The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 11, 2020

Filed:

Feb. 09, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Christopher Daniel Caruso, Greenville, SC (US);

Aaron A. Yarbrough, Greenville, SC (US);

Daniel Alan Hynum, Simpsonville, SC (US);

James Robert Tobin, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F03D 1/06 (2006.01); B29C 70/52 (2006.01); B29C 51/26 (2006.01); B33Y 80/00 (2015.01); B29D 99/00 (2010.01); B29C 33/00 (2006.01); B29C 64/106 (2017.01); B29K 105/06 (2006.01); B29L 31/08 (2006.01); B29C 51/12 (2006.01); B29C 51/10 (2006.01);
U.S. Cl.
CPC ...
F03D 1/0675 (2013.01); B29C 33/0016 (2013.01); B29C 51/266 (2013.01); B29C 64/106 (2017.08); B29C 70/52 (2013.01); B29D 99/0028 (2013.01); B33Y 80/00 (2014.12); B29C 51/10 (2013.01); B29C 51/12 (2013.01); B29K 2105/06 (2013.01); B29K 2995/0082 (2013.01); B29L 2031/085 (2013.01); F05B 2230/24 (2013.01); F05B 2280/6003 (2013.01); Y02E 10/721 (2013.01); Y02P 70/523 (2015.11);
Abstract

The present disclosure is directed methods for manufacturing spar caps for wind turbine rotor blades. In certain embodiments, the method includes forming an outer frame of the spar cap via at least one of three-dimensional (3D) pultrusion, thermoforming, or 3D printing. As such, the outer frame has a varying cross-section that corresponds to a varying cross-section of the rotor blade along a span thereof. The method also includes arranging a plurality of structural materials (e.g. layers of pultruded plates) within the pultruded outer frame of the spar cap and infusing the structural materials and the outer frame together via a resin material so as to form the spar cap. The resulting spar cap can then be easily incorporated into conventional rotor blade manufacturing processes and/or welded or bonded to an existing rotor blade.


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