Aluminum alloy product having good combinations of mechanical an

Metal treatment – Process of modifying or maintaining internal physical... – Heating or cooling of solid metal

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

148692, 148693, 148694, 148701, 148417, 148418, 148439, 420532, C22F 104

Patent

active

054964261

ABSTRACT:
An improved high strength aluminum alloy product having good combinations of strength, toughness, corrosion resistance and the ability to be subjected in sheet or strip form to roll forming or shaping operations to produce elongate stringer or other aerospace structural reinforcing members. The alloy consists essentially of about 7.6 to 8.4% zinc, about 1.8 to 2.2% magnesium, about 2 to 2.6% copper and at least one element selected from zirconium, vanadium and hafnium present in a total amount not exceeding about 0.5%, preferably about 0.05 to 0.25% zirconium, the balance aluminum and incidental elements and impurities. The improved strip is preferably produced by homogenizing, hot rolling and thermally treating or annealing at about 750.degree. to 850.degree. F., preferably around 800.degree. F., followed by cold rolling to a reduction in thickness of between about 20 and 50 or 60%, preferably in the neighborhood of about 25 to 35% which, in turn, is followed by a two-stage thermal annealing treatment including heating, preferably within about 650.degree. to about 700.degree. F. followed by controlled cooling or ramping down to one or more temperatures within preferably around 425.degree. to 475.degree. F. The sheet or strip so produced can be taper rolled to vary the thickness along the length of the strip which, following such taper rolling, if employed, is preferably solution heat treated and quenched, straightened, roll shaped in a plurality of roll shaping operations to produce a structural shape cross section which is then artificially aged to develop the desired properties for the aerospace application.

REFERENCES:
patent: 2248185 (1941-07-01), Nock
patent: 3198676 (1965-08-01), Sprowls et al.
patent: 3231435 (1966-01-01), Rotsell et al.
patent: 3287185 (1966-11-01), Vachet et al.
patent: 3305410 (1967-02-01), Sublett et al.
patent: 3563814 (1971-02-01), Lyle et al.
patent: 3645804 (1972-02-01), Ponchel
patent: 3791876 (1974-02-01), Kroger
patent: 3836405 (1974-09-01), Staley et al.
patent: 3856584 (1974-12-01), Cina
patent: 3881966 (1975-05-01), Staley et al.
patent: 3945861 (1976-03-01), Anderson et al.
patent: 3947297 (1976-03-01), Reimann et al.
patent: 4063936 (1977-12-01), Nagase et al.
patent: 4069072 (1978-01-01), Develay et al.
patent: 4126448 (1978-11-01), Moore et al.
patent: 4189334 (1980-02-01), Dubost et al.
patent: 4193822 (1980-03-01), Adam et al.
patent: 4200476 (1980-04-01), Dubost et al.
patent: 4305763 (1981-12-01), Quist et al.
patent: 4345951 (1982-08-01), Coupry et al.
patent: 4431467 (1984-02-01), Staley et al.
patent: 4477292 (1984-10-01), Brown
patent: 4629517 (1986-12-01), Lifka et al.
patent: 4732610 (1988-03-01), Hildeman et al.
patent: 4828631 (1989-05-01), Ponchel et al.
patent: 4832758 (1989-05-01), Brown
patent: 4863528 (1989-09-01), Brown et al.
patent: 4954188 (1990-09-01), Ponchel et al.
patent: 5221377 (1993-06-01), Hunt, Jr. et al.
"Precipitation Hardening and Stress Corrosion in AlZnMg.sub.3 ", W. Gruhl et al, Z. Metallkunde, vol. 55, No. 10, pp. 577-582 (1964).
"Thermomechanical Treatments on High Strength Al-Zn-Mg(--Cu) Alloys", E. DiRusso et al, Metallurgical Tansactions, vol. 4, pp. 1133-1144 (Apr. 1973).
"New Technique for Reducing Susceptibility to Stress-Corrosion of High Strength Aluminum Alloys", B. Cina et al, Published by the Pittsburgh Chapter of the American Society for Metals (1974).
"A New Approach to the Problem of Stress Corrosion Cracking in 7075-T6 Aluminum", W. Wallace et al, Canadian Aeronautics and Space Journal, vol. 27, No. 3, pp. 222-232 (1981).
"Microstructural Study of a High-Strength Stress-Corrosion Resistant 7075 Aluminum Alloy", K. Rajan et al, Journal of Materials Science, vol. 17, pp. 2817-2824 (1982).
"Retrogression and reaging response of 7475 aluminum alloy", M. U. Islan et al, Metals Technology, vol. 10, pp. 386-392 (Oct. 1983).
Report: "Investigation to Improve the Stress-Corrosion Resistance of Aluminum Aircraft Alloys Through Alloy Additions and Specialized Heat Treatment", J. T. Staley, under Navair N00019-68-C-0146 (Navair Report).

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Aluminum alloy product having good combinations of mechanical an does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aluminum alloy product having good combinations of mechanical an, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aluminum alloy product having good combinations of mechanical an will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1410261

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.