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MIL-T-9047

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MIL-T-9047 properties and heat treatment forged piece, Including MIL-T-9047 application and specifications, We have all specifications,Including MIL-T-9047 steel plate, MIL-T-9047 sheet, MIL-T-9047 square steel, MIL-T-9047 flat bar,MIL-T-9047 round bar,MIL-T-9047 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-9047 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-9047 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 MIL-T-9047 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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