IP Library › Granted Patent US 10,336,435
Granted Patent B2
US 10,336,435 · App. 15/118,548 · Granted Jul 2, 2019

Erosion resistant blade and blade coating

Inventors: Rajesh S. Kumar (Ellington, CT); Robert A. Barth (South Windsor, CT); Wayde R. Schmidt (Pomfret Center, CT)
Assignee: SIKORSKY AIRCRAFT CORPORATION
B64C11/205B32B3/12B32B5/028B32B5/18B32B15/08B32B15/095B32B27/065B32B27/12B32B27/283B32B27/40C08G18/61C09D175/04C09D183/04C09D183/10B32B2250/03B32B2250/04B32B2255/26B32B2266/0278B32B2266/06B32B2307/554B32B2307/584B32B2307/712B32B2307/714B32B2405/00B32B2603/00B32B2605/18C08G77/458
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Quick Facts
Patent No.
US 10,336,435
App. No.
15/118,548
Granted
Jul 2, 2019
Kind
B2
Abstract

Airfoil blades are disclosed having a coating thereon that includes a polyurethane, a polysiloxane, and a linking agent that promotes a connection between the polyurethane and the polysiloxane.

Claims (11)

1. An airfoil blade having a coating disposed on a leading edge thereof, the coating comprising a polyurethane, a polysiloxane, and a linking agent that promotes a connection between the polyurethane and the polysiloxane; wherein the polyurethane and the polysiloxane are in separate layers with the linking agent disposed between the polyurethane layer and the polysiloxane layer.

2. The airfoil blade of claim 1 , wherein the linking agent is a polyurethane-polysiloxane copolymer.

3. The airfoil blade of claim 1 , wherein the linking agent is a coupling agent comprising functional groups reactive with groups on the polyurethane and functional groups reactive with groups on the polysiloxane.

4. The airfoil blade of claim 3 , wherein the coupling agent is a functionalized particle.

5. The airfoil blade of claim 1 , wherein the linking agent is a layer comprising a polyurethane-polysiloxane copolymer, disposed between the polyurethane layer and the polysiloxane layer.

6. The airfoil blade of claim 1 , wherein the linking agent is a multi-cellular structure disposed between the polyurethane layer and the polysiloxane layer.

7. The airfoil blade of claim 6 , wherein the multi-cellular structure is a polymer foam.

8. The airfoil blade of claim 7 , wherein the polymer foam is a polyurethane foam.

9. The airfoil blade of claim 1 , wherein the airfoil blade is a helicopter rotor blade.

10. The airfoil blade of claim 1 , wherein the airfoil blade further comprises polysiloxane layer on a surface of the airfoil blade away from of the leading edge.

11. An airfoil blade having a coating disposed on a leading edge thereof, the coating comprising a polyurethane, a polysiloxane, and a linking agent that promotes a connection between the polyurethane and the polysiloxane, wherein the coating comprises polyurethane segments and polysiloxane segments in a co-planar configuration in the same layer or planar segment.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 12, 2016
From: KUMAR, RAJESH S.; BARTH, ROBERT A.; SCHMIDT, WAYDE R.
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 039414/0911 →
Continuity (1)
Related Publication 20170043860A1 · Feb 16, 2017
Cited By (1)
US 12,351,342