Out-of-Autoclave Prepreg Introduction - Centre of Structure ...
Out-of-Autoclave Prepreg Introduction - Centre of Structure ...
Out-of-Autoclave Prepreg Introduction - Centre of Structure ...
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<strong>Out</strong>-<strong>of</strong>-<strong>Autoclave</strong> <strong>Prepreg</strong> <strong>Introduction</strong><br />
Advanced Composites Processing<br />
Bryan Louis
<strong>Out</strong>line<br />
• <strong>Introduction</strong> (OOA prepreg)<br />
• Examples<br />
• History<br />
• Modern OOA prepreg development<br />
• Summary<br />
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<strong>Out</strong>-<strong>of</strong>-<strong>Autoclave</strong> <strong>Prepreg</strong>s<br />
• <strong>Prepreg</strong>s designed specifically for processing without the autoclave<br />
• Potential processing cost reduction<br />
• <strong>Autoclave</strong>s are expensive equipment capital<br />
• Less expensive tooling material (OOA typically low-moderate cure<br />
temperature)<br />
• *Energy savings<br />
• Larger manufacturer and subcontractor base<br />
• No size limitations imposed by the autoclave<br />
• Large interest in aerospace sector<br />
• Including primary structures<br />
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<strong>Out</strong>-<strong>of</strong>-<strong>Autoclave</strong> <strong>Prepreg</strong> Applications<br />
• Major application sectors <strong>of</strong> OOA prepreg:<br />
• Marine<br />
• Infrastructure<br />
• Wind energy<br />
• Tidal energy<br />
• Prototyping in aerospace<br />
• Airplane structures<br />
• Tooling<br />
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<strong>Out</strong>-<strong>of</strong>-<strong>Autoclave</strong> <strong>Prepreg</strong>s<br />
vs<br />
• Resin system designed for oven cure<br />
• Vacuum-bag-only processing<br />
• Target: laminate properties comparable to autoclave processing<br />
Traditional OOA prepregs have a HIGH final void content<br />
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Key differences from autoclave prepreg<br />
• <strong>Autoclave</strong> prepreg (AC)<br />
• Typical cure temperatures 180C<br />
• Laminate quality (void reduction) achieved by hydrostatic pressure forcing entrapped<br />
air and volatiles into solution<br />
• <strong>Out</strong>-<strong>of</strong>-autoclave prepreg (OOA)<br />
• Low cost oven/vacuum bag process<br />
• Laminate quality (void reduction) achieved by extracting entrapped gases and<br />
volatiles prior to gelation<br />
• “breathable” prepregs<br />
• Viscosity during cure cycle (Rheology) critical – remain “breathable” for sufficient time<br />
• AC prepregs cannot simply be cured out <strong>of</strong> autoclave<br />
• High voidage!<br />
• Resin rheology is not tuned for dependence on vacuum extraction <strong>of</strong> entrapped gases<br />
and volatiles<br />
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Examples<br />
• Spaceship 2 and White<br />
Knight 2 (Virgin Galactic)<br />
• Scaled Composites<br />
(California, USA)<br />
• OOA Material: Advanced<br />
Composites Group<br />
MTM45-1 (Umeco)<br />
Source: http://www.virgingalactic.com/multimedia/album/graphics-and-illustrations/<br />
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Examples<br />
• Bombardier Learjet 85<br />
• Bombardier Aerospace<br />
• Fuselage and wings<br />
• OOA Material: Cytec<br />
5320<br />
Source: http://www.learjet85.com/en/multimedia.html#a64-74<br />
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History<br />
• Original OOA systems not for structural applications<br />
• Low mechanical properties<br />
• Developed for prototyping<br />
• Oven cure only<br />
• Low temperature cure (cheap tooling)<br />
• Early attempts for processing autoclave prepreg oven-only<br />
was unsuccessful<br />
• Years for prepreg manufacturers to understand OOA<br />
material requirements<br />
• Void removal without high applied pressure<br />
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Source: SAMPE Seattle OOA tutorial. Chris Ridgard, 2010<br />
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Source: SAMPE Seattle tutorial. Chris Ridgard, 2010<br />
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Modern OOA <strong>Prepreg</strong> development<br />
• Newer OOA prepreg systems has been aided by a better<br />
understanding <strong>of</strong> mechanisms <strong>of</strong> air extraction<br />
• Tailoring resin rheology<br />
• Modern OOA prepreg systems developed early 2000’s<br />
• Quality similar to autoclave processed prepreg systems<br />
• Void free<br />
• Similar mechanical performance<br />
Source: SAMPE Seattle OOA<br />
tutorial. Chris Ridgard, 2010<br />
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Modern OOA <strong>Prepreg</strong> development<br />
• Low void content is achieved by “breathing” out <strong>of</strong><br />
entrapped gases and volatiles<br />
• Partial impregnations<br />
• Resin rheology<br />
• Air pathways can be created by partially impregnating<br />
prepreg<br />
• Initial dry regions (prior to cure) are wetted out during resin cure<br />
cycle<br />
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Boeing demonstrator launch fairing<br />
• Constructed <strong>of</strong> Cytec 5320 prepreg<br />
Sectioned Boeing fairing<br />
Cross-section cut <strong>of</strong> laminate<br />
Source: Composites World. www.compositesworld.com<br />
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America’s cup racing boat<br />
• Team Alinghi 2003 America’s cup challenger<br />
Source: Advanced Composites Group<br />
• Advanced Composite Group VTM 264 Unidirectional<br />
Carbon/epoxy<br />
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Tooling<br />
Tool <strong>of</strong> a Volvo 70 sailboat (two days to laminate)<br />
Source: SAMPE Seattle tutorial. Chris Ridgard, 2010<br />
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Source: SAMPE Baltimore OOA tutorial. Chris Ridgard, 2012<br />
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Source: SAMPE Baltimore OOA tutorial. Chris Ridgard, 2012<br />
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Source: SAMPE Seattle OOA tutorial. Chris Ridgard, 2010<br />
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OOA <strong>Prepreg</strong> Summary<br />
• OOA prepreg can give laminates with similar quality to<br />
autoclave processed<br />
• Potential alternative to autoclave processed prepreg<br />
• Proper processing is key to OOA prepreg laminate quality<br />
• Gas extraction is key for OOA processing<br />
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