Cleaning assembly for leading edges of airfoils

Patent metadata

Field	Value
Publication number	US-10640236-B2
Application number	US-201715784790-A
Country	US
Kind code	B2
Filing date	Oct 16, 2017
Priority date	Oct 19, 2016
Publication date	May 5, 2020
Grant date	May 5, 2020

Abstract

A cleaning assembly for leading edges of airfoils, in particular airfoil profiles of aircraft or spacecraft, has a cleaning device that is provided with at least one cleaning member and is intended for applying mechanical pressure to a planar region of an airfoil, and has a drive having at least one drive element, which drive moves the cleaning device along the surface to be cleaned. It is proposed to adhesively hold the cleaning device on the airfoil by the at least one cleaning member and/or for the at least one cleaning member to have a sticky surface and for the at least one cleaning member to be dimensionally stable and have flexible contours.

First claim

The invention claimed is:

1. A cleaning assembly for cleaning a leading edge of an airfoil, the cleaning assembly comprising:
a cleaning device comprising at least one cleaning member, which is dimensionally stable and has flexible contours, for applying mechanical pressure to a planar region of the airfoil; and
a drive having at least one drive element on either side of the leading edge of the airfoil, wherein the drive is configured to move the cleaning device along the leading edge of the airfoil to be cleaned;
wherein the cleaning device is adhesively held onto the leading edge of the airfoil by the at least one cleaning member.

2. The cleaning assembly of claim 1 , wherein the cleaning device encompasses at least some regions of the leading edge of the airfoil by the at least one cleaning member when in a use position.

3. The cleaning assembly of claim 1 , wherein the cleaning device comprises a securing structure.

4. The cleaning assembly of claim 1 , comprising a flexible drive member that connects and is arranged between the two drive elements.

5. The cleaning assembly of claim 1 , wherein the drive elements are each connected to a support member on each side of the airfoil.

6. The cleaning assembly of claim 5 , wherein the support member is in a form of a bar.

7. The cleaning assembly of claim 1 , wherein the drive elements are drive motors.

8. The cleaning assembly of claim 1 , wherein the at least one cleaning member comprises a strip that extends between two drive members spaced apart from one another along an edge of the airfoil.

9. The cleaning assembly of claim 8 , wherein the cleaning member comprises a strip that forms a continuous belt that is connected at its ends, in a manner of a conveyor belt.

10. The cleaning assembly of claim 1 , wherein the cleaning device comprises a plurality of cleaning members.

11. The cleaning assembly of claim 10 , wherein the cleaning members are arranged regularly.

12. The cleaning assembly of claim 1 , comprising a plurality of cleaning members that are able to be arranged to form a row in a manner of a chain with adjacent cleaning members, wherein the row extends between opposite support members.

13. The cleaning assembly of claim 1 , wherein the cleaning device comprises a plurality of rows of cleaning members.

14. The cleaning assembly of claim 1 , wherein the cleaning device comprises a cover device that has a flexible shape and is configured to follow an adjustment of a shape of the cleaning device to the airfoil.

15. The cleaning assembly of claim 1 , wherein the cleaning device has a stabilizing surface.

16. The cleaning assembly of claim 15 , wherein the stabilizing surface is arranged on a cover device.

17. The cleaning assembly of claim 1 , wherein the cleaning device comprises at least one sensor configured to determine a position of the cleaning device on the airfoil.

18. A cleaning assembly for cleaning a leading edge of an airfoil, the cleaning assembly comprising:
a cleaning device that comprises at least one cleaning member, which is dimensionally stable and has flexible contours, for applying mechanical pressure to a planar region of the airfoil; and
a drive having at least one drive element on either side of the leading edge of the airfoil, wherein drive is configured to move the cleaning device along the leading edge of the airfoil to be cleaned;
wherein the at least one cleaning member has a sticky surface.

19. A method for operating a cleaning assembly to clean a leading edge of an airfoil, comprising at least:
providing a driven cleaning device having at least one sticky cleaning member, which is dimensionally stable and has flexible contours;
arranging the cleaning device on the airfoil and establishing adhesive contact with the leading edge of the airfoil to be cleaned; and
moving, using a drive having at least one drive element on either side of the leading edge of the airfoil, the cleaning device along the leading edge of the airfoil to clean the leading edge of the airfoil.

20. The cleaning assembly of claim 7 , wherein the drive elements are brushless electric motors.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Storm Stefan
• Kirn Johannes

Classifications

• B64F5/30 Primary

  Cleaning aircraft · CPC title

• F01D25/002 Primary

  Cleaning of turbomachines · CPC title

• B08B13/00

  Accessories or details of general applicability for machines or apparatus for cleaning · CPC title

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title

• B08B7/0028

  by adhesive surfaces · CPC title