发明名称 Rocket motor thrust chamber alloy - from forged copper-silver -zirconium
摘要 <p>The alloy contains 0.05-0.5% pref. 0.25-0.45% Zr, 2-6% pref. 2.5-3.5% Ag, 94-98% Cu. The chamber, of which the outer walls are provided with cooling channels, is produced by forging the vacuum-melted alloy ingot. The forging is solution treated for 1.5-3 h at 1600-1700 degrees (870-927 degrees C), quenched to room temp. and aged for 2-6 h at 850-950 degrees F (454-510 degrees C).</p>
申请公布号 FR2132409(A1) 申请公布日期 1972.11.17
申请号 FR19720011761 申请日期 1972.04.04
申请人 NORTH AMERICAN ROCKWELL 发明人
分类号 F02K9/64;(IPC1-7):02K11/00;22C9/00;02K9/00 主分类号 F02K9/64
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