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China 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings

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10 Pieces	Contact Supplier

Local Area:	Zhengzhou, Henan, China
R&D Capacity:	OEM, ODM, Other
Payment Terms:	LC, T/T, D/P, PayPal, WesternUnion, MoneyGram

Processing Object:	Metal
Molding Style:	Hot Forging
Molding Technics:	Gravity Casting

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Product Description

2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
Chemical Composition of 2B50AlloySiFeCuMnMgCrNiZnTiZrOthersAlEachTotal2B500.7~1.20.701.8~2.60.4~0.80.4~0.80.01~0.200.100.300.02~0.10-0.050.15Remainder
AlloyAlloy seriesMean features2B50Al-Cu-MnThe alloy is heat-treated with heat treatment, and the Al-Cu-Mg-Si is a heat treated aluminum alloy. The chemical composition of the alloy is equal to that of 2A50, and the properties of all kinds are basically the same. It has high plasticity in hot state, forging and forging temperature at 420~470 ºC. The alloy is used to make jet engine complex forging parts, such as compressor impeller, impeller and impeller.
Technical standardd/mmRm /MpaA5/%Not less thanHB 5202≤223651223~16037510161~2403658
Technical StandardTypeLLTSTHBSRm/MpaRp0.2/MpaA5/%Rm/MpaRp0.2/MpaA5/%Rm/MpaA5/%GJB 2351Free forgings365-8.0345-6.03354.095Die forgings38027510.03652457.03455.0100HB 5204Free forgings365-9.0345-6.03354.095Die forgings38027511.03652457.03455.0100
Typical room temperature mechanical properties of aluminum alloy impeller die forgings of 2B50 T6Test DirectionTension strength Rm9(Mpa)Yield strength RP0.2(Mpa)A/%MinimumMaximumMinimumMaximumL(longitudinal)38047028039017.1LT(Long transverse)38046527538015.3ST(Short transverse)38545028037013.7