least one second fiber reinforced polymer component is electro-conductively connected to a second electrically conductive foil, the at least one sprayed layer of electrically conductive particles being at least partly formed between the first and second electrically conductive foils and the associated structural component being one of a joggled panel, shell, stringer, rib, frame and beam of a rotary wing aircraft and that the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component being implemented as panels or shells of the rotary wing aircraft, with the interspace exhibiting a width that is comprised in a range between 1 mm and 10 mm.

2. The structural arrangement of claim 1 , wherein the at least one sprayed layer of electrically conductive particles fills the interspace at least partly.

3. The structural arrangement of claim 1 ,
wherein the first and second electrically conductive foils are separated in the interspace by at least one slot, the at least one sprayed layer of electrically conductive particles being provided for bridging the at least one slot.

4. The structural arrangement of claim 3 ,
wherein the first electrically conductive foil is at least approximately L-, C- or Z-shaped.

5. The structural arrangement of claim 1 , wherein the second electrically conductive foil is at least approximately L- or C-shaped.

6. The structural arrangement of claim 1 , wherein the associated structural component is connected to a third electrically conductive foil, the third electrically conductive foil being electro-conductively connected to the first electrically conductive foil and the second electrically conductive foil.

7. The structural arrangement of claim 6 ,
wherein the third electrically conductive foil is at least approximately plate-shaped.

8. The structural arrangement of claim 1 ,
wherein the electrically conductive connection exhibits an electrical resistance of less than 1 mΩ between the first electrically conductive foil and the second electrically conductive foil.

9. The structural arrangement of claim 1 ,
wherein the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component are rigidly attached to the associated structural component by means of associated fixation means that comprise at least one of screws, rivets, bolts and structural bonding.

10. A method of manufacturing a structural arrangement from at least one first fiber reinforced polymer component, at least one second fiber reinforced polymer component and an associated structural component, the method comprising:
providing the at least one first fiber reinforced polymer component at least partly with a first electrically conductive foil and the at least one second fiber reinforced polymer component at least partly with a second electrically conductive foil;
rigidly attaching the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component to the associated structural component, wherein an interspace is created that spaces the at least one first fiber reinforced polymer component and the at least one second fiber reinforced polymer component apart from each other, wherein a slot is at least partly created between the first electrically conductive foil and the second electrically conductive foil; and
spraying electrically conductive particles in the interspace onto the slot for creating a sprayed layer of electrically conductive particles, the at least one sprayed layer of electrically conductive particles being provided for electro-conductively interconnecting at least partly the first electrically conductive foil and the second electrically conductive foil.

11. The method of claim 10 ,
wherein spraying of the electrically conductive particles is performed by means of a thermal spray technology.

12. The method of claim 11 ,
wherein the thermal spray technology comprises a cold gas spray method.

13. A rotary wing aircraft with a structural arrangement according to claim 1 .

Assignees

• Airbus Helicopters Deutschland GmbH

Inventors

• Rack Andreas
• Rosplesch David
• Jonke Dietrich

Classifications

• B29C65/562 Primary

  using extra joining elements, i.e. which are not integral with the parts to be joined (using plastic snap elements B29C65/58; using plastic rivets B29C65/601) · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title

• C23C24/04

  Impact or kinetic deposition of particles · CPC title

• B05D1/025

  using gas close to its critical state · CPC title

• B64C1/12

  Construction or attachment of skin panels · CPC title