Wind turbine blades
10232528 ยท 2019-03-19
Assignee
Inventors
Cpc classification
B29C70/545
PERFORMING OPERATIONS; TRANSPORTING
Y02P70/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B24B19/005
PERFORMING OPERATIONS; TRANSPORTING
B24B27/0608
PERFORMING OPERATIONS; TRANSPORTING
Y02P70/50
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F03D1/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C70/302
PERFORMING OPERATIONS; TRANSPORTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B24B19/14
PERFORMING OPERATIONS; TRANSPORTING
B29C67/0044
PERFORMING OPERATIONS; TRANSPORTING
B29B11/02
PERFORMING OPERATIONS; TRANSPORTING
B29C70/84
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/003
PERFORMING OPERATIONS; TRANSPORTING
B29C70/021
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/02
PERFORMING OPERATIONS; TRANSPORTING
B29C67/00
PERFORMING OPERATIONS; TRANSPORTING
B29B11/02
PERFORMING OPERATIONS; TRANSPORTING
B24B19/14
PERFORMING OPERATIONS; TRANSPORTING
F03D1/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B24B19/00
PERFORMING OPERATIONS; TRANSPORTING
B29D99/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/84
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of making a longitudinal reinforcing structure for a wind turbine blade. The method comprises a) providing an elongate master strip (62) of reinforcing material having substantially flat first and second surfaces, the distance between the first and second surfaces defining the thickness of the master strip; and b) dividing the master strip transversely to form a first strip and a shorter master strip, the respective strips being arranged end to end such that a trailing end of the first strip is located adjacent a new leading end of the master strip. The step of dividing the master strip comprises removing material from a dividing region extending through the entire thickness of the master strip, wherein the dividing region is shaped such that a chamfer (19c) at the trailing end (19b) of the first strip is created and a chamfer (63a) at the new leading end (63) of the master strip is created when the master strip is divided.
Claims
1. A method of making a longitudinal reinforcing structure for a wind turbine blade, the method comprising: a. providing an elongate master strip of reinforcing material having substantially flat first and second surfaces, the distance between the first and second surfaces defining the thickness of the master strip; and b. dividing the master strip transversely to form a first strip and a shorter master strip, the respective strips being arranged end to end such that a trailing end of the first strip is located adjacent a new leading end of the master strip; wherein the elongate master strip of reinforcing material includes a pultruded length of carbon-fiber reinforced plastic, and wherein the step of dividing the master strip comprises removing material from a dividing region extending through the entire thickness of the master strip, wherein the dividing region is shaped such that a chamfer at the trailing end of the first strip is created and/or a chamfer at the new leading end of the master strip is created when the master strip is divided.
2. The method of claim 1, wherein the dividing region tapers through the thickness of the master strip moving in a direction from the first surface towards the second surface of the master strip such that a longitudinal extent of the dividing region is narrower at the second surface of the master strip than at the first surface.
3. The method of claim 1, comprising grinding the master strip to remove material from the dividing region.
4. The method of claim 3, comprising moving a grinding device such as a grinding drum through the thickness of the master strip from the first surface of the master strip towards the second surface of the master strip.
5. The method of claim 4, comprising moving the grinding device in a curved path relative to the master strip so as to form curved chamfers at the trailing end of the first strip and/or at the new leading end of the master strip.
6. The method of claim 1, comprising further shaping the chamfer at the trailing end of the first strip by removing material from a shaping region of the first strip.
7. The method of claim 6, comprising further shaping the chamfer at the new leading end of the master strip by removing material from a shaping region of the master strip.
8. The method of claim 7, comprising using the grinding device to further shape the chamfers at the trailing end of the first strip and at the new leading end of the master strip.
9. The method of claim 7, comprising moving the new leading end of the master strip in a feed direction before removing material from the shaping region of the master strip.
10. The method of claim 1, further comprising creating a chamfer in a leading end of the first strip.
11. The method of claim 10, further comprising creating a chamfer in a leading end of the master strip before dividing the master strip transversely to form the first strip, wherein the chamfered leading end of the master strip becomes the leading end of the first strip when the master strip is divided.
12. The method of claim 1, further comprising feeding the master strip along a feed path in a feed direction towards a dividing station at which the master strip is divided and chamfered.
13. The method of claim 12, wherein the grinding device travels over a longitudinal extent in the feed direction, the longitudinal extent being substantially equal to the length of the chamfer at the trailing end of the first strip and/or the length of the chamfer at the new leading end of the master strip.
14. The method of claim 12, wherein after the master strip has been divided, the method further comprises feeding the first strip along the feed path in the first direction away from the dividing station.
15. The method of claim 12, comprising feeding a first predetermined length of the master strip past a dividing and chamfering device associated with the dividing station such that the dividing region of the master strip is located adjacent the dividing and chamfering device, wherein the first predetermined length is substantially the length of the first strip.
16. The method of claim 1, further comprising dividing the master strip transversely to form a second strip, wherein the new chamfered leading end of the master strip becomes a leading end of the second strip and the step of dividing the master strip to form the second strip also serves to create a chamfer at a trailing end of the second strip and a chamfer in an adjacent new leading end of the master strip.
17. The method of claim 16, further comprising feeding a second predetermined length of the master strip past the dividing and chamfering device before dividing the master strip to form the second strip, wherein the second predetermined length is substantially the length of the second strip.
18. The method of claim 17, wherein the second predetermined length is substantially equal to the first predetermined length such that the first and second strips are substantially the same length.
19. The method of claim 17, wherein the first and second predetermined lengths are different such that the second strip is shorter than the first strip or vice versa.
20. The method of claim 17, comprising successively feeding predetermined lengths of the master strip past the dividing and chamfering apparatus and dividing and chamfering the master strip to form a plurality of strips of substantially the same length or of differing lengths.
21. The method of claim 1, further comprising cutting an end region of the or each strip longitudinally thereby to narrow said end so that the strip(s) can be accommodated in a relatively narrow end of a wind turbine blade.
22. The method of claim 1, further comprising stacking the first strip with one or more similar strips to form the longitudinal reinforcing structure for a wind turbine blade.
23. The method of claim 22, wherein the method further comprises stacking the strips inside a wind turbine blade mould, or stacking the strips outside a wind turbine blade mould and transferring the stack of strips into the wind turbine blade mould.
24. The method of claim 22, further comprising integrating the strips in the stack by means of resin between the adjacent strips.
25. A method of making a wind turbine blade comprising: a) providing a plurality of strips made according to the method of claim 1; b) stacking the strips inside a wind turbine blade mould, or stacking the strips outside a wind turbine blade mould and transferring the stack of strips into the wind turbine blade mould; c) arranging other components of a wind turbine blade in the wind turbine blade mould; and d) integrating the components to form the blade.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
(13)
(14) Referring to
(15) The master strip 62 is fed by a feeding means 64 from the feed station 60 to a dividing station 70 arranged inline with the feed station 60. At the dividing station 70, the master strip 62 is divided into smaller strip sections 18 that form the strips 18 that are subsequently stacked to form the spar caps 15a, 15b, 16a, 16b. Also at the dividing station 70, the strips 18 are shaped so that they can be accommodated in the relatively narrow tip region of the blade. Specifically, the strips 18 are cut in a longitudinal direction such that they become narrower towards one end when viewed in plan view. This process will be described in more detail later. The strips 18 are then fed on to a mould tool, in this case a wind turbine blade mould 20, where the strips 18 are stacked and integrated to form the spar caps 15a, 15b, 16a, 16b.
(16) The dividing station 70 will now be described in further detail. The dividing station 70 comprises a dividing and chamfering apparatus 100 and a cutting apparatus 200 for narrowing the ends of the strips. The dividing and chamfering apparatus 100 is arranged in an up-stream position (i.e. towards the feed station 60) and is shown in more detail in
(17)
(18) The grinding drum 104, drive motor 106 and drive shaft 105 are mounted on a carriage 110. The carriage 110 is slidably mounted on a rail 112, so that the grinding drum 104 can be displaced back and forth along a direction X indicated on
(19) The grinding drum 104, rail 112, parts of the drive system 108 and a region of the master strip 62 that is close to the grinding drum 104, are shielded by a casing (not shown in the Figures). The casing prevents access to the grinding drum 104 and other moving parts of the apparatus 100 when they are in use, for safety reasons.
(20) Downstream of the dividing and chamfering apparatus 100 is a platform 150, visible in
(21) Referring to
(22) The cutting apparatus 200 comprises a series of clamping mechanisms 202 comprising hydraulic clamps 203. The clamps 203 hold the strip 18 in place on the platform 150 during the cutting process. A cutting mechanism 204 is arranged above the platform 150. The cutting mechanism 204 comprises a circular saw 206, in this case a diamond saw, that can be rotated to cut a strip 18 supported on the platform 150. Rotation of the circular saw 206 is controlled by a motor 208.
(23) The cutting mechanism 204 is mounted on a rail 210 (
(24) Use of the dividing and chamfering apparatus 100 and the cutting apparatus 200 in dividing, chamfering, and cutting the strips 18 will now be described.
(25) Referring again to
(26) The dividing and chamfering process will now be described in detail with reference to
(27) The path of the grinding drum 104 is controlled by the servomechanisms. In this case, the grinding drum 104 is moved along a substantially parabolic path to create a substantially parabolic chamfered end surface 63a in the master strip 62.
(28) Once the initial chamfered surface 63a has been created in the leading end 63 of the master strip 62, the feed process is continued and the master strip 62 is advanced in the feed direction F. Referring now to
(29) Once the predetermined length L of the master strip 62 has been fed past the grinding drum 104 and the feed process suspended, a dividing region 66 of the master strip 62 is then located beneath the grinding drum 104. The master strip 62 will be divided and chamfered by removing material from the dividing region 66.
(30) The dividing region 66 is shown in detail in
(31) Once located in place, the master strip 62 is ready to be divided.
(32) The grinding drum 104 is rotated and is moved downwardly in the Z direction towards an upper surface 68a of the master strip 62 to begin grinding, as shown in
(33) As grinding continues, the grinding drum 104 is moved downwardly in the Z direction to grind deeper into the master strip 62, as shown in
(34) Referring still to
(35) As the dividing region 66 (
(36) In the dividing and chamfering process described above, the individual strips 18 are divided from the master strip 62 at the shallowest point of the parabolic curve of the ground surface 69. This is particularly advantageous as it means that the strips 18 decrease to zero thickness at their ends. This zero thickness is particularly effective in ensuring stress transfer between the stacked strips 18 in the finished spar cap 15a, 15b, 16a, 16b.
(37) Once each strip 18 has been divided and chamfered, the strip 18 is fed along the platform 150 to the cutting apparatus 200 of
(38) Once the first angled cut has been made, the circular saw 206 is then moved in the Y direction and positioned alongside the second longitudinal edge of the strip 18. The circular saw 206 is then moved back in the X direction to cut the second longitudinal edge on a return pass. Alternatively, the circular saw 206 may first be moved backward in the X direction to its initial position, then moved in the Y direction towards the second longitudinal edge of the strip and finally forward in the X direction to cut the second edge on a second forward pass.
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(40) After the cutting process has been completed, the clamps 203 are removed, and the strip 18 is fed onwards towards the blade mould 20 for stacking and integration into the wind turbine blade 10.
(41) In this way, the apparatus 50 described provides a simple, mechanised method of processing an elongate master strip 62 into a plurality of smaller strips 18 to make an elongate reinforcing structure such as a spar cap 15a, 15b, 16a, 16b. In particular, the strips 18 can be simultaneously divided and chamfered by virtue of the dividing and chamfering apparatus 100, and separate dividing and chamfering stages are not required. Furthermore, two strip ends can be chamfered simultaneously.
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(43) Once the predetermined length L of the master strip 62 has been fed past the grinding drum 104 and the feed process has been suspended, the dividing region 66 of the master strip 62 is located beneath the grinding drum 104. To divide and chamfer the master strip 62, the grinding drum 104 is rotated and is moved downwardly in the Z direction towards the upper surface 68a of the master strip 62 to begin grinding material away from the dividing region 66.
(44) As grinding continues, the grinding drum 104 is moved further downward in the Z direction to grind deeper into the master strip 62, as shown in
(45) In this process, the drum 104 moves only downwardly in the Z direction, and is not moved back and forth in the X direction during the dividing and chamfering process. In this way, and as seen in
(46) Referring now to
(47) Once the strip 18 has been formed, the process then repeats and the grinding drum 104 is used to divide and chamfer the master strip 62 again to create a second strip 18 having a chamfered leading end 19a, and a chamfered trailing end 19b, and to create a chamfered surface 63a at the leading end 63 of the remaining length of the master strip 62. The process continues in this manner to create a succession of strips 18 each having chamfered leading and trailing ends 19a, 19b until the master strip 62 has been depleted. The strips 18 may then be fed onwards for cutting in the manner already described.
(48)
(49) This process differs from the process illustrated in
(50) The chamfered end surfaces 19c, 63a are shaped by using the grinding drum 104 to remove material from a shaping region 67 that incorporates the respective chamfered end surfaces 19c, 63a. The shaping region 67 in the vicinity of the chamfered end surface 19c of the divided strip 18 is shown in detail in
(51) The chamfered end surfaces 19c, 63a are shaped one-at-a-time to create relatively shallow chamfers at the ends of the strips 18, 62, as will now be described.
(52) First, the chamfered end surface 19c at the trailing end 19b of the strip 18 is shaped by removing material from a shaping region 67 near the chamfered end surface 19c. The divided strip 18 and master strip 62 remain in place. The drum 104 is displaced in the X direction towards one end of the shaping region 67, to a left-most position as shown in
(53) Once the chamfered end surface 19c of the divided strip 18 has been shaped to create a relatively shallow chamfer, the divided strip 18 is moved onwards in the feed direction F for further processing.
(54) Next, the chamfered end surface 63a at the leading end 63 of the remaining master strip 62 is shaped by removing material from a shaping region 67 near that chamfered end surface 63a.
(55) Referring to
(56) As indicated by the dashed lines in
(57) Once the chamfered end surface 63a of the master strip 62 has been shaped as required, the dividing, chamfering and further shaping process can be repeated to produce more divided strips 18.
(58) In the embodiments where the grinding drum is moved in the X direction as well as the Z direction, the drum need not be moved in an arcuate motion to form a parabolic chamfered surface, but may be moved in any manner to grind a chamfered surface of any shape.
(59) In embodiments where the chamfered end surfaces are further shaped after an initial dividing and chamfering process, the drum may be moved in any suitable manner to further shape the end surfaces. For example, the drum may begin in an upper position, such that it is moved downwardly from the upper surface of the strip to the lower surface of the strip, as has been described with reference to
(60) Other embodiments of the invention are envisaged that are similar to the embodiment illustrated in
(61) The master strip need not be divided and chamfered by grinding, but may be divided and chamfered by any other suitable means, such as, for example, laser cutting. Thus, the dividing and chamfering device need not be a grinding drum, but may be any suitable device, such as a laser.
(62) Additional processing stages may be added at any stage of the manufacturing process. If the cutting stage is not required, the cutting process may be omitted.
(63) The strips need not be fed directly to the mould tooling after processing, but may be fed for example to further processing areas, or to a storage area. The mould tooling need not be a blade mould, but may be a mould suitable for forming spar caps separately, for later integration into wind turbine blades.