AA 7050 is a heat treatable alloy that has very high mechanical properties and high fracture toughness. Popular with the aerospace industry, AA 7050 offers good stress and corrosion cracking resistance and high strength at subzero temperatures.PropertiesGeneralPropertyValueCommentDensity2.7 - 2.85 g

AA 7050 is a heat treatable alloy that has very high mechanical properties and high fracture toughness. Popular with the aerospace industry, AA 7050 offers good stress and corrosion cracking resistance and high strength at subzero temperatures.PropertiesGeneralPropertyValueCommentDensity2.7 - 2.85 g

Aluminum AA 6063 is an architectural alloy that offers users a high resistance to corrosion and excellent finishing characteristics. Easy to extrude with fair machinability, AA 6063 can be both hot and cold formed and is commonly available as T6 temper as well as T4 temper.PropertiesGeneralPropertyV

Aluminum Alloy AA 2219, an age-hardenable alloy is produced with a copper additive. It is well-known for its excellent structural strength and it’s used for numerous high temperature applications. It is a suitable alloy for many metalworking processes including machining, forming, heat treatment,

Aluminum Alloy AA 2219, an age-hardenable alloy is produced with a copper additive. It is well-known for its excellent structural strength and it’s used for numerous high temperature applications. It is a suitable alloy for many metalworking processes including machining, forming, heat treatment,

Aluminum Alloy AA 2219, an age-hardenable alloy is produced with a copper additive. It is well-known for its excellent structural strength and it’s used for numerous high temperature applications. It is a suitable alloy for many metalworking processes including machining, forming, heat treatment,

DIN S355J2G3 is a corrosion resistant, low alloy structural steel, that is known for its good forming properties and high durability. It offers high strength and can be welded to other weldable steels.PropertiesGeneralPropertyTemperatureValueConditionRelated StandardsShapeDensity20 °C7.83 g/cm³norma

DIN S235J2G3 is a low carbon steel primary for structural use. For european steel standards DIN S235J2G3 (DIN/EN 1.0116) was replaced by the steel grade EN S235J2 (DIN/EN 1.0117) according to EN 10025 (1994-03).PropertiesGeneralPropertyTemperatureValueConditionRelated StandardsShapeDensity20 °C7.85

The alloy Al99,85Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependen

The alloy Al99,85Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependen

DIN 3.3211 is a readily available alloy that has good surface finish and ability to be anodized.Easy of weldability and brazability with nice surface finish. Resistance to corrosion from seawater and atmospheric conditions. Suitable for hot forging.PropertiesGeneralPropertyValueConditionRelated Stan

This cold and hot hardenable material reaches mechanical strength from 200 to 250 MPa with A5-elongation at break of approx. 10 %. In the warm and cold-hardened state this alloy is only limited ductile, in the soft material condition however well. Weldability, corrosion resistance and anodising of

This cold and hot hardenable material reaches mechanical strength from 200 to 250 MPa with A5-elongation at break of approx. 10 %. In the warm and cold-hardened state this alloy is only limited ductile, in the soft material condition however well. Weldability, corrosion resistance and anodising of

From the type of alloy AlMgSi is the alloy AlMgSi1 that, which used longest. This cold and/or hot hardenable material reaches strength values of 200 to 315 MPa with A5-elongation at break of approx. 6 to 18 %. In hot and cold-hardened condition is this alloy only limited formable, in the soft materi

From the type of alloy AlMgSi is the alloy AlMgSi1 that, which used longest. This cold and/or hot hardenable material reaches strength values of 200 to 315 MPa with A5-elongation at break of approx. 6 to 18 %. In hot and cold-hardened condition is this alloy only limited formable, in the soft materi

Alloy AlCu2MgNi (AlCuMgFeNi) is an especially for aircraft construction modified alloy of type AlCuMg. Beside 2,5 % Cu it contains 1,5 % Mg as well as 1,1 % Fe and Ni. It is a natural and artificial ageable, high-strength alloy and achieves tensile strength values up to 430MPa at A5-ductile yiled of

Alloy AlCu2MgNi (AlCuMgFeNi) is an especially for aircraft construction modified alloy of type AlCuMg. Beside 2,5 % Cu it contains 1,5 % Mg as well as 1,1 % Fe and Ni. It is a natural and artificial ageable, high-strength alloy and achieves tensile strength values up to 430MPa at A5-ductile yiled of

Aluminum DIN 3.1355, known for its use in aircraft industry, is an alloy that offers excellent strength. When in the annealed condition it is readily formed and has good machinability. Though it has a relatively low level of corrosion resistance, it can be machined to a high finish.PropertiesGeneral

DIN 3.1255 is an alloy with strength, machinability and welding capabilities, Aluminum Alloy DIN 3.1255 is an excellent option. It is a precipitation hardening alloy that maintains strength after heat treatment.PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.8 g/cm³T652EN 573-3, EN

The alloy AlMn1Mg0,5 is similarly to AlMn1 in its properties. It reaches strength up to F 25. The alloy belongs to the nature-hard aluminum materials. A strength increase can only occure by cold forming. It is very well hot and cold formable and is suitable to the deep-drawing (no lappet formation).