OEM 2219 Aluminium Forging Parts for Rocket Liquid Fuel Tank / Vehicle Material

Material

Aluminum Alloy 2219

Process

Forging+CNC+Heat Treatment

Surface Treatment

Transparent / Color Anodized;Hard Anodizing;Powder Coating;
Sandblasting, Laser Carving, Silk Screening;
Nickel-Plated, Chrome, Galvanized, Silver/Gold Plating;
Black Oxide Coating; Polishing; etc...

Manufacture Ability

Depends on The Complexity Of Different Products And Quantities

Experience

Aluminum Machining Service For 12 Years

Packaging

Standard Export Wooden Pallets
Another Request According To Your Need

MOQ

1pcs

Sample

Can be Customized

Mold

Can be Customized

Lead Time

Mold For 15-20 Days

Process For 15-20 Days

OEM

Can be Customized

Chemical Composition of 2219

Alloy

Si

Fe

Cu

Mn

Mg

Zr

Zn

Ti

v

Others

Al

Each

Total

2219

≤0.2

0.3

5.80-6.80

0.20--0.4

≤0.02

0.10--0.25

≤0.1

0.02-0.1

0.05-0.15

0.05

0.15

Rest

Material

Temper

Thickness

Tensile Strength (ksi)

Yield Strength (ksi)

Elongation in 2" (%)

Alloy 2219 (QQ-A-250/30)

0

0.020"-2.00

32 max

16 max

12

Alloy 2219 (QQ-A-250/30)

T351

0.250"-2.00"

46

28

10

Alloy 2219 (QQ-A-250/30)

T851

0.250"-2.00"

62

46

7-8

Material

Temper

Thickness

Tensile Strength (ksi)

Yield Strength (ksi)

Elongation in 2" (%)

Alloy 2219 (AMS 4094)

T81/ T851

0.020"-0.039"

49

37

6

Alloy 2219 (AMS 4094)

T81/ T851

0.039"-0.099"

55

41

7

Alloy 2219 (AMS 4094)

T81/ T851

0.099"-0.249"

58

43

7

Alloy 2219 (AMS 4094)

T81/ T851

0.245"-0.499"

58

42

8

Alloy

Type

Temper

Portrait

Transverse

HBS

Standard

σ_b/MPa

σ_{p 0.2}/MPa

δ/%

σ_b/MPa

σ_{p 0.2}/MPa

δ/%

2219

Die forging

T6

375

255

8

375

255

8

100

GJB 2351

Free forging

355

235

8

355

235

8

100

Die forging

T6

375

255

8

375

255

8

100

HB 5204

Free forging

355

235

8

355

235

8

Alloy

Temper

Available airplane type

Application parts and typical parts

2219

Forgings: T6

MIG, B737-300,A320,Y8,ARJ21,JH7,J10

Rocket fuel tank, engine blade, airtight cockpit, hood, wing integral mailbox, fuselage internal structure, etc.