UNS G93106
UNS G93106 properties and heat treatment forged piece, Including UNS G93106 application and specifications, We have all specifications,Including UNS G93106 steel plate, UNS G93106 sheet, UNS G93106 square steel, UNS G93106 flat bar,UNS G93106 round bar,UNS G93106 forgings, we can own production and sales.
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We can produce the UNS G93106 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 requirement
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Chemical composition % of the ladle analysis of grade UNS G93106 and Standards
Allvac® 9310 UNS G93106, UNS H93100 Specialty steel
Categories: Metal; Ferrous Metal; Alloy Steel; AISI 9000 Series steel; Low Alloy Steel; Carbon Steel; Low Carbon steel
Material Notes: Uses: Automotive applications, structural components, gears, rods, heat-treatable shafts.
Property values are for samples in the metallurgical condition: 1630°F normalized.
Information provided by Allvac, An Allegheny Teledyne Company.
Key Words: AISI 9310; AMS 6260, 6265, 6267. ASTM A 29, A 331, A519, A 646
Physical Properties | Metric | English | Comments |
---|---|---|---|
Density | 7.86 g/cc | 0.284 lb/in³ | |
Mechanical Properties | Metric | English | Comments |
Hardness, Rockwell C | 27.0 | 27.0 | |
Tensile Strength, Ultimate | 907 MPa | 132000 psi | |
Tensile Strength, Yield | 571 MPa @Strain 0.200 % |
82800 psi @Strain 0.200 % |
|
Elongation at Break | 19.0 % | 19.0 % | |
Reduction of Area | 58.0 % | 58.0 % | |
Component Elements Properties | Metric | English | Comments |
Carbon, C | 0.10 % | 0.10 % | |
Chromium, Cr | 1.20 % | 1.20 % | |
Iron, Fe | 94.0 % | 94.0 % | as balance |
Manganese, Mn | 0.55 % | 0.55 % | |
Molybdenum, Mo | 0.12 % | 0.12 % | |
Nickel, Ni | 3.33 % | 3.33 % | |
Phosphorous, P | 0.010 % | 0.010 % | |
Silicon, Si | 0.25 % | 0.25 % | |
Sulfur, S | 0.010 % | 0.010 % |
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Machining performance
Download UNS G93106 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.