2024 T3510 T3511 Aircraft Aerospace Aluminum Extrusions Section for Aviation

2024 T3510 T3511 Aircraft Aerospace Extruded Aluminum Profiles for Aviation                                                            Chemical composition of 2024 alloyAlloySiFeCuMnMgCrNiZnTiZr        OthersAlEachTotal20240.50   0.503.8~4.90.3~0.91.2~1.80.10~0.250.15~0.050.15Remainder  AlloyAlloy seriesMain featuresΣb Value/MPaWorking temperature /ºC2024Al-Cu-MgThe heat-treated reinforced alloy is a common medium strength structural material, which can produce all kinds of semi-finished products. The commonly used T3 and T4, has high toughness and plasticity, good fatigue performance and anti crack performance, but poor corrosion resistance, less than 1mm thickness or molding, aluminum sheet and plate should be used, the short transverse properties and stress corrosion resistance are poor, not fusion welding and brazing.                390~48512.7~44.5≤220 12~T30.2032~0.228643428910~T420.254~0.50842726212~>0.508~6.324642726215~6.35~12.6742726212~12.7~25.44202627~>25.4~50.84132626~>50.8~76.24002624~T85112.7~25.44554005~>25.4~38.07464553935~  AlloyTemperTypeSize/inchTest DirectionFtu/KsiFty/ksiABAB2024T3Aluminum sheetδ0.01~0.128L64654748T63644243T351Aluminum sheetδ0.129~0.249L65664748T64654243δ0.250~0.499L64664850T64664244δ0.500~1.000L63654850T63654244 δ1.001~1.500L62644750T62644244δ1.501~2.000L62644749T62644244 δ2.001~3.000L60624648T60624244S52543840δ3.001~4.000L57594346T57594143S49513839   T4Aluminum sheetδ0.010~0.249    L62644042T62644042   T81Aluminum sheet         δ0.010~0.249    L67685961T67685860   T851Aluminum sheetδ0.250~0.499L67685860T67685860T3 Aluminum sheetδ0.0080~0.009L59604445T58593940δ0.0100~0.062L60614445T59603940δ0.063~0.128L62634547T61624042δ0.129~0.249L63644547T6263442T351Clad aluminum sheetδ0.250~0.499L62644648T62644042δ0.500~1.000L61634548T61634042Δ1.001~1.500L60624548T60624042Δ1.501~2.000L60624547T60624042Δ2.001~3.000L58604046T58604042S52543840Δ3.001~4.000L55573941T55573941S49513839T4Clad aluminum sheetδ0.010~0.062L58593638T58593638δ0.063~0.128L61623839T61623839T42Clad aluminum sheetδ0.008~0.009L55573435T55573435δ0.010~0.062L57593435T57593435δ0.063~0.249L60623638T60623638T851Clad aluminum sheetδ0.250~0.499L65665658T65665658T3T3510T3511Aluminum profileThe cross-sectional area less than 20 square inches δ≤0.249L57614247T54583741The cross-sectional area less than 20 square inches δ0.250~0.499L60624447T56573840The cross-sectional area less than 20 square inches δ0.500~0.749L60624447T54563739The cross-sectional area less than 20 square inches δ0.750~1.499L65704654T56603743The cross-sectional area less than 20 square inches δ1.500~2.999L70745254T55583941The cross-sectional area less than 20 square inches δ3.000~4.999L70745254T54573941T3Aluminum pipeδ0.018~0.024L64664245δ0.025~0.049L64664245δ0.050~0.259L64664245δ0.260~0.500L64664245          2024Welding propertiesAlloyResistance weldingMelting weldingArgon arc weldingNote2024GoodWorseWorseFor gas welding and argon arc welding of aluminum alloy as solder, tend to form crystalline cracks; 4A01 alloy solder, forming cracks tend to be significantly reduced, but the strength of welded joint is greatly reduced, such as heat treatment after welding, the joint strength is close to the substrate, but the ductility decreases.  Typical application of 2024 aluminum alloyAlloyFeaturesTemperAircraft typeApplication parts and typical parts2024In a typical aluminum alloy, good performance, high strength, good heat tolerance, used in the manufacture of 150 DEG working parts, heat treatment strengthening effect, poor corrosion resistance, can improve the corrosion resistance of aluminum.Aluminum sheet: O,T3,T361,T4,T72,T861Aluminum plate: O,T351,T361,T851,T861Aluminum pipe:O,T3Pipe,Profile,round bar,wire:Cold working aluminum round bar:O,T13,T351,T4,T6,T851Cold working aluminum wire:O,T13,T36,T4,T6Rivet wire: T4B737-300,A320,Y8,ARJ21,JH7,J10The fuselage skin, central wing stringers, wingtip assembly skin, web frame etc..  /* January 22, 2024 19:08:37 */!function(){function s(e,r){var a,o={};try{e&&e.split(",").forEach(function(e,t){e&&(a=e.match(/(.*?):(.*)$/))&&1