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UNS R56400 Ti Alloy

Description

UNS R56400 Ti Alloy Ti Alloy and Mechanical Properties, Chemical Element, Cross Reference, Datasheet.

Datasheet for: Steel Grades:Ti Alloy: UNS R56400 Ti Alloy

Chemical composition(mass fraction)(wt.%) of the UNS R56400 Ti Alloy

 

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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:
Titanium Ti-6Al-4V (Grade 5), Annealed
Titanium Ti-6Al-4V (Grade 5), STA
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.





Hot tags:UNS R56400 steel plate, UNS R56400 sheet, UNS R56400 square steel, UNS R56400 flat bar,UNS R56400 round bar,UNS R56400 forgings

 
 

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Mechanical Properties of steel grade UNS R56400 Ti Alloy

Yield
Rp0.2 (MPa)
Tensile
Rm (MPa)
Impact
KV/Ku (J)
Elongation
A (%)
Reduction in cross section on fracture
Z (%)
As-Heat-Treated Condition Brinell hardness (HBW)
772 (≥) 698 (≥) 31 34 44 Solution and Aging, Annealing, Ausaging, Q+T,etc 212

Physical Properties of steel grade UNS R56400 Ti Alloy

Temperature
(°C)
Modulus of elasticity
(GPa)
Mean coefficient of thermal expansion 10-6/(°C) between 20(°C) and Thermal conductivity
(W/m·°C)
Specific thermal capacity
(J/kg·°C)
Specific electrical resistivity
(Ω mm²/m)
Density
(kg/dm³)
Poisson’s coefficient, ν
12 - -     0.23 -  
824 623 - 21.3 412   -  
933 - 23 42.2   142 232

Heat Treatment of steel grade UNS R56400 Ti Alloy

Heat treated : 1112°C - 1315°C

Technological Curves of steel grade UNS R56400 Ti Alloy

Cross Reference Table (Equivalent Grade) of UNS R56400 Ti Alloy

Grade Standard Country Application
UNS G10300 UNS USA General use carbon steel bar
UNS G10050 UNS USA General use carbon steel bar
UNS G10060 UNS USA General use carbon steel bar
UNS G10080 UNS USA General use carbon steel bar
UNS G10110 UNS USA General use carbon steel bar
ASTM 1012 ASTM USA General use carbon steel bar
UNS G10120 UNS USA General use carbon steel bar
UNS G10130 UNS USA General use carbon steel bar
UNS G10150 UNS USA General use carbon steel bar
UNS G10160 UNS USA General use carbon steel bar
UNS G10170 UNS USA General use carbon steel bar
UNS G10180 UNS USA General use carbon steel bar
UNS G10190 UNS USA General use carbon steel bar
UNS G10200 UNS USA General use carbon steel bar
UNS G10210 UNS USA General use carbon steel bar
UNS T72301 UNS USA Carbon tool steel
W2-A ASTM USA Carbon tool steel
UNS T72302 UNS USA Carbon tool steel
UNS S42800 UNS USA Martensitic special steel
UNS S43100 UNS USA Martensitic special steel

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