alt picture | © copyright picture
Process Data Sheet

EOS NickelAlloy IN939 for EOS M 290 I 40 µm

EOS M 290 - 40 µm - TRL 7

Process Information Metal

This is the process description

System Setup EOS M 290
EOS Material set IN939_040_HiPerM291
Required Software Plan EOS BUILD
Software Requirements

EOSPRINT 2.6 or newer

EOSYSTEM 2.10 or newer

Recoater Blade HSS (High Speed Steel), Ceramic, Carbon Fiber Brush, Nitrile Butadiene Rubber (NBR)
Build Platform Temperature 80 °C
Nozzle EOS Grid Nozzle
Inert gas Argon, Nitrogen
Sieve 63 µm
Additional Information
Layer Thickness 40 µm
Volume Rate 3.6 mm³/s
Exposure Strategy Swimlanes
Wall Thickness Typical 0.3 - 0.4 mm mm
Typical Dimensional Change after HT [%] +0.2% %

Chemical and Physical Properties of Parts

Chemical composition of built parts is compliant to EOS NickelAlloy IN939 powder chemical composition.

Footnotes Part properties 

Microstructure of the Produced Parts

Defects Thickness Result Number of Samples
Average Defect Percentage - 0.01 % 10
Average Defect Percentage 20 µm 0.3 % 10
Density EN ISO 3369 Thickness Result Number of Samples
Average Density 40 µm > 8.15 g/cm³ -
Density AMS 2774 Thickness Result Number of Samples
Average Density 30 µm 8.10 g/cm³ 15

Mechanical Properties Heat Treated

EN ISO 6892-1 Room Temperature Yield Strength [MPa] Tensile Strength [MPa] Elongation at Break [%] Reduction of Area Z [%] Number of Samples
Vertical 1100 1500 13 - -
Horizontal 1130 1520 11 - -

HT description mech properties 1

Footnotes Mech properties 

Mechanical Properties As Manufactured

EN ISO 6892-1 Room Temperature Yield Strength [MPa] Tensile Strength [MPa] Elongation at Break [%] Reduction of Area Z [%] Number of Samples
Vertical 740 1090 28 - -
Horizontal 880 1160 24 - -

Hardness

EN ISO 6508 Heat Treated
Value 48
Unit HRC
Number of samples 10
EN ISO 6508 As Manufactured
Value 10
Unit HRC
Number of samples 10
EN ISO 6508 As Manufactured
Value 33
Unit HRC
Number of samples 10

Impact Toughness

EN ISO 148-1, Charpy-V As Manufactured
Typical Impact Toughness 110
Layer Thickness 20 µm
Specific Exposure Set Default

HT description Impact toughness

Footnotes Impact toughness

EN ISO 148-1, Charpy-V As Manufactured
Typical Impact Toughness 120
Layer Thickness 30 µm
Specific Exposure Set Default

HT impact toughness 2

Footnotes impact toughness 2

Stress Rupture Performance

AMS 2774 As Manufactured Stress [Mpa] Temperature [°C] Time to Rupture
[hrs] Elongation
[%] RA
[%]
Vertical 10 25 1 15 16
Horizontal 11 16 2 18 19

stress rupture performance description

Fatigue

HT Fatigue - NOT SHOWING UP!!

Low cycle fatigue performance of horizontally and vertically oriented samples at temperatures of 25 °C, 650 °C, 750 °C and 850 °C. The data represents cycles to failure for different strain amplitudes. No HIP was applied. Method, standard, cycles: axial, strain controlled testing according to ASTM E606

Footnotes for Fatigue 1

As Manufactured
Fatigue Strength [MPa] 550

HT description fatigue 2 - not showing up!

method fatigue 2

Footnotes fatigue 2

Thermal Conductivity

AMS 2774 Orientation [W/m*K]
As Manufactured Vertical 10
As Manufactured Horizontal 20

HT Description thermal conductivity 1

Footnotes Thermal cond 1

HT thermal conductivity 2

Foot notes thermal conductivity 2

Surface Roughness

EOS NickelAlloy IN939 parameters were developed for optimized dimensional accuracy of internal cooling features, which are essential to hot gas path components in gas turbines. This comes with a compromise on downskin roughness. Whenever possible, for parts where optimized dimensional accuracy of internal cooling features is not needed, EOS recommends to switch off downskin exposure, to improve downskin roughness and buildability at low angles, and to increase process speed.

Creep performance

AMS 2774 As Manufactured
Value 110
Unit MPa

Footnotes Misc. add prop. 1 :  The stress-rupture performance of EOS NickelAlloy IN939 was tested on vertically oriented samples, in heat-treated condition. No HIP was applied. The data presents the Larson-Miller Parameter values achieved at stress levels of 100 MPa, 250 MPa and 450 MPa. Standard: ASTM E139

add prop 2

Value value
Unit unit

footnotes prop 2

Electrical Conductivity

HT electrical conductivity 1

Footnotes electrical conductivity 1

AMS 2774 Orientation Typical Electrical Conductivity [%IACS]
HIP / 40 µm / Default Vertical 10-15
HIP / 40 µm / Default Horizontal 12-18

HT elect conductivity 2

footnotes elect conduct 2

AMS 2774 Orientation Typical Electrical Conductivity [%IACS]
Heat Treated / 50 µm / Application optimised - Inductors Vertical > 5
Heat Treated / 50 µm / Application optimised - Inductors Horizontal > 6

HT elect cond 3

footnotes sample prep 3

Coefficient of Thermal Expansion

ASTM E228 As Manufactured Temperature
12.18*10-6/K 25 – 100 ºC
12.89*10-6/K 25 – 200 ºC
13.78*10-6/K 25 – 400 ºC
13.49*10-6/K 25 – 600 ºC
13.99*10-6/K 25 – 800 ºC
15.06*10-6/K 25 – 900 ºC

Description HT CTE 25-100

Description HT CTE 25-200

Description HT CTE 25-400

Description HT CTE 25-600

Description HT CTE 25-800

Description HT CTE 25-900

Footnotes CTE 25-100

Footnotes CTE 25-200

Footnotes CTE 25-400

Footnotes CTE 25-600

Footnotes CTE 25-800

Footnotes CTE 25-900

ASTM E228 Heat Treated Temperature
11.79*10-6/K 25 – 100 ºC
12.64*10-6/K 25 – 200 ºC
13.64*10-6/K 25 – 400 ºC
14.27*10-6/K 25 – 600 ºC
15.29*10-6/K 25 – 800 ºC
16.32*10-6/K 25 – 900 ºC

Description 2 HT CTE 25-100

Description 2 HT CTE 25-200

Description 2 HT CTE 25-400

Description 2 HT CTE 25-600

Description 2 HT CTE 25-800

Description 2 HT CTE 25-900

Footnotes 2 CTE 25-100

Footnotes 2 CTE 25-200

Footnotes 2 CTE 25-400

Footnotes 2 CTE 25-600

Footnotes 2 CTE 25-800

Footnotes 2 CTE 25-900

Generate und open PDF