| Type of Document |
Dissertation |
| Author |
Li, Min-Chung
|
| URN |
etd-10202005-102827 |
| Title |
Thermoplastic composite consolidation |
| Degree |
PhD |
| Department |
Materials Engineering Science |
| Advisory Committee |
| Advisor Name |
Title |
| No Advisors Found |
|
| Keywords |
- Thermoplastic composites.
|
| Date of Defense |
1993-10-05 |
| Availability |
restricted |
Abstract
Fabrication of high-quality composites from thennoplastic prepregs requires careful
selection of the processing cycles so that intimate contact at the ply interfaces is achieved
resulting in the fonnation of strong interply bonds and the process-induced residual stress
is minimized to ensure superior mechanical perfonnance. The void formation and the
consolidation mechanism were studied experimentally. A refined model was developed
to relate the processing parameters of pressure, temperature and time to the interply
intimate contact of thennoplastic composites. The model was developed by integrating
a prepreg surface topology characterization with a resin flow analysis. Both unidirectional
and cross-ply lay-ups were modeled. Two-ply unidirectional laminae fabricated from
graphite-polysulfone and graphite-PEEK prepregs and [0/90/0]Ţ laminates were
consolidated using different processing cycles. Optical microscopy and scanning acoustic
microscopy were used to obtain the degree of intimate contact data. Agreement between
the measured and calculated degree of intimate contact was good. A finite element model
was developed to analyze residual stresses in thermoplastic composites by combining a
plane-strain elasticity analysis and a temperature-dependent matrix properties. The
residual stress model takes into account the mismatch of the thermal expansion
coefficients and the crystallization shrinkage of the matrix. [O10/906]Ţ graphite-PEEK
laminates were manufactured at different cooling rates to verify the model. The induced
residual thermal defonnations were measured by a shadow moire system. The model
accurately estimated the out-of-plane displacement of the non-symmetrical laminates.
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