UNS R54810 Ti Alloy
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UNS R54810 properties and heat treatment forged piece, Including UNS R54810 application and specifications, We have all specifications，Including UNS R54810 steel plate, UNS R54810 sheet, UNS R54810 square steel, UNS R54810 flat bar,UNS R54810 round bar,UNS R54810 forgings, we can own production and sales.
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Specialized high quality steel
We have the advantages of equipment, technologies and price
forged/hot rolling/ extrusion of steel
We can produce the UNS R54810 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.
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Chemical composition % of the ladle analysis of grade UNS R54810 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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MTA811 / 14136
Machining performance
Download UNS R54810 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.
