US2003213537A1PendingUtilityA1

Aluminum alloys

51
Priority: Feb 28, 2001Filed: Mar 6, 2003Published: Nov 20, 2003
Est. expiryFeb 28, 2021(expired)· nominal 20-yr term from priority
Inventors:Alex Cho
C22F 1/053C22C 21/10
51
PatentIndex Score
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Cited by
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Claims

Abstract

A process for thermally treating an article made from an aluminum alloy. The process comprises providing the aluminum alloy that consists essentially of from about 5.7 to about 6.7 wt. % of zinc, less than 2.2 wt. % copper, less than 4.2 wt. % of the total weight percent of magnesium and copper combined, and less than 10.60 wt. % of the total weight percent of magnesium, copper and zinc combined, the balance being substantially aluminum, incidental elements and impurities. The article is artificially aged at a first temperature. The article is heated to a second temperature, wherein the second temperature is higher than the first temperature. The article is artificially aged at the second temperature of from about 290 to about 360° F. for a duration of at least 6 hours. The article is cooled from the second temperature to 200° F. at a cooling rate of from about 20 to about 4 0 ° F./hour.

Claims

exact text as granted — not AI-modified
What is claimed is:  
     
         1 . A process for thermally treating an article made from an aluminum alloy, the process comprising: 
 providing the aluminum alloy consisting essentially of from about 5.7 to about 6.7 wt. % of zinc, less than 2.2 wt. % copper, less than 4.2 wt. % of the total weight percent of magnesium and copper combined, and less than 10.60 wt. % of the total weight percent of magnesium, copper and zinc combined, the balance being substantially aluminum, incidental elements and impurities;    solid solution heat treating the article;    quenching the article, heating the article to a first temperature;    artificially aging the article at the first temperature    heating the article to a second temperature, wherein the second temperature is higher than the first temperature,    artificially aging the article at the second temperature of from about 290 to about 360° F. for a duration of at least 6 hours, and    cooling the article from the second temperature to 200° F. at a cooling rate of from about 20 to about 40° F./hour.    
     
     
         2 . The process of  claim 1 , wherein the aluminum alloy comprises from about 1.9 to about 2.1 wt. % magnesium.  
     
     
         3 . The process of  claim 1 , wherein the aluminum alloy comprises from about 2.0 to 2.2 wt. % of copper.  
     
     
         4 . The process of  claim 1 , wherein the aluminum alloy further includes from about 0.08 to about 0.12 wt. % of zirconium.  
     
     
         5 . The process of  claim 1  further including performing cold work to the article.  
     
     
         6 . The process of  claim 1 , wherein the heat up rate from the first temperature to the second temperature is from about 25 to about 4 0 ° F./hour.  
     
     
         7 . The process of  claim 1 , wherein the cooling rate from the second temperature to 200° F. is from about 20 to about 3 0 ° F./hour.  
     
     
         8 . The process of  claim 7 , wherein the cooling rate is from about 25 to about 30° F./hour.  
     
     
         9 . The process of  claim 1 , wherein the first temperature is from about 220° F. to about 280° F. and artificially aging the article at the first temperature occurs for a duration of at least 30 minutes.  
     
     
         10 . The process of  claim 9 , wherein the first temperature is from about 240 to about 260° F. and artificially aging the article at the first temperature occurs for a duration of from about 6 to about 10 hours.  
     
     
         11 . The process of  claim 1 , wherein the second temperature is from about 310 to about 330° F. and artificially aging the article at the second temperature occurs for a duration of from about 18 to about 30 hours.  
     
     
         12 . The process of  claim 11 , wherein the second temperature is from about 310 to about 330° F. and the artificially aging the article at the second temperature occurs for a duration of from about 22 to about 28 hours.  
     
     
         13 . The product formed by the process of  claim 1 .  
     
     
         14 . A process for artificially aging a solution heat treated aluminum alloy, the process comprising: 
 providing the aluminum alloy consisting essentially of from about 5.7 to about 6.7 wt. % of zinc, less than 2.2 wt. % copper, less than 4.2 wt. % of the total weight percent of magnesium and copper combined, and less than 10.60 wt. % of the total weight percent of magnesium, copper and zinc combined, the balance being substantially aluminum and incidental elements and impurities,    artificially aging the article at the first temperature,    heating the article to a second temperature, wherein the second temperature is higher than the first temperature;    artificially aging the article at the second temperature of from about 290 to about 360° F. for a duration of at least 6 hours; and    cooling the article from the second temperature to 200° F. at a cooling down rate of from about 20 to about 40° F./hour.    
     
     
         15 . The process of  claim 14 , wherein the aluminum alloy comprises from about 2 to 2.2 wt. % copper.  
     
     
         16 . The process of  claim 14 , wherein the aluminum alloy further includes from about 0.08 to about 0. 12 wt. % of zirconium.  
     
     
         17 . The process of  claim 14 , wherein the heat up rate from the first temperature to the second temperature is from about 25 to about 40° F./hour.  
     
     
         18 . The process of  claim 14 , wherein the cooling rate from the second temperature to 200° F. is from about 20 to about 30° F./hour.  
     
     
         19 . The process of  claim 18 , wherein the cooling rate is from about 25 to about 30° F./hour.  
     
     
         20 . The process of  claim 14 , wherein the first temperature is from about 220° F. to about 280° F. and artificially aging the article at the first temperature occurs for a duration of at least 30 minutes.  
     
     
         21 . The process of  claim 20 , wherein the first temperature is from about 240 to about 260° F. and artificially aging the article at the first temperature occurs for a duration of from about 6 to about 10 hours.  
     
     
         22 . The process of  claim 14 , wherein the second temperature is from about 310 to about 330° F. and artificially aging the article at the second temperature occurs for a duration of from about 18 to about 30 hours.  
     
     
         23 . The process of  claim 22 , wherein the second temperature is from about 310 to about 330° F. and the artificially aging the article at the second temperature occurs for a duration of from about 22 to about 28 hours.  
     
     
         24 . The product formed by the process of  claim 14 .  
     
     
         25 . The product formed by the process of  claim 14 , wherein the product is adapted to be used in aerospace wings, bulkhead and spars.  
     
     
         26 . A process for artificially aging a solution heat treated aluminum alloy, the process comprising: 
 providing the aluminum alloy consisting essentially of from about 5.7 to about 6.7 wt. % of zinc, less than 2.2 wt. % copper, less than 4.2 wt. % of the total weight percent of magnesium and copper combined, and less than 10.60 wt. % of the total weight percent of magnesium, copper and zinc combined, the balance being substantially aluminum and incidental elements and impurities,    artificially aging the article at the first temperature;    heating the article to a second temperature, wherein the second temperature is higher than the first temperature, the heat up rate from the first temperature to the second temperature is from about 25 to about 4 0 ° F./hour.    artificially aging the article at the second temperature of from about 290 to about 360° F. for a duration of at least 6 hours; and    cooling the article from the second temperature to 200° F. at a cooling down rate of from about 20 to about 40° F./hour.    
     
     
         27 . The process of  claim 26 , wherein the aluminum alloy comprises from about 2 to 2.2 wt. % copper.  
     
     
         28 . The process of  claim 26 , wherein the aluminum alloy further includes from about 0.08 to about 0.12 wt. % of zirconium.  
     
     
         29 . The process of  claim 26 , wherein the heat up rate from the first temperature to the second temperature is from about 25 to about 30° F./hour.  
     
     
         30 . The process of  claim 29 , wherein the cooling rate from the second temperature to 200° F. is from about 25 to about 30° F./hour.  
     
     
         31 . The process of  claim 26 , wherein the first temperature is from about 220° F. to about 280° F. and artificially aging the article at the first temperature occurs for a duration of at least 30 minutes.  
     
     
         32 . The process of  claim 31 , wherein the first temperature is from about 240 to about 260° F. and artificially aging the article at the first temperature occurs for a duration of from about 6 to about 10 hours.  
     
     
         33 . The process of  claim 26 , wherein the second temperature is from about 310 to about 330° F. and artificially aging the article at the second temperature occurs for a duration of from about 18 to about 30 hours.  
     
     
         34 . The process of  claim 33 , wherein the second temperature is from about 310 to about 330° F. and the artificially aging the article at the second temperature occurs for a duration of from about 22 to about 28 hours.  
     
     
         35 . The product formed by the process of  claim 26 .  
     
     
         36 . The product formed by the process of  claim 26 , wherein the product is adapted to be used in aerospace wings, bulkhead and spars.

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