IP Library › Granted Patent US 12,104,034
Granted Patent B2
US 12,104,034 · App. 18/465,719 · Granted Oct 1, 2024

Expandable media with flexible skin as tooling for composite parts

Inventors: Xiaoxi Wang (Mukilteo, WA); Gary E. Georgeson (Tacoma, WA); Jonathan A. Santiago (Seattle, WA)
Assignee: THE BOEING COMPANY
C08J9/236C08J9/18C08J2201/032C08J2300/22C08J2300/26
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Quick Facts
Patent No.
US 12,104,034
App. No.
18/465,719
Granted
Oct 1, 2024
Kind
B2
Abstract

A method of curing a composite part, including placing an uncured composite part on a mandrel, placing a plurality of expandable pellets on the uncured composite part, expanding the plurality of expandable pellets, applying a positive pressure to the uncured composite part, and curing the uncured composite part.

Claims (38)

1. A method of curing a composite part, comprising:

placing an uncured composite part on a mandrel;

placing a plurality of expandable pellets on the uncured composite part;

expanding the plurality of expandable pellets;

applying a positive pressure to the uncured composite part; and

curing the uncured composite part,

wherein each of the plurality of expandable pellets comprises:

a blowing agent,

a polymer matrix configured to hold the blowing agent, and

a flexible skin configured to encapsulate the polymer matrix and the blowing agent,

wherein the flexible skin is at least partially permeable with respect to the blowing agent or a gas released by the blowing agent, and

wherein the flexible skin is configured to restrict an escape of the blowing agent or the gas released by the blowing agent to control an expansion of each of the plurality of expandable pellets.

2. The method of claim 1 , wherein placing the uncured composite part on the mandrel comprises placing the uncured composite part within a mold holding the mandrel.

3. The method of claim 2 , wherein the mold is configured to hold the plurality of expandable pellets, such that the plurality of expandable pellets apply a positive pressure to the uncured composite part when expanded.

4. The method of claim 1 , wherein the mandrel applies heat to the uncured composite part during a curing process.

5. The method of claim 1 , wherein the uncured composite part defines one or more internal cavities, and wherein placing the plurality of expandable pellets on the uncured composite part comprises placing the plurality of expandable pellets inside the one or more internal cavities.

6. The method of claim 1 , wherein expanding the plurality of expandable pellets comprises expanding the plurality of expandable pellets in response to a predetermined change in condition or triggering event.

7. The method of claim 6 , wherein the predetermined change in condition or triggering event comprises a change in temperature.

8. The method of claim 3 , wherein applying the positive pressure to the uncured composite part comprises applying a positive pressure to the uncured composite part as the plurality of expandable pellets expand within the mold.

9. The method of claim 8 , wherein the plurality of expandable pellets at least partially deform to squeeze into small gaps between the plurality of expandable pellets and inner or outer surfaces of the uncured composite part.

10. The method of claim 8 , wherein the plurality of expandable pellets at least partially deform to squeeze between the plurality of expandable pellets and the mold and mandrel as the plurality of expandable pellets expand.

11. The method of claim 1 , wherein curing the uncured composite part comprises subjecting the uncured composite part to a combination of heat and pressure configured to cure the uncured composite part.

12. The method of claim 11 , wherein curing the uncured composite part comprises curing the uncured composite part while the plurality of expandable pellets apply a positive pressure to the uncured composite part.

13. The method of claim 11 , wherein curing the uncured composite part comprises applying a curing temperature to the uncured composite part.

14. The method of claim 12 , wherein the plurality of expandable pellets apply a consolidation pressure to the uncured composite part.

15. The method of claim 14 , wherein the expandable pellets are the only source of a consolidation pressure applied to the uncured composite part.

16. The method of claim 1 , further comprising:

recharging the plurality of expandable pellets; and

re-using the plurality of expandable pellets.

17. The method of claim 1 , wherein the polymer matrix comprises a thermoplastic polymer.

18. The method of claim 1 , wherein the flexible skin comprises a thermoplastic elastomers (TPE).

19. The method of claim 1 , wherein the blowing agent is configured to release a gas according to a change in condition or triggering event.

20. An expandable pellet for use in the curing of composite parts, comprising:

a blowing agent,

a polymer matrix configured to hold the blowing agent, and

a flexible skin configured to encapsulate the polymer matrix and the blowing agent,

wherein the flexible skin is at least partially permeable with respect to the blowing agent or a gas released by the blowing agent, and

wherein the flexible skin is configured to control an expansion of the expandable pellet.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 12, 2023
From: WANG, XIAOXI; GEORGESON, GARY E.; SANTIAGO, JONATHAN A.
To: THE BOEING COMPANY
Reel/Frame 064880/0705 →
Continuity (2)
Division 17445183 · Aug 16, 2021
Related Publication 20240002624A1 · Jan 4, 2024