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Aluminum-Silicon Alloy Having Improved Properties at Elevated Temperatures and Articles Cast TherefromAn aluminum alloy suitable for high temperature applications, such as heavy duty pistons and other internal combustion applications. having the following composition, by weight percent (wt %): Silicon: 11.0-14.0; Copper: 5.6-8.0; Iron: 0-0.8; Magnesium: 0.5-1.5; Nickel: 0.05-0.9; Manganese: 0.5-1.5; Titanium: 0.05-1.2; Zirconium: 0.12-1.2; Vanadium: 0.05-1.2; Zinc: 0.005-0.9; Strontium: 0.001-0.1; Aluminum: balance. In this alloy the ratio of silicon:magnesium is 10-25, and the ratio of copper:magnesium is 4-15. After an article is cast from this alloy, the article is treated in a solutionizing step which dissolves unwanted precipitates and reduces any segregation present in the original alloy. After this solutionizing step, the article is quenched, and is then aged at an elevated temperature for maximum strength.
Document ID
20020060119
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Lee, Jonathan A.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Chen, Po-Shou
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 20, 2013
Publication Date
June 4, 2002
Subject Category
Metals And Metallic Materials
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,399,020|NASA-Case-MFS-31294-S-CIP
Patent Application
US-Patent-Appl-SN-322768|US-Patent-Appl-SN-152469|US-Patent-Appl-SN-218675|US-Patent-Appl-SN-688729
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