NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Utilization of Induction Bonding for Automated Fabrication of TIGRA 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.
Document ID
19990041100
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Hinkley, Jeffrey A.
(NASA Langley Research Center Hampton, VA United States)
Johnston, Norman J.
(NASA Langley Research Center Hampton, VA United States)
Hulcher, A. Bruce
(Old Dominion Univ. Norfolk, VA United States)
Marchello, Joseph M.
(Old Dominion Univ. Norfolk, VA United States)
Messier, Bernadette C.
(Old Dominion Univ. Norfolk, VA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1999
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:209123
L-17787
NASA/TM-1999-209123
Report Number: NAS 1.15:209123
Report Number: L-17787
Report Number: NASA/TM-1999-209123
Funding Number(s)
PROJECT: RTOP 537-06-32-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available