DMLS

Solutions and Services

DMLS

Direct Metal Laser Sintering (DMLS) is a Metal Additive Manufacturing technology where a thin layer of metal powder is spread over the build platform and a high power laser scans the cross-section of the component, melting (or fusing) the metal particles together and creating the next layer. This layer by layer process is repeated hundreds or thousands of times until the entire part is manufactured.


Given the growing need for 3D Printing and the dearth of technological know-how in the industry, we at Innovae3D, offer complete 3D Printing solutions. We undertake 3D Printing projects from design, development and analysis to printing and post processing.

Our AM Eco-System:

Generic Information:

Max. part size:

250 x 250 x 300 mm

Dimensional Accuracy:

(+/-) 150-200 µm

Lead-time:

3-4 working days

Minimum Order Quantity:

1 No.

Some of the Materials that we cater to in Metal Additive Manufacturing are listed below with their properties and applications:

Material Alloy Designation Hardness Advantages Applications
Maraging Steel(MS1) 18% Ni Maraging 300,European 1.2709,German X3NiCoMoTi 18-9-5 35-37 HRC Built, Post Hardened to 50-56 HRC Easily Machinable & Excellent polishability Injection moulding,Tooling,Conformal Cooling
Aluminium AlSi10mg Typical Casting Alloy Approx 119 ± 5 HBW Low Weight, Good Thermal Properties Automotive, Racing
Stainless steel (316L) ASTM F138 85 HRB Corrosion and pitting resistance Surgical tools,Food and chemical plants
Stainless steel(PH1) 15-5 PH, DIN 1.4540 and UNS S15500 30-35 HRC Built, Post Hardened to 40 HRC High Hardness & strength Prototype/Production parts
Stainless steel(GP1) 17-4, European 1.4542, German X5CrNiCuNb16 -4 230 ± 20 HV1 Built Ground & Polished to 250-450 HV1 High Toughness and Ductility Engineering Applications
Titanium (T -64) ASTM F2924 320 ± 15 HV5 Light weight,High strength,Corrosion Resistance Aerospace Motorsport Racing
Nickel Alloy IN178 UNS N07718, AMS 5662, AMS 5664, W.Nr 2.4668, DIN NiCr19Fe19NbMo3 30 HRC Built, Post Hardened 47 HRC Heat and Corrosion Resistance Turbines,Rockets,Aerospace
Cobalt Chrome (MP1) ISO 5832-4 and ASTM F75 35-45 HRC Built High Temperature Resistance Turbines and Engine parts
Have a Metal AM requirement?