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Tool Design for Composite part cured in Vacuum bag Autoclave method

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Aerospace
Feb 21, 2012
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I have started design of tool (Mold/Fixture) that can be used to make composite part by vacuum bag method. Composite final envelop dimension is 35L X 16W X 3H (inches). Looking for tooling design guidelines what the parameters to consider?
Material option for tooling: Alum, Steel, Invar
 
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Cure temp: 120 deg Celsius
Heating method: Vacuum bag Autoclave
Dimensional tolerance: General tolerance
Laminate or sandwich: prepeg laminate
Qty: TBD
 
There are many materials that can be used as a tooling material.
If the mold is not split type that needs to be screwed together you can use soft material - epoxy tooling board - for instance Renshape BM5060. This material is temp resistance up to 140 C and very easy to mill / machine.

If mold is split then use aluminum.

Most carbon fiber manufacturer use aluminum or epoxy tooling boards as a material for the tooling.
If you need to produce many parts per day, then making 1 master model (from aluminum or epoxy tooling board) and then molding as much composite molds (using epoxy resin and carbon or glass fabric) as needed on this master model is preferred.

You can read more practical tips about carbon composites here: [URL unfurl="true"]http://www.dexcraft.com/carbon-fiber-composites[/url]

Carbon fiber composites
 
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