NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Time-Temperature-Precipitation Behavior in Al-Li Alloy 2195Transmission electron microscopy was used to study time-temperature-precipitation (TTP) behavior in aluminum-lithium (Al-Li) 2195 alloy. Al-Li 2195 (nominally Al + 4 percent Cu + 1 percent Li + 0.3 percent Ag + 0.3 percent Mg + 0.1 percent Zr) was initially solutionized for 1 hr at 950 F and then stretched 3 percent. Heat treatments were conducted for up to 100 hr at temperatures ranging from 200 to 1,000 F. TTP diagrams were determined for both matrix and subgrain boundaries. Depending upon heat treatment conditions, precipitate phases (such as GP zone, theta'', theta', theta, delta', T1, TB, and T2) were found in the alloy. The TTP diagrams were applied as a guide to avoid T1 precipitation at subgrain boundaries, as part of an effort to improve the alloy's cryogenic fracture toughness (CFT). New understanding of TTP behavior was instrumental in the development of a two-step artificial aging treatment that significantly enhanced CFT in Al-Li 2195.
Document ID
20020030744
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Chen, P. S.
(IIT Research Inst. Huntsville, AL United States)
Bhat, B. N.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2002
Subject Category
Metals And Metallic Materials
Report/Patent Number
M-1043
NASA/TM-2002-211548
NAS 1.15:211548
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available