Methods for manufacturing wind turbine rotor blade panels having printed grid structures

Patent metadata

Field	Value
Publication number	US-10913216-B2
Application number	US-201715818936-A
Country	US
Kind code	B2
Filing date	Nov 21, 2017
Priority date	Nov 21, 2017
Publication date	Feb 9, 2021
Grant date	Feb 9, 2021

Abstract

A method for manufacturing a rotor blade panel of a wind turbine includes placing a mold of the rotor blade panel relative to a computer numeric control (CNC) device. The method also includes forming one or more fiber-reinforced outer skins in the mold. The method also includes printing and depositing, via the CNC device, printing and depositing, via the CNC device, a plurality of rib members that intersect to form at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more fiber-reinforced outer skins before the one or more fiber-reinforced outer skins have cooled from forming. Further, the grid structure bonds to the fiber-reinforced outer skin(s) as the structure is deposited. In addition, the plurality of rib members include, at least, a first rib member extending in a first direction and a second rib member extending in a different, second direction. Moreover, the first rib member has a varying height along a length thereof.

First claim

What is claimed is:

1. A method for manufacturing a rotor blade skin, the method comprising:
placing a mold of the rotor blade skin relative to a computer numeric control (CNC) device;
forming one or more fiber-reinforced outer skin layers in the mold using at least one of vacuum infusion, thermoforming, vacuum forming, pressure forming, the one or more fiber-reinforced outer skin layers constructed, at least in part, of a first thermoplastic material, wherein the formed one or more fiber-reinforced outer skin layers comprise one or more resin-rich areas of the first thermoplastic material; and,
forming at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more fiber-reinforced outer skin layers via an additive manufacturing process, the additive manufacturing process comprising printing and depositing, via the CNC device, the 3 D reinforcement grid structure onto the inner surface of the one or more fiber-reinforced outer skin layers in the one or more resin-rich areas before the one or more fiber-reinforced outer skin layers have cooled from forming, the grid structure being formed of a second thermoplastic material that bonds to the one or more resin-rich areas of the one or more fiber-reinforced outer skin layers as the grid structure is being printed and deposited, the first and second thermoplastic materials being different.

2. The method of claim 1 , further comprising placing the mold of the rotor blade skin into a bed of the CNC device.

3. The method of claim 1 , wherein the grid structure comprises a plurality of rib members comprising, at least, a first rib member and a second rib member, the first rib member extending in a first direction and the second rib member extending in a different, second direction, the first rib member having a varying height along a length thereof, the second rib member having a uniform height along a length thereof.

4. The method of claim 3 , wherein the plurality of rib members further comprises a first set of rib members comprising the first rib member and a second set of rib members comprising the second rib member.

5. The method of claim 4 , further comprising printing a maximum height of at least one the first set of rib members or the second set of rib members at a location substantially at a maximum bending moment in the rotor blade skin occurs.

6. The method of claim 5 , further comprising printing at least one tapering end for each of the first set of rib members from the maximum height, the at least one tapering end tapering towards the inner surface of the one or more fiber-reinforced outer skins.

7. The method of claim 6 , wherein a slope of the tapering end is linear.

8. The method of claim 6 , wherein a slope of the tapering end is non-linear.

9. The method of claim 4 , wherein the second set of rib members each have a different height from adjacent rib members in the second set of rib members.

10. The method of claim 9 , further comprising printing each of the second set rib members such that rib members having greater heights are located towards a center location.

11. The method of claim 3 , wherein the first direction is generally parallel to a chord-wise direction of the rotor blade skin and the second direction is generally parallel with a span-wise direction of the rotor blade skin.

12. The method of claim 1 , further comprising printing an outline of the grid structure and building up the grid structure in multiple passes.

13. The method of claim 1 , further comprising printing a plurality of grid structures onto the inner surface of the one or more fiber-reinforced outer skins, the plurality of grid structures being in separate and distinct locations on the inner surface.

14. The method of claim 3 , wherein at least one of the first set of rib members or the second set of rib members are evenly spaced.

15. The method of claim 3 , wherein at least one of the first set of rib members or the second set of rib members are un-evenly spaced.

16. The method of claim 3 , further comprising printing the plurality of rib members using at least of one varying rib direction, varying rib angle, varying materials, varying thicknesses, or varying cross-sectional shapes.

17. A method for manufacturing a rotor blade skin, the method comprising:
placing a mold of the rotor blade skin relative to a computer numeric control (CNC) device;
forming one or more fiber-reinforced outer skin layers in the mold using a first manufacturing process, the one or more fiber-reinforced outer skin layers constructed of a first thermoplastic material, the first manufacturing process comprising at least one of vacuum infusion, thermoforming, vacuum forming, pressure forming, wherein the formed one or more fiber-reinforced outer skin layers comprise one or more resin-rich areas of the first thermoplastic material; and,
forming at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more fiber-reinforced outer skin layers via a second manufacturing process, the second manufacturing process comprising printing and depositing, via the CNC device, the at least one three-dimensional (3-D) reinforcement grid structure onto the inner surface of the one or more fiber-reinforced outer skin layers before the one or more fiber-reinforced outer skin layers have cooled from forming, the grid structure being formed of a second thermoplastic material that bonds to the one or more fiber-reinforced outer skin layers as the grid structure is being printed and deposited, the first and second thermoplastic materials being different.

18. The method of claim 17 , wherein the grid structure comprises a plurality of curved rib members.

19. The method of claim 17 , wherein the grid structure comprises at least one rib member forming a waveform.

Assignees

• Gen Electric

Inventors

• Tobin James Robert
• Merzhaeuser Thomas
• Anderson Todd

Classifications

• B29D99/0014

  provided with ridges or ribs, e.g. joined ribs · CPC title

• B29C70/747

  Applying material, e.g. foam, only in a limited number of places or in a pattern, e.g. to create a decorative effect · CPC title

• B29D99/0028

  hollow blades · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B33Y10/00

  Processes of additive manufacturing · CPC title