2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame

Product Details
Customization: Available
Processing Object: Metal
Molding Style: Hot Forging
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Registered Capital
3000000 RMB
Plant Area
101~500 square meters
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
  • 2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
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Overview

Basic Info.

Model NO.
2A14
Molding Technics
Gravity Casting
Application
Aviation
Material
Aluminium
Heat Treatment
Quenching
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

2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame
                                                            2A14 Chemical Property
Alloy Si Fe Cu Mn Mg Cr Ni Zn Ti Zr         Others Al
Each Total
2A14 0.50-1.2            0.70 3.9~5.0 0.4~1.2 0.2~0..8 0.10 ~ 0.25 0.15 ~ 0.05 0.15 Remainder

Alloy Alloy series Main features Σb Value /MPa Temperature/ºC
2A14 Al-Cu-Mg It's close to 2014. The main varieties are bars, profiles, forgings and plates, etc. It is suitable for high load parts with thick section. The welding performance of the alloy is good, and it does not show brittleness at the cold temperature. It can be used to make the welding parts under the cold working condition.

                375~460


<150
 
Technical indexes of common 2A14 aluminum alloy
Alloy Type Temper δor d/mm σb/MPa σp 0.2/MPa δ/% KIC or KC/MPa Technical Standard
2A14 Clad aluminum sheet O >0.5~10.0 ≤245 - 10 - GB/T 3880--1997
T6 >0.5~10.0 430 340 5 -
T62 >4.5~12.5
>12.5~40.0
pre-stretched aluminum plate T651 6.5~12.0 460 405 7 - GJB 1741--1997
>12.0~25.0 460 405 5 -
Aluminum round bar T62,T6 ≤22 440 - 10 - GB/T 3191--1998
>22~150 450 - 10  
High Strength Aluminum bar T62,T6     20~120 460 - 8 -
Extruded aluminum bar T4,T6        ≤22 440 - 10 - HB 5202--1982
23---160 450 - 10  
161--240 430 - 8 -
2A14 Extrusion aluminum profile T4 All thickness 375 205 10 - GJB 2507--1995
T6  ≤10 410 365 7.0  
>10 450 375 7.0 -
O All thickness 195--275 - - -
Free forgings T4 Weight≤750KG L:380
LT:365
ST:325
L:245 L:10
LT:8
ST:4
- GJB 2351-1995
  Weight>750KG L:375
LT:355
ST:325
L:235 L:8
LT:7
ST:4
-
Die forgings T4 - L:380
LT:365
ST:345
L:245
LT:235
L:11
LT:8
ST:6
- GJB 2351--1995
Free forgings T6 ≤30 L:410
LT:355
ST:335
- L:6
LT:4
ST:2
-
>30 L:380
LT:355
ST:335
- L:6
LT:4
ST:2
-
Die forgings ≤30 L:430
LT:390
ST:355
L:315 L:10
LT:6
ST:4
-
>30 L:410
LT:390
ST:355
L:295 L:8
LT:6
ST:3
-

2A14 Welding performance
Alloy Resistance welding Melting welding Argon arc welding Note
2A14 Good Ok - During welding, the tendency of heat crack is larger, so it is necessary to limit the content of iron impurities in the matrix, and the qualified filler can be obtained by using special filler.
 
Alloy Temper Model Application parts and typical parts
2A14 Aluminum sheet: O,T6,T62
Aluminum plate: T651
Aluminum round bar:T62,T6
Aluminum Cold working bar:O,T4,T6
Free forgings: T4,T6
ARJ21,Z9 Window Frame
Detailed Photos

2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame2A14 T4 T6 Aircraft Aerospace Aviation Aluminum Forgings for Window Frame



 

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