Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil

Product Details
Customization: Available
Type: Titanium Wire
Application: Industrial, Medical
Manufacturer/Factory, Group Corporation
Diamond Member Since 2024

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  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
  • Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
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  • Overview
  • Product Description
  • Detection
  • Processing
  • Packaging & Shipping
  • Company Profile
  • FAQ
Overview

Basic Info.

Model NO.
6al-2sn-4zr-2mo
Grade
Ti-6al-4V Eli
Shape
Square
Key Words
6al-2sn-4zr-2mo Coil/Strip
Thickness
5mm - 100mm
Width
6mm - 1219mm
Length
as Your Requirments
Surface
Black, Bright, Polished, Pickling
Sample
Free-Sample
MOQ
100kgs
Condition
Annealed;Heat Treatment;
T.S.(≥ MPa)
752
Stock
in Stock
Transport Package
Wooden Package
Specification
6Al-2Sn-4Zr-2Mo
Trademark
LORK
Origin
China
HS Code
7505120000
Production Capacity
50000kg/Month

Product Description

Product Description

 

Introduction

Lork Group specializes in the supply of Grade 23 Ti 6Al 4V ELI alloy raw materials and processing, alloys, stainless steel, metal quality development, welcome your inquiries

Titanium 6Al-2Sn-4Zr-2Mo, also known as 6-2-4-2, is an alpha-beta Titanium. Primarily used for its combination of tensile strength, creep strength, and toughness, Ti 6-2-4-2 has good creep resistance up to 550°C and up to 0.1% Silicon is frequently added to further improve the creep resistance of the alloy. Ti 6-2-4-2 alloy is produced by primary melting under vacuum (VAR), electron beam (EB) melting or plasma arc cold hearth melting (PAM). Primary melting is followed by single or double vacuum arc re-melting (VAR).

The forging and machining characteristics of Ti 6-2-4-2 are similar to those of Ti 6Al-4V and weldability of Ti 6-2-4-2 is fair, using AMS 4952 weld wire. Several different treatments are also available. Ti 6-2-4-2 is capable of being heat-treated to higher strengths in greater section sizes than 6Al-4V. Widely used in forged components, 6-2-4-2 beta forged material has enhanced strength, ductility and a combination of good low-cycle fatigue and fatigue crack growth resistance. This alloy is used in the intermediate compressor stages of turbine engines for disks and blades, seals, and for airframe parts.

Titanium 6Al-2Sn-4Zr-2Mo Alloy Application Industries

  • Compressor blades
  • Turbine engine components
  • Discs
  • Impellers
  • Afterburner structures
  • Airframe skins
  • Seals

6Al-2Sn-4Zr-2Mo Titanium Alloy Chemical Composition

The chemical composition of 6Al-2Sn-4Zr-2Mo alloy is outlined in the following table.

Element Content (%)
Titanium, Ti 88.0
Aluminum, Al 6.0
Tin, Sn 2.0
Zirconium, Zr 4.0
Molybdenum, Mo 2.0
Nitrogen, N ≤ 0.5
Iron,Fe ≤0.25
Oxygen, O ≤ 0.15
Hydrogen, H ≤ 0.15
Carbon, C ≤ 0.1
Silicon, Si ≤ 0.06 - 0.1

6Al-2Sn-4Zr-2Mo Titanium Alloy Mechanical Properties

The following table shows mechanical properties of 6Al-2Sn-4Zr-2Mo alloy.
Properties Metric Imperial
Tensile strength 860 MPa 125000 psi
Yield strength 790 MPa 115000 psi
Poisson's ratio 0.342 0.342
Elastic modulus 113.8 GPa 16510 ksi
Shear modulus 44.0 GPa 6380 ksi
Elongation at break 15% 15%
Hardness, Brinell 326 326
Hardness, Knoop 354 354
Hardness, Rockwell C 35 35
Hardness, Vickers 341 341

6Al-2Sn-4Zr-2Mo Titanium Alloy Physical Properties

The physical properties of 6Al-2Sn-4Zr-2Mo alloy are tabulated below.

Properties Metric Imperial
Density 4.54 g/cm3 0.164 lbs/in3
Melting Point 1588-1716 °C 2890-3120 °F

6Al-2Sn-4Zr-2Mo Titanium Alloy Thermal Properties

The thermal properties of 6Al-2Sn-4Zr-2Mo alloy are tabulated below.

Properties Metric Imperial
Modulus of Elasticity 16.5 x 103 11.4 x 103
Ultimate Tensile Strength 135 930
Yield Strength(0.2% offset) 135 930
Elongation 8% 8%
 

Equivalent materials to 6Al-2Sn-4Zr-2Mo alloy are as follows:

  • AMS 4919
  • AMS 4952
  • AMS 4975
  • AMS 4976
  • DIN 3.7164
  • GE B50 TF22
  • GE B50TF21
  • GE B50TF22
  • GE C50TF7
  • MIL F-83142
  • MIL T-81915
  • MIL T-9046
  • MIL T-9047
  • PWA 1220
  • UNS R54620

Detection

 

Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil

Processing

Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
 

Packaging & Shipping

 

Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil
Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil

Company Profile

 

Lork AMS 4952/Uns R54620/AMS 4976 Titanium 6-2-4-2 Alloy Strip for Airframe Skins 6al-2sn-4zr-2mo Titanium Alloy Coil

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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