Methods of joining rotor blade components using thermoplastic welding

Patent metadata

Field	Value
Publication number	US-10641240-B2
Application number	US-201715437527-A
Country	US
Kind code	B2
Filing date	Feb 21, 2017
Priority date	Feb 21, 2017
Publication date	May 5, 2020
Grant date	May 5, 2020

Abstract

The present disclosure is directed to methods for joining rotor blade components using thermoplastic welding. The method includes arranging a first thermoplastic component and a second thermoplastic component together at an interface, determining a size of a tolerance gap between the first and second components at the interface, placing a thermoplastic insert between the first and second components at the interface, the insert being larger than the tolerance gap, heating the insert and the first and second components such that the insert begins to flow so as to fill the tolerance gap between the first and second components, applying pressure to the interface such that the insert and the first and second blade components remain substantially in direct contact with each other at the interface, and welding the insert and the first and second components together at the interface, wherein the heat and the applied pressure between the insert and the first and second components at the interface maintain the insert and the first and second substantially in direct contact at the interface during welding.

First claim

What is claimed is:

1. A method for welding thermoplastic rotor blade components together the method comprising:
arranging a first thermoplastic rotor blade component and a second thermoplastic rotor blade component together at an interface;
determining a size of a tolerance gap between the first and second thermoplastic rotor blade components at the interface;
placing a thermoplastic insert between the first and second thermoplastic rotor blade components at the interface, the thermoplastic insert being larger than the tolerance gap;
heating the thermoplastic insert and the first and second thermoplastic rotor blade components such that the thermoplastic insert begins to flow so as to fill the tolerance gap between the first and second thermoplastic rotor blade components;
applying pressure to the interface such that the thermoplastic insert and the first and second thermoplastic rotor blade components remain substantially in direct contact with each other at the interface; and,
subsequently welding the thermoplastic insert and the first and second thermoplastic rotor blade components together at the interface, wherein the heat and the applied pressure between the thermoplastic insert and the first and second thermoplastic rotor blade components at the interface maintain the thermoplastic insert and the first and second rotor blade components substantially in direct contact at the interface during welding.

2. The method of claim 1 , wherein at least a portion of the thermoplastic insert seeps from the interface after the pressure and heat is applied.

3. The method of claim 2 , further comprising at least one of removing at least a portion of the thermoplastic insert that seeps from the interface or smoothing at least a portion of the thermoplastic insert that seeps from the interface.

4. The method of claim 1 , wherein placing the thermoplastic insert between the first and second thermoplastic components at the interface further comprises coating one or more layers of a thermoplastic resin onto one or more of the first and second thermoplastic components at the interface.

5. The method of claim 1 , wherein placing the thermoplastic insert between the first and second thermoplastic components at the interface further comprises:
placing a temporary barrier onto one of the first or second thermoplastic components at the interface,
pouring one or more un-polymerized components into the temporary barrier;
allowing the one or more un-polymerized components to polymerize so as to form the thermoplastic insert; and,
removing the temporary barrier.

6. The method of claim 1 , wherein placing the thermoplastic insert between the first and second thermoplastic components at the interface further comprises:
applying one or more coats of un-polymerized components at the interface; and,
allowing the one or more coats of un-polymerized components to polymerize so as to form the thermoplastic insert.

7. The method of claim 1 , wherein the thermoplastic insert further comprises at least one of a wire mesh, tape, a shim, a conductive material, an adhesive, or one or more fiber materials embedded therein.

8. The method of claim 7 , wherein the fiber material comprises at least one of glass fibers, carbon fibers, polymer fibers, ceramic fibers, nanofibers, wood fibers, bamboo fibers, or metal fibers.

9. The method of claim 1 , further comprising securing the thermoplastic insert and the first and second thermoplastic rotor blade components together during welding so as to maintain the substantially direct contact.

10. The method of claim 9 , wherein securing the first and second thermoplastic rotor blade components together during welding further comprises:
applying, via an adjustable tooling device, one or more point loads at the interface so as to cause the thermoplastic insert to flex against the first and second thermoplastic components.

11. The method of claim 1 , wherein the first thermoplastic rotor blade component is concave or convex and the second thermoplastic rotor blade component comprises a different curvature than the first rotor blade component.

12. The method of claim 1 , further comprising supporting at least one of the first or second thermoplastic rotor blade components during welding so as to prevent distortion of the components during welding.

13. The method of claim 1 , further comprising welding a plurality of discrete welds at the interface so that point loads are applied thereto.

14. The method of claim 1 , wherein the first thermoplastic component comprises a raised area and the second thermoplastic component comprises a recessed area, the raised and recessed areas forming an interference fit between the first and second rotor blade thermoplastic components.

15. The method of claim 13 , further comprising applying adhesive within the recessed area and subsequently welding the first and second thermoplastic rotor blade components together.

16. A method for welding thermoplastic rotor blade components together, the method comprising:
arranging a first thermoplastic rotor blade component and a second rotor blade thermoplastic component together at an interface;
applying a plurality of discrete, point welds at the interface such that one or more point loads are applied at the interface so as to cause the first thermoplastic rotor blade component to flex to fit the second thermoplastic rotor blade component; and,
subsequently welding the arranged first and second thermoplastic rotor blade components together at the interface, wherein the plurality of discrete, point welds maintain contact between the first and second thermoplastic rotor blade components at the interface during welding.

17. The method of claim 16 , further comprising supporting at least one of the first or second thermoplastic rotor blade components during welding so as to prevent distortion of the components during welding.

18. The method of claim 16 , further comprising placing at least one filler material between the first and second thermoplastic rotor blade components at the interface, wherein the filler material comprises at least one of a tape, a shim, or an adhesive.

Assignees

• Gen Electric

Inventors

• Tobin James Robert
• Yarbrough Aaron A
• Hynum Daniel Alan
• Caruso Christopher Daniel

Classifications

• B29C66/1122

  Single lap to lap joints, i.e. overlap joints (B29C66/45, B29C66/472, B29C66/52272 take precedence) · CPC title

• B29C65/488

  being longitudinal, e.g. fibres · CPC title

• B29C66/54

  Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles · CPC title

• B29L2031/085

  Wind turbine blades · CPC title

• B29C66/1142

  Single butt to butt joints · CPC title