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

Rene 80

Rene 80 Superalloy Overview
Mchining
  • Milling
  • Grinding
  • Turning
  • Deep hole drilling
Heat treatment
  • Normalizing,Annealing,Tempering,Quenching,
  • Hardening and tempering,Seasoning,Surface hardening,Carburizing
Material Group S - Superalloys (Heat resistant and Titanium)
Sub-Group Superalloy
Tensile Strength [N/mm^2]
Machinability Range 15% - 45%
Base composition Nickel-Cobalt
Nominal chemistry Ni 14Cr 9.5Co 5Ti 4Mo 4W 3Al
Recommended process technology Brazing
Achieved surface function Dimensional Restoration

Get Rene 80 Alloy as per Standards Click Here

 

Rene 80 Specification

 

Table of Content

Rene 80 Nickel-Based Superalloy Supplier in India At Factory Price, Refer Composition

Rene 80 Chemical Composition
Element Content (wt%)
Cobalt (Co) 9
Molybdenum (Mo) 4
Chromium (Cr) 14
Tungsten (W) 4
Aluminum (Al) 3
Titanium (Ti) 5
Nickel (Ni) Balance
Boron (B) Max 0.015
Equivalent International Designations for Material René 80
Standard Name
ANFOR NC14K9T5DWA
Key Features of Rene 80 Superalloy
  • Excellent Fatigue Resistance
  • Exceptional Thermal Stability
  • High Oxidation Resistance
  • Strong Grain Boundary Strength
  • Superior High-Temperature Strength

Buy High-Temperature UNS N07080 Alloy For Aircraft and Power Generation Systems, Check Mechanical Properties

Rene 80 Superalloy Applications
Rene 80 Superalloy Applications

 

UNS N07080 Alloy Mechanical Properties
Property Value
Tensile Strength (MPa) 1200-1300
Yield Strength (MPa) ~1000
Creep Strength High at >850°C
Hardness (HRC) 35-40
Elongation (%) 10-12
Elastic Modulus (GPa) ~215
Rene 80 Superalloy Physical Properties
Property Value
Density (g/cm³) 8.79
Melting Point (°C) 1340
Thermal Conductivity (W/m·K) 11.5
Modulus of Elasticity (GPa) 211
Cutting Speeds Recomendations for Heat resistant Ni or Co Based Rene 80 Alloy
Application Vc (SFM) Vc (m/min)
Turning 200-590 60-180
Milling 150-440 45-135
Parting 130-380 40-115
Grooving 180-520 55-160
Drilling 180-520 55-160
Recommended Insert Cutting Edge Geometry for Material René 80
Honing Size 0.02-0.05 mm / 0.001-0.002"
Rake Angle 13° -18°
Land Angle Neutral
Land Width 0.10-0.20 mm / 0.004-0.008"
Ground Insert Recommended
UNS N07080 Cutting Parameters
Operation Coolant Pressure (bar) Speed (m/min) Depth of Cut (mm)
Roughing 100-120 15-25 2.0-3.0
Finishing 120-150 30-40 0.3-0.8

Stockist Of Amdry Rene 80 in Mumbai Suitable to Work At Temperature up to 1300°F, see Heat Treatment

Amdry Rene 80 Aging Heat Treatments
T(°C) t (h)
850 1000, 2000, 5000, 10000, 20000
900
950
1000
1050 1000, 2000, 5000, 10000
EN 2.4952 Heat Treatment
Tempering Quenching Normalizing Annealing Q & T
CNC Machining Challenges for Rene 80
  • Tool Wear and Edge Chipping
  • Work Hardening
  • Heat Generation

 

Understand Difference Between Rene 77 vs Rene 80 Here
Rene 77 vs Rene 80
Property Rene 77 Rene 80
Density ≈ 8.6 g/cm³ ≈ 7.7-8.0 g/cm³
Melting Point ~ 1340‑1380 °C ~ 1370‑1400 °C
Service/Use Temperature Up to ~900 °C ~760‑982 °C
Tensile Strength ~ 1150‑1250 MPa ~ 1158 MPa
Yield Strength ~ 800‑950 MPa ~ 1034 MPa
Thermal Conductivity ~ 13.2 W/m·K @100 °C ~ 42.7 W/m·K @100 °C
Rene 80 Superalloy Tool Selection
Parameter Recommendation
Coating AlTiN or TiSiN PVD (3-5 µm)
Geometry Positive rake angle (6-8°), sharp cutting edge (~0.05 mm)
Tool Material Carbide (K20-K30) or CBN inserts for finishing
Rene 80 Alloy Processing Range
Steel Grade Specification Processing Range
Rene 80 Round Bar Φ1 to Φ2000
Forging Pipe/tube/slugs/donuts/cubes/other shapes
Tubings OD: Φ4-410; WT: 1-35 mm
Square-shape steel/Flate bar 10 to 1000
Steel Plate/Sheet 0.08 to 800(T)*10 to 1500(W)*Long
Steel coils and strip THK:0.1mm Width:1500mm
Rene 80 Superalloy’s Machinability
  • Single Crystal Casting
  • Equiaxed Crystal Casting
  • Superalloy Directional Casting
  • Powder Metallurgy Turbine Discs
  • Superalloy Precision Forging
  • Superalloy 3D Printing
  • CNC Machining
  • Superalloy Welding
  • Hot Isostatic Pressing (HIP)
  • Vacuum Investment Casting

 

Offer Age-hardened Nickel-chromium Alloys EN 2.4952 Material With Outstanding Oxidation Resistance
EN 2.4952 Material Thermal Properties
Properties Conditions
T (°C) Treatment
Thermal Conductivity (W/m-K) 42.7 100  -
Specific Heat (J/kg-K) 477 50-100  -
Surface Treatment for Machined Rene 80 Parts
  • Heat Treatment
  • Superalloy Welding
  • Thermal Barrier Coating (TBC)
  • Electrical Discharge Machining (EDM)
  • Deep Hole Drilling
  • Material Testing and Analysis
  • Hot Isostatic Pressing (HIP)

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