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Titanium Sheed Plate Foil ASTM B381 ASTM B265 Aerospace Medical
| Place of Origin | CHINA |
|---|---|
| Brand Name | CSTY |
| Certification | GB/T19001-2016/ISO9001:2015 |
| Model Number | ASTM B265、ASTM F136、ASTM F67、AMS4928 |
| Minimum Order Quantity | 50kg |
| Price | $35.00 - $125.00/ kg |
| Packaging Details | wooden case,carton Packaging can be according to customer requirements. |
| Delivery Time | 15~20 work days |
| Payment Terms | L/C, T/T, Western Union, MoneyGram,Paypal |
| Supply Ability | 5000 Kilogram/Kilograms per Month |
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xProduct Details
| Yield Strength | ≥828 MPa | Rolling Process | Hot Rolled, Cold Rolled |
|---|---|---|---|
| Keywords | TC18/BT22 Titanium Alloy Sheets | Titanium Plate Material | Titanium Alloy Plate Grade 7(Pd) |
| Width | 100mm-3000mm | Production Standards | ASTM B265 |
| Surface Process | Acid Wash, Sand Blasting, Polished | Inventory | Various Sizes In Stock |
| Supply Shape | In Coil, In Flat,or Filmed | With | 300-1000mm |
| Materials | Titanium | Surface Treatment | Polished, Anodized, Sandblasted |
| Advantages | High Elongation Rate | Stock | Titanium Gr1/2 Stock |
| Condition | Anneal,cold Rolled | ||
| Highlight | Medical Titanium Sheed Plate Foil,ASTM B265 Titanium Sheed Plate Foil,Aerospace Titanium Sheed Plate Foil |
||
Product Description
Description
AMS 4911 aerospace-grade titanium sheet is a standard specification covering the chemical, mechanical, and metallurgical requirements for titanium and titanium alloy materials used in aerospace and high-performance industries.
It defines the requirements for bars, billets, forgings, rings, and plates, including heat treatment, testing, and inspection procedures.
AMS 4911 titanium plate (commonly Grade 5 / Ti-6Al-4V / UNS R56400) is widely recognized for its:
High strength-to-weight ratio
Excellent corrosion resistance
Non-magnetic properties
Good formability and weldability
Because of these advantages, the AMS 4911 titanium sheet is extensively used across aerospace, automotive, medical, and consumer product applications.
Other Aerospace Standards
AMS 4900
AMS 4901
AMS 4902
AMS 4911
AMS 4914
Specifications
| Parameter | Description |
|---|---|
| Grade | Grade 5 / Ti-6Al-4V / UNS R56400 |
| Application | Aerospace |
| State | Annealed |
| Surface | Pickled |
| Thickness | 0.5–20 mm |
| Length | ≤ 3600 mm |
| Width | ≤ 2000 mm |
| MOQ | 100 kg |
| Bend Test | Meets 105° bend requirement |
Physical Properties
| Grade | Tensile Strength (MPa) | Yield Strength (MPa) | Elongation (%) |
|---|---|---|---|
| Gr1 | 240 | 170 | 24 |
| Gr2 | 345 | 275 | 20 |
| Gr4 | 550 | 483 | 15 |
| Gr5 | 895 | 828 | 10 |
| Gr7 | 400 | 275 | 18 |
| Gr9 | 620 | 483 | 15 |
| Gr12 | 483 | 348 | 18 |
| Gr23 | 793 | 759 | 10 |
Chemical Composition (Wt%)
| Grade | Fe (max) | O (max) | N (max) | C (max) | H (max) | Pd (max) | Al | V | Ni (max) | Mo (max) |
|---|---|---|---|---|---|---|---|---|---|---|
| Gr1 | 0.20 | 0.18 | 0.03 | 0.08 | 0.015 | — | — | — | — | — |
| Gr2 | 0.30 | 0.25 | 0.03 | 0.08 | 0.015 | — | — | — | — | — |
| Gr4 | 0.50 | 0.40 | 0.05 | 0.08 | 0.015 | — | — | — | — | — |
| Gr5 | 0.40 | 0.20 | 0.05 | 0.08 | 0.015 | — | 5.5–6.7 | 3.5–4.5 | — | — |
| Gr7 | 0.30 | 0.25 | 0.03 | 0.08 | 0.015 | 0.12–0.25 | — | — | — | — |
| Gr9 | 0.25 | 0.15 | 0.03 | 0.08 | 0.015 | — | 2.5–3.5 | 2.0–3.0 | — | — |
| Gr12 | 0.30 | 0.25 | 0.03 | 0.08 | 0.015 | — | 0.6–0.9 | 0.2–0.4 | — | — |
| Gr23 | 0.25 | 0.03 | 0.03 | 0.08 | 0.0125 | — | 5.5–6.5 | 3.5–4.5 | — | — |
| Ti | Balance |
Applications
-
Aerospace:
Used in airframes, aircraft engines, landing gear, and airfoils due to high strength and light weight. -
Automotive:
Suitable for wheels, suspension parts, exhaust systems, and performance components. -
Medical:
Ideal for implants, prosthetics, and surgical instruments because of its biocompatibility and corrosion resistance. -
Consumer Products:
Commonly used in eyewear, bicycles, golf clubs, watches, and high-end kitchenware.
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