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UNS R56400 Ti Alloy

Data Table for: Steel Grades : Ti Alloy : UNS R56400 Ti Alloy

Chemical composition(mass fraction)(wt.%)

Mechanical Properties

  • Quantity
  • Value
  • Unit
  • Young's modulus
  • Tensile strength
  • Elongation
  • Fatigue
  • Yield strength
  • 200000 - 200000
  • 650 - 880
  • 8 - 25
  • 275 - 275
  • 350 - 550
  • MPa
  • MPa
  • %
  • MPa
  • MPa

Physical Properties

  • Quantity
  • Value
  • Unit
  • Thermal expansion
  • Thermal conductivity
  • Specific heat
  • Melting temperature
  • Density
  • Resistivity
  • 10 - 10
  • 25 - 25
  • 460 - 460
  • 1450 - 1510
  • 7700 - 7700
  • 0.55 - 0.55
  • e-6/K
  • W/m.K
  • J/kg.K
  • °C
  • kg/m3
  • Ohm.mm2/m

Heat Treatment:

Annealing

Quenching

Tempering

Normalizing

Q & T

Can produce UNS R56400 Ti Alloy specifications and size

  • Steel grade
  • Specification
  • Processing range(mm)
  • UNS R56400 Ti Alloy
  • UNS R56400 Ti Alloy
  • UNS R56400 Ti Alloy
  • UNS R56400 Ti Alloy
  • UNS R56400 Ti Alloy
  • UNS R56400 Ti Alloy
  • Φ1 to Φ2000
  • 10 to 1000
  • 0.08 to 800(T)*10 to 1500(W)*Long
  • Pipe/tube/slugs/donuts/cubes/other shapes
  • OD: Φ4-410; WT: 1-35 mm
  • THK:0.1mm Width:1500mm

Description

 

Our to produce better steel-based products are the main used in industrial manufacturing various types Ti AlloyUNS R56400 plate,UNS R56400 Round Bar,UNS R56400 forgings,UNS R56400 suppliers, UNS R56400 Stock,UNS R56400 sheet, UNS R56400 flat bar, UNS R56400 pipe,UNS R56400 tube,UNS R56400 mould,UNS R56400 round ingot,UNS R56400 cold-rolled steel,UNS R56400 coil,UNS R56400 strap steel,UNS R56400 hot-rolled steel,UNS R56400 medium plate, UNS R56400 heavy plate,UNS R56400 shapped bar,UNS R56400 hexahedral bar,UNS R56400,UNS R56400 slab ingot,UNS R56400 slab,UNS R56400 price,UNS R56400 square bar,UNS R56400 square steel,UNS R56400 wire.Extending the industrial all kinds of mechanical industrial parts machining and, at the same time, using fine heat treatment process,tempering,hardening,heating,bright annealing,rotary hearth.chemical composition and Improving mechanical properties of UNS R56400.

 

UNS R56400 Ti Alloy

Our advantages

UNS R56400 properties and heat treatment forged piece, Including UNS R56400 application and specifications, We have all specifications,Including UNS R56400 steel plate, UNS R56400 sheet, UNS R56400 square steel, UNS R56400 flat bar,UNS R56400 round bar,UNS R56400 forgings, we can own production and sales.


Introduction to Our Products:

Specialized high quality steel

We have the advantages of equipment, technologies and price

forged/hot rolling/ extrusion of steel


We can produce the UNS R56400 has the following specifications:

Round bar steel: 1mm to 3000mm

Square-shape steel: 1mm to 2000mm

Plate steel:0.1mm to 2500mm

Width: 10mm to 2500mm

Lenth: We can supply any lenth based on the customer's requirement.

Forging: Shafts with flanks/pipes/tubes/slugs/donuts/cubes/other shapes

Tubings: OD: φ6-219 mm, with wall thickness ranging from 1-35 mm.

Finished goods condition: hot forging/hot rolling + annealing/normalizing + tempering/quenching + tempering/any conditions based on the customer's requirement

Surface conditions: scaled (hot working finish)/ground/rough machining/fine machining/based on the customer's requirement

Furnaces for metallurgical processing: electrode arc + LF/VD/VOD/ESR/Vacuum consumable electrode.

Ultrasonic inspection: 100% ultrasonic inspection for any inperfections or based on the customer's requirementExcellent service for all kinds of industries,with advantages of technologies, equipment and price.

We serve you with our honesty, integrity, and professionality.


Chemical composition % of the ladle analysis of grade UNS R56400 and Standards

 

Allvac® 6-4 Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy
Material Notes: Data provided by Allvac.
Applications: Blades, discs, rings, airframe, fasteners, components. Vessels, cases, hubs, forgings. Standard, rotor/premium grades.

 

Key Words: UNS R56400; AMS 4906, 4920, 4928, 4965, 4967; MIL-T-9047, -81556, Ti-6Al-4V; Ti-6-4; ASTM B 348, B 381, F 1472; Allvac, an Allegheny Teledyne Company

 

 

Physical Properties Metric English Comments
Density 4.43 g/cc 0.160 lb/in³
 
Mechanical Properties Metric English Comments
Hardness, Brinell 304 304 Estimated from Rockwell C value for Brinell test with 3000 kg load/10 mm diameter ball
Hardness, Knoop 330 330 Estimated from Rockwell C value.
Hardness, Rockwell C 32 32
Hardness, Vickers 318 318 Estimated from Rockwell C value.
Tensile Strength, Ultimate 931 MPa 135000 psi
Tensile Strength, Yield 862 MPa
@Strain 0.200 %
125000 psi
@Strain 0.200 %
Elongation at Break 15.0 % 15.0 %
Reduction of Area 30.0 % 30.0 %
 
Component Elements Properties Metric English Comments
Aluminum, Al 6.0 % 6.0 %
Carbon, C <= 0.10 % <= 0.10 %
Hydrogen, H <= 0.015 % <= 0.015 %
Iron, Fe 0.20 % 0.20 %
Nitrogen, N 0.030 % 0.030 %
Oxygen, O <= 0.20 % <= 0.20 %
Titanium, Ti 89.0 % 89.0 % as balance
Vanadium, V 4.0 % 4.0 %

 

Users viewing this material also viewed the following:
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Allvac® 6-4ELI Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Titanium Ti-6Al-4V (Grade 5), Annealed Bar
Titanium Ti-6Al-4V (Grade 5), STA Bar

NALL45 / 14795




Machining performance

Download UNS R56400 the mechanical properties of the report, the report provides detailed performance analysis and application. Download >>


Principal Design Features

One of the most widely used precipitation hardening grades in the business. While soft and ductile in the solution annealed condition, it is capable of high properties with a single precipitation or aging treatment. Characterized by good corrosion resistance, high harness, toughness and strength.


Machinability

Long, gummy chips characterize this alloys machinability. It can be machined in the annealed condition, however condition H1150M will yield best results. Post machining solution treatment of parts will be required prior to final hardening if machining in this condition.


Heat Treatment

CONDITION A--Soak at 1900 F (1038 C) for 30 minutes and cool below 60 F (16 C) for complete martensite transformation. CONDITION H 950- Treat Condition A material at 900 F(482 C) for 1 hour, air cool.. CONDITION H925, H1025, H1075, H1100, H1150- Soak solution treated material for 4 hours at specified temperature, air cool, CONDITION H1150M- Soak solution treated material at 1400 F (760 C) for 2 hours, air cool, then re-heat to 1150 F (620 C) for 4 hours and air cool.


Welding

Successfully welded by common fusion and resistance methods, this alloy should not be joined by oxyacetylene welding. AWS E/ER630 filler metal is recommended if required.


Forging

Soak for 1 hour at 2150 F (1177 C) prior to forging. Do not work below 1850 F (1010 C). Post-work solution treatment is required prior to final hardening.





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