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Direct Metal Laser Sintering (DMLS)


GPI Prototype is a service provider of Direct Metal Laser Sintering (DMLS), the latest technology in rapid prototype and direct digital manufacturing services. As one of the first DMLS service providers in the country, GPI produces metal parts for applications ranging from prototypes to production. DMLS technology is ideal for a variety of applications including the creation of conformal cooling channels within tools and tooling inserts, as well as customized medical implants.


Utilizing the DMLS process, metal parts of the most complex geometries are built layer-by-layer (down to 20 microns) directly from 3D CAD data, automatically, without tooling. The parts have excellent mechanical properties equivalent to wrought materials, high detail resolution and exceptional surface quality. The metal powder is melted entirely to create a fully dense, fine, homogenous structure. Unique geometric freedom of design enables DMLS to form cavities and undercuts which, with conventional methods, can only be produced with great difficulty, if at all.

Additionally, when a part needs to be tested and re-designed over and over, the lead time for receiving a traditionally tooled part can create a large bottleneck in the final production process. DMLS produces parts that are extremely high quality, and can be built in a matter of hours or days rather than weeks. This ability to generate functional metal prototypes in short order radically impacts design processes, accelerating design cycles with time to market by creating the opportunity for multiple redesigns and builds.

Depending on size and geometries, in some cases the turnaround time for a part can be as little as a few hours. Furthermore, these parts can undergo functional testing in the environment for which they were designed. This technology delivers unlimited potential for engineers to create previously impossible solutions, embracing a new era of design-driven manufacturing.





MARKETS SERVED:


Rapid Tooling

Aerospace

Medical & Dental

Automotive

Jewelry & Art

Custom Automation

Architecture

Pharmaceutical

Health & Beauty

Food & Beverag

 

MACHINES:

EOS M280 (uses Argon when using titanium, aluminum and Inconel (Grade 625 and 718) and nitrogen)

EOS M270 (only uses nitrogen)

Machine size (X x Y x Z)

M280 = 9 x 9 x 10.5’’ or 228 x 228 x 304 mm 

M270 = 9 x 9 x 7.5’’ or 228 x 228 x 190 mm

Minimum Feature size = .015’’ or .38 mm

Minimum wall thickness is .3mm - .4mm or .012” - .014”

Layer Thickness = 20 or 40 microns

Typical tolerances are .005" on 1st inch, .002" thereafter

Beam thickness: .008’’ or .2032 mm



MATERIALS (MOST COMMON):

Stainless Steel (Ph1)

Grade is equivalent to 15-5 stainless

Hardness (HRC) 30 – 35; post hardened up to 40 HRC

Thermal conductivity 13.8 +/- .8 W/mC

Heat capacity 460 degrees C; 470 degrees C if hardened

Layer thickness 20 or 40 Micron Layers

Stainless Steel (GP1)

Grade is equivalent to 17-4 stainless

Hardness (HRC) 20 – 25, if post hardened up to 45 HRC

Thermal conductivity:

20 degrees C = 13 W/mC

100 degrees C = 14 W/mC

200 degrees C = 15 W/mC

300 degrees C = 16 W/mC

Heat capacity 550 degrees C. Post-process stress-relieving @ 650 degrees C for 1 hour.

Layer thickness 20 or 40 Micron Layers

Cobalt Chrome (MP1)

Hardness (HRC) 35-45, then stress relieved

Thermal conductivity:

20 degrees C = 13 W/mC

300 degrees C = 18 W/mC

500 degrees C = 22 W/mC

1000 degrees C = 33 W/mC

Heat capacity 1150 degrees C. Post-process stress-relieving @ 1050 degrees C for 2 hours.

Layer thickness 20 or 40 Micron Layers

Maraging Steel (MS1)

Hardness (HRC) 33-37, 50-54 after age hardening for 6 hours

Thermal conductivity 15 +/- .8 W/mC

Heat capacity 450 degrees C

Layer thickness 20 or 40 Micron Layers

 

AVAILABLE METAL MATERIALS: Click on the material type to view a data sheet.


Material Characteristics Applications

Stainless Steel (PH1)

15-5 Mechanical Properties
20 or 40 Micron Layers
30-35 HRC Built
Post Hardened to 40 HRC

Prototype / Production Parts
Can Be Polished

Stainless Steel (GP1)

17-4 Mechanical Properties
20 or 40 Micron Layers
250-400 HV Hardness
Post Hardenable

Prototype / Production Parts
Can Be Polished

Cobalt Chrome (MP1)

High Carbon CoCr Alloy
20 or 40 Micron Layers
35-45 HRC Built

Prototype / Production Parts
Can Be Polished

Maraging Steel (MS1) - Tooling Steel

Maraging (Tooling) Steel
20 or 40 Micron Layers
33-37 HRC Built
Post Hardened to 50-54 HRC

Can Be Polished
Conformal Cooling Channels
Tooling

Titanium Alloy Ti-64

Pre-Alloyed Ti6AlV4
30 Micron Layers
41-44 HRC Built

Prototype / Production Parts
Can Be Polished

Aluminium AlSi10Mg

Master Alloy Aluminum
30 Micron Layers
120 +/- 5 HBW Built
Post Hardened to 112 +- 5 HBW

Prototypes / Small Production
Low Weight Applications
Thermal Parts

NickelAlloy IN718

Nickel Based Heat Resistant Alloy
20 Micron Layers
30 HRC Built
Post Hardened 47 HRC

Turbine Engines
Rocket & Space Applications
Chemical Industry Parts



Finishes:


1) Shot peened (Media = ceramic or metal beads)

2) Shot/Sand blasted, (Media = alumina oxide)

3) Brush finish (must be mirror polished 1st)

4) Light sanded (no extra material needed)

5) Medium polished (add .003 - .008 material)

6) Mirror polished (add .003 - .008 material)

DMLS can build both functional and visual parts.

 

* Conformal Cooling PDF
* EOS M270 PDF
* Mechanical Test Data PDF
* Finishing Options for Direct Metal Laser Sintering (DMLS)

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