• 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
  • 2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings

2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings

Processing Object: Metal
Molding Style: Hot Forging
Molding Technics: Gravity Casting
Application: Aviation
Material: Aluminium
Heat Treatment: Quenching
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Basic Info.

Model NO.
2B50
Surface Treatment
Zinc/Chrome Plating,Anodizing
Forging Tolerance
+/-0.2mm
Standard
ANSI
Certification
CE, ISO 9001:2008
Service
OEM ODM
Transport Package
Export Standard Wooden Pallet or as Your Requsts
Specification
According to Customer Requirement
Trademark
Chalco Aluminum
Origin
Henan China
HS Code
7218100000
Production Capacity
5000pieces/Month

Product Description

2B50 T6 Aircraft Aerospace Aviation Aluminum Forgings
Chemical Composition of 2B50
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr Others Al
Each Total
2B50 0.7~1.2 0.70 1.8~2.6 0.4~0.8 0.4~0.8 0.01~0.20 0.10 0.30 0.02~0.10 - 0.05 0.15 Remainder
 
Alloy Alloy series Mean features
2B50 Al-Cu-Mn The 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 standard d/mm Rm /Mpa A5/%
Not less than
HB 5202 ≤22 365 12
23~160 375 10
161~240 365 8
 
Technical Standard Type L LT ST HBS
Rm/Mpa Rp0.2/Mpa A5/% Rm/Mpa Rp0.2/Mpa A5/% Rm/Mpa A5/%
GJB 2351 Free forgings 365 - 8.0 345 - 6.0 335 4.0 95
Die forgings 380 275 10.0 365 245 7.0 345 5.0 100
HB 5204 Free forgings 365 - 9.0 345 - 6.0 335 4.0 95
Die forgings 380 275 11.0 365 245 7.0 345 5.0 100
 
Typical room temperature mechanical properties of aluminum alloy impeller die forgings of 2B50 T6
Test Direction Tension strength Rm9(Mpa) Yield strength RP0.2(Mpa) A/%
Minimum Maximum Minimum Maximum
L(longitudinal) 380 470 280 390 17.1
LT(Long transverse) 380 465 275 380 15.3
ST(Short transverse) 385 450 280 370 13.7



















 

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