Protective mat for leading edges of airfoil elements

Patent metadata

Field	Value
Publication number	US-10266247-B2
Application number	US-201514634730-A
Country	US
Kind code	B2
Filing date	Feb 28, 2015
Priority date	Mar 3, 2014
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

A device for protecting an airfoil element made of a complex comprising a polymer film, a metal strip deposited on a part of the polymer film and an adhesive element to attach the polymer film on the airfoil element. The polymer film forms a protection against sand abrasion. The metal strip forms a protection against water abrasion of the airfoil element on which the complex is attached.

First claim

The invention claimed is:

1. An airfoil element protection device, comprising:
a complex comprising a polymer film, a metal strip deposited on a portion of the polymer film, and an adhesive element to bond the polymer film to an airfoil element,
wherein the polymer film forms a protection against sand erosion and the metal strip forms a protection against water erosion of the airfoil element to which the airfoil element protection device is bonded thereto;
wherein the complex is built as an adhesive standalone foil to be bonded on the airfoil element, said foil being formed in counter-relief to fit a profile of a leading edge of the airfoil element comprising areas of low incidence and areas of high incidence, the polymer film being shaped to cover one or more areas of low incidence of the airfoil element, the metal strip being shaped to cover only an area of high incidence of the airfoil element so that the metal strip is disposed between polymer strips,
wherein the polymer film has a thickness between 50 and 350 μm, and wherein the metal strip has a thickness between 20 and 150 μm.

2. The airfoil element protection device according to claim 1 , wherein the metal strip is bonded to the polymer film.

3. The airfoil element protection device according to claim 1 , wherein the metal strip is welded to the polymer film.

4. The airfoil element protection device according to claim 1 , wherein the metal strip is embedded in the polymer film.

5. The airfoil element protection device according to claim 4 , wherein the metal strip is embedded by hot application to the polymer film.

6. The airfoil element protection device according to claim 1 , wherein the metal strip comprises a base configured to be bonded to the airfoil element, sheets of the polymer film being positioned on either side of the metal strip.

7. The airfoil element protection device according to claim 1 , wherein the polymer film comprises a lower sheet on which the metal strip is laid and two upper sheets joined together with the lower sheet on either side of the metal strip.

8. The airfoil element protection device according to claim 2 , further comprising a sealing varnish covering an interface area between the metal strip and the polymer film.

9. The airfoil element protection device according to claim 1 , wherein edges of the metal strip extended by the polymer film are bevelled edges.

10. The airfoil element protection system comprising the airfoil element device according to claim 1 accompanied by an assembly jig and forms, with this jig, a kit that can be adapted outside of a factory.

11. The airfoil element covered with the airfoil element protection device as claimed in claim 1 , wherein the metal strip covers the leading edge of the airfoil element and the polymer film covers a lower surface portion and an upper surface portion of the airfoil element around the leading edge.

12. A helicopter blade covered with the airfoil element protection device according to claim 1 , wherein the metal strip covers the leading edge of the helicopter blade and the polymer film covers a lower surface portion and an upper surface portion of the helicopter blade around the leading edge.

13. The airfoil element protection device according to claim 1 , wherein the adhesive element has a thickness of approximately 50 μm.

14. The airfoil element protection device according to claim 1 , wherein the thickness of the polymer film is between 50 and 300 μm.

15. The airfoil element protection device according to claim 1 , wherein the thickness of the metal strip is between 20 and 100 μm.

16. The airfoil element protection device according to claim 1 , wherein the metal strip has a width between 2 to 10 cm.

17. The airfoil element protection device according to claim 16 , wherein the width of the metal strip on a root side is greater than the width of the metal strip on a blade tip side.

18. The airfoil element protection device according to claim 16 , wherein a width of the polymer film on a root side is greater than the width of the polymer film on a blade tip side.

19. An airfoil element protection device, comprising:
a complex comprising a polymer film, a metal strip deposited on a portion of the polymer film, and an adhesive element to bond the polymer film to an airfoil element,
wherein the polymer film forms a protection against sand erosion and the metal strip forms a protection against water erosion of the airfoil element to which the airfoil element protection device is bonded thereto;
wherein the complex is built as an adhesive standalone foil to be bonded on the airfoil element,
said foil being formed in counter-relief to fit a profile of a leading edge of the airfoil element comprising areas of low incidence and an area of high incidence,
the polymer film being shaped to cover one or more areas of low incidence of the airfoil element,
the metal strip only covering the area of high incidence of the airfoil element so that the metal strip is disposed between polymer strips.

20. The airfoil element protection device of claim 19 wherein the metal strip has a width between 2 to 10 cm.

Assignees

• Airbus Sas
• Airbus Helicopters

Inventors

• Aliaga Daniel
• Guillou Marie-Paule
• Campazzi Elisa
• Navarre Thomas

Classifications

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• B64C11/205 Primary

  for protecting blades, e.g. coating · CPC title

• B64C27/473

  Constructional features · CPC title

• Y02T50/673

  Cross-Sectional Technologies · mapped topic