| MOQ: | 1PCS |
| Price: | Negotiations |
| Standard Packaging: | wooden pallet |
| Delivery Period: | 10~20days |
| Payment Method: | T/T, L/C |
| Supply Capacity: | 10000 pcs /per month |
| Material | Aluminum Alloy 2219 |
| Process | Forging + CNC + Heat Treatment |
| Surface Treatment |
|
| Manufacture Ability | Depends on The Complexity Of Different Products And Quantities |
| Experience | Aluminum Machining Service For 12 Years |
| Packaging | Standard Export Wooden Pallets Custom packaging available upon request |
| MOQ | 1 piece |
| Sample | Customizable |
| Mold | Customizable |
| Lead Time | Mold: 15-20 Days Process: 15-20 Days |
| OEM | Customizable |
| Alloy | Si | Fe | Cu | Mn | Mg | Zr | Zn | Ti | V | Others Each | Others Total | Al |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 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 σb/MPa | Portrait σp 0.2/MPa | Portrait δ/% | Transverse σb/MPa | Transverse σp 0.2/MPa | Transverse δ/% | HBS | Standard |
|---|---|---|---|---|---|---|---|---|---|---|
| 2219 | Die forging | T6 | 375 | 255 | 8 | 375 | 255 | 8 | 100 | GJB 2351 |
| Free forging | 355 | 235 | 8 | 355 | 235 | 8 | 100 | |||
| 2219 | 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. |
| MOQ: | 1PCS |
| Price: | Negotiations |
| Standard Packaging: | wooden pallet |
| Delivery Period: | 10~20days |
| Payment Method: | T/T, L/C |
| Supply Capacity: | 10000 pcs /per month |
| Material | Aluminum Alloy 2219 |
| Process | Forging + CNC + Heat Treatment |
| Surface Treatment |
|
| Manufacture Ability | Depends on The Complexity Of Different Products And Quantities |
| Experience | Aluminum Machining Service For 12 Years |
| Packaging | Standard Export Wooden Pallets Custom packaging available upon request |
| MOQ | 1 piece |
| Sample | Customizable |
| Mold | Customizable |
| Lead Time | Mold: 15-20 Days Process: 15-20 Days |
| OEM | Customizable |
| Alloy | Si | Fe | Cu | Mn | Mg | Zr | Zn | Ti | V | Others Each | Others Total | Al |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 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 σb/MPa | Portrait σp 0.2/MPa | Portrait δ/% | Transverse σb/MPa | Transverse σp 0.2/MPa | Transverse δ/% | HBS | Standard |
|---|---|---|---|---|---|---|---|---|---|---|
| 2219 | Die forging | T6 | 375 | 255 | 8 | 375 | 255 | 8 | 100 | GJB 2351 |
| Free forging | 355 | 235 | 8 | 355 | 235 | 8 | 100 | |||
| 2219 | 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. |