Composite material with controlled fracture regions

Patent metadata

Field	Value
Publication number	US-9914282-B2
Application number	US-201514827414-A
Country	US
Kind code	B2
Filing date	Aug 17, 2015
Priority date	Sep 5, 2014
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

A composite component includes a plurality of layers. A fracture region includes at least one fracture inducing layer in an overlapping relationship with at least one of the plurality of layers.

First claim

What is claimed is:

1. A composite component comprising:
a plurality of layers;
a fracture region including at least one fracture inducing layer in overlapping relationship between the plurality of layers, wherein the fracture inducing layer includes a discontinuity at the fracture region and the discontinuity includes a plurality of perforations forming an opening extending between opposing sides of the at least one fracture inducing layer and at least one of the plurality of layers is configured to remain substantially intact when the at least one fracture inducing layer fails; and
wherein the composite component is an airfoil and includes a first portion defining a base portion of the airfoil and a second portion defining a tip portion of the airfoil with the first portion configured to separate from the second portion along the fracture region.

2. The composite component of claim 1 , wherein the at least one fracture inducing layer is configured to fail prior to the at least one layer.

3. The composite component of claim 1 , wherein the plurality of layers are configured to withstand a first loading and the at least one fracture inducing layer is configured to withstand a second loading, the first loading is greater than the second loading.

4. The composite component of claim 1 , wherein the at least one fracture inducing layer includes a first portion having a first strength and a second portion having a second strength greater than the first strength, wherein the first portion is located at least partially within the fracture region.

5. The composite component of claim 1 , wherein an outermost layer of the composite material includes fiberglass and at least one interior layer of the composite includes at least one of fiberglass, graphite, Kevlar, or woven fabric material.

6. A method of designing a composite component comprising:
forming a composite component with a plurality of layers to withstand a first loading;
forming a fracture region in the composite component with at least one fracture inducing layer to withstand a second loading, wherein the first loading is greater than the second loading and the fracture inducing layer includes a severed fiber; and
wherein the composite component is an airfoil and includes a first portion defining a base portion of the airfoil and a second portion defining a tip portion of the airfoil with the first portion configured to separate from the second portion along the fracture region.

7. The method of claim 6 , further comprising maintaining at least one of the plurality of layers substantially intact when the at least one fracture inducing layer fails.

8. The method of claim 6 , wherein the fracture inducing layer includes a discontinuity located in the fracture region.

9. The method of claim 8 , wherein the discontinuity includes a plurality of perforations in the at least one fracture inducing layer.

10. The method of claim 6 , wherein the first portion includes a first strength, the second portion includes a second strength greater than the first strength, and the first portion is located at least partially within the fracture region.

11. The method of claim 6 , wherein at least one of the plurality of layers includes fiberglass, graphite, Kevlar, or woven fabric material.

12. The method of claim 6 , wherein the second loading is approximately 90-95% of the first loading.

13. The method of claim 6 , wherein failure of the at least one fracture inducing layer includes the first portion of the at least one fracture inducing layer moving relative to the second portion of the at least one fracture inducing layer.

Assignees

• United Technologies Corp

Inventors

• Roach James T
• Lussier Darin S

Classifications

• B32B5/145

  Variation across the thickness of the layer · CPC title

• B32B17/00

  Layered products essentially comprising sheet glass, or glass, slag, or like fibres · CPC title

• B32B2307/544

  Torsion strength; Torsion stiffness · CPC title

• B32B2307/546

  Flexural strength; Flexion stiffness · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title