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§÷®Æ¤¶²Ð¡G¡]Alloy 7075¡^

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¬O²Ä¤@¦¸¦¨¥\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¤@­Ó«Ü¦nªº¥­¿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.  

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

http://www.3566t.com/sell/miaoshun/3062551.html http://www.35667.com/

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)

PLATE

Temper                         T651                                 T7651

Specification                                    

MIL-HDBK-5                 Approved

BARE SHEET                                                         ALCLAD SHEET

Specification                  ,24               ,25,26

MIL-HDBK-5                                                                                                                              Approved                                                                                                                              Approved

¬°¤FÀ°§U¯èªÅ²£·~­ì²£°Ó¡]OEM¡^¶}µo¤Î«Ø³y§C­«¶q¡B§Cªo¯Ó¡B§C±Æ©ñ¡B»·¹Bµ{¡B°ª¦¨¥»®Ä¯qªº«È¾÷©M³f¾÷¡A¹ï©ó¨ÑÀ³°Ó¦Ó¨¥¬°¦U¨î³y°Ó´£¨Ñ§Þ³N¤ä«ùªº·N¸qÅܱo¤é¯q­«­n¡C¾T¨î«~¨ÑÀ³°Óªº¥D­n¬D¾Ô¬O¡A»P¶Ç²Îªº¶°¦¨¬Û¤ñ­ì§÷®Æªº¯S©Ê²Õ¦X¤£±o­­¨î¾ãÅéµ²ºcªº©Ê¯à¡C¦]¦¹¡A¾TªOªº­Y·F­­¨î¥[¤j¡A¥H«OÃÒ½è¶q«Ü¤jªº³¡¥ó¥[¤u¡CªO§÷ªº§Ü¯h³Ò©Ê¡B¶´©Ê©M©µ®i©Êµ¥­Y·F¥D­n¯S©Ê±o·N´£¤É¡A¨Ï±o²£«~©Ê¯à¯à°÷»PÁë³yµ¥¨ä¥L²£«~§ÎºAªº©Ê¯à¬Û·B¬ü¡C¦¹¥~¡AªO§÷ªº³Ñ¾lÀ³¤O±±¨î¦b°ò¦aªº¤ô¥­¡A¨Ï±o§Y¨Ï¦b¤Ø¤o³W®æ©MÁa¾î¬Û¤ñ«Ü¤j®É¤´¯àµL§á¦±ªº¥i¥[¤u©Ê¡C

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                ¥ø·~¼ö½u¡]Tel¡^¡G0769-82990080

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                 ªA°È¼ö½u¡G400-666-4378

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                ¥ø·~¶l½c¡Gliuping@alcoa-dydt.com

                 ¥ø·~ºô¯¸¡Ghttp://www.alcoa-dydt.com

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