Mandrel for autoclave curing applications

Patent metadata

Field	Value
Publication number	US-9238335-B2
Application number	US-35092809-A
Country	US
Kind code	B2
Filing date	Jan 8, 2009
Priority date	Jul 10, 2008
Publication date	Jan 19, 2016
Grant date	Jan 19, 2016

Abstract

A mandrel used to cure a composite part layup has an elastic body and at least one internal open space therein. The internal open space is configured to allow substantially uniform thermal expansion of the body during curing.

First claim

What is claimed is:

1. A method of fabricating a composite part, comprising:
forming a mandrel, said mandrel a single unitary component having a generally solid body of elastic material;
determining thermal expansion characteristics of the mandrel;
forming at least one internal open space in the mandrel that will result in substantially uniform thermal expansion of the mandrel during curing of the composite part, thereby creating an opening in the mandrel, and forming includes selecting, based on the thermal expansion characteristics, a shape of the opening that will result in the substantially uniform thermal expansion;
placing a composite part layup over the mandrel; and
curing the composite part.

2. The method of claim 1 , further comprising:
selecting the shape of the opening using finite element analysis.

3. The method of claim 1 , wherein forming the at least one internal open space and forming the mandrel are performed substantially simultaneously.

4. The method of claim 1 , wherein forming the at least one internal open space includes forming an opening passing longitudinally through the mandrel.

5. The method of claim 1 , further comprising:
forming a plurality of internal open spaces in the mandrel body collectively configured to allow substantially uniform thermal expansion of the body.

6. The method of claim 1 , wherein forming the at least one internal open space includes selecting a cross sectional shape and a position of the at least one internal open space within the mandrel.

7. The method of claim 1 , wherein curing the composite part layup is performed in an autoclave.

8. A method of fabricating a composite part, comprising:
selecting an elastic mandrel material;
determining thermal expansion characteristics of the elastic mandrel material;
selecting an external shape of the mandrel;
forming the elastic mandrel material into the selected mandrel shape, said mandrel a single unitary component having a generally solid body;
performing, using the thermal expansion characteristics, a finite element analysis to determine a size, a number, and a cross sectional shape of a plurality of internal open spaces within in the mandrel that will result in substantially uniform thermal expansion of the mandrel;
forming the internal open spaces within the mandrel based on results of the finite element analysis;
placing a composite part layup over the mandrel; and
curing the composite part in an autoclave using the mandrel.

Assignees

• Robins Brian G
• Willden Kurtis
• Hunter Ethan W
• Mcmanus Nika
• Boeing Co

Inventors

• Robins Brian G
• Willden Kurtis
• Hunter Ethan W
• Mcmanus Nika

Classifications

• B29C33/76

  Cores (B29C33/02 - B29C33/70, {B29C41/40, B29C53/74, B29C53/82} take precedence) · CPC title

• B29C33/405

  Elastomers, e.g. rubber (B29C33/50 takes precedence) · CPC title

• B29C70/44 Primary

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title

• B64C1/065

  Spars · CPC title

• B29D99/001

  Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings (articles with hollow walls B29D24/00) · CPC title