Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar

Product Details
Customization: Available
Shape: Round.Square.Rectangle
Application: Transportation Tools, Door & Window, Glass Wall, Heat Sink, Decorations
Manufacturer/Factory, Group Corporation
Diamond Member Since 2024

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  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
  • Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
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  • Overview
  • Product Description
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  • FAQ
Overview

Basic Info.

Technique
Cold Rolled, Hot Rolled
Grade
2000 Series
Temper
O - H112
Surface Treatment
Color Coated
Alloy
Alloy
Key Words
Aluminum 2219 Bar/Rod
Diameter
5mm - 500mm
Length
as Your Requirments
Sample
Free-Sample
MOQ
100kgs
Surface
Polished, Mirror, Hl, 180 Grit, 400 Grit, 600 Grit
Stock
in Stock
Trade Term
Fob CIF CFR EXW etc
Transport Package
Wooden Package
Specification
ASTM B209/ AMS-QQ-A-250/AMS 4462
Trademark
LORK
Origin
China
HS Code
7505120000
Production Capacity
50000kg/Month

Product Description

Product Description

 

Introduction

LORK exports a wide range of 2219 Aluminum tube which performs brilliantly in large temperature and concentration ranges. 
 

2219 Aluminum is a precipitation/age-hardening alloy with excellent strength and mechanical properties. This copper-containing alloy features extreme toughness and excellent stress corrosion resistance when treated. 2219 is readily machinable and is useful over a temperature range of -452°F to 600°F. It is also readily weldable and has good fracture toughness. In the T8 condition, it is resistant to stress corrosion cracking.

Aluminum 2219 is typically used in a range of aerospace products, with high-temperature structural applications including space boosters and fuel tanks.

2219 Aluminum Alloy Applications

• Supersonic aircraft skin
• Structural members
• High strength weldments
• Space boosters
• Fuel tanks
• Aircraft parts

Aluminum 2219 Specifications

AMS 4031 - 0/F Sheet, Plate
AMS 4066 - T8511 Drawn, Seamless Tubing
AMS 4068 - T3511 Drawn, Seamless Tubing
AMS 4094 -  T81 Clad Sheet / T851 Clad Plate
AMS 4095 -T31 Clad Sheet / T351 Clad Plate
AMS 4096 -0 Clad Sheet / Plate
AMS 4143 - T6 Forgings / Rolled or Forged Rings
AMS 4144 - T852/T851 Hand Forgings
AMS 4162 - T8511 Extrusions
AMS 4313 - T351/T352 Forgings/Rolled or forged rings
DMS1719 - T81 Alclad Sheet
QQ-A-250/30 - 2219 Bare Sheet, Plate
QQ-A-367
QQ-A-430
MIL-A-22771
MIL-A-46118
MIL A-46808
MIL A-8920
ASTM B209
ASTM B211
ASTM B221
ASTM B241
ASTM B316
SAE J454

2219 Aluminum Alloy Chemical Composition

The following table shows the chemical composition of Aluminium / Aluminum 7050 alloy.

Element Content (%)
Aluminum, Al 93.0
Copper, Cu 6.3
Magnesium, Mg 0.30
Zirconium, Zr 0.18
Vanadium, V 0.10
Titanium, Ti 0.06

2219 Aluminum Alloy Physical Properties

Properties Metric Imperial
Density 2.84 g/cm3 0.103 lb/in3
Melting Point 543 - 643 °C 1010-1190°F
Specific Heat Capacity 0.864 J/g-°C 0.207 BTU/lb-°F
 

2219 Aluminum Alloy Mechani Mechanical

Properties Metric Imperial
Hardness, Brinell 115 115
Hardness, Knoop 145 145
Hardness, Rockwell A 45.5 45.5
Hardness, Rockwell B 72 72
Hardness, Vickers 130 130
Ultimate Tensile Strength 414 MPa 60000 psi
Tensile Yield Strength 290 MPa 42000 psi
Elongation at Break 10% 10%
Modulus of Elasticity 73.1 GPa 10600 ksi
Poisson's Ratio 0.33 0.33
Fatigue Strength 103 MPa 15000 psi
Shear Modulus 27 GPa 3920 ksi
Shear Strength 255 MPa 37000 psi
     
     
     

2219 Aluminum Alloy Thermal Properties

Properties Metric Imperial
CTE, linear 68°F 22.3 µm/m-°C 12.4 µin/in-°F
CTE, linear 250°C 24.1 µm/m-°C 13.4 µin/in-°F
Specific Heat Capacity 0.864 J/g-°C 0.207 BTU/lb-°F
Thermal Conductivity 120 W/m-K 833 BTU-in/hr-ft²-°F
Solidus 543°C 1010°F
Liquids 643 °C 1190 °F

Detection

Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar

 

Processing

Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
 

Packaging & Shipping

 

Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar
Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar

Company Profile

 

Lork AMS 4031/AMS 4094/AMS 4095/AMS 4096 Aluminum Alloy Rod for Aircraft Parts Aluminum Alloy 2219 Bar

FAQ


Q1: Do you accept the trial order ?
A1: Yes,if we have the exactly size in stock.we can delivery even 1 piece/meter .

Q2: Can I have free sample before making orders?

A2: Yes,we can supply free sample as requirement,but buyer needs to pay the freight charges ,the freight fee will return to buyer after making order.

Q3: How do you control the quality ?
A3: MTC and PMI will be sent before shipment,any 3rd party inspection if need .

Q4: How about your delivery time ?
A4: Generally delivery time is 15 working days .

Q5: How can I quickly get the price list ?
A5: Directly click "chat now" or send us email with detail specifications,you will get the official price list in 1 hour .

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