Improved lithium aluminum alloy system

Details Improved lithium aluminum alloy system Improved lithium aluminum alloy system

C - Chemistry, Metallurgy

22

C

C22C 21/00 (2006.01) C22C 21/06 (2006.01) C22F 1/04 (2006.01) C22F 1/047 (2006.01)

Patent

CA 2089171

An aluminum based alloy useful in aircraft and airframe structures which has low density and consists essentially of the following general formula: Mg a Li b Zn c Ag d Al bal, wherein a ranges from 0.5 to 10 %, b ranges from 0.5 to 3.0 %, c ranges from 0.1 to 5.0 %, d ranges from 0.1 to 2.0 %, and bal indicates the balance of the alloy is aluminum, with the proviso that the total amount of alloying elements cannot exceed 12.0 %, with the further proviso that when a ranges from 7.0 to 10.0 %, b cannot exceed 2.5 % and c cannot exceed 2.0 %.

Affiliated with

Also associated with

Rating

Improved lithium aluminum alloy system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Improved lithium aluminum alloy system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Improved lithium aluminum alloy system will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1545085