Manufacture of thermoplastic matrix composite stiffened panel using flexible co-woven prepreg

Xue Feng An; Ming Zhang; Bang Ming Tang; Xiao Su Yi

Manufacture of thermoplastic matrix composite stiffened panel using flexible co-woven prepreg

Xue Feng An, Ming Zhang, Bang Ming Tang, Xiao Su Yi

Research output: Journal Publication › Article › peer-review

Abstract

PEEK matrix composites exhibit great toughness and damage resistance. But the severe processing conditions and poor drapability result in in-efficiency in curved surface forming. This difficulty can be solved by flexible co-woven prepreg technology, facilitating the manufacture of complex curved surface structure with high quality and efficiency. The advantage of this flexible prepreg was demonstrated through the manufacture of stiffened panels with L stiffers and U stiffers, respectively.

Original language	English
Pages (from-to)	217-221
Number of pages	5
Journal	Hangkong Cailiao Xuebao/Journal of Aeronautical Materials
Volume	26
Issue number	3
Publication status	Published - Jun 2006
Externally published	Yes

Keywords

Co-consolidation
Curved surface forming
Flexible prepreg
Thermoplastic matrix composite

ASJC Scopus subject areas

Ceramics and Composites
Aerospace Engineering
Metals and Alloys
Materials Chemistry

Cite this

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abstract = "PEEK matrix composites exhibit great toughness and damage resistance. But the severe processing conditions and poor drapability result in in-efficiency in curved surface forming. This difficulty can be solved by flexible co-woven prepreg technology, facilitating the manufacture of complex curved surface structure with high quality and efficiency. The advantage of this flexible prepreg was demonstrated through the manufacture of stiffened panels with L stiffers and U stiffers, respectively.",

keywords = "Co-consolidation, Curved surface forming, Flexible prepreg, Thermoplastic matrix composite",

author = "An, {Xue Feng} and Ming Zhang and Tang, {Bang Ming} and Yi, {Xiao Su}",

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AU - An, Xue Feng

AU - Zhang, Ming

AU - Tang, Bang Ming

AU - Yi, Xiao Su

PY - 2006/6

Y1 - 2006/6

N2 - PEEK matrix composites exhibit great toughness and damage resistance. But the severe processing conditions and poor drapability result in in-efficiency in curved surface forming. This difficulty can be solved by flexible co-woven prepreg technology, facilitating the manufacture of complex curved surface structure with high quality and efficiency. The advantage of this flexible prepreg was demonstrated through the manufacture of stiffened panels with L stiffers and U stiffers, respectively.

AB - PEEK matrix composites exhibit great toughness and damage resistance. But the severe processing conditions and poor drapability result in in-efficiency in curved surface forming. This difficulty can be solved by flexible co-woven prepreg technology, facilitating the manufacture of complex curved surface structure with high quality and efficiency. The advantage of this flexible prepreg was demonstrated through the manufacture of stiffened panels with L stiffers and U stiffers, respectively.

KW - Co-consolidation

KW - Curved surface forming

KW - Flexible prepreg

KW - Thermoplastic matrix composite

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SN - 1005-5053

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JO - Hangkong Cailiao Xuebao/Journal of Aeronautical Materials

JF - Hangkong Cailiao Xuebao/Journal of Aeronautical Materials

IS - 3

ER -

Manufacture of thermoplastic matrix composite stiffened panel using flexible co-woven prepreg

Abstract

Keywords

ASJC Scopus subject areas

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