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Al-Li alloys with low density and high fracture toughness.

机译:具有低密度和高断裂韧性的Al-Li合金。

摘要

Based alloy UTIL ALUMINUM IN STRUCTURES OF AIRCRAFT AND AEROSPACE HAVING A LOW density, high strength and high fracture resistance consists essentially of the following formula: CUALIBMGCAZREALBAL WHERE A, B, C, D, EY BAL INDICATE QUANTITY IN PERCENTAGE OF WEIGHT aLLOY COMPONENTS AND WHERE LESS THAN LESS THAN 2.4 3.5, 1.35 BOTTOM BOTTOM AB 1.8, O.25 LOWER AC LESS THAN 0.65, AD 0.25 BOTTOM BOTTOM BOTTOM AE 0.65 and 0.08 LESS THAN 0.25, AND alloy has a density of 0.0945 to 0.0960 lbs / IN3.PREFERENTEMENTE, THE RELATIONSHIP BETWEEN THE COMPONENTS OF COPPER AND LITHIUM also contains the following tests: 6.5 BOTTOM BOTTOM AA + 2.5B 7.5, 2B-0.8 BELOW LOWER AA 3.75B-1.9 .
机译:具有低密度,高强度和高抗断裂性的飞机和飞机结构中的基合金UTIL铝基本上由下式组成:CUALIBMGCAZREALBAL其中A,B,C,D,EY BAL表示重量合金成分和位置的数量小于2.4 3.5、1.35底部AB 1.8,O.25较低AC小于0.65,底部0.25 AE底部0.65和0.08小于0.25,合金的密度为0.0945至0.0960 lbs / IN3.PREFERENTEMENTE,铜和锂的成分之间的关​​系还包含以下测试:6.5底部AA + 2.5B 7.5,2B-0.8以下AA 3.75B-1.9。

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