# US 10,864,687 B2 · Radius fillers for composite structures, composite structures that include radius fillers, and systems and methods of forming the same

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- Number: US 10,864,687 B2
- Document ID: US10864687B2
- Status: Granted
- Kind: B2
- Application number: 16/021,314
- Filed: 2018-06-28
- Published: 2018-11-01
- Granted: 2020-12-15
- Earliest claimed: 2014-04-03
- Assignees: The Boeing Company
- Applicants: The Boeing Company
- Inventors: Douglas A. McCarville; Juan C. Guzman; Jordan Oliver Birkland; Ryan Shaw Tidwell; Robert L. Anderson
- Web page: https://patentgrep.com/patent/US10864687B2

## CPC

- B29D 99/0005: {Producing noodles, i.e. composite gap fillers, characterised by their construction}
- B32B 5/02: characterised by structural features of a {fibrous or filamentary} layer {(layer formed of metallic wires B32B15/02; layer formed of natural mineral fibres B32B19/02; layer formed of wood fibres B32B21/02)}
- B32B 27/00: Layered products comprising {a layer of} synthetic resin {(fibrous or filamentary layer made of a synthetic resin B32B5/02; particulate layer made of a synthetic resin B32B5/16; foamed layer made of a synthetic resin B32B5/18)}
- B29C 70/52: Pultrusion, i.e. forming and compressing by continuously pulling through a die
- B29K 2105/0872: {Prepregs}
- B29L 2031/3082: {Fuselages}
- B29L 2031/3085: {Wings}
- B32B 2605/18: Aircraft
- Y10T 428/24521: with component conforming to contour of nonplanar surface
- Y10T 428/24612: Composite web or sheet
- B29D: PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE (making granules B29B9/00; making preforms B29B11/00)
- B32B: LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B29C: SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING (making preforms B29B11/00; making laminated products by combining previously unconnected layers which become one product whose layers will remain together B32B37/00 - B32B41/00)
- B29K: INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR {MOULDS, } REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29L: INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION

## Abstract

Radius fillers for composite structures and composite structures that include radius fillers are disclosed herein. The radius fillers include a plurality of lengths of composite tape. Each of the plurality of lengths of composite tape includes a respective plurality of lengths of reinforcing fibers and a resin material. The plurality of lengths of reinforcing fibers in each of the plurality of lengths of composite tape defines a fiber axis direction. Each of the plurality of lengths of composite tape defines a respective fiber axis direction that is based, at least in part, on material properties of a transition region defined by a plurality of plies of composite material that defines an elongate void space within which the radius filler is configured to extend. The composite structures include the radius fillers.

## Claims

### Claim 1

A radius filler for a composite structure, wherein the composite structure includes a plurality of plies of composite material that converge within a transition region to define an elongate void space, wherein the plurality of plies of composite material defines a material property gradient of the transition region, wherein the material property gradient of the transition region includes a mathematical description of a variation in at least one material property with direction within the transition region, and further wherein the radius filler is configured to extend within the elongate void space, the radius filler comprising:
a plurality of lengths of composite tape;
wherein the plurality of lengths of composite tape includes a first set of plies that defines a first edge and a second set of plies that defines a second edge, and further wherein the first edge and the second edge are in contact with one another.

### Claim 2 (depends on 1)

The composite structure of claim 1, wherein:
(i) each of the plurality of lengths of composite tape includes a respective plurality of lengths of reinforcing fibers and a resin material;
(ii) the plurality of lengths of reinforcing fibers in each of the plurality of lengths of composite tape defines a fiber axis direction; and
(iii) each of the plurality of lengths of composite tape defines a respective fiber axis direction that is selected based, at least in part, on the material property gradient of the transition region.

### Claim 3 (depends on 2)

The radius filler of claim 2, wherein the radius filler defines an apex region within a plane that is perpendicular to a longitudinal axis of the radius filler and further wherein at least one of the plurality of lengths of composite tape defines a respective fiber axis direction that is directed into the apex region.

### Claim 4 (depends on 1)

The radius filler of claim 1, wherein the plurality of lengths of composite tape is in physical contact with one another within the radius filler.

### Claim 5 (depends on 1)

A composite structure, comprising:
a plurality of plies of composite material that converges within a transition region to define an elongate void space; and
the radius filler of claim 1, wherein the radius filler extends within the elongate void space.

### Claim 6 (depends on 5)

The composite structure of claim 5, wherein the radius filler is operatively affixed to the plurality of plies of composite material.

### Claim 7 (depends on 5)

The composite structure of claim 5, wherein the composite structure includes at least one of an aircraft, a portion of the aircraft, a fuselage barrel of the aircraft, a portion of the fuselage barrel of the aircraft, a wing of the aircraft, a portion of the wing of the aircraft, a stabilizer of the aircraft, and a portion of the stabilizer of the aircraft.

### Claim 8 (depends on 5)

The composite structure of claim 5, wherein a material property gradient of the radius filler corresponds to the material property gradient of the transition region.

### Claim 9 (depends on 5)

The composite structure of claim 5, wherein a material property gradient of the radius filler matches the material property gradient of the transition region to within 20% of the material property gradient of the transition region at an interface between the transition region and the radius filler.

### Claim 10 (depends on 5)

The composite structure of claim 5, wherein the material property gradient of the transition region is at least one of:
(i) a two-dimensional material property gradient of the transition region; and
(ii) a three-dimensional material property gradient of the transition region.

### Claim 11 (depends on 5)

The composite structure of claim 5, wherein the material property gradient of the transition region has a first gradient value in a first direction that extends along the elongate void space, a second gradient value in a second direction that is perpendicular to the first direction, and a third gradient value in a third direction that is perpendicular to the first direction and to the second direction, and further wherein a material property gradient of the radius filler corresponds to the material property gradient of the transition region in at least two of the first direction, the second direction, and the third direction.

### Claim 12 (depends on 5)

The composite structure of claim 5, wherein the material property gradient of the transition region includes a stiffness gradient of the transition region and a material property gradient of the radius filler includes a stiffness gradient of the radius filler.

### Claim 13 (depends on 5)

The composite structure of claim 5, wherein the material property gradient of the transition region includes a coefficient of thermal expansion gradient of the transition region and a material property gradient of the radius filler includes a coefficient of thermal expansion gradient of the radius filler.

### Claim 14 (depends on 5)

The composite structure of claim 5, wherein the material property gradient of the transition region includes a stress gradient of the transition region and a material property gradient of the radius filler includes a stress gradient of the radius filler.

### Claim 15 (depends on 14)

The composite structure of claim 14, wherein the stress gradient of the transition region defines a principal stress region within the transition region and a principal stress direction within the principal stress region, wherein the principal stress direction is measured perpendicular to a longitudinal axis of the elongate void space.

### Claim 16 (depends on 15)

The composite structure of claim 15, wherein each of the plurality of lengths of composite tape includes a respective plurality of lengths of reinforcing fibers, wherein the plurality of lengths of reinforcing fibers in each of the plurality of lengths of composite tape defines a fiber axis direction, and further wherein at least one of the plurality of lengths of composite tape defines a respective fiber axis direction that extends within a portion of the radius filler that is located within the principal stress region and is at least substantially parallel to the principal stress direction.

### Claim 17 (depends on 15)

The composite structure of claim 15, wherein any plane that passes through the radius filler and is perpendicular to the principal stress direction intersects the plurality of lengths of reinforcing fibers of at least one of the plurality of lengths of composite tape.

### Claim 18 (depends on 5)

The composite structure of claim 5, wherein the radius filler at least substantially fills the elongate void space.

### Claim 19 (depends on 5)

The composite structure of claim 5, wherein each of the plurality of lengths of composite tape includes a respective plurality of lengths of reinforcing fibers and a resin material, wherein the material property gradient of the transition region includes a resin shrinkage gradient of the transition region that describes shrinkage of resin material within the plurality of plies of composite material during curing of the composite structure, and further wherein a material property gradient of the radius filler includes a resin shrinkage gradient of the radius filler that describes shrinkage of resin material within the radius filler during curing of the composite structure.

### Claim 20 (depends on 5)

The composite structure of claim 5, wherein the plurality of plies of composite material includes a first ply of composite material, a second ply of composite material, and a third ply of composite material, wherein the first ply of composite material and the second ply of composite material define a first contact region therebetween, wherein the second ply of composite material and the third ply of composite material define a second contact region therebetween, wherein the third ply of composite material and the first ply of composite material define a third contact region therebetween, and further wherein the first contact region, the second contact region and the third contact region terminate within the elongate void space.