Method and apparatus for forming contoured composite laminates

Patent metadata

Field	Value
Publication number	US-10399284-B2
Application number	US-201615240529-A
Country	US
Kind code	B2
Filing date	Aug 18, 2016
Priority date	May 16, 2014
Publication date	Sep 3, 2019
Grant date	Sep 3, 2019

Abstract

A composite laminate such as a hat-type stringer is formed on a contoured mandrel using a combination of mechanical sweeping and vacuum forming.

First claim

What is claimed is:

1. Apparatus for forming plies of material onto a mandrel having contours, comprising:
a ply sweeper comprising a plurality of fingers configured to deflect outwardly to sweep the plies onto the contours of the mandrel;
a presser independently displaceable relative to the ply sweeper for pressing a portion of the plies against the mandrel, the presser including a rib connected to at least one powered actuator, and a pair of flexible wings extending outwardly from the rib and engageable with the mandrel; and
the at least one powered actuator coupled with the presser for displacing the presser relative to the ply sweeper.

2. The apparatus of claim 1 , wherein the ply sweeper includes a tube having a plurality of slots therein and the plurality of fingers defined between the slots configured to engage and press the plies against the contours of the mandrel.

3. The apparatus of claim 1 , wherein:
the powered actuator includes a pneumatic cylinder having a cylinder rod, and
a coupling connecting an end of the cylinder rod with the presser.

4. The apparatus of claim 3 , wherein the coupling includes a slot in the presser and a pivotal connection slidable within the slot.

5. The apparatus of claim 1 , wherein:
the presser includes a plurality of presser sections attached to each other and arranged end-to-end, and
each of the presser sections is formed of a flexible material allowing the presser to conform to the contours of the mandrel.

6. Apparatus for forming composite plies on a mandrel contoured along its length and having a cap, a pair of webs and a pair of flanges configured to form a hat-shaped stringer, comprising:
a frame;
a ply sweeper mounted on the frame and configured to sweep the composite plies down onto and over the pair of webs of the mandrel using a plurality of fingers of the ply sweeper configured to deflect outwardly;
a presser mounted on the frame and extendable relative to the ply sweeper, the presser being configured to press a portion of the composite plies against the cap of the mandrel, the presser including a rib connected to at least one linear actuator and a pair of flexible wings extending outwardly from the rib and engageable with the mandrel; and
the at least one linear actuator mounted on the frame and coupled with the presser for extending the presser relative to the ply sweeper.

7. The apparatus of claim 6 , wherein:
the ply sweeper includes a tube having a plurality of slots therein and fingers defined between the slots configured to engage and press the composite plies against the webs of the mandrel.

8. The apparatus of claim 6 , wherein the at least one linear actuator is a pneumatic cylinder mounted on the frame and having a displaceable piston rod coupled with the presser.

9. The apparatus of claim 6 , wherein:
the ply sweeper includes opposing sets of spaced apart, flexible fingers having fingertips, and
the presser is extendable by the at least one linear actuator beneath the fingertips.

10. The apparatus of claim 6 , wherein:
the presser includes a plurality of presser sections attached together and arranged end-to-end, and
the presser is formed of a flexible material allowing the presser to conform to the contoured length of the mandrel.

11. The apparatus of claim 6 , further comprising:
a coupling between the at least one linear actuator and the presser allowing the presser to conform to the contour of the mandrel.

12. The apparatus of claim 11 , wherein the coupling includes a slot in the presser and a pivotal connection slidable within the slot connecting the presser with the at least one linear actuator.

13. A method of forming a composite stiffener contoured along its length, comprising:
placing at least one composite ply over a mandrel;
positioning a ply sweeper and a presser above the mandrel, wherein the ply sweeper comprises a plurality of fingers configured to deflect outwardly to sweep the at least one composite ply onto contours of the mandrel, and wherein the presser includes a rib connected to at least one powered actuator, and a pair of flexible wings extending outwardly from the rib and engageable with the mandrel;
extending the presser relative to the ply sweeper using the at least one powered actuator coupled to the presser;
clamping a portion of the composite ply against the mandrel, including moving the presser and the ply sweeper toward the mandrel until the presser forces the portion of the composite ply against the mandrel; and
sweeping the composite ply down over the mandrel using the plurality of fingers while the portion of the composite ply is clamped against the mandrel.

14. The method of claim 13 , wherein extending the presser includes extending a pair of piston rods.

15. The method of claim 14 , further comprising:
retracting the pair of piston rods as the ply sweeper sweeps the composite ply down over the mandrel.

16. The method of claim 13 , further comprising:
attaching a plurality of presser sections together end-to-end; and
pivotally coupling the presser with the powered actuator to allow the presser to conform to the contoured length of the mandrel.

17. The method of claim 13 , wherein clamping a portion of the composite ply against the mandrel includes applying a force to the presser using the powered actuator.

18. The method of claim 13 , wherein clamping a portion of the composite ply against the mandrel includes centering the presser on the mandrel using the flexible wings of the presser.

Assignees

• Boeing Co

Inventors

• Prause Richard Alexander
• Modin Andrew Elmer

Classifications

• B29C70/543

  Fixing the position or configuration of fibrous reinforcements before or during moulding (for non-woven fabrics D04H3/08) · CPC title

• B29K2263/00

  Use of {EP, i.e.} epoxy resins {or derivatives thereof} as reinforcement · CPC title

• B29K2307/04

  Carbon · CPC title

• B29L2009/00

  Layered products · CPC title

• B29C70/342

  using isostatic pressure · CPC title