Fabrication panels
Sheet for bending, welding and general fabrication work.
Mill-finish and application-led aluminum sheet for fabrication, transport, marine and general engineering.

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90 original product records are available in this category. Showing 1-9.

7475 T7351 aircraft aluminum Plate is a high strength material and mainly used to manufacture key parts such as aircraft frames, skins, and landing gears.
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Aerospace aluminum is preferred because of high strength to weight ratio, ductility and resistance to corrosion. It is also non-magnetic. There is a wide range of variations in the compositions of aluminium alloys for specific functions in an aircraft. 7475 aluminum alloy, American deformed aluminum alloy is also a main aluminum alloy used in aerospace industry. It belongs to Al-Zn-Mg-Cu aluminum alloy, which is used for aluminum-clad and non-aluminum-clad plates for the fuselage, wing skeletons, stringers, etc., having both high strength and high toughness. Available aluminum sheet grade 1000 series:1050,1060,1070,1080,1100,1145,1200,1235, etc. 2000 series:2014,2017,2018,2024,2025,2219, 2219,2618a etc. 3000 series:3003,3004,3102,3104,3105,3005, etc. 4000 series:4032,4043, 4017, etc 5000 series: 5005,5052,5454,5754,5083,5086,5182,5082, etc. 6000 series:6061,6063,6262,6101, etc 7000 series:7072,7075,7003, 7475, etc 8000 series: 8011, etc. Temper of aluminum sheet: O, H, W, F, T H:H12, H14, H16, H18, H19, H22, H24, H26, H32, H34, H111, H112, H114, H116 T: T0-T651 Size of aluminum sheet Thickness:0.2-6.0mm Width:100-2400mm Length:200-11000mm
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7175 T351 aviation aluminum plate is a high-strength, high-hardness aviation aluminum plate that is commonly used to manufacture aircraft structural parts.
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Aerospace grade 7075-T651 aluminum plate — ultra-high strength (572 MPa). Used in aircraft structures, defense, and high-performance tooling. Thickness 6-150mm. AMS 4045 compliant.
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7075 (UNS A97075) aluminumu plate is an aerospace aluminum alloy with cold finished or extruded aluminum wrought alloy with high strength, adequate machinability.
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7075 aluminum alloy (AA7075) is an aluminum alloy with zinc as the primary alloying element. It has excellent mechanical properties and exhibits good ductility, high strength, toughness, and good resistance to fatigue. It has moderated formability when in the fully soft, annealed temper and can be heat-treated to strength levels that are comparable to many steel alloys. In fact, grade 7075 aluminum is stronger than many types of mild steel. 7075-T6 aluminum has nearly double the strength-to-weight of grade 2 titanium the 7075 Al alloy is most preferred by the aircraft industry. The composition of this specific Al alloy is 5.1–6.1% zinc, 2.1–2.9% magnesium, 1.2–2.0% copper and less than 0.5% of silicon, iron, manganese, titanium, chromium and other trace metals Size of aluminum sheet Thickness:0.2-6.0mm Width:100-2400mm Length:200-11000mm Mother coil: CC or DC Weight: About 2mt per pallet for general size MOQ: 5 -15 ton per size Protection: paper inter layer, white film, blue film, black-white film, micro bound film, according to your requirement. Surface: clean and smooth, no bright speck, corrosion, oil, slotted, etc. Standard product: GBT3880, JIS4000, EN485, ASTM-B209 Delivery time: about 30days after receiving the deposit Payment: T/T, L/C at sight
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