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24 records · Page 2

Intermediate temperature thermomechanical processing of Al 2090 for superplasticity

The Al-Cu-Li phase diagram indicates that during thermomechanical processing of Al 2090 at 300 C both T(1) and T(2) phases will precipitate. Following work on Al-Mg-X alloys, it is possible that TMP at such temperatures might promote intragranular formation of these phases and promote microstructural refinement during recrystallization. Microstructural analyses reveal that the T(2) phase in Al 2090 may play a similar role to the beta-phase in Al-Mg-X alloys during microstructural evolution. Mechanical property data indicate that Al 2090 can be moderately (215-245 percent) superplastic at 370 C following processing at 300 C.

Hales, S. J.↗

NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA2ST)

The NASA-UVA Light Aerospace Alloy and Structures Technology (LA2ST) Program continues a high level of activity. Progress achieved between 1 Jan. and 30 Jun. 1993 is reported. The objective of the LA2ST Program is to conduct interdisciplinary graduate student research on the performance of next generation, light weight aerospace alloys, composites, and thermal gradient structures in collaboration with NASA-Langley researchers. The following projects are addressed: environmental fatigue of Al-Li-Cu alloys; mechanisms of localized corrosion and environmental fracture in Al-Cu-Li-Mg-Ag alloy X2095 and compositional variations; the effect of zinc additions on the precipitation and stress corrosion cracking behavior of alloy 8090; hydrogen interactions with Al-Li-Cu alloy 2090 and model alloys; metastable pitting of aluminum alloys; cryogenic fracture toughness of Al-Cu-Li + In alloys; the fracture toughness of Weldalite (TM); elevated temperature cracking of advanced I/M aluminum alloys; response of Ti-1100/SCS-6 composites to thermal exposure; superplastic forming of Weldalite (TM); research to incorporate environmental effects into fracture mechanics fatigue life prediction codes such as NASA FLAGRO; and thermoviscoplastic behavior.

Gangloff, Richard P.↗

Friction Plug Weld Repair for the Space Shuttle External Tank

Lockheed Martin Space Systems, Michoud Operations in New Orleans, LA is the manufacturer of the External Fuel Tanks (ET) for the Space Transportation System (STS). The ET contains and delivers the propellants used by the Orbiters three main engines. Additionally, it also serves as the structural backbone for the Orbiter and the two Solid Rocket Boosters (SRB), which combined, constitute the STS. In 1994, NASA established that in order to launch the International Space Station, the performance of the STS must be improved. One option was to reduce the weight of the ET, which would enable sufficient increase in performance. With the development of the Weldalite(R) series of Al-Cu-Li alloys in the late 1980's, Lockheed Martin was postured to replace the current A12219 fuel tanks with the high strength, light weight A12195 alloy. With the use of A12195 and some component redesign, the weight of the Super Lightweight (SLWT) ET was reduced by approximately 7,000 pounds, which added as much capability to the Space Shuttle. Since June 1998, seven STS missions have been successful with the use of the SLWT ET's.

Hartley, Paula J.↗

Materials Data on LiAlCu2 by Materials Project

LiCu2Al is Heusler structured and crystallizes in the cubic Fm-3m space group. The structure is three-dimensional. Li is bonded in a body-centered cubic geometry to eight equivalent Cu and six equivalent Al atoms. All Li–Cu bond lengths are 2.55 Å. All Li–Al bond lengths are 2.94 Å. Cu is bonded in a body-centered cubic geometry to four equivalent Li and four equivalent Al atoms. All Cu–Al bond lengths are 2.55 Å. Al is bonded in a distorted body-centered cubic geometry to six equivalent Li and eight equivalent Cu atoms.

36 MATERIALS SCIENCE↗

Materials Data on Li4(AlCu2)3 by Materials Project

Li4(Cu2Al)3 is Frank-Kasper $\mu$ Phase-derived structured and crystallizes in the hexagonal P6_3/mmc space group. The structure is three-dimensional. there are four inequivalent Li sites. In the first Li site, Li is bonded in a 1-coordinate geometry to three equivalent Li, nine equivalent Cu, and four Al atoms. All Li–Li bond lengths are 2.93 Å. There are three shorter (2.79 Å) and six longer (2.97 Å) Li–Cu bond lengths. There are one shorter (2.62 Å) and three longer (2.86 Å) Li–Al bond lengths. In the second Li site, Li is bonded in a 1-coordinate geometry to three equivalent Li, nine equivalent Cu, and four Al atoms. There are three shorter (2.79 Å) and six longer (2.97 Å) Li–Cu bond lengths. There are one shorter (2.62 Å) and three longer (2.86 Å) Li–Al bond lengths. In the third Li site, Li is bonded in a 6-coordinate geometry to six equivalent Cu and six Al atoms. All Li–Cu bond lengths are 2.71 Å. All Li–Al bond lengths are 3.15 Å. In the fourth Li site, Li is bonded in a 6-coordinate geometry to six equivalent Cu and six Al atoms. All Li–Cu bond lengths are 2.72 Å. All Li–Al bond lengths are 3.15 Å. Cu is bonded to five Li, four equivalent Cu, and three Al atoms to form CuLi5Al3Cu4 cuboctahedra that share corners with two equivalent AlLi6Cu6 cuboctahedra, corners with thirteen equivalent CuLi5Al3Cu4 cuboctahedra, edges with five equivalent CuLi5Al3Cu4 cuboctahedra, faces with three equivalent AlLi6Cu6 cuboctahedra, and faces with ten equivalent CuLi5Al3Cu4 cuboctahedra. There are two shorter (2.42 Å) and two longer (2.48 Å) Cu–Cu bond lengths. There are one shorter (2.49 Å) and two longer (2.63 Å) Cu–Al bond lengths. There are four inequivalent Al sites. In the first Al site, Al is bonded to six Li and six equivalent Cu atoms to form AlLi6Cu6 cuboctahedra that share corners with twelve equivalent CuLi5Al3Cu4 cuboctahedra, edges with six equivalent AlLi6Cu6 cuboctahedra, and faces with eighteen equivalent CuLi5Al3Cu4 cuboctahedra. In the second Al site, Al is bonded in a 1-coordinate geometry to seven Li, six equivalent Cu, and one Al atom. All Al–Cu bond lengths are 2.63 Å. The Al–Al bond length is 2.74 Å. In the third Al site, Al is bonded in a 1-coordinate geometry to seven Li, six equivalent Cu, and one Al atom. The Al–Li bond length is 2.62 Å. The Al–Al bond length is 2.74 Å. In the fourth Al site, Al is bonded in a 1-coordinate geometry to seven Li, six equivalent Cu, and one Al atom. There are one shorter (2.62 Å) and six longer (3.15 Å) Al–Li bond lengths. All Al–Cu bond lengths are 2.63 Å.

36 MATERIALS SCIENCE↗

Materials Data on LiAl2Cu by Materials Project

Al2CuLi is Heusler structured and crystallizes in the cubic Fm-3m space group. The structure is three-dimensional. Li is bonded in a distorted body-centered cubic geometry to six equivalent Cu and eight equivalent Al atoms. All Li–Cu bond lengths are 3.01 Å. All Li–Al bond lengths are 2.60 Å. Cu is bonded in a distorted body-centered cubic geometry to six equivalent Li and eight equivalent Al atoms. All Cu–Al bond lengths are 2.60 Å. Al is bonded in a body-centered cubic geometry to four equivalent Li and four equivalent Cu atoms.

36 MATERIALS SCIENCE↗