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:
Dec. 21, 2021

Filed:

Nov. 05, 2014
Applicant:

Lm Wp Patent Holding A/s, Kolding, DK;

Inventor:
Assignee:
Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 65/00 (2006.01); B29C 65/50 (2006.01); F03D 1/06 (2006.01); B29C 70/30 (2006.01); B29D 99/00 (2010.01); F03D 13/10 (2016.01); B29C 65/48 (2006.01); B29L 31/08 (2006.01); B29C 65/52 (2006.01);
U.S. Cl.
CPC ...
B29C 66/54 (2013.01); B29C 65/483 (2013.01); B29C 65/5014 (2013.01); B29C 65/5042 (2013.01); B29C 66/1226 (2013.01); B29C 66/12261 (2013.01); B29C 66/721 (2013.01); B29C 66/723 (2013.01); B29C 70/30 (2013.01); B29D 99/0028 (2013.01); F03D 1/0675 (2013.01); F03D 13/10 (2016.05); B29C 65/505 (2013.01); B29C 65/5021 (2013.01); B29C 65/52 (2013.01); B29C 66/02241 (2013.01); B29C 66/02245 (2013.01); B29C 66/221 (2013.01); B29C 66/223 (2013.01); B29C 66/71 (2013.01); B29C 66/727 (2013.01); B29C 66/7212 (2013.01); B29C 66/72329 (2013.01); B29L 2031/085 (2013.01); F05B 2280/6003 (2013.01); Y02E 10/72 (2013.01); Y02P 70/50 (2015.11);
Abstract

A method of manufacturing a wind turbine blade is described, the blade being formed from at least a pair of blade shells being joined together. For at least a portion of the wind turbine blade, the blade shells are joined by an overlamination applied between the edges of the blade shells, thereby substantially reducing or eliminating the need for a structural adhesive to join the blade shells, particularly in the area of the leading edge of the blade or the root region of the blade trailing edge. The overlamination can be formed from the same material as the blade shells themselves, thereby minimising the possibility of structural faults or cracks due to differences in materials or stiffness levels at the interface between the blade shells.


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