Composite member

Patent metadata

Field	Value
Publication number	US-10273937-B2
Application number	US-201615166849-A
Country	US
Kind code	B2
Filing date	May 27, 2016
Priority date	May 28, 2015
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A composite member comprises first and second elongate composite elements. Each has a wedge shaped end with a complimentary tapered end surface. At least one of the components is formed of a stack of fiber layers impregnated in resin, with the tapered end surface being formed by each fiber layer extending longitudinally progressively further than the adjacent layer towards the thin end of the wedge at which the fiber layers have the greatest longitudinal extent. The components are joined at their tapered ends by an adhesive, and the properties of the cured composite material of the at least one component and/or the properties of the adhesive are different in the vicinity of the thin end of the wedge as compared to the rest of the tapered surface in order to reduce the stress concentrations in this region.

First claim

What is claimed is:

1. A composite member comprising:
a first elongate composite element; and
a second elongate composite element,
wherein each elongate composite element comprises a wedge shaped end with a complimentary tapered end surface; at least one of the first elongate composite element or the second elongate composite element being formed of a stack of fibre layers impregnated in resin, the respective tapered end surface being formed by each fibre layer extending longitudinally progressively further than a previous adjacent fibre layer towards a thin end of the wedge shaped end, at which the fibre layers have the greatest longitudinal extent; the first elongate composite element and the second elongate composite element being joined at their tapered end surfaces by an adhesive;
wherein properties of a cured composite material of the at least one of the first elongate composite element or the second elongate composite element or properties of the adhesive are different in the vicinity of the thin end of the wedge shaped end as compared to the rest of the tapered end surface in order to reduce stress concentrations in the thin end.

2. The composite member according to claim 1 , wherein the properties of the cured composite material may be one or more selected from the following group: fibre layer thickness, fibre/resin volume, fibre material, resin material, and longitudinal spacing between fibre layers.

3. The composite member according to claim 2 , wherein the different properties in the vicinity of the thin end of the wedge shaped end extend across the full longitudinal length of the at least one of the first elongate composite element or the second elongate composite element.

4. The composite member according to claim 1 , wherein the different properties in the vicinity of the thin end of the wedge shaped end do not extend across the full longitudinal length of the at least one of the first elongate composite element or the second elongate composite element.

5. The composite member according to claim 1 , wherein the composite member is a spar cap for use in a wind turbine blade.

6. The composite member according to claim 5 , wherein the first elongate composite element is a spar cap element, and the second elongate composite element is a connection piece joined at one end to the first elongate composite element and at an opposite end to a third element which is a second spar cap element.

7. A method of forming a composite member according to claim 1 , the method comprising applying the adhesive to at least one of the tapered end surfaces, bringing the tapered end surfaces together and curing the composite material and the adhesive.

Assignees

• Blade Dynamics Ltd

Inventors

• Hayden Paul Trevor
• Behmer Harald

Classifications

• B32B2262/0269

  Aromatic polyamide fibres · CPC title

• B32B19/06

  next to a fibrous or filamentary layer · CPC title

• B29L2031/085

  Wind turbine blades · CPC title

• B29C66/73753

  the to-be-joined area of at least one of the parts to be joined being partially cured, i.e. partially cross-linked, partially vulcanized · CPC title

• B29C66/73751

  the to-be-joined area of at least one of the parts to be joined being uncured, i.e. non cross-linked, non vulcanized · CPC title