Method for manufacturing a wind turbine rotor blade

Patent metadata

Field	Value
Publication number	US-9422916-B2
Application number	US-201113267244-A
Country	US
Kind code	B2
Filing date	Oct 6, 2011
Priority date	Oct 13, 2010
Publication date	Aug 23, 2016
Grant date	Aug 23, 2016

Abstract

A method for forming a profile for a hollow component is provided. A first composite fiber layer is laid out on a first surface corresponding to a first profile section of the component. A second composite fiber layer is laid out in a second surface corresponding to a second profile section of the component. A collapsed bag is laid out in onto the first composite fiber layer. The bag and the first composite fiber layer are fixed to the first surface. First and second mould elements are coupled such that the first surface and the second surface correspond to the first and second profiles. The bag is inflated such that the first composite fiber layer is pressed to the first surface and the second composite fiber layer is pressed to the second surface so that the first and second layers are coupled to form the profile.

First claim

The invention claimed is:

1. A method for forming a profile for a hollow blade component for a wind turbine, the method comprising:
a) laying out a first composite fibre layer on a first mould surface of a first mould element, wherein the first mould surface corresponds to a first profile section of the hollow blade component to be manufactured, wherein the first composite fibre layer is larger than the first mould surface such that the first composite fibre layer forms a surplus section that extends over an edge of the first mould surface;
b) laying out a second composite fibre layer in a second mould surface of a second mould element, wherein the second mould surface corresponds to a second profile section of the hollow blade component to be manufactured;
c) laying out a bag in a collapsed state onto the first composite fibre layer;
d) fixing the bag and the first composite fibre layer to the first mould surface;
e) after (a), (b), (c) and (d) coupling the first mould element to the second mould element in such a way, that the first mould surface and the second mould surface correspond to the profile of the hollow blade component to be manufactured, wherein the coupling of the first mould element to the second mould element causes the surplus section to move relative to the first mould surface responsive to gravity so as to become partially overlapped with the second composite fibre layer in the second mould element, and
f) after (e) inflating the bag in such a way that the first composite fibre layer is pressed to the first mould surface, the second composite fibre layer is pressed to the second mould surface, and the surplus section is pressed to the second composite fibre layer, so that the first composite fibre layer and the second composite fibre layer are coupled to form the profile to be manufactured.

2. The method according to claim 1 , wherein the fixing comprises sucking off air between the bag and the first mould surface such that the bag and the first composite fibre layer are fixed to the first mould surface by underpressure.

3. The method according to claim 2 , wherein the adjusting comprises:
bringing together the first mould element with the second mould element, wherein, when the surplus section is in the predetermined position, the surplus section overlaps partially with the second composite fibre layer in the second mould element.

4. The method according to claim 1 , wherein the second composite fibre layer is larger than the second mould surface such that the second composite fibre layer forms a further surplus section that extends over an edge of the second mould surface, and wherein the coupling of the first mould element to the second mould element further comprises
adjusting the first mould element to the second mould element in such a way that the further surplus section overlaps partially with the first composite fibre layer in the first mould element.

5. The method according to claim 1 , wherein before coupling the first mould element to the second mould element the method further comprises
mounting a web to the first composite fibre layer or to the second first composite fibre layer in such a way that after coupling of the first mould element to the second mould element the web is coupled with the first composite fibre layer and the second composite fibre layer for reinforcing the hollow blade component to be manufactured.

6. The method according to claim 1 , wherein before coupling the first mould element to the second mould element the method further comprises
mounting a web to the first composite fibre layer, and
mounting a further web to the second composite fibre layer in such a way that after coupling of the first mould element to the second mould element the web and the further web are coupled with each other for reinforcing the hollow blade component to be manufactured.

7. The method according to claim 1 , wherein the inflating of the bag comprises sucking off air between:
the bag and the first mould surface; and
the bag and the second mould surface, such that the bag presses the first composite fibre layer to the first mould surface and the second composite fibre layer to the second mould surface.

8. The method according to claim 1 , wherein the inflating of the bag comprises
blowing pressurized air into the bag such that the bag presses the first composite fibre layer to the first mould surface and the second composite fibre layer to the second mould surface.

Assignees

• Schibsbye Karsten
• Siemens Ag

Inventors

• Schibsbye Karsten

Classifications

• F05B2230/00

  Manufacture · CPC title

• F03D1/0675 Primary

  of the blades · CPC title

• B29C70/446

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• Y02E10/721

  Cross-Sectional Technologies · mapped topic

• Y02E10/722

  Cross-Sectional Technologies · mapped topic