Titanium Alloy Shell Gr5 Welded Shell For Torpedo Aerospace Chemical Industry

Place of Origin China
Brand Name Changsheng
Certification ISO 9001;2015
Model Number ASTM
Minimum Order Quantity 50kg
Price $15.00 - $30.00/ kg
Packaging Details wooden case,carton Packaging can be according to customer requirements.
Delivery Time 15~20 work days
Payment Terms L/C, D/A, D/P, T/T, Western Union, MoneyGram
Supply Ability 5000 Kilogram/Kilograms per Month

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Product Details
Materials Titanium Alloy Application Marine,Aerospace And Defensing
Standard AMS 4911/AMS 4900/AMS 4901/AMS 4902/AMS 4914 Processing CNC, Forge, Rolling And Welded
Origin Baoji City, China Other Grade Titanium Gr5/TA10
Stock Titanium Gr1/2 Stock Hardness Generally In The Range Of 32-38 HRC
Yield Strength 800 MPa Others Mateiral Titanium
Lengh 2000-6000mm Key Word Ti 6Al4V Alloy Titanium Plates
Surface Process Polished, Anodized, Sandblasted Techique Cold Rolled
Length 100mm - 6000mm Techinique Cold Rolling Or Hot Rolling
Feature High Elongation Rate Technique Cold Rolled
Thickness 0.1mm - 10mm
Highlight

Marine Titanium Alloy Sheet Shell

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Defending Titanium Alloy Sheet

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AMS 4911 Titanium Alloy Plate

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Product Description

Description

 

Titanium exhibits exceptional resistance to acid and alkali corrosion. When immersed in seawater for five years, it shows no signs of rusting — unlike steel, which corrodes and deteriorates rapidly in the same environment. This outstanding corrosion resistance makes titanium alloys ideal for marine applications such as ship hulls and submarine shells.

Titanium submarines offer several advantages:

Superior corrosion resistance: Seawater does not corrode titanium, ensuring long service life.

High-pressure resistance: Titanium submarines can dive 80% deeper than stainless-steel submarines without structural failure.

Non-magnetic properties: Titanium’s non-magnetic nature makes submarines less detectable by magnetic mines, enhancing stealth capabilities.

Deep-diving capability: While steel submarines risk collapse beyond 300 m depth, titanium submarines can safely operate below 300 m and withstand depth charges effectively.

Since the 1960s, titanium has become an irreplaceable material in deep-sea shipbuilding. Russia successfully built the world’s first all-titanium submarine in 1968 and later developed several “Alpha”-class submarines, each using approximately 3,000 t of titanium. Other models, such as the “Shark”-class nuclear submarine and the multipurpose 945 and 988 classes, also feature titanium alloy pressure-resistant hulls, enabling speeds and depths up to 800 m.

Titanium alloys are also widely used in:

 

Torpedo launch systems and high-pressure gas cylinders

Pumps, valves, pipelines, and propellers

Coolers and structural submarine components

These applications greatly enhance reliability and extend service life in harsh marine environments.

Common Titanium Alloy Grades

Grade Features and Applications
Ti-6Al-4V Heat-treatable alloy with excellent strength, weldability, and formability. Used for jet engine compressor blades, impellers, landing gear, fasteners, and structural components.
Ti-5Al-2.5Sn Non-heat-treatable alloy with good crack resistance and weldability. Used for gearboxes, casings, guide vanes, and pipelines.
Ti-8Al-1Mo-1V Non-heat-treatable alloy with good weldability and acceptable forgeability. Used for engine blades, impellers, and airframe structures.
Ti-6Al-6V-2Sn Heat-treatable alloy with excellent forgeability and strength, but poor weldability. Used for fasteners, air inlet control guides, and test components.
Ti-13V-11Cr-3Al Heat-treatable alloy with good formability and weldability. Used in forgings, airframe structures, skins, and fasteners.
Ti-2.25Al-11Sn-5Zr-1Mo-0.2Si Heat-treatable alloy with good crack resistance during forging. Used for high-strength structural parts.
Ti-6Al-2Sn-4Zr-2Mo Non-heat-treatable alloy with good forgeability and weldability. Used in compressor blades, impellers, and structural assemblies.
Ti-4Al-3Mo-1V Heat-treatable alloy with good forgeability and formability. Used for airframe structural components.

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 Mo Others
Gr1 0.20 0.18 0.03 0.08 0.015 Ti balance
Gr2 0.30 0.25 0.03 0.08 0.015 Ti balance
Gr4 0.50 0.40 0.05 0.08 0.015 Ti balance
Gr5 0.40 0.20 0.05 0.08 0.015 5.5–6.7 3.5–4.5 Ti balance
Gr7 0.30 0.25 0.03 0.08 0.015 0.12–0.25 Ti balance
Gr9 0.25 0.15 0.03 0.08 0.015 2.5–3.5 2.0–3.0 Ti balance
Gr12 0.30 0.25 0.03 0.08 0.015 0.6–0.9 0.2–0.4 Ti balance
Gr23 0.25 0.03 0.03 0.08 0.0125 5.5–6.5 3.5–4.5 Ti balance

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