Systems and tooling for manufacturing composite parts and related methods

Patent metadata

Field	Value
Publication number	US-9895848-B2
Application number	US-201514693363-A
Country	US
Kind code	B2
Filing date	Apr 22, 2015
Priority date	Apr 22, 2015
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

Disclosed systems and tooling for manufacturing flanged ducts may improve upon prior art manufacturing techniques, such as by increasing ease of manufacturing and/or quality of resulting parts formed by the systems and tooling. One example of tooling includes a first tool piece that may be coupled to a base, and a second tool piece that is selectively coupled to and removable from the first tool piece. When positioned together in a closed position, the first tool piece and second tool piece form a composite material-receiving surface and a flange surface on which composite material may be placed and cured in order to form a composite part, such as a flanged duct. Such tooling may allow for placement of composite material over a male radius of the tooling, thereby improving ergonomics of the manufacturing process, as compared to attempting to place composite material into a female radius of prior art tooling.

First claim

The invention claimed is:

1. A tool for manufacturing a composite part, the tool comprising:
a first tool piece comprising a first flange surface, a second flange surface opposite the first flange surface, and a first composite material-receiving surface extending from the first flange surface to the second flange surface, wherein the first flange surface is arranged at a non-parallel angle with respect to the second flange surface; and
a second tool piece comprising a third flange surface, a fourth flange surface opposite the third flange surface, and a second composite material-receiving surface extending from the third flange surface to the fourth flange surface, wherein the tool is configured to be selectively moved between a closed position and an open position, wherein, in the closed position, the second tool piece is positioned adjacent the first tool piece, the third flange surface and the first flange surface are parallel to one another, the second flange surface and the fourth flange surface are parallel to one another, and the first composite material-receiving surface is arranged facing the second composite material-receiving surface such that the first composite material-receiving surface and the second composite material-receiving surface define a tool space in which the composite part may be formed, the tool space having a longitudinal tool axis extending through a center of the tool space, from the first flange surface towards the second flange surface, wherein, in the closed position, the first composite material-receiving surface and the second composite material-receiving surface are configured to receive a composite material that is configured to form the composite part, and wherein, in the open position, at least a portion of the second tool piece is spaced apart from the first tool piece.

2. The tool according to claim 1 , wherein the first tool piece comprises a first flange plate and a second flange plate, the first flange plate defining the first flange surface and a first inner surface, the second flange plate defining the second flange surface and a second inner surface, wherein the first flange plate and the second flange plate are arranged such that the first inner surface and the second inner surface face one another, wherein the second tool piece comprises a third flange plate and a fourth flange plate, the third flange plate being defined by the third flange surface and a third inner surface, the fourth flange plate being defined by the fourth flange surface and a fourth inner surface, and wherein the third flange plate and the fourth flange plate are arranged such that the third inner surface and the fourth inner surface face one another, the tool further comprising:
a plurality of first spacer plates positioned between the first flange plate and the second flange plate of the first tool piece, each of the first spacer plates having a first upper spacer surface and a first lower spacer surface separated by a first thickness that defines a first coupling surface extending around a first spacer perimeter, a first portion of the first coupling surface being coupled to the first inner surface and a second portion of the first coupling surface being coupled to the second inner surface; and
a plurality of second spacer plates positioned between the third flange plate and the fourth flange plate of the second tool piece, each of the second spacer plates having a second upper spacer surface and a second lower spacer surface separated by a second thickness that defines a second coupling surface extending around a second spacer perimeter, a first portion of the second coupling surface being coupled to the third inner surface and a second portion of the second coupling surface being coupled to the fourth inner surface.

3. The tool according to claim 2 , further comprising a removable cover configured to be placed on the tool such that it at least partially covers a first gap between the first flange plate and the second flange plate, and such that it at least partially covers a second gap between the third flange plate and the fourth flange plate, wherein the removable cover is configured to engage at least a portion of the plurality of first spacer plates and at least a portion of the plurality of second spacer plates.

4. A system configured for manufacturing a composite part from a composite material, the composite part comprising a tubular portion extending from a first end to a second end, and a first flange extending radially outward from the tubular portion, the first flange being positioned adjacent the first end of the tubular portion and being formed integrally with the tubular portion, the system comprising:
a tool, the tool comprising:
a first tool piece comprising a first flange surface, a second flange surface opposite the first flange surface, and a first composite material-receiving surface extending from the first flange surface to the second flange surface, wherein the first flange surface is arranged at a non-parallel angle with respect to the second flange surface; and
a second tool piece comprising a third flange surface, a fourth flange surface opposite the third flange surface, and a second composite material-receiving surface extending from the third flange surface to the fourth flange surface, wherein the tool is configured to be selectively moved between a closed position and an open position, wherein, in the closed position, the second tool piece is positioned adjacent the first tool piece, the third flange surface and the first flange surface are parallel to one another, the second flange surface and the fourth flange surface are parallel to one another, and the first composite material-receiving surface is arranged facing the second composite material-receiving surface such that the first composite material-receiving surface and the second composite material-receiving surface define a tool space in which the composite part may be formed, the tool space having a longitudinal tool axis extending through a center of the tool space, from the first flange surface towards the second flange surface, and wherein, in the open position, at least a portion of the second tool piece is spaced apart from the first tool piece; and

a vacuum device configured to draw a vacuum against the first composite material-receiving surface, the second composite material-receiving surface, and the first flange surface of the tool, such that the composite material received thereon is pressed against the first composite material-receiving surface, the second composite material-receiving surface, and the first flange surface of the tool, wherein the system is configured to cure the composite material, thereby forming the composite part, the composite part being selectively removable from the tool after it is cured.

5. The system according to claim 4 , further comprising the composite material, wherein the composite material is a pre-impregnated composite fabric material.

6. The system according to claim 4 , further comprising a heat source configured to apply heat and pressure to the composite material and the tool.

7. The system according to claim 4 , further comprising the composite part and the composite material, wherein the composite part comprises a part inner surface and a part outer surface, the part inner surface defining a hollow interior space inside the composite part, wherein the composite material comprises a material inner surface and an opposite, material outer surface, wherein the system is configured such that the composite material is placed such that the material outer surface is placed on the first composite material-receiving surface and the second composite material-receiving surface of the tool, wherein the material outer surface is configured to bec

Assignees

• Boeing Co

Inventors

• Thompson Michael P
• Layton Otis Franklin

Classifications

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29C70/446

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• B29C70/443 Primary

  and impregnating by vacuum or injection · CPC title

• B29L2031/30

  Vehicles, e.g. ships or aircraft, or body parts thereof {(vanes or blades B29L2031/08, air bags B29L2022/027)} · CPC title

• B29C70/342

  using isostatic pressure · CPC title