Methods and apparatuses for forming composite parts from multi-ply prepreg composite charges

Patent metadata

Field	Value
Publication number	US-12275201-B2
Application number	US-202117384440-A
Country	US
Kind code	B2
Filing date	Jul 23, 2021
Priority date	Oct 8, 2020
Publication date	Apr 15, 2025
Grant date	Apr 15, 2025

Abstract

A method of forming a composite part from a mufti-ply prepreg composite charge comprises reducing pressure inside a bladder, located in a chamber that is at atmospheric pressure, below the atmospheric pressure. The method also comprises placing the multi-ply prepreg composite charge, having a first shape, in the chamber and reducing pressure inside the chamber below the atmospheric pressure. The method additionally comprises, while maintaining pressure inside the chamber below the atmospheric pressure, expanding the bladder within the chamber by increasing pressure inside the bladder to the atmospheric pressure, so that the multi-ply prepreg composite charge is compressed between the bladder and a forming tool, which is located inside the chamber, and the multi-ply prepreg composite charge is configured by the forming tool to a second shape, different from the first shape. The method also comprises curing the multi-ply prepreg composite charge, having the second shape.

First claim

What is claimed is:

1. A method of forming a composite part from a multi-ply prepreg composite charge, the method comprising steps of:
reducing pressure inside a bladder, located in a chamber that is at atmospheric pressure, below the atmospheric pressure;
placing the multi-ply prepreg composite charge, having a first shape, in the chamber;
reducing pressure inside the chamber below the atmospheric pressure;
while maintaining the pressure inside the chamber below the atmospheric pressure, expanding the bladder within the chamber by increasing the pressure inside the bladder to the atmospheric pressure, so that:
the bladder comprises a first bladder volume and a second bladder volume;
a forming tool is positioned between the first bladder volume and the second bladder volume;
the multi-ply prepreg composite charge is compressed between the bladder and the forming tool; and
the multi-ply prepreg composite charge is configured by the forming tool to a second shape, different from the first shape; and

curing the multi-ply prepreg composite charge, having the second shape, by recirculating hot air between the first bladder volume and the second bladder volume to heat the multi-ply prepreg composite using the bladder.

2. The method according to claim 1 , wherein, during the step of reducing the pressure inside the chamber below the atmospheric pressure, the multi-ply prepreg composite charge is separated from the forming tool by a gap.

3. The method according to claim 2 , wherein:
the chamber comprises a chamber housing and a chamber lid, coupled to the chamber housing and pivotable relative to the chamber housing;
the step of reducing the pressure inside the chamber below the atmospheric pressure and the step of expanding the bladder within the chamber by increasing the pressure inside the bladder to the atmospheric pressure while maintaining the pressure inside the chamber below the atmospheric pressure each comprises providing a seal between the chamber lid and the chamber housing; and
the forming tool is attached to and is supported by the chamber lid.

4. The method according to claim 1 , further comprising a step of heating the mufti-ply prepreg composite charge before the step of expanding the bladder within the chamber.

5. The method according to claim 4 , wherein the step of heating the mufti-ply prepreg composite charge before the step of expanding the bladder within the chamber is performed after the step of reducing the pressure inside the chamber below the atmospheric pressure.

6. The method according to claim 4 , wherein the step of heating the multi-ply prepreg composite charge before the step of expanding the bladder within the chamber and the step of reducing the pressure inside the chamber below the atmospheric pressure are performed concurrently.

7. The method according to claim 4 , wherein:
the step of heating the multi-ply prepreg composite charge before the step of expanding the bladder within the chamber is performed using a heater; and
the bladder is positioned between the heater and the multi-ply prepreg composite charge.

8. The method according to claim 4 , wherein the step of heating the multi-ply prepreg composite charge before the step of expanding the bladder within the chamber is performed using a bladder surface heater, incorporated into the bladder.

9. The method according to claim 4 , wherein the step of heating the multi-ply prepreg composite charge before the step of expanding the bladder within the chamber is performed using a blanket heater, positioned between the bladder and the multi-ply prepreg composite charge.

10. The method according to claim 9 , wherein the step of curing the multi-ply prepreg composite charge comprises heating the multi-ply prepreg composite charge using the blanket heater, positioned between the multi-ply prepreg composite charge and the forming tool.

11. The method according to claim 1 , wherein the step of expanding the bladder within the chamber comprises fluidically coupling the bladder to atmosphere.

12. The method according to claim 1 , wherein the step of curing the multi-ply prepreg composite charge comprises heating the multi-ply prepreg composite charge using a forming-tool heater, incorporated into the forming tool.

13. The method according to claim 1 , further comprising a step of heating the multi-ply prepreg composite charge using a bladder surface heater, incorporated into the bladder.

14. The method according to claim 1 , further comprising a step of introducing the hot air into the bladder.

15. The method according to claim 1 , wherein the step of recirculating the hot air between the first bladder volume and the second bladder volume is performed using a thermal module, fluidically coupled to the first bladder volume and the second bladder volume.

16. The method according to claim 1 , wherein the first bladder volume is fluidically coupled to the second bladder volume via a duct, external to the bladder.

17. The method according to claim 1 , wherein the first bladder volume is fluidically coupled to the second bladder volume via a passage, internal to the bladder.

18. A composite forming method comprising:
positioning a multi-ply prepreg composite charge having a first shape in a chamber between a bladder and a forming tool;
reducing a pressure inside the chamber below atmospheric pressure;
with the pressure inside the chamber below the atmospheric pressure, increasing a pressure inside the bladder to the atmospheric pressure to expand the bladder such that:
the bladder comprises a first bladder volume and a second bladder volume; and
the forming tool is positioned between the first bladder volume and the second bladder volume;

compressing the multi-ply prepreg composite charge between the bladder and the forming tool into a second shape that is different from the first shape; and
circulating hot air between the first bladder volume and the second bladder volume to heat the multi-ply prepreg composite using the bladder and to cure the multi-ply prepreg composite charge in the second shape.

19. The composite forming method of claim 18 , further comprising reducing the pressure inside the bladder below the atmospheric pressure to separate the multi-ply prepreg composite charge from the forming tool by a gap before reducing the pressure inside the chamber below the atmospheric pressure.

20. The composite forming method of claim 18 , further comprising recirculating the hot air between the first bladder volume and the second bladder volume using a thermal module that is fluidically coupled to the first bladder volume and the second bladder volume.

Assignees

• Boeing Co

Inventors

• Modin Andrew E
• Martin Dorekia
• Heath Richard E
• Anderson Eric C
• Handolescu Caleb J
• Prause Richard Alexander
• Hargrove Michael C
• Register Justin H

Classifications

• B29L2031/3076

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

• B29C70/54

  Component parts, details or accessories; Auxiliary operations {, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing} · CPC title

• B29C43/52

  Heating or cooling · CPC title

• B29C43/56

  Compression moulding under special conditions, e.g. vacuum · CPC title

• B29C2043/561

  under vacuum conditions · CPC title