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FSX 414

FSX 414 Alloy High Lights
Category High alloy steel
Class High temperature corrosion Alloy steel
Type Austenitic standard
Common Names Chromium-Manganese-FSX-414
Designations Execution standard: ASTM, UNS, AISI, DIN, EN, DIN, SEW, ISO, JIS, NF, BS, GB
Heat treated 1956°C - 1484°C.
Specific Heat 390-430 J/kg·K
Oxidation Resistance Excellent up to ~1050-1100 °C
Service Temperature 980-1050 °C

Get FSX 414 Super Alloy as per Standards Click Here

 

FSX 414 Specification

 

Table of Content

FSX 414 Cobalt Base Superalloy Supplier in India For High-Temperature Components At Discounted Price

FSX 414 Cobalt Base Superalloy Mechanical Properties
Properties  Conditions
T (°C) Treatment
Poisson's Ratio 0.27-0.30 25  
Elastic Modulus (GPa) 190-210 25  
Tensile Strength (Mpa) 515 25 annealed (sheet, strip) more
Yield Strength (Mpa) 275
Elongation (%) 40 
Reduction in Area (%) -
Fsx 414 Density
Density (×1000 kg/m3) 7.8
Key Properties of Fsx 414 Material
  • Superior high-temperature strength
  • High oxidation and corrosion resistance
  • Excellent creep resistance
  • Optimized for additive manufacturing
  • High wear resistance

Stockist Of Precipitation-Hardening FSX 414 Material in Mumbai With Oxidation Resistance Up to 900°c

Fsx 414 Super Alloy Thermal Properties
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  -
Surface Stability of GTA-Welded FSX-414
Material Natural Gas Diesel Oil + Sea Salt
1600°F / 6057 Hrs. 1800°F / 604 Hrs. 1600°F / 600 Hrs. 1800°F / 600 Hrs.
M.P. M.P.(l) S.L.(2) M.P. S.L. M.P. S.L. M.P. S.L.
FSX-414 Base 4.2 0.3 3.5 0.3 4.2 0.4 5.3 0.3
3D Printing Technology for FSX-414 Powder
3D Printing Technology Recommended FSX-414 Powder
Direct Energy Deposition (DED) Gas-atomized powder (50-150µm)
Binder Jetting Irregular or spherical powder (30-80µm)
Laser Powder Bed Fusion (LPBF) Gas-atomized spherical powder (15-45µm)
Electron Beam Melting (EBM) Gas-atomized powder (45-105µm)
Thermal Fatigue Resistance of GTA-Welded FSX-414
Peripheral Radius (In.) No. of Cracks Cycles to Crack Longest Crack (In.) Total Crack Length (In.)
FSX-414 L-605 FSX-414* L-605* FSX-414 L-605 FSX-414 L-605 Base Material
0.010 2 4 < 5 < 5 0.094 0.095 0.182 0.171 0.036
0.010 2 1 < 5 < 5 0.082 0.185 0.112 0.185 -
0.010 5 4 < 5 < 5 0.055 0.080 0.196 0.156 -
0.020 2 3 < 5 < 5 0.170 0.054 0.285 0.089 0.033
0.020 4 2 15 < 5 0.035 0.064 0.120 0.081 -
0.020 2 2 < 5 10 0.405 0.060 0.505 0.096 -
0.030 2 0 50 >50 0.035 0 0.050 0 0.021
0.030 1 1 15 15 0.330 0.032 0.330 0.032 -
0.030 2 0 20 41 0.010 0.015 0.010 0.015 -
0.040 1 1 10 < 5 0.012 0.014 0.012 0.014 0.020
0.040 2 2 < 5 20 0.095 0.018 0.117 0.031 -
0.040 2 1 41 25 0.035 0.060 0.045 0.060 -
Fsx 414 Scrap Electric Properties
Properties  Conditions
T (°C) Treatment
Electric Resistivity (10-9W-m) 690 25   -
Thermal-Fatigue Resistance of EB-Welded FSX-414
Peripheral Radius (in.) Crack Initiation
Avg. Cycles to Crack (Smooth)
Crack Propagation After 50 Cycles
Avg. Crack Length (in.) (Notched)
Base Weld Base Weld
0.010 49 41 0.020 0.098
0.030 111 63 0.020 0.066
0.020 71 43 0.024 0.110
0.040 116 82 0.008 0.060

Refer Cobalt-Based High-Temperature FSX 414 Alloy Chemical Composition and Equivalent Here

FSX 414 Alloy Chemical Composition
Component Elements Properties Metric English
Carbon, C  0.25 % 0.25 %
Silicon, Si  <= 1.0 % <= 1.0 %
Tungsten, W  7.0 % 7.0 %
Boron, B  0.012 % 0.012 %
Chromium, Cr  29.5 % 29.5 %
Cobalt, Co  <= 48.738 % <= 48.738 %
Iron, Fe  <= 2.0 % <= 2.0 %
Manganese, Mn  <= 1.0 % <= 1.0 %
Nickel, Ni  10.5 % 10.5 %
Fsx 414 Material Welding Parameters
Parameter Value
Technique Manual GTA/cold wire
Base Material Condition Solution treated
Welding Current 60 to 80 amps
Welding Voltage approximately 12 volts SPDC
Shielding 15 cfh argon
Electrode 1/16" diameter, 2% thoriated tungsten, ground to 90° conical tip
FSX 414 Cobalt Base Superalloy Advantages and Challenges
Advantages Challenges
Large-scale part production Requires post-processing
High-speed production Requires sintering & infiltration
High precision, fine details Requires optimized laser parameters
Low residual stress Limited material availability
Get High Strength FSX- 414 With Density 8.6 kg/dm³ For Repairing and Welding Gas Turbine Components
Fsx 414 Super Alloy Applications
Fsx 414 Super Alloy Applications

 

Fsx 414 Alloy Rupture Strength
Properties Metric English
Rupture Strength     
  • 21.4 MPa
  • @Temperature 1090 °C,
  • Time 360000 sec
  • 3100 psi
  • @Temperature 2000 °F,
  • Time 100 hour
  • 34.5 MPa
  • @Temperature 982 °C,
  • Time 3.60e+6 sec
  • 5000 psi
  • @Temperature 1800 °F,
  • Time 1000 hour
  • 55.2 MPa
  • @Temperature 982 °C,
  • Time 360000 sec
  • 8000 psi
  • @Temperature 1800 °F,
  • Time 100 hour
  • 117 MPa
  • @Temperature 816 °C,
  • Time 3.60e+6 sec
  • 17000 psi
  • @Temperature 1500 °F,
  • Time 1000 hour
  • 152 MPa
  • @Temperature 816 °C,
  • Time 360000 sec
  • 22000 psi
  • @Temperature 1500 °F,
  • Time 100 hour
FSX 414 Super Alloy in Various Forms like Various Forms, Such as Valves, Flanges, and Pipe Fittings
Various Forms of FSX 414 Super Alloy
  • Valves
  • Flanges
  • Pipe Fittings
  • Bars / Rods
  • Custom Shapes & Blades
  • Rings / Segments
  • Investment Cast Components

 

Production Methods of FSX-414 Powder
Production Method Particle Shape
Gas Atomization (GA) Spherical
Plasma Atomization (PA) Highly Spherical
Vacuum Induction Melting + Gas Atomization (VIGA) Spherical
Water Atomization (WA) Irregular

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