Method for manufacturing composite airfoils

Patent metadata

Field	Value
Publication number	US-10773464-B2
Application number	US-201715819057-A
Country	US
Kind code	B2
Filing date	Nov 21, 2017
Priority date	Nov 21, 2017
Publication date	Sep 15, 2020
Grant date	Sep 15, 2020

Abstract

The present disclosure is directed to an apparatus and method for manufacturing a composite component. The apparatus includes a mold onto which the composite component is formed. The mold is disposed within a grid defined by a first axis and a second axis. The apparatus further includes a first frame assembly disposed above the mold and a plurality of machine heads coupled to the first frame assembly within the grid in an adjacent arrangement along the first axis. At least one of the mold or the plurality of machine heads is moveable along the first axis, the second axis, or both. At least one of the machine heads of the plurality of machine heads is moveable independently of one another along a third axis. A second frame assembly is moveable above the mold along the first axis, the second axis, or both. The second frame assembly includes a holding device. The holding device affixes to and releases from an outer skin to place and displace the outer skin at the mold.

First claim

What is claimed is:

1. A method of manufacturing a composite component, the method comprising:
placing one or more fiber-reinforced outer skins on a mold via a holding device moveable along one or more of a first axis, a second axis, and a third axis;
applying pressure onto the one or more fiber-reinforced outer skin and the mold to seal at least a perimeter of the one or more fiber-reinforced outer skins onto the mold;
heating at least a portion of the one or more fiber-reinforced outer skins to at least a first temperature threshold, wherein the first temperature threshold corresponds to a temperature at least approximately between a glass transition temperature and a melting temperature of a resin in the one or more fiber-reinforced outer skins; and,
forming a plurality of rib members that intersect at a plurality of nodes to form at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more fiber-reinforced outer skins, wherein the grid structure bonds to the one or more fiber-reinforced outer skins as the grid structure is being deposited.

2. The method of claim 1 , further comprising:
applying, via the holding device, heat to at least a portion of the fiber-reinforced outer skins.

3. The method of claim 1 , wherein applying pressure onto the one or more fiber-reinforced outer skins comprises pulling the one or more fiber-reinforced outer skins onto the mold via a vacuum applied through a surface of the mold, through the one or more fiber-reinforced outer skins, or both.

4. The method of claim 3 , wherein applying pressure onto the one or more fiber-reinforced outer skins comprises pressing the one or more fiber-reinforced outer skins onto the mold at least along the third axis via the holding device.

5. The method of claim 1 , wherein the plurality of rib structures comprises, at least, a first rib structure extending in a first direction and a second rib structure extending in a different, second direction, at least one of the first rib member or the second rib member having a varying height along a length thereof.

6. The method of claim 1 , wherein forming the plurality of rib members comprises printing and depositing the grid structure via a material deposition tool.

7. The method of claim 1 , wherein forming the plurality of rib members comprises applying a composite fiber tape onto the inner surface of the one or more fiber-reinforced outer skins via a tape deposition tool.

8. The method of claim 1 , further comprising:
translating, via a first frame assembly, a plurality of machine heads along the first axis, the second axis, or the third axis proximate to the one or more fiber-reinforced outer skins.

9. The method of claim 1 , further comprising:
translating, via a second frame assembly, the holding device along the first axis, the second axis, or the third axis.

10. The method of claim 1 , wherein forming the plurality of rib structures is via a plurality of machine heads arranged along at least one of the first axis or the second axis, and wherein at least one of the plurality of machine heads is independently moveable along the third axis.

11. A method of manufacturing a plurality of composite components, the method comprising:
placing a first fiber-reinforced outer skin onto a first mold via a holding device moveable along one or more of a first axis, a second axis, and a third axis;
applying pressure onto the first outer skin and the first mold to seal at least a perimeter of the first outer skin onto the first mold;
heating at least a portion of the first fiber-reinforced outer skin to at least a first temperature threshold;
forming a plurality of rib members that intersect at a plurality of nodes to form at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more first fiber-reinforced outer skins, wherein the grid structure bonds to the one or more first fiber-reinforced outer skins as the grid structure is being deposited;
placing a second fiber-reinforced outer skin onto a second mold via the holding device, wherein the second mold is disposed adjacent to the first mold;
heating at least a portion of the second fiber-reinforced outer skin to at least the first temperature threshold;
applying pressure onto the second outer skin and the second mold to seal at least a perimeter of the second outer skin onto the second mold;
forming a plurality of rib members that intersect at a plurality of nodes to form at least one three-dimensional (3-D) reinforcement grid structure onto an inner surface of the one or more second fiber-reinforced outer skins, wherein the grid structure bonds to the one or more second fiber-reinforced outer skins as the grid structure is being deposited; and
removing the first outer skin from the first mold via the holding device.

12. The method of claim 11 , further comprising:
applying, via the holding device, heat to at least a portion of the second fiber-reinforced outer skin.

13. The method of claim 11 , further comprising:
translating, via a first frame assembly, a plurality of machine heads along one or more of the first axis, the second axis, or the third axis proximate to the first outer skin; and
translating, via a second frame assembly, the holding device along one or more of the first axis, the second axis, or the third axis proximate to the second mold when the plurality of machine heads is proximate to the first outer skin at the first mold.

14. The method of claim 11 , further comprising:
translating, via a first frame assembly, a plurality of machine heads along one or more of the first axis, the second axis, or the third axis proximate to the second outer skin; and
translating, via a second frame assembly, the holding device along one or more of the first axis, the second axis, or the third axis proximate to the first mold when the plurality of machine heads is proximate to the second outer skin at the second mold.

Assignees

• Gen Electric

Inventors

• Tobin James Robert
• Johnson Stephen Bertram

Classifications

• B29C70/38 Primary

  Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns {(application heads for tyres B29D30/28)} · CPC title

• B29C66/721 Primary

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title

• Y02P70/50

  Manufacturing or production processes characterised by the final manufactured product · CPC title

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title

• B33Y70/00

  Materials specially adapted for additive manufacturing · CPC title