Metallic dimpled doubler

Patent metadata

Field	Value
Publication number	US-10351229-B2
Application number	US-201515303674-A
Country	US
Kind code	B2
Filing date	Mar 12, 2015
Priority date	May 15, 2014
Publication date	Jul 16, 2019
Grant date	Jul 16, 2019

Abstract

A rotor blade is provided. The rotor blade includes a blade portion, a tip cap formed to define a dimple, a fastener and a doubler. The fastener includes a flat-headed shaft and is disposable such that the flat-headed shaft extends through the blade portion and the tip cap at the dimple. The fastener is configured to urge the blade portion toward the tip cap. The doubler includes a dimpled portion disposable between the tip cap and a portion of the flat-headed shaft at the dimple and an exterior portion. The exterior portion is disposable flush with respective exterior surfaces of the blade portion and the flat-headed shaft.

First claim

What is claimed is:

1. A rotor blade, comprising:
a blade portion;
a tip cap formed to define a dimple;
a fastener including a flat-headed shaft and being disposable such that the flat-headed shaft extends through the blade portion and the tip cap at the dimple, the fastener being configured to urge the blade portion toward the tip cap; and
a doubler including a dimpled portion disposable between the tip cap and a portion of the flat-headed shaft at the dimple and an exterior portion, which is disposed flush with respective exterior surfaces of the blade portion and the flat-headed shaft.

2. The blade according to claim 1 , wherein the blade portion encases a core material.

3. The blade according to claim 1 , wherein the blade portion comprises:
a main blade portion; and
a distal blade portion recessed from the main blade portion.

4. The blade according to claim 3 , wherein the flat-headed shaft extends through the distal blade portion.

5. The blade according to claim 3 wherein the exterior surfaces include an exterior surface of the main blade portion.

6. The blade according to claim 1 , wherein the dimple, the fastener and the dimpled portion are correspondingly plural in number.

7. The blade according to claim 6 , wherein the adjacent ones of the plural fasteners are staggered.

8. The blade according to claim 1 , wherein the doubler comprises metallic materials.

9. The blade according to claim 1 , further comprising sealant disposed between the blade portion and the tip cap and between the blade portion and the doubler.

10. The blade according to claim 1 , further comprising an erosion strip disposed flush with the doubler exterior portion and with the respective exterior surfaces of the blade portion and the flat-headed shaft.

11. A doubler for a blade, comprising:
a first planar section including an exterior portion defining a first plane and a dimpled portion at which a fastener including a flat-headed shaft is disposable to extend through a portion of the blade and a tip cap with an exterior surface of the flat-headed shaft flush with the exterior portion;
a second planar section disposed beyond a periphery of the first planar section and defining a second plane; and
a tapered section interposed between the periphery of the first planar section and the second planar section, the tapered section being tapered from the first plane to the second plane.

12. The doubler according to claim 11 , wherein the dimpled portion comprises a frusto-conical ramp tapered away from the first plane in a same direction as tapering of the tapered section.

13. The doubler according to claim 11 , wherein the first and second planar sections and the tapered section comprise metallic materials.

14. The doubler according to claim 11 , wherein the dimpled portion is plural in number, the plural dimpled portions being aligned with one another.

15. A blade including upper and lower surface doublers in accordance with the doubler of claim 14 , wherein the plural dimpled portions of the upper surface doubler are staggered with respect to the plural dimpled portions of the lower surface doubler.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Simkulak Richard Joseph
• Shimkus Michael J

Classifications

• B64C27/463 Primary

  Blade tips · CPC title

• B64C2027/4733

  Rotor blades substantially made from particular materials · CPC title

• B64C2027/4736

  from composite materials · CPC title

• B64C27/473

  Constructional features · CPC title

• Y02E10/721

  Cross-Sectional Technologies · mapped topic