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Ti8Al1Mo1V

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Ti8Al1Mo1V properties and heat treatment forged piece, Including Ti8Al1Mo1V application and specifications, We have all specifications,Including Ti8Al1Mo1V steel plate, Ti8Al1Mo1V sheet, Ti8Al1Mo1V square steel, Ti8Al1Mo1V flat bar,Ti8Al1Mo1V round bar,Ti8Al1Mo1V 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 Ti8Al1Mo1V 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 Ti8Al1Mo1V and Standards

Titanium Ti-8Al-1Mo-1V (Ti-8-1-1), Beta Annealed, Aged
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Near Alpha Titanium Alloy

Material Notes: Information provided by Allvac and the references. Annealed at 1065ºC, Aged at 595ºC.

Applications: Fan & compressor blades, discs, spacers, seals, rings. Excellent creep resistance.

5 other heat treatments of this alloy are in MatWeb.

Key Words: Ti8Al1Mo1V, UNS R54810; Ti-811

Physical Properties Metric English Comments
Density  4.37 g/cc 0.158 lb/in³
 
Mechanical Properties Metric English Comments
Tensile Strength, Ultimate  1020 MPa 148000 psi
Tensile Strength, Yield  900 MPa 131000 psi
Elongation at Break  13.0 % 13.0 %
Modulus of Elasticity  120 GPa 17400 ksi unspecified heat treatment
Poissons Ratio  0.320 0.320 duplex annealed
Shear Modulus  46.0 GPa 6670 ksi
 
Electrical Properties Metric English Comments
Electrical Resistivity  0.000197 ohm-cm 0.000197 ohm-cm
 
Thermal Properties Metric English Comments
CTE, linear  8.50 µm/m-°C
@Temperature 20.0 °C
4.72 µin/in-°F
@Temperature 68.0 °F
  9.20 µm/m-°C
@Temperature 250 °C
5.11 µin/in-°F
@Temperature 482 °F
  10.1 µm/m-°C
@Temperature 500 °C
5.61 µin/in-°F
@Temperature 932 °F
Specific Heat Capacity  0.502 J/g-°C 0.120 BTU/lb-°F
Thermal Conductivity  6.00 W/m-K 41.6 BTU-in/hr-ft²-°F
Melting Point  <= 1540 °C <= 2800 °F Liquidus
Liquidus  1540 °C 2800 °F
Beta Transus  1040 °C 1900 °F
 
Component Elements Properties Metric English Comments
Aluminum, Al  7.35 - 8.35 % 7.35 - 8.35 %
Carbon, C  <= 0.0800 % <= 0.0800 %
Hydrogen, H  <= 0.0150 % <= 0.0150 %
Iron, Fe  <= 0.300 % <= 0.300 %
Molybdenum, Mo  0.750 - 1.25 % 0.750 - 1.25 %
Nitrogen, N  <= 0.0500 % <= 0.0500 %
Other, each  <= 0.100 % <= 0.100 %
Other, total  <= 0.400 % <= 0.400 %
Oxygen, O  <= 0.120 % <= 0.120 %
Titanium, Ti  88.185 - 91.15 % 88.185 - 91.15 % As Balance; Elemental Compostions per ASTM B265
Vanadium, V  0.750 - 1.25 % 0.750 - 1.25 %

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Titanium Ti-8Al-1Mo-1V (Ti-8-1-1)
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Titanium Ti-6Al-4V (Grade 5), Annealed

MTA811 / 14136




Machining performance

Download Ti8Al1Mo1V 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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