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Rulon Bearings

Aluminum 5024-H116 Al-Scandium Alloy
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 5000 Series Aluminum Alloy

Material Notes: Scandium containing alloy is suggested for aerospace applications. Features good weldability, excellent damage tolerance, good corrosion resistance, creep-formable.

Composition information provided by the Aluminum Association and is not for design. Mechanical property data for creep formed sheet provided by Aleris.

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Physical PropertiesMetricEnglishComments
Density 2.65 g/cc0.0957 lb/in³
 
Mechanical PropertiesMetricEnglishComments
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 GPa10400 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 GPa10700 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-m½31.9 ksi-in½Ke; T-L; Δae = 0 mm
 40.0 MPa-m½36.4 ksi-in½Ke; L-T; Δae = 0 mm
 90.0 MPa-m½81.9 ksi-in½Ke; T-L; Δae = 10 mm
 120 MPa-m½109 ksi-in½Ke; T-L; Δae = 20 mm
 120 MPa-m½109 ksi-in½Ke; L-T; Δae = 20 mm
 150 MPa-m½137 ksi-in½Ke; L-T; Δae = 40 mm
 155 MPa-m½141 ksi-in½Ke; T-L; Δae = 40 mm
 170 MPa-m½155 ksi-in½Ke; L-T; Δae = 60 mm
 175 MPa-m½159 ksi-in½Ke; T-L; Δae = 60 mm
 185 MPa-m½168 ksi-in½Ke; L-T; Δae = 80 mm
 
Component Elements PropertiesMetricEnglishComments
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 %

References for this datasheet.

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