Abstract
In efforts to reduce weight and potentially reduce costs of aircraft, airframe manufacturers have been increasing their use of composite materials. A major problem with composite structures is that they lack the electrical and thermal characteristics of the metal structures they are replacing. Low cost, structural conductive prepreg materials are now being developed by Hexcel to offer solutions to these very difficult problems. These materials, which are being marketed under the Thorstrandtm trade mark, are based on MBAssociate’s aluminum coated E-glass fiber.
This paper will provide the background on the basic fiber, and detail how this fiber has been designed into systems that provide an airframe structure with the electrical and thermal conductivity that is necessary for the satisfactory electrical and thermal performance of the structure.
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References
Report of SAE Committee AE4 Special Task F, Lightning Test Waveforms and Techniques for Aerospace Vehicles and Hardware, May 5, 1976.
Plumer, J. A., Simulated Lightning Tests on Graphite Laminates Protected with Thorstrand Aluminized Glass Cloth, Lightning Technologies, Inc., August 10, 1979.
Plumer, J. A., Simulated Lightning Tests on Kevlar and Graphite Laminates Protected with Thorstrand Aluminized Glass Cloth and Flame-Sprayed Aluminum, Lightning Technologies, Inc., March 1981.
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© 1981 Applied Science Publishers Ltd
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Patz, G.L. (1981). Electrically Conductive Prepreg Systems. In: Marshall, I.H. (eds) Composite Structures. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-8120-1_28
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DOI: https://doi.org/10.1007/978-94-009-8120-1_28
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-009-8122-5
Online ISBN: 978-94-009-8120-1
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