LMD project data

Laser metal deposition in numbers: what LMD delivers in real projects

Across 20 published projects, Exafuse has used laser metal deposition (LMD) to apply layers from about 1.5 mm to 20 mm, build parts weighing over 150 kg and repair a spindle within 24 hours. The table links each publicly documented figure to its project context.

Key figures

Key figures at a glance

Each figure comes from the linked project. These are documented examples, not universal process guarantees.

FigureValueProject
Total mass in one projectmore than 750 kgDuisburg bridge project
Largest individual componentmore than 150 kgDuisburg bridge project
Thickest documented coating20 mm Inconel 625Forging hammer and round die
Local repair build-up10–20 mmForging hammer
Thinnest documented target layerabout 1.5 mmValve-seat and wear ring
Thin-wall buildabout 1.8 mm wall, more than 1,070 layers, about 50 h750 mm multi-material nozzle
Fastest documented repair24 hoursSpindle with Inconel 718
CNC LMD build envelope2 × 1 × 2 m (4 m³)Equipment overview
Robotic LMD rotary tableup to 1,000 kgEquipment overview

Project comparison

Selected published projects

Materials that have not been publicly named remain open. Material, process and inspection planning are assessed separately for every new part.

ProjectTaskMaterialPublished figures
Duisburg bridge projectNew build / infrastructurenot publicly specifiedmore than 750 kg; six structural nodes; individual parts over 150 kg
Forging hammer and round dieRepair and coatingInconel 625170 mm radius; 20 mm coating; local build-up of 10–20 mm
Undersized spindleRepairInconel 71885 mm coating length; about 1.75 mm machining allowance; 24 hours
Valve-seat and wear ringsWear protectionproject-specifictarget layers from about 1.5 mm to 3 mm
Rolling dieCoatingmultiple screened alloy variantsstarting diameter about 79 mm; build-up into the low 80 mm range
750 mm multi-material nozzleNew build / demonstratorInconel 625 and Inconel 718750 mm; about 1.8 mm wall; more than 1,070 layers; about 50 hours
130 mm drillBuild and functional layertungsten-carbide-containing final coating130 mm diameter
Turbo-generator rotor wedgesCoatingCuNi2SiCr on coppertemperature monitoring and an adapted process sequence
3 kW helical impellerMetal AM prototypenot publicly specified3 kW power class

How to use the data

Project figures are reference points, not transferable limits

Layer thicknessSuitable layer thickness depends on function, substrate, geometry, heat input, machining allowance and inspection.
Part sizeBuild envelope, weight, access, fixturing, rotation and finishing must work together.
TimeThe documented 24-hour repair was one specific project. New lead times depend on damage, material, finishing and inspection.
Technical boundaryThe tables do not replace a feasibility assessment or project-specific acceptance process.

Publication details

Authorship and technical context

Revision 1.0
AuthorJulian Krell, material scientist and managing director at Exafuse
Dr.-Ing. Julian KrellMaterials scientist and managing director

Material selection, feasibility and project scope

Technical reviewerManish Sharma, AI and R&D lead for process monitoring and LMD/DED systems at Exafuse
Manish SharmaIndustrial AI and decision systems

Process monitoring, image processing and LMD/DED data systems

Reference basis
Approved public project material

This project example documents the published application. It is not a general qualification or guarantee for other parts and materials.

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