Propeller blade and method

Patent metadata

Field	Value
Publication number	US-9920629-B2
Application number	US-201414185368-A
Country	US
Kind code	B2
Filing date	Feb 20, 2014
Priority date	Feb 20, 2014
Publication date	Mar 20, 2018
Grant date	Mar 20, 2018

Abstract

A propeller blade includes an inner spar structure surrounding an inner spar foam core. Also included is a leading edge foam structure disposed proximate a leading edge of the inner spar structure. Further included is a trailing edge foam structure disposed proximate a trailing edge of the inner spar structure. Yet further included is an outer spar structure surrounding the inner spar structure, the leading edge foam structure and the trailing edge foam structure. Also included is a blade shell, a leading edge foam core located between the outer spar structure and the blade shell, and a trailing edge foam core located between the outer spar structure and the blade shell.

First claim

The invention claimed is:

1. A propeller blade comprising:
an inner spar structure surrounding an inner spar foam core;
a leading edge foam structure disposed proximate a leading edge of the inner spar structure;
a trailing edge foam structure disposed proximate a trailing edge of the inner spar structure;
an outer spar structure surrounding the inner spar structure, the leading edge foam structure and the trailing edge foam structure;
a blade shell;
a leading edge foam core located between the outer spar structure and the blade shell; and
a trailing edge foam core located between the outer spar structure and the blade shell, the inner spar structure, the outer spar structure and the blade shell simultaneously co-cured upon resin injection.

2. The propeller blade of claim 1 , wherein the inner spar structure comprises carbon.

3. The propeller blade of claim 1 , wherein the inner spar structure comprises fiberglass.

4. The propeller blade of claim 1 , further comprising an inner spar formed by the inner spar structure and the inner spar foam core, wherein the inner spar extends along an entire length of the propeller blade.

5. The propeller blade of claim 1 , further comprising an inner spar formed by the inner spar structure and the inner spar foam core, wherein the inner spar extends along a partial length of the propeller blade.

6. The propeller blade of claim 1 , further comprising a root disposed at least partially around the inner spar structure at an end of the propeller blade.

7. The propeller blade of claim 1 , wherein the leading edge foam core and the trailing edge foam core are injectable components.

8. The propeller blade of claim 1 , wherein the leading edge foam core and the trailing edge foam core are pre-molded inserts.

9. The propeller blade of claim 1 , wherein the leading edge foam core and the trailing edge foam core are pre-machined inserts.

10. The propeller blade of claim 1 , wherein the inner spar foam core comprises one of an injectable foam, a pre-molded insert, and a pre-machined insert.

11. A method of forming a propeller blade comprising:
forming an inner spar foam core;
braiding an inner spar structure to the inner spar foam core;
securing a leading edge foam structure to a leading edge of the inner spar structure;
securing a trailing edge foam structure to a trailing edge of the inner spar structure;
braiding an outer spar structure over the inner spar structure, the leading edge foam structure and the trailing edge foam structure;
installing a leading edge foam core to the outer spar structure;
installing a trailing edge foam core to the outer spar structure;
encasing the outer spar structure, the leading edge foam core and the trailing edge foam core with a blade shell
resin injecting the entire assembly of the propeller blade; and
curing the inner spar structure and the outer spar structure to the blade shell during resin injection of the propeller blade.

12. The method of claim 11 , wherein securing the leading edge foam structure and the trailing edge foam structure to the inner spar structure comprises placing winding composite rovings around the perimeter of the leading edge and trailing edge foam structures.

13. The method of claim 11 , wherein securing the leading edge foam structure and the trailing edge foam structure to the inner spar structure comprises wrapping strips of resin pre-impregnated fiberglass or carbon around the perimeter of the leading edge and trailing edge foam structures.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Nagle David P

Classifications

• B29L2031/087

  Propellers · CPC title

• B64C11/26

  Fabricated blades · CPC title

• B29D99/0025 Primary

  Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

• Y10T29/49336

  Blade making · CPC title

• F01D5/14 Primary

  Form or construction (selecting particular materials, measures against erosion or corrosion F01D5/28) · CPC title