MIL-T-9046 Ti Alloy Chemical composition and Mechanical properties
MIL-T-9046 Ti Alloy
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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.
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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.
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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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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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