Part first
Set the process boundary using real materials, drawings, samples and incoming variation.
APPLICATION BEFORE POWER
Aerospace components combine expensive materials, complex geometry and narrow acceptance windows across metallurgy, residual stress, coatings and traceability.
We start with material certification, heat treatment, part history, functional surfaces, NDT and documentation needs, then validate five-axis motion, optics, tooling, shielding and monitoring.
Set the process boundary using real materials, drawings, samples and incoming variation.
Convert appearance, cross-section, function and inspection into clear acceptance criteria.
Validate optics, motion, tooling, inspection and data as one production system.
MANUFACTURING SCENARIOS
Each application has different material, geometry, quality and takt constraints; the equipment must be configured from the real task.
Airframe and complex thin-wall parts require controlled fixturing, distortion, shielding and metallurgy.
Tip and local-damage repair require controlled heat input, dilution and downstream treatment.
Blade holes require controlled shape, taper, recast layer, heat input and position.
Curved, thin-wall and complex parts require coordinated access, focus and toolpath.
Oxide and old coating removal must protect the base material during MRO.
Serial numbers and repair records must be durable, readable and performance-safe.
CORE PROCESSES
Process pages explain the technical route; final parameters and equipment still require validation with the real part.
Joining and repair of titanium structures, blades and precision aerospace parts.
Five-axis contours in thin-wall, curved and complex components.
Blade cooling holes, microholes and precision through-holes.
Oxide, coating and pre-repair surface preparation.
Serial, batch and MRO traceability.
ENGINEERING INPUTS
Complete inputs turn a generic equipment quote into a manufacturing solution built around the part, quality criteria and takt time.
Provide drawings, material grade, thickness, surface condition and representative samples.
Define joints, tolerances, datum, access, fixturing and no-damage zones.
Specify functional, appearance, dimensional and inspection acceptance criteria.
Confirm cycle time, loading, vision, traceability, MES, safety and environmental requirements.
MATERIAL MATRIX
Open a material guide to review grades, forms, process boundaries and relevant equipment.
Airframe, engine and lightweight high-strength structures
↗02Turbine blades and high-temperature components
↗03Engine hot-section and critical structures
↗04Airframe, cabin and lightweight components
↗05Airframe, interior and mixed-material structures
↗06Thermal barrier, protection and MRO surface treatment
↗VALIDATION WORKFLOW
Keep the process window, quality inspection, takt time and line interfaces in one validation chain.
Confirm materials, parts, drawings, quality criteria and production targets.
Establish repeatable parameter boundaries around the critical variables.
Record inspection results and stability using agreed methods.
Freeze the optics, motion, tooling, safety and data architecture.
RECOMMENDED EQUIPMENT
These links lead to published systems. Final configuration depends on the real part, quality criteria and sample-validation results.

Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗
Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗
Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗
Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗
Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗
Explore this system as a starting point; the final configuration is matched to your part, process and production requirements.
View equipment ↗FAQ
If you already have parts, materials or current-process data, submit them for a focused assessment.
No. Start with the part, material, quality target and cycle time, then validate the laser source, optics, motion and automation configuration.
Yes. Representative samples and agreed acceptance criteria are used to establish a repeatable process window.
Yes, after reviewing robot, PLC, MES, safety, loading, changeover and inspection interfaces.
Share drawings, material data, samples, quality standards, current process, target output and planned integration.
BUILD THE RIGHT PROCESS
Submit material, drawings, quality, takt and integration requirements so we can define the process and equipment route.