India's Largest Stockist and Supplier Of Nickel Alloys Since 2007

Mar M246

Mar M246 Overview
Category High alloy steel
Class High temperature corrosion Alloy steel
Type Austenitic standard
Common Names Chromium-Manganese-MAR-M 246
Density 8.5 g/cm³
Standard AMS
Specific Heat ~430-500 J/kg·K
Service Temperature up to ~1000-1050 °C
Heat Treatment
  • Normalizing, Quenching
  • Annealing, Tempering

Get Mar M246 Material as per Standards Click Here

 

Mar M246 Specification

 

Table of Content

MAR M 246 Superalloys Supplier in India in Various Forms At Best Price

Alloy Mar M246 MAR-M 246 Forms
Product type Products Dimension Processes
Steel Bar Round Bar, Flat Bar, Square Bar Φ8-1200mm*L Forging, hot rolling and cold rolling, Cast
Plates / Sheets Plates / Sheets 0.08-200mm(T)*W*L Forging, hot rolling and cold rolling
Coil / Strip Steel Coil /Steel Strip 0.03-16.0x1200mm Cold-Rolled & Hot-Rolled
Pipes / Tubes Seamless Pipes/Tubes, Welded Pipes/Tubes OD:6-219mm x WT:0.5-20.0mm Hot extrusion, Cold Drawn, Welded
Mar M246 Material Equivalent Grade
ASTM GB
Mar-M246 K246
MAR-M 246 Superalloys Conditions & Properties
  • +AC Annealed to achieve spheroidization of the carbides
  • +QT Quenched and tempered
  • +WW Warm worked
  • +N Normalized
  • +NT Normalized and tempered
  • +AT Solution annealed
  • +C Cold drawn / Hard
  • +CR Cold rolled
  • +PE Peeled
  • +T Tempered
  • +A Soft annealed

Offer Excellent Strength Mar M246 Alloy Which is Used as Cast Steel in Turbine Blades

Mar M246 Alloy Applications
Mar M246 Alloy Applications

 

Deliver Status of GB MAR M 246 Superalloys
Product type Deliver Status
Plates / Sheets Annealed, Solution and Aging, Q+T, ACID-WASHED, Shot Blasting
Steel Bar Black, Rough Turning, Shot Blasting,
Coil / Strip Annealed, Solution and Aging, Q+T, ACID-WASHED, Shot Blasting
Pipes / Tubes Annealed, Solution and Aging, Q+T, ACID-WASHED

Stockist Of Nickel Cobalt Based Mar M246 Material in Mumbai , Refer Chemical Composition

Nickel Cobalt Based Mar M246 Material Chemical Composition
Elements Min.(≥) Max.(≤)
Cr 8.00 10.00
Ni - Bal
Mo 2.25 2.75
Co 9.00 11.00
W 9.00 11.00
C 0.13 0.17
Fe - 1.00
Ta 1.25 1.75
Zr 0.03 0.08
B 0.010 0.020
Si - 0.20
Mn - 0.20
S - 0.015
Al 5.25 5.75
Cu - 0.10
Ti 1.25 1.75
Solution and Aging of MAR-M246 Nickel-Based Superalloy
Conditions Value
Solution Temperatures 1200 °C and 1250 °C
Solution Time 330 min
Aging Temperatures 780 °C, 880 °C, 980 °C
Aging Times 5 h, 20 h, 80 h
Software Used JMatPro (Ni database) for γ′ solvus, solidus, liquidus calculations
Characterization Techniques SEM/EDS and SEM-FEG
Microstructure at 1250 °C Solutioning Homogeneous γ matrix; carbides and uniformly distributed cubic γ′ precipitates
γ′ Size After Aging at 780 °C & 880 °C (5-80 h) No significant change compared to solution-treated sample
γ′ Size After Aging at 980 °C Significant increase in γ′ particle size, especially after 80 h
Check Corrosion Resistance GB MAR M 246 Cast Steel Density and Mechanical Properties
MAR M 246 Cast Steel Mechanical Properties
Tensile strength Rm (MPa) Proof strength Rp0.2 (MPa) Impact energy KV (J) Reduction in cross section on fracture Z (%) Elongation at fracture A (%) As-Heat-Treated Condition Brinell hardness (HBW)
435 (≥) 878 (≥) 43 12 13 Solution and Aging, Annealing, Ausaging, Q+T,etc 322
Stress Rupure Property of Alloy Mar M246
Condition Stress Rupure Property
Cast Temperature ºC Stress N/mm2 A % Life hr
871±2 414 >4 >24
-
GB MAR M 246 Superalloys Heat Treatment
Normalizing Quenching Annealing Tempering Q & T
MAR-M 246 High Temperature Steel Advantanges
  • Excellent High-Temperature Strength
  • Superior Creep Resistance
  • Outstanding Oxidation and Corrosion Resistance
  • Good Thermal Fatigue Resistance
  • High Microstructural Stability

 

Find Solution Treated At MAR-M 246 High Temperature Steel Suitable to Work At Temperature 885°C, Refer Physical Propeties
Physical Properties of of Grade MAR-M 246
Property Density kg/dm3 Temperature T °C/F Specific heat J / kgK Thermal conductivity W/mK Modulus of elasticity kN/mm2 Expansion rate Electric resistance µΩ·cm Temp. °C/°F Creep strain limit (10000h) (Rp1,0) N/mm2 Creep rupture strength (10000h) (Rp1,0) N/mm2
182 (≥) 488 (≥) 12 21 14 341 341 Solution and Aging, Annealing, Ausaging, Q+T,etc 644 357 944
Thermal Properties of High Alloy Mar M246
Properties  Conditions
T (°C) Treatment
Thermal Expansion (10-6/ºC) 17.5 0-100 more  -
Thermal Conductivity (W/m-K) 16.2 100 more  -
Specific Heat (J/kg-K) 500 0-100   -
Grade MAR M 246 Electric Properties
Properties  Conditions
T (°C) Treatment
Electric Resistivity (10-9W-m) 690 25   -
High Alloy Mar M246 Temprature Range
Services Temperature Range (°C)
Operating Temperature 850 - 980 °C
Maximum Service Temperature ~1000 - 1050 °C
Solution Heat Treatment Temperature 1200 - 1250 °C
Aging Temperature (Low) 750 - 820 °C
Aging Temperature (Standard) 850 - 900 °C
Aging Temperature (High) 950 - 1000 °C
Aluminide Coating on Mar-M246 Nickel Superalloy
Coating Temperature (°C) Coating Time (hours) Coating Thickness (μm) Weight Gain (%) Coating
Layer Major phase
700 9 91.36 ± 1.35 5.05 Outer Ni2Al3 + NiAl3
Inner Ni2Al3
800 9 142.0 ± 4.17 8.24 Outer Ni2Al3 + NiAl3
Inner Ni2Al3
900 9 192.7 ± 1.29 10.59 Unique Ni2Al3
1000 9 299.9 ± 1.24 13.31 Ni2Al3

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