IP Library › Granted Patent US 8,721,829
Granted Patent B2
US 8,721,829 · App. 11/660,122 · Granted May 13, 2014

Method of cutting off laminate layers, eg a glass fibre or carbon-fibre laminate layer in the blade of a wind turbine

Inventors: Torben Krogsdal Jacobsen (Lunderskov, DK); Morten Dahl (Kolding, DK)
Assignee: LM Glasfiber A/S
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Quick Facts
Patent No.
US 8,721,829
App. No.
11/660,122
Granted
May 13, 2014
Kind
B2
Abstract

The invention relates to a method of cutting off laminate layers for use in a fiber-reinforced laminate object comprising a number of combined laminate layers, wherein, along a section of the at least one rim of the laminate layer, a tapering cut is performed through the thickness of the laminate layer, whereby the thickness of the laminate layer is reduced. Since not only the number of laminate layers, but also the thickness of the individual laminate layers are reduced, a laminate layer is accomplished that can be used in a laminate object, by which both the issues of areas rich in resin, air pockets and the risk of delamination are reduced. The invention also relates to a laminate layer for use in a fiber-reinforced laminate object comprising a number of combined laminate layers and a fiber-reinforced laminate object in the form of the blade of a wind turbine, wherein the blade of the wind turbine comprises a number of combined laminate layers.

Claims (11)

1. A method of forming a fibre-reinforced laminate object, comprising the steps of:

forming a number of non-impregnated fibre layers including an upper layer, a lower layer, and at least one intermediate layer between the upper layer and the lower layer;

performing a tapering cut on at least a portion of at least one of the upper layer, the lower layer and the at least one intermediate layer to form a tapered layer whereby a thickness of the tapered layer is reduced; and

applying a resin in order to combine the fibre layers and form the fibre-reinforced laminate object.

2. The method according to claim 1 , wherein the taper cut forms an acute angle between the tapered layer and an adjacent layer.

3. The method according to claim 1 , wherein the tapered layer is cut off in a concave curve.

4. The method according to claim 1 , wherein the tapered layer is cut off in a convex curve.

5. The method according to claim 1 , wherein the tapered layer is cut using a finger cutter.

6. The method according to claim 1 , wherein the tapered layer is the intermediate layer.

7. The method according to claim 1 , wherein the tapered layer is the upper layer.

8. The method according to claim 1 , wherein the tapered layer is the lower layer.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 9, 2007
From: JACOBSEN, TORBEN KROGSDAL; DAHL, MORTEN
To: LM GLASFIBER A/S
Reel/Frame 019242/0196 →
Priority Claims (1)
DK 2004 01225 · Aug 13, 2004 · national
Continuity (1)
Related Publication 20080145615A1 · Jun 19, 2008