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Hybrid Wound Filaments for Greater Resistance to ImpactsA hybrid material containing wound filaments made of a hybrid of high-strength carbon fibers and poly(phenylene benzobisoxazole) [PBO] fibers is discussed. This hybrid material is chosen in an effort to increase the ability of the pressure vessel to resist damage by low-speed impacts (e.g., dropping of tools on the vessel or bumping of the vessel against hard objects during installation and use) without significantly increasing the weight of the vessel. While the basic concept of hybridizing fibers in filament-wound structures is not new, the use of hybridization to increase resistance to impacts is an innovation, and can be expected to be of interest in the composite-pressure-vessel industry. The precise types and the proportions of the high-strength carbon fibers and the PBO fibers in the hybrid are chosen, along with the filament-winding pattern, to maximize the advantageous effects and minimize the disadvantageous effects of each material. In particular, one seeks to (1) take advantage of the ability of the carbon fibers to resist stress rupture while minimizing their contribution to vulnerability of the vessel to impact damage and (2) take advantage of the toughness of the PBO fibers while minimizing their contribution to vulnerability of the vessel to stress rupture. Experiments on prototype vessels fabricated according to this concept have shown promising results. At the time of reporting the information for this article, research toward understanding and optimizing the performances of PBO fibers so as to minimize their contribution to vulnerability of the pressure vessel to stress rupture had yet to be performed.
Document ID
20090020604
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
DeLay, Thomas K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Patterson, James E.
(HyPerComp Engineering, Inc. Brigham City, UT, United States)
Olson, Michael A.
(HyPerComp Engineering, Inc. Brigham City, UT, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Publication Information
Publication: NASA Tech Briefs, January 2008
Subject Category
Composite Materials
Report/Patent Number
MFS-31838-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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