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Friction Stir Welding for Aluminum Metal Matrix Composites (MMC's) (Center Director's Discretionary Fund, Project No. 98-09)This technical memorandum describes an investigation of using friction stir welding (FSW) process for joining a variety of aluminum metal matrix composites (MMC's) reinforced with discontinuous silicon-carbide (SiC) particulate and functional gradient materials. Preliminary results show that FSW is feasible to weld aluminum MMC to MMC or to aluminum-lithium 2195 if the SiC reinforcement is <25 percent by volume fraction. However, a softening in the heat-affected zone was observed and is known to be one of the major limiting factors for joint strength. The pin tool's material is made from a low-cost steel tool H-13 material, and the pin tool's wear was excessive such that the pin tool length has to be manually adjusted for every 5 ft of weldment. Initially, boron-carbide coating was developed for pin tools, but it did not show a significant improvement in wear resistance. Basically, FSW is applicable mainly for butt joining of flat plates. Therefore, FSW of cylindrical articles such as a flange to a duct with practical diameters ranging from 2-5 in. must be fully demonstrated and compared with other proven MMC joining techniques for cylindrical articles.
Document ID
20000004679
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Lee, J. A.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Carter, R. W.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ding, J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 1999
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/TM-1999-209876
M-953
NAS 1.15:209876
Report Number: NASA/TM-1999-209876
Report Number: M-953
Report Number: NAS 1.15:209876
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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