Process Data Sheet

EOS NickelAlloy IN718 for EOS M 290 | 40 µm

EOS M 290 - 40 µm - TRL 9

System Setup EOS M 290
EOS Material set IN718_040_PerformanceM291
Powder Product No. 9011-0020 / 9030-0022
Software Requirements

EOSPRINT 1.7 or newer

EOSPRINT 2.6 or newer and EOSYSTEM 2.9 or newer

Recoater Blade HSS (High Speed Steel)
Nozzle EOS Grid Nozzle
Inert gas Argon
Sieve 63 µm
Additional Information
Layer Thickness 40 µm
Volume Rate 4.2 mm³/s
Min. Wall Thickness 0.3 - 0.4 mm

Chemical and Physical Properties of Parts

Microstructure of the Produced Parts

Defects Thickness Result Number of Samples
Average Defect Percentage 40 µm 0.03 % -
Density EN ISO 3369 Thickness Result Number of Samples
Average Density 40 µm ≥ 8.15 g/cm³ -

Mechanical Properties

Mechanical Properties Heat Treated

Room Temperature | Yield Strength [MPa] Tensile Strength [MPa] Elongation at Break A [%] Reduction of Area Z [%] Modulus of elasticity [GPa] Number of Samples
Vertical 1145 1375 17 - - -
Horizontal 1240 1505 12 - - -

Heat treatment procedure conform to Aerospace Material Specification AMS 2774 and AMS 5662. 
As manufactured microstructure for additively manufactured IN718 consists of gamma phase (γ). Heat treatment for IN718 is required to produce desired microstructure and part properties (gamma double prime precipitates, γ"). Heat treatment is also used to relieve stresses.

Step 1: 
Solution Anneal: hold at 954 °C (1750 °F ) for 1 hour per 25mm (0.98 inch) of thickness, air (/argon) cool

Step 2: 
Ageing treatment; hold at 718 °C (1325 °F ) 8 hours, furnace cool to 621 °C (1150 °F ) and hold at 621 °C (1150 °F ) for total precipitation time of 18 hours, air (/argon) cool

Mechanical Properties As Manufactured

EN ISO 6892-1 Room Temperature | 40 µm Yield Strength [MPa] Tensile Strength [MPa] Elongation at Break A [%] Reduction of Area Z [%] Modulus of elasticity [GPa] Number of Samples
Vertical 650 970 32 - - -
Horizontal 800 1090 25 - - -

Hardness

Heat Treated
Value 47
Unit HRC
Heat Treated
Value 466
Unit HB

Surface Roughness

Surface Roughness From To
Sa (µm) - -
Ra (µm) - -

Coefficient of Thermal Expansion

Temperature
13.1*10-6/K 25 – 100 ºC
13.7*10-6/K 25 – 200 ºC
14.1*10-6/K 25 – 300 ºC
14.4*10-6/K 25 – 400 ºC
14.7*10-6/K 25 – 500 ºC
15*10-6/K 25 – 600 ºC
15.5*10-6/K 25 – 700 ºC
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