Aleris AA5024-H116 Aluminum Magnesium Scandium Alloy

Category	Metal , Nonferrous Metal , Aluminum Alloy , 5000 Series Aluminum Alloy
Manufacturer	Aleris
Trade Name
Port	Ningbo port,China
Trade Terms	FOB, CFR, CIF
Payment Terms	L/C, T/T, Western Union
Download PDF	Aleris AA5024-H116 Aluminum Magnesium Scandium Alloy.pdf
Price	EMAIL US sales@lookpolymers.com

Material Notes:

Features good weldability, excellent damage tolerance, good corrosion resistance, creep-formability. Aleris AlMgSc alloy AA5024 H116 allows simplification of the manufacturing process of aircraft fuselage components. With AA5024 H116 AlMgSc, stringer reinforced aircraft fuselage components can be either Laser Beam Welded (LBW) or Friction Stir Welded (FSW) when the individual parts are still flat, without any prior treatment. The single or double curvature of the fuselage part required for the aircraft body is achieved by creep forming at elevated temperature.Recommended for use as fuselage skin sheet with medium strength but excellent damage tolerance and corrosion properties and can potentially replace traditionally used 2xxx alloys even as drop-in solution.Temper, AMS and MMPDS registration pending. AA5024 H116 is covered by the Airbus specification AIMS 03-04-055 Information and property data for creep formed and welded (if applicable) sheet provided by Aleris.

Physical Properties	Metric	English	Comments
Density	2.65 g/cc	0.0957 lb/in³

Mechanical Properties	Metric	English	Comments
Tensile Strength, Ultimate	315 MPa @Thickness 1.60 mm	45700 psi @Thickness 0.0630 in	LT Direction
	375 MPa @Thickness 3.00 mm	54400 psi @Thickness 0.118 in	LT Direction
	375 MPa @Thickness 7.00 mm	54400 psi @Thickness 0.276 in	LT Direction
	380 MPa @Thickness 3.00 mm	55100 psi @Thickness 0.118 in	L Direction
	380 MPa @Thickness 7.00 mm	55100 psi @Thickness 0.276 in	L Direction
	395 MPa @Thickness 1.60 mm	57300 psi @Thickness 0.0630 in	L Direction
Tensile Strength, Yield	305 MPa @Thickness 3.00 mm	44200 psi @Thickness 0.118 in	L Direction
	305 MPa @Thickness 7.00 mm	44200 psi @Thickness 0.276 in	L Direction
	305 MPa @Thickness 3.00 mm	44200 psi @Thickness 0.118 in	LT Direction
	305 MPa @Thickness 7.00 mm	44200 psi @Thickness 0.276 in	LT Direction
	310 MPa @Thickness 1.60 mm	45000 psi @Thickness 0.0630 in	LT Direction
	315 MPa @Thickness 1.60 mm	45700 psi @Thickness 0.0630 in	L Direction
Elongation at Break	15 % @Thickness 1.60 mm	15 % @Thickness 0.0630 in	L Direction
	15 % @Thickness 3.00 mm	15 % @Thickness 0.118 in	L Direction
	15 % @Thickness 7.00 mm	15 % @Thickness 0.276 in	L Direction
	17 % @Thickness 7.00 mm	17 % @Thickness 0.276 in	LT Direction
	18 % @Thickness 3.00 mm	18 % @Thickness 0.118 in	LT Direction
	19 % @Thickness 1.60 mm	19 % @Thickness 0.0630 in	LT Direction
Tensile Modulus	72.0 GPa	10400 ksi
Compressive Strength	295 MPa @Thickness 7.00 mm	42800 psi @Thickness 0.276 in	L Direction
	300 MPa @Thickness 7.00 mm	43500 psi @Thickness 0.276 in	LT Direction
	305 MPa @Thickness 3.00 mm	44200 psi @Thickness 0.118 in	LT Direction
	305 MPa @Thickness 3.00 mm	44200 psi @Thickness 0.118 in	L Direction
	315 MPa @Thickness 1.60 mm	45700 psi @Thickness 0.0630 in	LT Direction
	325 MPa @Thickness 1.60 mm	47100 psi @Thickness 0.0630 in	L Direction
Compressive Modulus	74.0 GPa	10700 ksi
Fatigue Strength	145 MPa @# of Cycles 1.00e+6	21000 psi @# of Cycles 1.00e+6	T-L
	145 MPa @# of Cycles 300000	21000 psi @# of Cycles 300000	T-L
	175 MPa @# of Cycles 100000	25400 psi @# of Cycles 100000	T-L
	180 MPa @# of Cycles 80000	26100 psi @# of Cycles 80000	T-L
	190 MPa @# of Cycles 50000	27600 psi @# of Cycles 50000	T-L
	290 MPa @# of Cycles 10000	42100 psi @# of Cycles 10000	T-L
	365 MPa @# of Cycles 1000	52900 psi @# of Cycles 1000	T-L
Fracture Toughness	35.0 MPa-m½	31.9 ksi-in½	K<sub>e</sub>; T-L; Δa<sub>e</sub> = 0 mm
	40.0 MPa-m½	36.4 ksi-in½	K<sub>e</sub>; L-T; Δa<sub>e</sub> = 0 mm
	90.0 MPa-m½	81.9 ksi-in½	K<sub>e</sub>; T-L; Δa<sub>e</sub> = 10 mm
	120 MPa-m½	109 ksi-in½	K<sub>e</sub>; T-L; Δa<sub>e</sub> = 20 mm
	120 MPa-m½	109 ksi-in½	K<sub>e</sub>; L-T; Δa<sub>e</sub> = 20 mm
	150 MPa-m½	137 ksi-in½	K<sub>e</sub>; L-T; Δa<sub>e</sub> = 40 mm
	155 MPa-m½	141 ksi-in½	K<sub>e</sub>; T-L; Δa<sub>e</sub> = 40 mm
	170 MPa-m½	155 ksi-in½	K<sub>e</sub>; L-T; Δa<sub>e</sub> = 60 mm
	175 MPa-m½	159 ksi-in½	K<sub>e</sub>; T-L; Δa<sub>e</sub> = 60 mm
	185 MPa-m½	168 ksi-in½	K<sub>e</sub>; L-T; Δa<sub>e</sub> = 80 mm

Component Elements Properties	Metric	English	Comments
Aluminum, Al	92.95 - 95.95 %	92.95 - 95.95 %	As Balance
Chromium, Cr	<= 0.10 %	<= 0.10 %
Copper, Cu	<= 0.20 %	<= 0.20 %
Iron, Fe	<= 0.40 %	<= 0.40 %
Magnesium, Mg	3.9 - 5.1 %	3.9 - 5.1 %
Manganese, Mn	<= 0.20 %	<= 0.20 %
Other, each	<= 0.05 %	<= 0.05 %
Other, total	<= 0.15 %	<= 0.15 %
Scandium, Sc	0.10 - 0.40 %	0.10 - 0.40 %
Silicon, Si	<= 0.25 %	<= 0.25 %
Titanium, Ti	<= 0.20 %	<= 0.20 %
Zinc, Zn	<= 0.25 %	<= 0.25 %
Zirconium, Zr	0.05 - 0.20 %	0.05 - 0.20 %

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