NDLI: Utilization of induction bonding for automated fabrication of tigr

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Utilization of induction bonding for automated fabrication of tigr

Content Provider	NASA Technical Reports Server (NTRS)
Author	Johnston, Norman J. Hulcher, A. Bruce Hinkley, Jeffrey A. Messier, Bernadette C. Marchello, Joseph M.
Copyright Year	1999
Description	A laboratory study of magnetic induction heat bonding of titanium foil and graphite fiber reinforced polymer prepreg tape, TiGr, demonstrated that the process is a viable candidate for low cost fabrication of aircraft structure made of this new material form. Data were obtained on weld bonding of PIXA and PETI-5 prepreg to titanium. Both the foil and honeycomb forms of titanium were investigated. The process relies on magnetic susceptor heating of titanium, not on high frequency heating of graphite fiber. The experiments showed that with a toroid magnet configuration, good weld bonds might be obtained with heating times of a few seconds. These results suggest the potential is good for the induction heating process to achieve acceptable commercial production rates.
File Size	2428355
Page Count	44
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19990041100
Archival Resource Key	ark:/13960/t49p8090n
Language	English
Publisher Date	1999-04-01
Access Restriction	Open
Subject Keyword	Composite Materials Magnetic Induction Welding Laboratories Fiber Composites Research High Frequencies Graphite-polyimide Composites Toroids Induction Heating Foils Materials Fabrication Prepregs Heating Low Cost Titanium Metal-metal Bonding Honeycomb Structures Aircraft Structures Technology Utilization Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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