NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
2195 Aluminum-Copper-Lithium Friction Plug Welding DevelopmentTechnology developments and applications of friction plug welding is presented. This friction repair welding technology is being studied for implementation on the Space Transportation System's Super Light Weight External Tank. Single plug repairs will be used on a vast majority of weld defects, however, linear defects of up to several inches can be repaired by overlapping plug welds. Methods and results of tensile, bend, simulated service, surface crack tension and other tests at room and cryogenic temperatures is discussed. Attempts to implement Friction Plug Welding has led to both tool and process changes in an attempt to minimize expansive tooling and lengthy implementation times. Process control equipment and data storage methods intended for large scale production will also be addressed. Benefits include increased strength and toughness, decreased weld repair time, automated and highly reliable process, and a lower probability of having to re-repair defect locations.
Document ID
19990064400
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Takeshita, Rike P.
(Lockheed Martin Michoud Space Systems New Orleans, LA United States)
Hartley, Paula J.
(Lockheed Martin Michoud Space Systems New Orleans, LA United States)
Baker, Kent S.
(Lockheed Martin Michoud Space Systems New Orleans, LA United States)
Date Acquired
August 18, 2013
Publication Date
January 1, 1997
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Welding Trends
Location: Pine Mountain, GA
Country: United States
Start Date: June 1, 1998
Sponsors: American Welding Society
Funding Number(s)
CONTRACT_GRANT: NAS8-36200
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available