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Recent progress in NASA Langley textile reinforced composites program

Authors :
Dexter, H. Benson
Harris, Charles E
Johnston, Norman J
Source :
FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 2
Publication Year :
1992
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1992.

Abstract

The NASA LaRC is conducting and sponsoring research to explore the benefits of textile reinforced composites for civil transport aircraft primary structures. The objective of this program is to develop and demonstrate the potential of affordable textile reinforced composite materials to meet design properties and damage tolerance requirements of advanced aircraft structural concepts. In addition to in-house research, the program was recently expanded to include major participation by the aircraft industry and aerospace textile companies. The major program elements include development of textile preforms, processing science, mechanics of materials, experimental characterization of materials, and development and evaluation of textile reinforced composite structural elements and subcomponents. The NASA Langley in-house focus is as follows: development of a science-based understanding of resin transfer molding (RTM), development of powder-coated towpreg processes, analysis methodology, and development of a performance database on textile reinforced composites. The focus of the textile industry participation is on development of multidirectional, damage-tolerant preforms, and the aircraft industry participation is in the areas of design, fabrication and testing of textile reinforced composite structural elements and subcomponents. Textile processes such as 3D weaving, 2D and 3D braiding, and knitting/stitching are being compared with conventional laminated tape processes for improved damage tolerance. Through-the-thickness reinforcements offer significant damage tolerance improvements. However, these gains must be weighed against potential loss in in-plane properties such as strength and stiffness. Analytical trade studies are underway to establish design guidelines for the application of textile material forms to meet specific loading requirements. Fabrication and testing of large structural components are required to establish the full potential of textile reinforced composite materials.

Subjects

Subjects :
Composite Materials

Details

Language :
English
Database :
NASA Technical Reports
Journal :
FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 2
Publication Type :
Report
Accession number :
edsnas.19950022054
Document Type :
Report