System and method for assisting in the manufacture of a wind turbine blade shell

Patent metadata

Field	Value
Publication number	US-10118352-B2
Application number	US-201314893221-A
Country	US
Kind code	B2
Filing date	May 31, 2013
Priority date	May 31, 2013
Publication date	Nov 6, 2018
Grant date	Nov 6, 2018

Abstract

A method of manufacturing a wind turbine blade shell part is described. Fiber mats and a root end insert are laid up in a mould part in a layup procedure by use of an automated layup system. The fiber mats are laid up by use of a buffer so that the fiber mats may continuously be laid up on the mould surface, also during a cutting procedure. The root end insert is prepared in advance and mounted on a mounting plate. The root end insert is lowered onto the mould by use of the mounting plate and a lowering mechanism. After the wind turbine blade shell has been moulded, the mounting plate is removed.

First claim

The invention claimed is:

1. A fibre mat layup system for laying up and cutting fibre mats in a mould for the manufacture of a fibre-reinforced composite part, wherein the fibre-reinforced composite part comprises a part for a wind turbine blade wherein the system is adapted to laying up the fibre mat as the system is moved in a longitudinal direction along the mould, and wherein the system comprises:
a first drive roller for advancing the fibre mat,
a cutting device for cutting the fibre mat,
a first clamping device for clamping the fibre mat, while the fibre mat is being cut by the cutting device,
a buffer roller providing a buffer length for the fibre mat and being arranged downstream of the first drive roller, the first clamping device and the cutting device, the buffer roller being movable so as to vary the buffer length of the fibre mat, and
a second drive roller for advancing the fibre mat and being arranged downstream of the buffer roller.

2. The fibre mat layup system according to claim 1 , wherein the fibre mat is supplied from a fibre mat roll.

3. The fibre mat layup system according to claim 1 , wherein the system further comprises a draping device arranged downstream of the second drive roller.

4. The fibre mat layup system according to claim 3 , wherein the draping device comprises one or more rollers.

5. The fibre mat layup system according to claim 3 , wherein the draping device comprises a number of brushes.

6. The fibre mat layup system according to claim 1 , wherein the cutting device is a sonic knife.

7. The fibre mat layup system according to claim 1 , wherein the cutting device is a rotary cutter.

8. The fibre mat layup system according to claim 1 , wherein the system is adapted to lay out fibre mats having a width of at least 20 cm.

9. The fibre mat layup system according to claim 1 , wherein the system is adapted to lay up fibre mats with a speed of between 25 m/minute and 100 m/minute.

10. The fibre mat layup system according to claim 1 , wherein the system is adapted to slow down a movement speed thereof during the cutting of the fibre mat.

11. The fibre mat layup system according to claim 1 , wherein the first drive roller is arranged substantially vertical above the second drive roller, and is further arranged substantially vertical above the first clamping device.

12. The fibre mat layup system according to claim 1 , wherein the buffer roller is arranged so as to be movable in a substantially horizontal direction.

13. The fibre mat layup system according to claim 1 , wherein the buffer roller is resiliently biased.

14. The fibre mat layup system according to claim 13 , wherein the buffer roller is biased by use of gas pressure.

15. The fibre mat layup system according to claim 13 , wherein the buffer roller is biased by use of a spring.

16. The fibre mat layup system according to claim 1 , wherein the buffer roller may be locked in a disengaged position, where the buffer length is minimised.

17. A method of manufacturing a composite part, in particular a part for a wind turbine blade, such as an aerodynamic shell part, wherein fibre mats are laid up in a mould part in a layup procedure by use of an automated fibre mat layup system, wherein the layup procedure comprises the steps of:
a) delivering a supply of one or more fibre mats to the fibre mat layup system;
b) laying up a first length of a fibre mat onto a surface of the mould along a first longitudinal part of the mould by moving the fibre mat layup system in a longitudinal direction of the mould;
c) clamping a first part of the fibre mat with a first clamping device;
d) cutting the fibre mat at a cutting position with a cutting device;
e) laying up a second length of the fibre mat, while step d) is performed, by continuing to move the fibre mat layup system along the mould, while a buffer length arranged downstream of the first part of the fibre mat is being reduced, the buffer length for the fibre mat being provided by a buffer roller, the buffer roller being positioned downstream of a first drive roller, the first clamping device and the cutting device; and
f) repeating steps a)-e) to define a plurality of laid out fibre mats defining the composite part.

18. The method according to claim 17 , wherein the buffer length in step e) is reduced by varying the position of the buffer roller.

19. The method according to claim 18 , wherein the delivery of the one or more fibre mats in step a) involves advancing the one or more fibre mats to a position, where the one or more fibre mats extend from a first drive roller to the buffer roller arranged downstream of the first drive roller and further onto a second drive roller arranged downstream of the buffer roller.

20. The method according to claim 19 , wherein the delivery is carried out while the buffer roller is in a retracted position, and wherein the first drive roller advances the fibre mat until the fibre mat engages the second drive roller.

21. The method according to claim 20 , wherein the buffer roller subsequently is moved to an engaged position.

22. The method according to claim 20 , wherein the fibre mat layup system after step e) is moved to a new start position for laying up a fibre mat, while a subsequent delivery of a supply of one or more fibre mats to the fibre mat layup system fibre mat is carried out.

23. The method according to claim 17 , wherein the fibre mat layup system during step b) is moved along the mould at a first speed, and wherein the fibre mat layup system in step e) is moved along the mould at a second speed being lower than the first speed.

Assignees

• Lm Wp Patent Holding As
• Lm Wp Patent Holdings As

Inventors

• Borsting Dennis Andre
• Mortensen Ivan Engmark
• Fuglsang Lars
• Christiansen Per Kjaer

Classifications

• B29D99/0025

  Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

• F05B2230/00

  Manufacture · CPC title

• B32B38/0004

  Cutting, tearing or severing, e.g. bursting; Cutter details (cutting in general B26D; laminating combined with punching or perforating B32B38/04; removing all or part of the layers B32B38/10; cutting in combination with laying up and registration B32B38/185 takes precedence) · CPC title

• B29C70/386 Primary

  Automated tape laying [ATL] · CPC title

• B29L2031/085

  Wind turbine blades · CPC title