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

Rene 77

Rene 77 High Alloy Overview
Particle Size 45 μm, or customized
Material Group S - Superalloys (Heat resistant and Titanium)
Sub-Group Superalloy
Tensile Strength [N/mm^2]
Machinability Range 15% - 45%
Purity Nickel, Chromium, Cobalt, Aluminum, Molybdenum
Shape Spherical Powder
Process Gas atomized (GA) or Plasma rotating electrode powder (PREP)
Particle Size Distribution 0-25, 15-45, 15-53, 45-105, 45-150um or sieved as required

Get Spherical Rene 77 Powder as per Standards Click Here

 

Rene 77 Specification

 

Table of Content

Material René 77 Supplier in India, Refer Chemical Composition

René 77 Chemical Composition
Element Content (wt%)
Cobalt (Co) 16
Tungsten (W) 3.5
Iron (Fe) Max 0.5
Nickel (Ni) Balance
Molybdenum (Mo) 4.75
Aluminum (Al) 5.75
Titanium (Ti) 3.5
Chromium (Cr) 15
Equivalent International Designations for Material René 77
Standard Name
ANFOR NC15K15ADT
Key Features of Rene 77 Superalloy
  • Superior Creep Resistance
  • Excellent Thermal Fatigue Resistance
  • High Mechanical Strength
  • Oxidation and Corrosion Resistance
  • Long Service Life at High Temperatures

Buy High Strength Rene 77 Nickel-Cobalt Based Superalloy Suitable to Work At 900 °C

Rene 77 Alloy Heat Treatment
Normalizing Annealing Tempering Quenching Q & T
RENE® 77 Cutting Speeds Recomendations for Heat resistant Ni or Co Based
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
Standards for Rene 77 Powder
Standards
UNS Number N07777
AMS Standards AMS 5390
ASTM Standards ASTM B637
ISO Standards ISO 15156
Results of Creep Test of Superalloy Rene 77
CoAl₂O₄ concentration, %mass. A₄, % tₓ, h Z, %
0 16 33.3 16.24
5 13.2 38.5 15.4
10 16.65 38.4 21

Stockist Of Spherical Rene 77 Powder in Mumbai For Turbine Engine Components and Aerospace Parts

Rene 77 Alloy Applications
Rene 77 Alloy Applications

 

Rene 77 High Alloy Tool Selection
Parameter Recommendation
Tool Material Carbide (K20-K30) or CBN inserts for finishing
Geometry Positive rake angle (6-8°), sharp cutting edge (~0.05 mm)
Coating AlTiN or TiSiN PVD (3-5 µm)
Cutting Parameters for Material René 77
Operation Speed (m/min) Depth of Cut (mm) Coolant Pressure (bar) Feed (mm/rev)
Finishing 30-40 0.3-0.8 120-150 0.05-0.10
Roughing 15-25 2.0-3.0 100-120 0.15-0.25
Surface Treatment for Machined Rene 77 Parts
  • Heat Treatment
  • Superalloy Welding
  • Thermal Barrier Coating (TBC)
  • Electrical Discharge Machining (EDM)
  • Deep Hole Drilling
  • Hot Isostatic Pressing (HIP)
  • Material Testing and Analysis

 

Macrostructure of Superalloy Rene 77
The section thickness mm Cobalt aluminate concentration, %mass. A, mm² (0%) A, mm² (10%) s, mm² (10%) f (0%) s, mm² (5%) s, mm² (0%) A, mm² (5%) f (5%) f (10%)
49 0% 6.38 1.49 1.92 2.07 4.70 6.06 3.79 1.97 2.18
29 0% 6.83 1.39 3.32 1.88 5.79 7.52 4.38 2.02 2.20
23 0% 13.33 1.80 3.15 1.71 5.84 11.68 4.48 2.00 2.57
17 0% 6.62 0.86 1.51 2.24 2.30 7.15 1.50 2.19 2.53
11 0% 3.46 0.48 0.56 2.33 2.27 3.90 1.49 2.27 2.50
5 0% 1.14 0.30 0.34 2.10 0.69 1.30 0.40 2.18 2.78
Get Creep Resistance RENE® 77 Superalloy With Density 8.73 g/cm³, Check Mechanical Properties
Mechanical Properties of Rene 77 High Alloy
Property Value
Tensile Strength (MPa) 1000-1200
Yield Strength (MPa) ~900
Creep Strength High at elevated temperatures
Hardness (HRC) 35-40
Elongation (%) 10-12
Elastic Modulus (GPa) 210
Spherical Rene 77 Powder Physical Properties
Property Value
Density (g/cm³) 8.73
Melting Point (°C) 1395
Modulus of Elasticity (GPa) 210
Thermal Conductivity (W/m·K) 12
Available Sizes and Forms of Rene 77 Powder
Form Available Sizes
Powder 15 to 45 microns
Bars/Rods 0.5 inches to 4 inches
Sheets/Plates 1 mm to 50 mm
Recommended Insert Cutting Edge Geometry for Rene 77 Material
Honing Size 0.02-0.05 mm / 0.001-0.002"
Rake Angle 13° -18°
Ground Insert Recommended
Land Angle Neutral
Land Width 0.10-0.20 mm / 0.004-0.008"
Rene 77 Superalloy’s Machinability
  • Vacuum Investment Casting
  • Powder Metallurgy Turbine Disc
  • Single Crystal Casting
  • Equiaxed Crystal casting
  • Superalloy 3D Printing
  • Superalloy Directional Casting
  • Superalloy Precision Forging

 

Find Afnor NC15K15ADT Material in Different Forms, See Material Properties
Afnor NC15K15ADT Material Thermal Properties
Thermal Expansion (10-6/ºC) 17.5
Thermal Conductivity (W/m-K) 16.2
Specific Heat (J/kg-K) 500
RENE® 77 Superalloy Electric Properties
Electric Resistivity (10-9W-m) 690
CNC Machining Challenges for Rene 77
  • Tool Wear and Edge Chipping
  • Heat Generation
  • Work Hardening

 

Recommended Carbide Grades for Material René 77
Grade for Turning Grade for Parting Off Grade for Grooving Grade for Milling
RS15T FM2543 FM2533 FM125
RS25T FM2553 KM15 TS20
RS35T KM15 GC1125 S30T
FM524 GC1105 IC806 (IC804) S40T
FM2533 GC1145 IC808 (IC908) IC808 (IC908)
KM15 IC807 (IC907) IC830 (IC328) IC830 (IC928)
TN15 IC808 (IC908) KCU10 KC510M
TS20 IC830 (IC328) KCU25 KC522M
ZR10 CP500 WSM13S KCSM40
IC806 (IC804) AH725 WSM23S F40M
IC807 (IC907) KCU10 WSM33S (WSM33) MS2500
IC830 (IC328) KCU25 WSM43S MS2050
TS2000 (CP200) WSM33S (WSM33) CP500 AH120
CP500 WSM13S CP600 AH725
TS2500 WSM23S AH905 MP9120
CP600 WSM43S AH725 MP9130
KCU10 (KC5010) AC520U AH7025 ACU2500
KCU25 (KC5025) AC1030U (AC530U) VP10RT ACM200
S05F AH7025 VP20RT ACM300
GC1105 AH725 VP30RT RS20M
GC1115 VP10RT AC520U RS30M
GC1125 VP20RT AC1030U (AC530U) RS40M
AH8005 VP30RT - PR1210
AH8015 - - PR1535
WSM10S (WSM10) - - PR1535
WSM01 - - JS1025(JP4120)
WSM20S (WSM20) - - PTH30H
WSM30S (WSM30) - - JM4160
MP9005 - - M6330
MP9015 - - 8215
VP20RT - - M8340
AC5005S (AC510U) - - M8345(M8346)
AC5015S - - WSM35S
AC5025S (AC520U) - - WSM45S
PR005S(PR1310) - - PC5300
PR015S - - PC8110
PR1125 - - PC5400
PR1325 - - PC3545
PR1535 - - YBG102
JP9115 - - YBG202
T6310(T8310) - - YBG205
T8330 - - -
T8345 - - -
PC8105 - - -
PC8110 - - -
PC8115 - - -
PC5300 - - -
PC9030(PC9070T) - - -
PC3030T(PC5400) - - -
YBG102(YBG105) - - -
YBG202 - - -
YBG205 - - -
YB9320 - - -
YBG302 - - -

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