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¥DÀç¡G¥N²z¬ü°êªâ¥i¼ÖALCOA¾T¦Xª÷¡F§åµo¼Ò¨ã¶i¤f¾T¦Xª÷¡B¥[®³¤j¼Ò¨ã¾T§÷¡BAL500¶i¤f@»G»k¶Wµw¾T¦Xª÷¡BQC-10¯èªÅ¶Wµw¾T¦Xª÷¡B6061-T651@¿i¶§·¥®ñ¤Æ¾T¦Xª÷¡B7075¥ú«G¾TÁ¡ªO¡B¶i¤f¾T´Î¡BA6061¶§·¥®ñ@»G»k¾TºÞ¡B1100¤u·~¯Â¾T±a¡B1050¯Â¾TªO¯èªÅ¶Wµw«p¾TªO¡B6061¶§·¥®ñ¤Æ¥[µw¾T´Î¡BQC-7¼Ò¨ã¦Xª÷¾T¡B7075-T651¶Wµw ¥N²z¬ü°êALcoa¾T¦Xª÷ªO¡B¤é¥»¦í¤Í/¯«¤á¾T¦Xª÷WELDURAL©MHOKOTOL¶Wµw¾T¦Xª÷Áú°ê»Z¶µ¦Xª÷¾T¡B«Xù´µ¾T¦Xª÷¼Ò¨ã¾T§÷¨T¨®¨î³y¾T§÷¶§·¥®ñ¤Æ¦Xª÷¾TªO¨¾ù×¾T¦Xª÷ªO°ª±j«×¶Wµw¯èªÅ¾T§÷¯Â¾TªO@»G»k¨¾ù×¾T¦Xª÷¶Wµw¯èªÅ¾T¦Xª÷¶i¤f¾T¦Xª÷ªO A7075¶Wµw¾T ¾T´Î 5052¶i¤f¾TªO¥¾ã¾TªO6061¾TºÞ 6061@¿i¾TºÞ ¥ú«GïªO
7075¥Ñ¬ü¾T¤½¥q¦b1943¦~±À¥X¡A¦b¯èªÅ¯è¤Ñ¤u·~¡A7075¦Ü¤µ¤@ª½¬O7xxx«Y¦C¦Xª÷ªº¥D¤O¤O¶q¡C³o¬O¦¸¦¨¥\ªº¦bAL-Zn-Mg-Cu«Y°ª±j«×¦Xª÷¤¤¨Ï¥Î¥[¤J¤F»Ì¦Xª÷¡A¨Ï¤§§Î¦¨¤F¨}¦nªº§ÜÀ³¤O»G»k¶}µõªºªO§÷²£«~¡A¨ä®Ä¯q¼vÅT²`¨è¡CÁöµM¨ä¥L7xxx¦Xª÷¦Ü¤µ¤]¤w¶}µo»P§ï¶i¤F¯S©wªºÄÝ©Ê¡A7075¤´µM¬O¤@ӫܦnªº¥¿Å¯èªÅ¯è¤ÑÀ³¥Î©Ò»Ýªº©Ê¯à°ò½u¡C
Alloy 7075 is Introduced by Alcoa in 1943, alloy 7075 has been the standard workhorse 7XXX series alloy within the aerospace industry ever since. It was the first successful Al-Zn-Mg-Cu high strength alloy using the beneficial effects of the alloying addition of chromium to develop good stress-corrosion cracking resistance in sheet products. Although other 7XXX alloys have since been developed with improved specific properties, alloy 7075 remains the baseline with a good balance of properties required for aerospace applications.
7075¦Xª÷Á¡ªO©M¤¤«pªO²£«~À³¥Î¹M¤Î¯èªÅ¯è¤Ñµ²ºc·í¤¤¡A¨ä¤¤¡A¾A¤¤ªº¶´©Ê©M»G»k©Êªº°ª±j«×µ²¦X¬O§÷®Æ©Ò¨ã¦³ªº¡C
Alloy 7075 sheet and plate products have application throughout aircraft and aerospace structures where a combination of high strength with moderate toughness and corrosion resistance are required.
¤Æ¾Ç¦¨¤À½d³ò¡]«¶q%¡^CHEMICAL COMPOSITON LIMIES (WT.%)
Si | 0.40 | Zn . . . | 5.1-6.1 |
Fe . . . | 0.50 | Ti . . . | 0.20 |
Cu . . . | 1.2-2.0 | Others, each . . . | 0.5 |
Mn . . . | 0.30 | Others, total . . . | 0.15 |
Mg . . . | 2.1-2.9 | Balance, Aluminum | |
Cr . . . | 0.18-0.28 |
Note: Value maximum if range not shown
¾÷±ñ©Ê¯à¡]MECHAN NICAL PROPERTIES¡^
Temper | Thickness in.(mm) | TENSILESTRENGTH Ksi¡]Mpa¡^ | YIEID STRENGTH Ksi¡]Mpa¡^ | ELONGATION % |
0 | 0.015-2.00 | 40 (max) | 21 (max) | 9-10 |
Sheet & plate T6 | (0.38-50.80) 0.008-0.249 | (276) 74-78 | (145) 63-69 |
5-8 |
Sheet T651 | (0.203-6.32) 0.250-4.000 | (510-538) 78-67 | (434-476) 67-54 |
9-3 |
Plate T76 | (6.35-101.60) 0.125-0.249 | (538-462) 73 | (462-372) 62 |
8 |
Sheet T7651 | (3.18-6.32) 0.250-1.000 | (503) 72-71 | (427) 61-60 |
8-6 |
Plate T73 | (6.35-25.40) 0.040-0.249 | (496-490) 67 | (421-414) 56 |
8 |
Sheet T7351 | (1.02-6.32) 0.250-4.000 | (462) 69-61 | (386) 57-48 |
7-6 |
Plate | (6.35-101.60) | (476-421) | (393-331) |
7075©Ò¦³ªºÈ³£¬O§Cªº¾î¦V¾÷±ñ©Ê¯à°£«D¥t¦³»¡©ú¡]ALLOY 7075 All values are minimum long transverse mechanical properties except where noted¡^
¦Xª÷7075¨å«¬ªºÂ_µõ¶´©ÊÈ¡]TYPICAL FRACTURE TOUGHNESS VALUES Alloy 7075 Plate¡^
7075 | T651 T7351 | 26 (28.6) 30 (32.0) | 22(24.2) 26 (28.6) |
PROCUREMENT SPECIFICATIONS
PLATE |
Temper T651 T7651 Specification QQ-A-250/13 QQ-A-250/24 MIL-HDBK-5 Approved |
BARE SHEET ALCLAD SHEET
|
Specification QQ-A-250/12,24 QQ-A-250/13,25,26 MIL-HDBK-5 Approved Approved |
¨ä¥L²£«~§Î¦¡¡]OTHERPRODUCT FORMS¡^
7XXX
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MN inch mm lbs/ft kg/m lbs/ft kg/m lbs/ft kg/m
¤Ï¦V 50 8.85 225 7.90 11.76 5.13 7.64 70.55 102.5
¤Ï¦V 50 7.65 x1.15 194 x30 3.95 5.88 2.56 3.82 70.55 102.5
¤Ï¦V 50 5.0 x2.75 127 x70 3.95 5.88 2.56 3.82 70.55 102.5
¤Ï¦V 50 5.90 x1.15 150 x2.54 3.78 1.56 2.46 70.55 102.5
¤Ï¦V 50 3.5 89 1.57 2.35 1.03 1.52 70.55 102.5
¤Ï¦V 50 2.35 60 0.98 1.47 0.63 0.95 70.55 102.5
¤Ï¦V 50 1.55 40 0.64 0.95 0.42 0.62 70.55 102.5
¥¿¦V 90 22 560 17.88 26.6 6.72 10 235 350
¥¿¦V 90 27.5 x4.5 700 x 120 17.68 26.6 6.72 10 235 350
¥¿¦V 90 29.5 x 2.35 750 x60 - - 6.72 10 235 350
¥¿¦V 90 28.5 x 4.5 730x120 - - 6.72 10 235 350
¥¿¦V 90 27.5 x7.05 700x180 - - 6.72 10 235 350
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7010 7050 7150 7175
ABM 3-1029 AIMS03-02-019 ABM 3-1031 AIMS 03-02-008
ABM 3-1030 AIMS03-02-022 AMS 4252 ASN-A3050
AMS 4204 ABM 3-1029 BAEM 1219 C.R.1.1.0.88
AMS 4205 ABM 3-1030 BAMS 516-006 SMS 003
ASN-A3098 AIR 9048 DMS 2308
ASN-A3101 AMS 4050 7475
BAC M 200 AMS 4201
7075
BAEM 1213 BAEM 1213 AIMS03-02-009
BAEM 1218 BAMS 516-001 AIR 9048 AIR 9048
DAN 422 BAMS 516-003 AMS 4045 AMS 4089
D.T.D. 5120 BMS 7-323 Type I AMS 4078 AMS 4090
D.T.D. 5130 BMS 7-323 Type III AMS-QQ-A-250/12 AMS 4202
EN 2684 CMS 516-001 AMS-QQ-A-250/13 ASN-A3053
EN 2687 CMS 516-003 AMS-QQ-A-250/24 ASN-A3476
MBBN6012 DAN 422 AMS-QQ-A-250/25 BAMS 516-002
MM0533 DGQT1.1.0.97 ASN-A3009 CMS 516-002
SM 9102 DGQT1.1.0.98 ASN-A3049 DAN 422
SMS 3206 DMS 2233 BS2 L.95 DMS 2184
STD 113644 DMS 2459 DAN 422 DMS 2234
TSM 42.03.66 DON 45 EN 2126 DON 45
TSM 42.03.67 DSN 1106 MMS 159 FMS-3004
TSM 42.03.71 EAC MS 1004 SONACA Spec. 7075 MEP 02-013 Std. Type
WL 3.4394 EN 3982 STD 113627 MEP 02-013 Type I
EN 3983 TH 5.316/3 MEP 02-013 Type II
KMB-SK2102 TH 5.316/5 MEP 02-013 Type III
7020
LMA-M7050 WL 3.4364 MM0565
AIR 9048 MEP 02-014 STD 113637
MFM 0017 TSM 42.03.68
MMS 1420 WL 3.4384
MMS 1439
NMS 7-323
OFWN 4037
STD 113643
STM 0887
TSM 42.03.69
TSM 42.03.70
WL 3.4144
¤åÄm-REFERENCES:
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3¡G MIL-H-6088¡A¾T¦Xª÷ªº¼ö³B²z¡C