Propeller blades having icephobic coating

Patent metadata

Field	Value
Publication number	US-10486795-B2
Application number	US-201715401140-A
Country	US
Kind code	B2
Filing date	Jan 9, 2017
Priority date	Jan 29, 2016
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

A propeller blade for rotation about a hub assembly is provided, wherein the propeller blade defines a radial direction along its length from a blade root to a blade tip, the propeller blade including a radially inner region, a radially outer region located between the blade root and the blade tip at a position where rotational forces on the blade are sufficient, in use, to remove ice from an uncoated blade, a coating disposed at least along a leading edge of the propeller blade, the coating including an icephobic material, wherein the coating extends along the propeller blade from the radially inner region to the radially outer region. The coating overlays a substrate portion of the propeller blade defining a color visually indicative of wear of the coating.

First claim

What is claimed is:

1. A propeller blade, comprising:
a radially inner region located between a propeller blade root and a portion of a length of the propeller blade;
a radially outer region located between the radially inner region and a propeller blade tip; and
a coating disposed at least along a leading edge of the propeller blade over the radially inner region and at least a portion of the radially outer region, wherein the coating includes an icephobic material;
wherein a first substrate portion defining a first color is located within the radially inner region and a second substrate portion defining a second color is located within the radially outer region.

2. The propeller blade of claim 1 , wherein the coating includes the first substrate portion or the second substrate portion.

3. The propeller blade of claim 1 wherein the coating further comprises a semi-transparent coating.

4. The propeller blade of claim 3 wherein the semi-transparent coating is selected to visually indicate wear in the icephobic material by revealing at least a portion of one of the first or second colors through the semi-transparent coating corresponding to the wear.

5. The propeller blade of claim 4 wherein the semi-transparent coating is further selected to visually indicate a level of wear in the icephobic material by revealing a visual gradient of one of the first or second colors, wherein the visual gradient indicates the level of wear.

6. The propeller blade of claim 1 wherein the coating extends along an entire length of the propeller blade.

7. The propeller blade of claim 1 wherein the coating further comprises a cohesive coefficient that varies radially along the length of the propeller blade.

8. The propeller blade of claim 7 , wherein the cohesive coefficient increases with increasing radius from the propeller blade root.

9. The propeller blade of claim 1 , wherein the coating extends from the leading edge of the propeller blade to approximately twenty-five percent along a chord length of the propeller blade.

10. The propeller blade of claim 1 , wherein the coating further comprises a set of layers.

11. The propeller blade of claim 10 , wherein the coating further comprises at least one of an adhesive layer, a polymer layer, or a neoprene layer in addition to the icephobic material.

12. The propeller blade of claim 10 wherein at least a subset of the set of layers defines at least one of the first substrate or second substrate, and the icephobic material defines a third color, different from the first and second colors and wherein the third color is selected to visually indicate wear in the icephobic material by revealing at least a portion of the first or second color corresponding to the wear.

13. A method of inspecting a propeller blade, comprising:
inspecting a radially inner region of the propeller blade, located between a blade root and fifty percent of a total length of the propeller blade, wherein the radially inner region of the propeller blade includes an icephobic coating overlying a first substrate having a first color;
inspecting a radially outer region of the propeller blade, located between the radially inner region and a blade tip of the propeller blade, wherein at least a portion of the radially outer region includes the icephobic coating overlying a second substrate having a second color;
identifying a portion of the propeller blade wherein at least one of the first color or the second color has been revealed;
comparing the identified portion of the propeller blade to an inspection criteria; and
when the comparison of the identified portion of the propeller blade satisfies the inspection criteria, initiating at least one of a maintenance operation or replacement of the propeller blade.

14. The method of claim 13 wherein the inspection criteria include a visual set of icephobic coating wear thresholds.

15. The method of claim 14 wherein the inspection criteria include a color gradient from the icephobic coating to one of the first color or the second color, and wherein the color gradient corresponds to the set of icephobic coating wear thresholds.

16. The method of claim 14 wherein the inspection criteria further comprise a first visual inspection criteria related to the inner region and a second visual inspection criteria related to the outer region, wherein the first visual inspection criteria and the second visual inspection criteria are different.

17. The method of claim 13 wherein the initiating the maintenance operation includes applying an icephobic coating to the identified portion of the propeller blade.

18. A propeller blade, comprising:
a radially inner region located between a blade root and fifty percent of the total length of the propeller blade;
a radially outer region located between the radially inner region and a blade tip of the propeller blade, where the radially outer region is located on the propeller blade where rotational forces on the propeller blade are sufficient, in use, to remove ice from an uncoated blade; and
a coating including an icephobic material disposed at least along a leading edge of the propeller blade over at least a portion of the radially inner region and at least a portion of the radially outer region;
wherein a first substrate portion defining a first color is located within the radially inner region, a second substrate portion defining a second color is located within the radially outer region, and the coating defines a third color, different from the first color and the second color, and wherein the coating is selected to reveal at least one of the first or second colors in response to wear.

19. The propeller blade of claim 18 , wherein the coating includes the first substrate portion or the second substrate portion.

20. The propeller blade of claim 18 wherein the coating further comprises a semi-transparent coating.

Assignees

• Ge Aviat Systems Ltd

Inventors

• Methven Paul Nicholas

Classifications

• B64C11/205 Primary

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

• B64D15/00

  De-icing or preventing icing on exterior surfaces of aircraft · CPC title

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• B64C11/20

  Constructional features · CPC title