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Mechanism for Self-Reacted Friction Stir WeldingA mechanism has been designed to apply the loads (the stirring and the resection forces and torques) in self-reacted friction stir welding. This mechanism differs somewhat from mechanisms used in conventional friction stir welding, as described below. The tooling needed to apply the large reaction loads in conventional friction stir welding can be complex. Self-reacted friction stir welding has become popular in the solid-state welding community as a means of reducing the complexity of tooling and to reduce costs. The main problems inherent in self-reacted friction stir welding originate in the high stresses encountered by the pin-and-shoulder assembly that produces the weld. The design of the present mechanism solves the problems. The mechanism includes a redesigned pin-and-shoulder assembly. The welding torque is transmitted into the welding pin by a square pin that fits into a square bushing with set-screws. The opposite or back shoulder is held in place by a Woodruff key and high-strength nut on a threaded shaft. The Woodruff key reacts the torque, while the nut reacts the tensile load on the shaft.
Document ID
20110020311
Acquisition Source
Marshall Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Venable, Richard
(Lockheed Martin Manned Space Systems New Orleans, LA, United States)
Bucher, Joseph
(Lockheed Martin Manned Space Systems New Orleans, LA, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2004
Publication Information
Publication: NASA Tech Briefs, October 2004
Subject Category
Mechanical Engineering
Report/Patent Number
MFS-31914
Report Number: MFS-31914
Distribution Limits
Public
Copyright
Public Use Permitted.
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