IP Library Granted Patent US 11,701,801
Granted Patent B2
US 11,701,801 · App. 16/291,535 · Granted Jul 18, 2023

Caul plate with feature for separating from composite part

Inventors: Daniel J. Wade (Carbonado, WA); Mathew K. Lathrop (Orting, WA)
Assignee: The Boeing Company
B29C37/0003B29C33/3842B29C70/443B29C70/541B29C70/542B29C70/549B29C70/681B29C2043/3655B29L2031/3076B64C3/18
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Quick Facts
Patent No.
US 11,701,801
App. No.
16/291,535
Granted
Jul 18, 2023
Kind
B2
Abstract

Systems and methods are provided for a caul plate having a feature for removal. One embodiment is a caul plate for forming a composite part. The caul plate includes a body that includes a lower surface which faces the composite part, and an upper surface that is opposite to the lower surface. The caul plate also includes a groove in the upper surface to accept a tool to slide the caul plate laterally from the composite part.

Claims (67)

1. An apparatus comprising:

a tool comprising a head;

a mandrel that retains a composite part, and includes sealing tape; and

a caul plate for the composite part, comprising:

a body that includes a lower surface which faces the composite part, and an upper surface that is opposite to the lower surface; and

a groove in the upper surface to accept the tool, that is physically distinct from the caul plate, for temporary attachment, wherein the groove is configured to receive force from the head of the tool that releases the caul plate from the composite part and slides the caul plate laterally from the composite part.

2. The apparatus of claim 1 wherein:

the groove is an indentation into the upper surface having walls to transfer a lateral force of the tool to the caul plate.

3. The apparatus of claim 1 wherein:

the groove is an indentation into the upper surface having a shape to receive the head of the tool.

4. The apparatus of claim 1 wherein:

a shape of the groove corresponds with a shape of the head of the tool.

5. The apparatus of claim 1 wherein:

the tool includes a shank attached to the head to pull the caul plate laterally.

6. The apparatus of claim 1 wherein:

the upper surface faces a vacuum bag during cure of the composite part.

7. The apparatus of claim 1 wherein:

the caul plate is made of a rigid material.

8. A method of fabricating a composite part, the method comprising:

providing a tool comprising a head,

machining a groove into an upper surface of a caul plate sized to receive the head of the tool;

positioning a lower surface of the caul plate on top of a preform;

curing the preform into the composite part;

inserting the tool into the groove in the upper surface of the caul plate for temporary attachment; and

removing the caul plate from the composite part by actuating the tool laterally to slide the caul plate off the composite part, wherein the composite part is retained by a mandrel and the mandrel includes sealing tape.

9. The method of claim 8 wherein:

the groove is an indentation into the upper surface having walls to transfer a lateral force of the tool to the caul plate.

10. The method of claim 8 wherein:

the groove is an indentation into the upper surface having a shape to receive the head of the tool.

11. The method of claim 8 wherein:

a shape of the groove corresponds with a shape of the head of the tool.

12. The method of claim 8 wherein:

the tool includes a shank attached to the head to pull the caul plate laterally.

13. The method of claim 8 wherein:

the upper surface faces a vacuum bag during the curing.

14. An apparatus comprising:

a tool comprising a head;

a mandrel that retains a composite part, and includes sealing tape; and

a caul plate for the composite part, comprising:

a body that includes a lower surface which faces the composite part, and an upper surface that is opposite to the lower surface;

a structural member directly protruding from the upper surface; and

a hole in the structural member to receive the tool, that is physically distinct from the caul plate, for temporary attachment, wherein the hole is configured to receive force from the head of the tool that releases the caul plate from the composite part and slides the caul plate laterally from the composite part, wherein

the body is U-shaped, with side members and a base member forming the body, and the structural member comprises a fin protruding vertically from the base member to align with a stringer of an aircraft.

15. The apparatus of claim 14 wherein:

each of the side members is integral with the base member.

16. The apparatus of claim 14 wherein:

the hole extends through the structural member to transfer a lateral force of the tool to the caul plate.

17. The apparatus of claim 16 wherein:

the tool includes a hook to insert through the hole to pull the caul plate laterally.

18. The apparatus of claim 16 wherein:

the tool includes a pin to insert through the hole to pull the caul plate laterally.

19. The apparatus of claim 14 wherein:

the structural member is integrated with the body of the caul plate.

20. The apparatus of claim 19 wherein:

the structural member and the body are made of a rigid material.

21. The apparatus of claim 1 wherein:

the groove is bounded by a floor that is sunken into the body.

22. The apparatus of claim 1 wherein:

the groove is disposed within a region of a tapered edge at the caul plate.

23. The apparatus of claim 1 wherein:

the caul plate is made of an elastically deformable shape memory material.

24. The apparatus of claim 14 wherein:

the hole comprises a hole indentation.

25. The apparatus of claim 14 wherein:

the hole is disposed within a region of a tapered edge at the caul plate.

26. The apparatus of claim 14 wherein:

the caul plate is made of an elastically deformable shape memory material.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 4, 2019
From: WADE, DANIEL J.; LATHROP, MATHEW K.
To: THE BOEING COMPANY
Reel/Frame 048493/0928 →
Continuity (1)
Related Publication 20200282669A1 · Sep 10, 2020