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:
Jun. 20, 2017

Filed:

May. 28, 2013
Applicant:

Vestas Wind Systems A/s, Aarhus N., DK;

Inventor:

Stephen Randall, Hampshire, GB;

Assignee:

Vestas Wind Systems A/S, Aarhus N., DK;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 70/68 (2006.01); F03D 1/00 (2006.01); B29D 99/00 (2010.01); F03D 1/06 (2006.01); B29C 70/34 (2006.01); F03D 13/10 (2016.01); B29L 31/08 (2006.01); B29K 63/00 (2006.01); B29K 105/08 (2006.01); B29K 309/08 (2006.01);
U.S. Cl.
CPC ...
F03D 1/001 (2013.01); B29C 70/34 (2013.01); B29C 70/68 (2013.01); B29D 99/0025 (2013.01); F03D 1/0675 (2013.01); F03D 13/10 (2016.05); B29K 2063/00 (2013.01); B29K 2105/089 (2013.01); B29K 2309/08 (2013.01); B29L 2031/085 (2013.01); Y02E 10/721 (2013.01); Y02P 70/523 (2015.11); Y10T 156/10 (2015.01);
Abstract

A structural shell for a wind turbine blade is formed from one or more elongate reinforcing members, each in the form of a stack () of pultruded fibrous composite strips positioned between two layers of structural foam (). The foam layers () have a thickness which is greater than that of the stack (). The edges of the foam layers () are formed with a void (). With the stack () and foam layers () positioned in a mould, a strip of pre-cured glass fibre () is placed on the stack () and the edges of the foam layers (). A vacuum is applied to the stack () and the foam layers (), causing the glass fibre strip () to press on the stack () and foam layers () and to conform to the underlying surfaces. As a result, the void () is reduced in size and the step-shaped transition between the surfaces of the stack () and the foam layers () transformed into a smooth transition, so as to reduce the stresses within the glass fibre strip () in the region of the abutment of the stack () and the foam layers (). In other embodiments, the stepped transition is smoothened by replacing the upper-edge region of each foam layer () with a strip of low-stiffness foam.


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