7075 T651 Aerospace Aluminium Plate Sheet

• Customization: Available
• Surface Treatment: Mill Finish
• Elongation: More Than 10%
• Model NO.: 7075 T651
• Application: Transportation Tools, Aviation
• Certification: ISO9001, ASTM, JIS, GB, En
• Grade: 7000 Series
• Alloy: Alloy
• Technique: Hot Rolled
• Temper: T651, T7351, T7651, T7451, T6151, T7751
• Transport Package: Export Standard Wooden Pallet
• Specification: According to Customer Requirement
• Trademark: Chalco Aluminum
• Origin: Henan China
• HS Code: 7606125900
• Production Capacity: 20000mt/Month

Product Description

7075 T651 Aerospace Aluminium Plate Sheet

The 7 ××× system alloy is an aluminum alloy with Zn as the main alloy element, which is a heat treatment to strengthen the aluminum alloy. The alloy is Mg, Al-Zn-Mg alloy, alloy has good thermal deformation, quenching range, can get high strength heat treatment in the appropriate conditions, can be welding performance is good, generally have good corrosion resistance, stress corrosion tendency is Aluminum Alloy weldable high strength.



Al-Zn-Mg-Cu alloy is developed by adding Cu in Al-Zn-Mg alloy on the basis of its strength is higher than 2××× series alloys, commonly known as the Aluminum Alloy ultra high strength, the yield strength of the alloy is close to the tensile strength, yield strength and tension strength rate high, strength ratio is very high, but the plastic and high temperature strength is low, should be at room temperature 120ºC below, use of force bearing structure, easy processing, good corrosion resistance and high toughness.

7xxx alloy series, because of its long history and varieties of materials, including sheet metal, aluminum plate, medium plate, heavy plate, forgings and extruded parts, has been series of materials and heat treatment. It has been the most widely used high-strength aluminum alloy. The 7175 alloys developed later are special forged alloys, and 7475 are mainly used in the manufacture of thin plates and thick plates. 7475 alloy is the best alloy in the 7075 series with damage tolerance.
 

Chemical Composition of 7×××Aluminum Alloy
Alloy		Zn	Mg	Cu	Cr	Zr	Ti	Si	Fe
7075 Series	7075	5.0~6.1	2.1~2.9	1.2~2.0	0.18~0.28	-	-	≤0.40	≤0.50
	7175	5.0~6.1	2.1~2.9	1.2~2.0	0.18~0.28	-	-	≤0.15	≤0.20
	7475	5.2~6.2	1.9~2.9	1.2~1.9	0.18~0.25	-	-	≤0.10	≤0.12
7050 Series	7050	5.7~6.7	1.9~2.9	2.0~2.6	0.04	0.08~0.15	-	≤0.12	≤0.15
	7010	5.7~6.7	2.1~2.6	1.5~2.0	0.04	0.11~0.17	-	≤0.12	≤0.15
	7150	5.9~6.9	2.0~2.7	1.9~2.5	0.04	0.08~0.15	-	≤0.10	≤0.15
	7055	7.6~8.4	1.8~2.3	2.0~2.6	0.04	0.08~0.15	-	≤0.10	≤0.15
7049 Series	7049	7.2~8.2	2.0~2.9	1.2~1.9	0.1~0.22	0.25 Zr+Ti		≤0.25	≤0.35
	7149	7.2~8.2	2.0~2.9	1.2~1.9	0.1~0.22	0.25 Zr+Ti		≤0.15	≤0.20
	7249	7.5~8.2	1.9~2.6	1.3~1.9	0.12~0.18	0.25 Zr+Ti		≤0.10	≤0.12
									≤0.15
7B50 Series	7B50	6.0-7.0	2.0-2.8	1.8-2.6	0.04	0.08-0.16	0.1	0.12	0.15
7A55 Series	7A55	7.5-8.5	1.8-2.8	1.8-2.5	0.04	0.08-0.20	0.10-0.25	0.10	0.10

Alu Sheet Specification

Alloy	Temper	Thickness (mm)	Width  (mm)
7075	T6,T73, T76,T74	0.5-3.5	800-2600
7475
7050		3.5-6.0	800-2900
7B50

Alu Plate Specification

Alloy	Temper	Thickness (mm)	Width  (mm)
7075	T651 T7351 T7651 T7451 T7751	6-12	800-2900
7475
7050		12-250	800-3800
7B50
7A55

Alu Sheet Mechanical Properties

Alloy	Temper	Typical Thickness	Rm(Mpa) Tensile Strength	Rp0.2(Mpa) Yield Stregth	(%) Elongation	Stangard
7075	T6	0.5-6.0	580	500	12	SAE AMS-QQ-A-250/12
7075	T73	0.5-6.0	480	405	12	SAE AMS-QQ-A-250/12
7075	T76	0.5-6.0	490	410	12	SAE AMS-QQ-A-250/12
7475	T61	0.5-6.0	540	460	12	SAE AMS 4084
7475	T761	0.5-6.0	510	435	12	SAE AMS 4085
7050	T76	0.5-6.0	535	485	10	SAE AMS 4243

Alu Plate Mechanical Properties

Alloy	Temper	Typical Thickness	Rm(Mpa) Tensile Strength	Rp0.2(Mpa) Yield Stregth	(%) Elongation	Stangard
7075	T651	6.0-225.0	570	495	10	SAE AMS 4045
7075	T7351	6.0-150.0	500	420	10	SAE AMS 4078
7475	T7651	6.0-50.0	510	435	10	SAE AMS 4089
7050	T7451	6.0-225.0	530	460	10	SAE AMS 4050
7050	T7651	6.0-100.0	550	480	10	SAE AMS 4201
7B50	T6151	6.0-50.0	600	550	12	-
7B50	T7751	6.0-100.0	590	540	10	-
7A55	T7751	6.0-50.0	635	605	10	-

Application parts and typical parts:

The thick section of the main structure of high load, such as the manufacture of fuselage frame and bulkhead, wing skin, extrusion reinforcing rod, stringers and ribs, forging parts, gear support member, beams, strengthening panels, flanges, important joints etc..