发明名称 ALUMINUM-SILICON ALLOY HAVING IMPROVED PROPERTIES AT ELEVATED TEMPERATURES
摘要 Disclosed is an aluminum alloy suitable for high temperature applications, such as heavy duty pistons and other internal combustion applications, having the composition, by weight percent (wt %): Silicon 6.0 to 14.0, Copper 3.0 to 8.0, Iron 0.01 to 0.8, Magnesium 0.5 to 1.5, Nickel 0.05 to 1.2, Manganese 0.01 to 1.0, Titanium 0.05 to 1.2, Zirconium 0.05 to 1.2, Vanadium 0.05 to 1.2, Strontium 0.001 to 0.10, Aluminum balance. After the article is cast from this alloy the article is treated to a solutionizing step which dissolves unwanted precipitates and reduces any segregation present in the original alloy. After the solutionizing step, the article is quenched and is then aged at an elevated temperature for maximum strength. Iron and manganese may be present as impurities in the alloy in amounts less than 1.0 wt.%.
申请公布号 WO0071772(A1) 申请公布日期 2000.11.30
申请号 WO1999US20314 申请日期 1999.09.03
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA) 发明人 LEE, JONATHAN, A.;CHEN, PO-SHOU
分类号 C22C21/04;C22C21/14;C22F1/043;(IPC1-7):C22F1/04;C22C21/16 主分类号 C22C21/04
代理机构 代理人
主权项
地址