Abstract
This paper reported an integrated manufacturing process of one thermoplastic composite article with L-shaped stiffers of poly(ether ether ketone) (PEEK) matrix carbon fiber reinforced composites. It was found that the stiffer margins were not well consolidated by directly press forming after laying up the designed number of fabric in mold. However, a matched-die press thermoforming from the preformed blank solved the problem. The L-shaped stiffers were then fixed in mold to co-consolidate with the multiple fabric for cover flat part and finally bonded to each other. When using such quick forming techniques, the fabrication cost could drop dramatically in large volume production of aerospace composites 3-D structural parts.
| Original language | English |
|---|---|
| Pages (from-to) | 16-20 |
| Number of pages | 5 |
| Journal | Hangkong Cailiao Xuebao/Journal of Aeronautical Materials |
| Volume | 25 |
| Issue number | 3 |
| Publication status | Published - Jun 2005 |
| Externally published | Yes |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
-
SDG 9 Industry, Innovation, and Infrastructure
Free Keywords
- Co-consolidation
- Low cost fabrication
- Thermoforming
- Thermoplastic composites
ASJC Scopus subject areas
- Ceramics and Composites
- Aerospace Engineering
- Metals and Alloys
- Materials Chemistry
Fingerprint
Dive into the research topics of 'Co-consolidating thermoplastic composite article after thermoforming stiffers'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver