Abstract: The casting alloy according to the invention is based on aluminum-iron-nickel and includes the following elements: iron 0.8 to 3.0% by weight nickel 0.1 to 3.5% by weight boron 40 to 300 ppm zinc 0-5% by weight tin 0-5% by weight copper 0-3% by weight manganese 0-1% by weight magnesium 0-0.6% by weight phosphorus 0-500 ppm Silicon 0-0.4%.

Abstract: A cast alloy including iron 0.8-3.0 wt. %, magnesium 0.01-9.0 wt. %, manganese 0-2.5 wt. %, beryllium 0-500 ppm, titanium 0-0.5 wt. %, silicon 0-0.8 wt. %, strontium 0-0.8 wt. %, phosphorus 0-500 ppm, copper 0-4 wt. %, zinc 0-10 wt. %, 0-0.5 wt. % of an element or a group of elements selected from the group consisting of chromium, nickel, molybdenum, zirconium, vanadium, hafnium, calcium, gallium and boron, and the remainder being aluminium and unavoidable impurities.

Abstract: An aluminium, magnesium and silicon-based die casting alloy having 5.0-7.0 wt. % magnesium, 1.5-7.0 wt. % silicon, 0.3-0.8 wt. % manganese, 0.03-0.5 wt. % iron, 0.01-0.4 wt. % molybdenum, 0.01-0.3 wt. % zirconium, 0-0.25 wt. % titanium, 0-0.25 wt. % strontium, 0-250 ppm phosphorus, 0-4 wt. % copper and 1-10 wt. % zinc, the remainder being aluminium and inevitable impurities.

Abstract: An aluminium, magnesium and silicon-based die casting alloy having 5.0-7.0 wt. % magnesium, 1.5-7.0 wt. % silicon, 0.3-0.8 wt. % manganese, 0.03-0.5 wt. % iron, 0.01-0.4 wt. % molybdenum, 0.01-0.3 wt. % zirconium, 0-0.25 wt. % titanium, 0-0.25 wt. % strontium, 0-250 ppm phosphorus, 0-4 wt. % copper and 1-10 wt. % zinc, the remainder being aluminium and inevitable impurities.

Abstract: A cast alloy including iron 0.8-3.0 wt. %, magnesium 0.01-9.0 wt. %, manganese 0-2.5 wt. %, beryllium 0-500 ppm, titanium 0-0.5 wt. %, silicon 0-0.8 wt. %, strontium 0-0.8 wt. %, phosphorus 0-500 ppm, copper 0-4 wt. %, zinc 0-10 wt. %, 0-0.5 wt. % of an element or a group of elements selected from the group consisting of chromium, nickel, molybdenum, zirconium, vanadium, hafnium, calcium, gallium and boron, and the remainder being aluminium and unavoidable impurities.

Abstract: A die casting alloy on an aluminum-silicon base with a composition having 8.5 to 11.5 wt. % of silicon, 0.1 to 0.5 wt. % of magnesium, 0.3 to 0.8 wt. % of manganese, 0.02 to 0.5 wt. % of iron, 0.005 to 0.5 wt. % of zinc, 0.1 to 0.5 wt. % of copper, 0.02 to 0.3 wt. % of molybdenum, 0.02 to 0.3 wt. % of zirconium, 10 to 200 ppm of gallium and optionally at least one of 30 to 300 ppm of strontium, 5 to 30 ppm of sodium, 1 to 30 ppm of calcium, 5 to 250 ppm of phosphorus, 0.02 to 0.25 wt. % of titanium, and 3 to 50 ppm of boron with the remainder being aluminium and unavoidable impurities. The alloy can be produced with a recycling rate of 50%.

Abstract: An aluminum alloy for components with increased rigidity, having a tensile yield strength Rp0.2>200 MPa and simultaneous elongation at break A>6% after a heat treatment, or a tensile yield strength Rp 0.2>120 MPa and simultaneously high elongation at break A>9% in the cast state, or >10% after a T6 heat treatment, in particular for structural and chassis components of a motor vehicle, containing 9 to 11.5 wt % silicon, 0.5 to 0.8 wt % manganese, 0.2 to 1.0 wt % magnesium, 0.1 to 1.0 wt % copper, 0.2 to 1.5 wt % zinc, 0.05 to 0.4 wt % zirconium, 0.01 to 0.4 wt % Cr, max. 0.2 wt % iron, max. 0.15 wt % titanium, 0.01 to 0.02 wt % strontium and the remainder as aluminum and production-related impurities with a maximum total of 0.5 wt %.

Abstract: Aluminum alloy for components having increased strength with a yield point Rp0.2>120 MPa and at the same time an elongation at break A>7% in the cast state, a yield point Rp0.2>200 MPa and at the same time an elongation at break A>6% after a T5 heat treatment or a yield point Rp0.2>200 MPa and at the same time a high elongation at break A>9% after a T6 heat treatment, in particular for structural and chassis parts of a motor vehicle.

Abstract: An aluminum alloy for components with increased rigidity, having a tensile yield strength Rp0.2>200 MPa and simultaneous elongation at break A>6% after a heat treatment, or a tensile yield strength Rp 0.2>120 MPa and simultaneously high elongation at break A>9% in the cast state, or >10% after a T6 heat treatment, in particular for structural and chassis components of a motor vehicle, containing 9 to 11.5 wt % silicon, 0.5 to 0.8 wt % manganese, 0.2 to 1.0 wt % magnesium, 0.1 to 1.0 wt % copper, 0.2 to 1.5 wt % zinc, 0.05 to 0.4 wt % zirconium, 0.01 to 0.4 wt % Cr, max. 0.2 wt % iron, max. 0.15 wt % titanium, 0.01 to 0.02 wt % strontium and the remainder as aluminum and production-related impurities with a maximum total of 0.5 wt %.

Abstract: Aluminium alloy for components having increased strength with a yield point Rp0.2>120 MPa and at the same time an elongation at break A>7% in the cast state, a yield point Rp0.2>200 MPa and at the same time an elongation at break A>6% after a T5 heat treatment or a yield point Rp0.2>200 MPa and at the same time a high elongation at break A>9% after a T6 heat treatment, in particular for structural and chassis parts of a motor vehicle.