UNS G51500
UNS G51500 properties and heat treatment forged piece, Including UNS G51500 application and specifications, We have all specifications，Including UNS G51500 steel plate, UNS G51500 sheet, UNS G51500 square steel, UNS G51500 flat bar,UNS G51500 round bar,UNS G51500 forgings, we can own production and sales.
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We can produce the UNS G51500 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 UNS G51500 and Standards
AISI 6150 steel, annealed, 25 mm (1 in.) round
Categories: Metal; Ferrous Metal; Alloy Steel; AISI 6000 Series steel; Low Alloy Steel; Carbon Steel; Medium Carbon steel
Material Notes: Annealed 815°C, furnace cooled 11°C per hour to 670°C, air cooled, 25 mm round.
Applications: Automotive leaf springs; also valve springs, piston rods, pump parts, and spline shafts. AISI 6150 and 6150H are directly hardenable to a medium level of hardness.
Key Words: AFNOR 50 CV 4 (Fr), UNI 50 CrV 4, JIS SUP 10, SS14 2230 (Sweden), B.S. 735 A 50, B.S. En. 47, ASTM A505, MIL-SPEC MIL-S-8503, SAE J404, SAE J412, SAE J770, DIN 1.8159, UNS G51500, AMS 6448, AMS 6450, AMS 7301, ASTM A231, ASTM A322, ASTM A331
| Physical Properties | Metric | English | Comments |
|---|---|---|---|
| Density | 7.85 g/cc | 0.284 lb/in³ | |
| Mechanical Properties | Metric | English | Comments |
| Hardness, Brinell | 197 | 197 | |
| Hardness, Knoop | 219 | 219 | Converted from Brinell hardness. |
| Hardness, Rockwell B | 92 | 92 | Converted from Brinell hardness. |
| Hardness, Rockwell C | 13.0 | 13.0 | Converted from Brinell hardness. Value below normal HRC range, for comparison purposes only. |
| Hardness, Vickers | 207 | 207 | Converted from Brinell hardness. |
| Tensile Strength, Ultimate | 670 MPa | 97200 psi | |
| Tensile Strength, Yield | 415 MPa | 60200 psi | |
| Elongation at Break | 23.0 % | 23.0 % | in 50 mm |
| Modulus of Elasticity | 205 GPa | 29700 ksi | Typical for steel |
| Bulk Modulus | 140 GPa | 20300 ksi | Typical for steel |
| Poissons Ratio | 0.290 | 0.290 | Calculated |
| Izod Impact | 27.0 J | 19.9 ft-lb | |
| Machinability | 55 % | 55 % | annealed and cold drawn. Based on 100% machinability for AISI 1212 steel. |
| Shear Modulus | 80.0 GPa | 11600 ksi | Typical for steel |
| Electrical Properties | Metric | English | Comments |
| Electrical Resistivity | 0.0000234 ohm-cm | 0.0000234 ohm-cm | Typical steel |
| Thermal Properties | Metric | English | Comments |
| Specific Heat Capacity | 0.475 J/g-°C | 0.114 BTU/lb-°F | Typical steel |
| Thermal Conductivity | 46.6 W/m-K | 323 BTU-in/hr-ft²-°F | Typical steel |
| Component Elements Properties | Metric | English | Comments |
| Carbon, C | 0.480 - 0.530 % | 0.480 - 0.530 % | |
| Chromium, Cr | 0.800 - 1.10 % | 0.800 - 1.10 % | |
| Iron, Fe | 97.095 - 97.72 % | 97.095 - 97.72 % | As remainder |
| Manganese, Mn | 0.700 - 0.900 % | 0.700 - 0.900 % | |
| Phosphorous, P | <= 0.0350 % | <= 0.0350 % | |
| Silicon, Si | 0.150 - 0.300 % | 0.150 - 0.300 % | |
| Sulfur, S | <= 0.0400 % | <= 0.0400 % | |
| Vanadium, V | >= 0.150 % | >= 0.150 % | |
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M615AA / 8223
Machining performance
Download UNS G51500 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.