366:
The T6 temper is usually achieved by homogenizing the cast 7075 at 450 °C for several hours, quenching, and then ageing at 120 °C for 24 hours. This yields the peak strength of the 7075 alloys. The strength is derived mainly from finely dispersed eta and eta' precipitates both within grains
397:
The retrogression and reage (RRA) temper is a multistage heat treatment temper. Starting with a sheet in the T6 temper, it involves overaging past peak hardness (T6 temper) to near the T7 temper. A subsequent reaging at 120 °C for 24 hours returns the hardness and strength to or very nearly to
385:
100–120 °C for several hours and then at 160–180 °C for 24 hours or more. The T7 temper produces a microstructure of mostly eta precipitates. In contrast to the T6 temper, these eta particles are much larger and prefer growth along the grain boundaries. This reduces the susceptibility to
375:
T651 temper 7075 has an ultimate tensile strength of 570 MPa (83,000 psi) and yield strength of 500 MPa (73,000 psi). It has a failure elongation of 3–9%. These properties can change depending on the form of material used. The thicker plates may exhibit lower strengths and
384:
T7 temper has an ultimate tensile strength of 505 MPa (73,200 psi) and a yield strength of 435 MPa (63,100 psi). It has a failure elongation of 13%. T7 temper is achieved by overaging (meaning aging past the peak hardness) the material. This is often accomplished by aging at
353:
of no more than 140 MPa (21,000 psi). The material has an elongation (stretch before ultimate failure) of 9–10%. As is the case for all 7075 aluminum alloys, 7075-0 is highly corrosion-resistant combined with generally acceptable strength profile.
610:
Due to its high strength, low density, thermal properties, and its ability to be highly polished, 7075 is widely used in mold tool manufacturing. This alloy has been further refined into other 7000 series alloys for this application, namely 7050 and 7020.
275:, but has significantly better corrosion resistance than the alloys from the 2000 series. It is one of the most commonly used aluminium alloys for highly stressed structural applications and has been extensively used in aircraft structural parts.
561:, including marine, automotive and aviation. These same properties lead to its use in rock climbing equipment, bicycle components, inline-skating-frames and hang glider airframes are commonly made from 7075 aluminium alloy. Hobby-grade
687:
7075 has been sold under various trade names including Zicral, Ergal, and Fortal
Constructal. Some 7000 series alloys sold under brand names for making molds include Alumec 79, Alumec 89, Contal, Certal, Alumould, and Hokotol.
362:
T6 temper 7075 has an ultimate tensile strength of 510–540 MPa (74,000–78,000 psi) and yield strength of at least 430–480 MPa (63,000–69,000 psi). It has a failure elongation of 5–11%.
313:, in 1935, but reverse engineered by Alcoa in 1943, after examining a captured Japanese aircraft. 7075 was standardized for aerospace use in 1945. 7075 was eventually used for airframe production in the
604:
of forged steel rods, but have less mass than their steel counterparts, resulting in lower mechanical stress during periods in which an engine is operated under full-throttle, high-RPM conditions.
739:
267:
as the primary alloying element. It has excellent mechanical properties and exhibits good ductility, high strength, toughness, and good resistance to fatigue. It is more susceptible to
573:
for the civilian market. In particular high-quality M16 rifle lower and upper receivers, as well as extension tubes, are typically made from 7075-T6 alloy. Desert
Tactical Arms,
554:
fighter. The aircraft was known for its excellent maneuverability which was facilitated by the higher strength of 7075 compared to previous aluminum alloys.
1597:
1039:
401:
RRA treatments can be accomplished with many different procedures. The general guidelines are retrogressing between 180 and 240 °C for 15 min 10 s.
756:
848:
702:
865:
720:
797:
2087:
958:
620:
314:
198:
971:
T Hashimoto, S Jyogan (Showa
Aluminium), K Nakata, Y G Kin and M Ushio (Osaka University): FSW joining of high strength Al alloy
1483:
1385:
1032:
2036:
585:
sticks, such as the STX sabre, and camping knife and fork sets. It is a common material used in competition yo-yos as well.
697:
1940:
1434:
290:, and less than a half percent of silicon, iron, manganese, titanium, chromium, and other metals. It is produced in many
1206:
729:
624:
1414:
1345:
102:
1736:
938:
Cina, Baruch M. REDUCING THE SUSCEPTIBILITY OF ALLOYS, PARTICULARLY ALUMINIUM ALLOYS, TO STRESS CORROSION CRACKING
264:
2082:
1025:
767:
ASM Handbook Volume 2: Properties and
Selection: Nonferrous Alloys and Special-Purpose Materials, 1990 pp. 137–38
386:
310:
82:
777:
703:
https://www.thomasnet.com/articles/metals-metal-products/all-about-7075-aluminum-properties-strength-and-uses/
899:
Park, J. K., and A. J. Ardell. "Microstructures of the
Commercial 7075 AI Alloy in the T651 and T7 Tempers".
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ASTM B210, ASTM B211, ASTM B221, AMS-QQ-A-225/9, AMS-QQ-A-200/11, AMS-QQ-A-250/12, AMS-WW-T-700/7
1970:
114:
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272:
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7000 series alloys such as 7075 are often used in transport applications due to their high
2046:
1067:
852:
724:
291:
2021:
597:
589:
350:
146:
2076:
607:
It has also been the standard material for crankcase guards on off-road motorcycles.
601:
565:
commonly use 7075 and 6061 for chassis plates. 7075 is used in the manufacturing of
268:
161:
712:
781:
Journal of Japan
Institute of Light Metals (Sumitomo Light Metal Ind. Ltd., Japan)
940:. Israel Aircraft Industries Ltd., assignee. Patent 3856584. 24 Dec. 1974. Print.
2001:
1980:
593:
550:
The world's first mass-production usage of the 7075 aluminum alloy was for the
238:
1995:
937:
628:
627:
SRB beam in the Inter-tank section. The forward- and aft skirt as well as the
17:
2026:
2016:
1990:
1062:
574:
566:
283:
819:"7075 (AlZn5.5MgCu, 3.4365, 2L95, A97075) Aluminum :: MakeItFrom.com"
581:
use it for their precision rifles. It is also commonly used in shafts for
2061:
1000:
Properties and
Selection: Nonferrous Alloys and Special-Purpose Materials
998:"Properties of Wrought Aluminum and Aluminum Alloys: 7075, Alclad 7075",
636:
582:
562:
142:
2041:
1945:
783:(in Japanese), Volume 39, Issue 5, p. 378. Retrieved: 22 November 2015.
43:
983:"U.S. Manned Rocket Propulsion Evolution Part 8.20: The Saturn V S-II"
2006:
1975:
1965:
1955:
1950:
778:"Extra super duralumin and successive aluminium alloys for aircraft."
287:
1017:
2011:
1960:
632:
279:
1021:
757:
Juan J. Valencia, Peter N. Quested, "Thermophysical
Properties"
309:
The first 7075 was developed in secret by a
Japanese company,
1002:, Vol. 2, ASM Handbook, ASM International, 1990, pp. 115–116.
808:
Canadian
Aeronautics and Space Journal, 1989 vol 35-36 p. 129
278:
7075 aluminium alloy's composition roughly includes 5.6–6.1%
349:
of no more than 280 MPa (40,000 psi), and maximum
588:
Another application for the 7075-series alloy has been in
708:
WHAT ARE THE DIFFERENCES BETWEEN 6061 AND 7075 ALUMINUM?
333:
The mechanical properties of 7075 depend greatly on the
951:"7075 Aluminum Alloy Properties, 7075-T6, T7351, T651"
1933:
1864:
1735:
1596:
1482:
1433:
1384:
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1081:
1055:
345:Un-heat-treated 7075 (7075-0 temper) has a maximum
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197:
180:
160:
155:
141:
124:
101:
81:
64:
59:
42:
37:
32:
713:7075 Aluminum: Get to Know its Properties and Uses
895:
893:
891:
1033:
325:Aluminium 7075A has a density of 2.810 g/cm.
8:
271:than many other aluminium alloys because of
1040:
1026:
1018:
376:elongation than the numbers listed above.
389:. T7 temper is equivalent to T73 temper.
55:2.81 g/cm (0.102 lb/cu in)
408:
981:McCutcheon, Kimble D. (3 August 2022).
841:
839:
749:
526:AS/NZS 1734, AS/NZS 1865, AS/NZS 1866
29:
7:
199:Linear thermal expansion coefficient
25:
792:Yoshida, Hideo (2020). Shoeisha.
730:Properties of 7075 aluminum alloy
718:Properties of 7075 aluminum alloy
569:for the U.S. military as well as
961:from the original on 2021-10-16.
855:(PDF), accessed October 13, 2006
77:71.7 GPa (10,400 ksi)
663:Aerospace/defense applications
577:, and French armament company
459:Designation (Material number)
410:Table of equivalent materials
1:
698:Northwest Airlines Flight 421
453:Numerical (Chemical symbols)
367:and along grain boundaries.
97:572 MPa (83.0 ksi)
27:Type of aluminium-zinc alloy
2104:
635:, the second stage of the
2037:Aluminium–scandium alloys
914:"ASM Material Data Sheet"
866:"ASM Material Data Sheet"
432:
429:
426:
423:
420:
417:
414:
387:stress corrosion cracking
265:aluminium alloy with zinc
176:477 °C (891 °F)
1941:Aluminium–lithium alloys
1013:Aluminum 7075 Properties
955:www.theworldmaterial.com
903:14A (1983): 1957. Print.
657:Regulating valve parts
615:Aerospace applications
315:Imperial Japanese Navy
216:Specific heat capacity
2088:Aluminium–zinc alloys
846:Alcoa 7075 data sheet
619:7075 was used in the
512:AlZnMgCu1,5 (3.4365)
329:Mechanical properties
232:Electrical properties
60:Mechanical properties
2052:Hypereutectic piston
1073:History of aluminium
639:was made from 7075.
505:(EN AW-AlZn5,5MgCu)
405:Equivalent materials
294:, some of which are
257:7075 aluminium alloy
182:Thermal conductivity
552:Mitsubishi A6M Zero
411:
162:Melting temperature
38:Physical properties
1971:Aluminium granules
1085:1000 series (pure)
876:on 16 October 2018
851:2013-08-29 at the
823:www.makeitfrom.com
723:2018-10-16 at the
669:Bicycle Chainrings
571:AR-15 style rifles
409:
398:T6 temper levels.
156:Thermal properties
2070:
2069:
1998:(aka R.R. alloys)
901:Metall. Trans. A.
798:978-4-86693-295-8
675:Archery equipment
672:Bicycle Gearboxes
648:Aircraft fittings
623:nozzles, and the
621:Space Shuttle SRB
559:specific strength
543:
542:
337:of the material.
254:
253:
16:(Redirected from
2095:
2083:Aluminium alloys
2057:Aluminium bronze
2032:Nickel aluminide
1068:Aluminium alloys
1049:Aluminium alloys
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872:. Archived from
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651:Gears and shafts
600:do not have the
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347:tensile strength
321:Basic properties
273:microsegregation
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83:Tensile strength
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1986:Devarda's alloy
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590:connecting rods
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2022:Magnox (alloy)
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1475:
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1462:
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1445:
1442:
1441:
1439:
1436:
1432:
1426:
1423:
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1418:
1416:
1415:3102&3303
1413:
1411:
1408:
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1403:
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1398:
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1390:
1387:
1383:
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1364:
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1359:
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1349:
1347:
1346:2224&2324
1344:
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1327:
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1319:
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1234:
1232:
1229:
1227:
1224:
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1219:
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1211:
1208:
1204:
1198:
1195:
1193:
1190:
1188:
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1183:
1180:
1178:
1175:
1173:
1170:
1168:
1165:
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1143:
1140:
1138:
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1130:
1128:
1125:
1123:
1120:
1118:
1115:
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1110:
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1103:
1100:
1098:
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1080:
1074:
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1058:
1054:
1050:
1043:
1038:
1036:
1031:
1029:
1024:
1023:
1020:
1014:
1011:
1010:
1006:
1001:
997:
996:
992:
984:
977:
974:
968:
965:
960:
956:
952:
946:
943:
939:
934:
931:
919:
915:
909:
906:
902:
896:
894:
892:
888:
875:
871:
867:
861:
858:
854:
850:
847:
842:
840:
836:
824:
820:
814:
811:
805:
802:
799:
795:
789:
786:
782:
779:
776:Yoshio, Baba.
773:
770:
764:
761:
758:
753:
750:
744:
740:
738:
736:
735:7075 aluminum
733:
731:
728:
726:
722:
719:
716:
714:
711:
709:
706:
704:
701:
699:
696:
695:
691:
689:
682:
680:
674:
671:
668:
665:
662:
659:
656:
654:Missile parts
653:
650:
647:
646:
642:
640:
638:
634:
630:
626:
625:external tank
622:
614:
612:
608:
605:
603:
599:
598:Aluminum rods
595:
591:
586:
584:
580:
576:
572:
568:
564:
560:
555:
553:
545:
538:
536:
532:
529:
527:
523:
520:
518:
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511:
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502:
499:
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458:
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413:
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392:
390:
388:
379:
377:
370:
368:
364:
357:
355:
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328:
326:
320:
318:
316:
312:
307:
305:
301:
297:
293:
289:
285:
281:
276:
274:
270:
269:embrittlement
266:
262:
258:
249:
245:
240:
235:
230:
226:
222:
217:
213:
209:
205:
200:
196:
193:130–150 W/m*K
192:
188:
183:
179:
175:
168:
163:
159:
154:
150:
148:
144:
140:
136:
132:
127:
123:
119:
116:
109:
104:
100:
96:
89:
84:
80:
76:
72:
67:
63:
58:
54:
50:
45:
41:
36:
31:
19:
18:7075 aluminum
1934:Named alloys
1800:
1056:Introduction
999:
976:
967:
954:
945:
933:
921:. Retrieved
917:
908:
900:
878:. Retrieved
874:the original
869:
860:
826:. Retrieved
822:
813:
804:
788:
780:
772:
763:
752:
686:
678:
643:Applications
618:
609:
606:
602:fatigue life
587:
556:
549:
535:GB/T 3880.2
534:
525:
516:
504:
489:
483:
482:ASTM B209,
471:Designation
447:Designation
400:
396:
383:
374:
365:
361:
344:
332:
324:
308:
303:
299:
295:
277:
260:
256:
255:
243:
227:714.8 J/kg*K
220:
203:
186:
166:
130:
107:
87:
70:
48:
2002:Hydronalium
1981:Birmabright
1866:8000 series
1739:7000 series
1600:6000 series
1486:5000 series
1437:4000 series
1388:3000 series
1209:2000 series
683:Trade names
594:drag racing
533:GB/T 3190;
524:AS 2848.1,
515:JIS H4000;
509:DIN 1725-1
503:EN AW-7075
441:AISI (UNS)
286:, 1.2–1.6%
282:, 2.1–2.5%
250:51.5 nOhm*m
239:resistivity
2077:Categories
1996:Hiduminium
745:References
666:Automotive
660:Worm gears
629:Interstage
567:M16 rifles
517:JIS H4040
430:Australia
103:Elongation
2027:MKM steel
2017:Magnalium
1991:Duralumin
1063:Aluminium
575:SIG Sauer
563:RC models
500:EN 573-3
490:(A97075)
474:Standard
468:Standard
462:Standard
456:Standard
450:Standard
444:Standard
438:Standard
371:7075-T651
335:tempering
304:7075-T651
284:magnesium
210:2.36*10 K
2062:AlSi10Mg
1598:Al-Mg-Si
959:Archived
923:22 April
880:22 April
849:Archived
828:22 April
721:Archived
692:See also
637:Saturn V
592:used in
583:lacrosse
497:AW-7075
494:ISO 209
424:Germany
393:7075-RRA
263:) is an
147:Rockwell
143:Hardness
33:A7075 T6
2042:Y alloy
1946:AlBeMet
1868:(misc.)
631:of the
380:7075-T7
358:7075-T6
300:7075-T6
292:tempers
237:Volume
44:Density
2007:Italma
1976:Alusil
1966:Alumel
1956:Alnico
1951:Alclad
796:
477:Grade
465:Grade
433:China
427:Japan
341:7075-O
296:7075-0
288:copper
261:AA7075
151:87 HRB
2012:Lo-Ex
1961:AlSiC
1737:Al-Zn
1611:6005A
1484:Al-Mg
1435:Al-Si
1386:Al-Mn
1207:Al-Cu
539:7075
530:7075
521:7075
488:7075
115:break
1925:8176
1920:8093
1915:8091
1910:8090
1905:8030
1900:8025
1895:8019
1890:8014
1885:8011
1880:8009
1875:8006
1856:7475
1851:7255
1846:7178
1841:7150
1836:7129
1831:7116
1826:7093
1821:7091
1816:7090
1811:7085
1806:7079
1801:7075
1796:7072
1791:7068
1786:7065
1781:7055
1776:7050
1771:7046
1766:7039
1761:7034
1756:7022
1751:7010
1746:7005
1727:6951
1722:6463
1717:6351
1712:6262
1707:6205
1702:6201
1697:6162
1692:6151
1687:6113
1682:6105
1677:6101
1672:6082
1667:6081
1662:6070
1657:6066
1652:6065
1647:6063
1642:6061
1637:6060
1632:6022
1627:6013
1622:6010
1617:6009
1607:6005
1588:5754
1583:5557
1578:5457
1573:5456
1568:5454
1563:5356
1558:5252
1553:5182
1543:5086
1538:5083
1533:5059
1528:5056
1518:5050
1513:5026
1508:5024
1503:5019
1498:5010
1474:4543
1469:4047
1464:4043
1459:4032
1454:4015
1449:4007
1444:4006
1425:3203
1420:3105
1410:3102
1405:3005
1400:3004
1395:3003
1376:2618
1371:2524
1366:2519
1361:2397
1356:2319
1351:2297
1341:2219
1336:2218
1331:2198
1326:2197
1321:2196
1316:2195
1311:2124
1306:2099
1301:2098
1296:2097
1291:2095
1286:2094
1281:2091
1276:2090
1271:2080
1266:2055
1261:2048
1256:2036
1251:2029
1246:2025
1241:2024
1236:2020
1231:2017
1226:2014
1221:2011
1216:2004
1197:1469
1192:1464
1187:1461
1182:1460
1177:1450
1172:1445
1167:1441
1162:1440
1157:1430
1152:1424
1147:1421
1142:1420
1137:1370
1132:1350
1127:1230
1122:1200
1117:1199
1112:1145
1107:1100
1102:1070
1097:1060
1092:1050
925:2018
882:2018
830:2018
794:ISBN
633:S-II
546:Uses
418:ISO
280:zinc
137:0.33
579:PGM
415:US
120:11%
113:at
2079::
1083:Al
957:.
953:.
916:.
890:^
868:.
838:^
821:.
317:.
306:.
302:,
298:,
1613:)
1609:(
1041:e
1034:t
1027:v
985:.
927:.
884:.
832:.
259:(
246:)
244:ρ
242:(
223:)
221:c
219:(
206:)
204:α
202:(
189:)
187:k
185:(
172:)
170:m
167:T
165:(
145:—
133:)
131:ν
129:(
110:)
108:ε
106:(
93:)
91:t
88:σ
86:(
73:)
71:E
69:(
51:)
49:ρ
47:(
20:)
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