UNS R56400
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.
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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 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.
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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 % | |
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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.