Pultrusion systems that apply lengthwise curvature to composite parts

Patent metadata

Field	Value
Publication number	US-11065830-B2
Application number	US-201715498434-A
Country	US
Kind code	B2
Filing date	Apr 26, 2017
Priority date	Apr 26, 2017
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

Systems and methods are provided for applying lengthwise curvature to composite parts. One embodiment is a method that includes fabricating a preform for a curved pultruded gap filler by continuously: heating fiber reinforced material to a sticking point temperature for a constituent material within the fiber reinforced material, and feeding the fiber reinforced material through a die that exhibits a curvature through which the fiber reinforced material travels while the fiber reinforced material is heated to the sticking point temperature, the die forming the fiber reinforced material into a preform for a gap filler. Fabricating the curved pultruded preform further includes varying path lengths of fibers within the preform as the preform passes through the die, and pulling the preform out of the die.

First claim

What is claimed is:

1. A method comprising:
fabricating a preform by continuously:
heating fiber reinforced material, comprising dry fibers and a binder, to a sticking point temperature for the binder that activates binding properties of the binder;
feeding the fiber reinforced material through a die that exhibits a curvature, wherein the fiber reinforced material travels through the curvature while the fiber reinforced material is at least at the sticking point temperature, the die forming the fiber reinforced material into a preform;
varying path lengths of fibers within the preform as the preform passes through the die;
cooling the preform below the sticking point temperature while the fiber reinforced material continues being shaped by the die, by driving pressurized fluid through the die and into direct contact with the preform within a cooling chamber of the die that entirely surrounds a portion of the preform; and
pulling the preform out of the die.

2. The method of claim 1 wherein:
feeding the fiber reinforced material through the die enforces slippage between fibers within the fiber reinforced material that reinforce the fiber reinforced material.

3. The method of claim 1 wherein:
the fiber reinforced material is a tape.

4. The method of claim 3 further comprising:
unwinding the tape from at least one spool.

5. The method of claim 1 wherein:
cooling the preform comprises applying a liquid directly to the preform.

6. The method of claim 1 wherein:
pulling the preform out of the die is performed after the preform has been cooled below the sticking point temperature.

7. The method of claim 1 wherein:
pulling the preform comprises continuously tensioning the preform by operation of driven rollers that clamp the preform and draw the preform out of the die, causing tension to be applied along the length of the fiber reinforced material.

8. The method of claim 1 further comprising:
unwinding, heating, feeding, cooling, and pulling the fiber reinforced material simultaneously at different locations.

9. The method of claim 1 wherein:
heating the fiber reinforced material is performed by a radiant heating element that heats the fiber reinforced material to between 150 and 200 degrees Celsius.

10. The method of claim 1 wherein:
cooling the preform comprises directing gas through the cooling chamber of the die and into passages that are in contact with the die, resulting in forced convective heat transfer.

11. The method of claim 1 wherein:
cooling the preform comprises cooling the die by directing water through the die.

12. The method of claim 1 further comprising:
utilizing a controller that regulates feeding by preventing tension from going outside of a target range, based on input from a sensor monitoring the preform.

13. The method of claim 1 wherein:
heating the fiber reinforced material is performed while the preform is being pulled.

14. The method of claim 1 further comprising:
forming the preform from multiple plies of the fiber reinforced material, wherein each of the multiple plies is sourced by a different spool.

15. The method of claim 1 wherein:
the fiber reinforced material comprises carbon fibers.

16. The method of claim 1 wherein:
the fiber reinforced material comprises a thermoset binder.

17. The method of claim 1 further comprising
utilizing the preform to for laying up a composite part.

18. The method of claim 1 further comprising:
feeding an angled tip of the fiber reinforced material through the die.

19. The method of claim 1 further comprising:
wrapping the preform circumferentially around a roller.

20. The method of claim 19 wherein:
wrapping the preform comprises wrapping the preform into a helical groove defined by the roller.

Assignees

• Boeing Co

Inventors

• Klimovski Andrew
• Ka-Tsun Lai Karlgren
• Zielinski Benjamin Stanislaw

Classifications

• B29B13/04

  by cooling {(cooling moulded articles or half products B29C35/16)} · CPC title

• Y02T50/40

  Weight reduction · CPC title

• B29C70/526 Primary

  Pultrusion dies, e.g. dies with moving or rotating parts (B29C70/523 takes precedence) · CPC title

• B29C70/528

  Heating or cooling · CPC title

• B29C70/527

  Pulling means · CPC title