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MIL-T-9046 Ti Alloy

Data Table for: Steel Grades : Ti Alloy : MIL-T-9046 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 MIL-T-9046 Ti Alloy specifications and size

  • Steel grade
  • Specification
  • Processing range(mm)
  • MIL-T-9046 Ti Alloy
  • MIL-T-9046 Ti Alloy
  • MIL-T-9046 Ti Alloy
  • MIL-T-9046 Ti Alloy
  • MIL-T-9046 Ti Alloy
  • MIL-T-9046 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 AlloyMIL-T-9046 plate,MIL-T-9046 Round Bar,MIL-T-9046 forgings,MIL-T-9046 suppliers, MIL-T-9046 Stock,MIL-T-9046 sheet, MIL-T-9046 flat bar, MIL-T-9046 pipe,MIL-T-9046 tube,MIL-T-9046 mould,MIL-T-9046 round ingot,MIL-T-9046 cold-rolled steel,MIL-T-9046 coil,MIL-T-9046 strap steel,MIL-T-9046 hot-rolled steel,MIL-T-9046 medium plate, MIL-T-9046 heavy plate,MIL-T-9046 shapped bar,MIL-T-9046 hexahedral bar,MIL-T-9046,MIL-T-9046 slab ingot,MIL-T-9046 slab,MIL-T-9046 price,MIL-T-9046 square bar,MIL-T-9046 square steel,MIL-T-9046 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 MIL-T-9046.

 

MIL-T-9046 Ti Alloy

Our advantages

MIL-T-9046 properties and heat treatment forged piece, Including MIL-T-9046 application and specifications, We have all specifications,Including MIL-T-9046 steel plate, MIL-T-9046 sheet, MIL-T-9046 square steel, MIL-T-9046 flat bar,MIL-T-9046 round bar,MIL-T-9046 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 MIL-T-9046 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 MIL-T-9046 and Standards

 

Allvac® 40, Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Categories: Metal; Nonferrous Metal; Titanium Alloy; Unalloyed/Modified Titanium
Material Notes: Data provided by Allvac.
Applications: Airframe components, cryogenic vessels, heat exchangers, CPI equipment, condenser tubing, pickling baskets.

 

Key Words: UNS R50400; AMS 4902, 4921, 4942; MIL-T-9046, -81556. ASTM F 67, Titanium Grade 2; ASTM B 265, 337, 338, 348; Allvac, an Allegheny Teledyne Company

 

 

Physical Properties Metric English Comments
Density 4.51 g/cc 0.163 lb/in³
 
Mechanical Properties Metric English Comments
Hardness, Rockwell B 80 80
Tensile Strength, Ultimate 345 MPa 50000 psi
Tensile Strength, Yield 276 MPa
@Strain 0.200 %
40000 psi
@Strain 0.200 %
Elongation at Break 20.0 % 20.0 %
Reduction of Area 30.0 % 30.0 %
 
Component Elements Properties Metric English Comments
Carbon, C <= 0.10 % <= 0.10 %
Hydrogen, H <= 0.015 % <= 0.015 %
Iron, Fe <= 0.30 % <= 0.30 %
Nitrogen, N <= 0.030 % <= 0.030 %
Oxygen, O <= 0.25 % <= 0.25 %
Titanium, Ti 99.0 % 99.0 % as balance

 

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Allvac® 30, Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
Allvac® 70, Titanium Alloy, Heat Treatment: 704°C (1300°F) Anneal
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Titanium Grade 2, Annealed
Allegheny Ludlum Grade 2 Titanium (UNS R50400)

NALL41 / 14791




Machining performance

Download MIL-T-9046 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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