Aerospace laser cleaning

Aerospace & Aviation

Pratt & Whitney, GE Aviation, and dozens of MRO shops across the tri-state. Turbine blade cleaning, composite prep, and coating removal on flight-critical parts. Precision cleaning where dimensional tolerance is measured in thousandths.

Aerospace Laser Cleaning Planning

Aerospace components operate under demanding temperature, stress, and dimensional requirements. Cooling passages, composite panels, fastener holes, and mating surfaces require controlled cleaning. When the substrate and contaminant are suitable, laser cleaning can reduce the dimensional risks associated with grinding and abrasive blasting.

Aerospace Laser Cleaning Applications

USE CASE 01

Turbine Engine Components

Evaluate blades, vanes, nozzles, combustion liners, and cases only against the customer’s engineering specification and approval path. Hot-section deposits, coating residue, carbon, cooling passages, dimensions, and surface condition may require a controlled trial plus inspection or measurement; no universal dimensional or media-residue outcome is promised. For components being prepared for examination, see our inspection and NDT surface preparation service.

USE CASE 02

Composite Preparation

Clean carbon fiber, fiberglass, and Kevlar composite surfaces for bonding, repair, and inspection. Remove contamination, failed coatings, and paint without fiber damage or delamination.
USE CASE 03

Landing Gear and Structural Components

Strip cadmium, chrome, and paint coatings from landing gear, structural fittings, and actuator housings. Prepare for NDI inspection and recoating. No hydrogen embrittlement risk from acid stripping.
Dimensional change
0
Media in cooling passages
0
Composite fiber damage
0

MRO

Shop compatible

Aerospace Laser Cleaning for Tooling and Approved Trials

An aerospace laser cleaning enquiry should begin with the customer’s engineering requirements. Identify the part or tool, alloy, coating, finish and approval route. A proposed cleaning method needs a defined trial and acceptance decision.

Planning Example for Non-Flight Production Tooling

For a proposed trial on metal composite-production tooling, provide the finish, coating and release-agent information. Ask the tooling engineer to mark the test area and specify the surface checks needed before further processing.

  • Identify critical geometry and protected areas.
  • Provide approved material and process requirements.
  • Agree on the trial record, inspection method and stop conditions.
  • Obtain the customer’s decision before expanding the scope.

Review metal composite-mold cleaning and inspector-defined surface preparation. Approved recurring tooling work can be discussed through Maintenance Contracts.

Aerospace Laser Cleaning Questions

Laser cleaning is increasingly specified in aerospace MRO for turbine components, composite prep, and coating removal. Qualification depends on your specific OEM specifications and customer requirements. We provide process documentation and test results for your engineering review.
Cadmium, chromium, paint (primer and topcoat), thermal barrier coatings, plasma spray, anodize, and conversion coatings. Multi-layer systems removed in controlled passes with parameter adjustment per layer.

Related Services & Industries

Aerospace Tooling and Component Evaluation

Aerospace-related laser cleaning should begin with the engineering requirement, not a general claim that the process is safe for every alloy or component. The part number, alloy, coating, heat treatment, surface condition, tolerance and next operation determine whether a test coupon or controlled trial is appropriate.

Tri-State should not process a flight-critical component, controlled repair or qualified surface-preparation step without the customer’s written specification and approval path.

Applications that may merit a controlled trial

  • Production tooling, fixtures and non-flight support equipment, including metal molds used for composite production.
  • Weld-area oxide or residue removal when the governing procedure permits it.
  • Selective coating or contamination removal from coupons, development parts or approved non-critical surfaces.

Plan recurring tooling work through Maintenance Contracts with the customer’s engineering requirements and approval path. For inspector-defined areas, review inspection and NDT surface preparation.

Project Scope Factors

Scope factorInformation needed
Engineering authorityDrawing, process specification, repair authority and written approval for the trial.
MaterialAlloy, coating, heat treatment, surface finish and dimensional limits.
Process evidenceTest coupon, parameter record, before-and-after inspection and acceptance criteria.
Contamination controlResidue identity, extraction, clean-area requirements and foreign-object controls.
Quality recordsOperator, equipment, date, settings, test location and inspection result.

Production rate should be established only after the approved test demonstrates the required endpoint without unacceptable change. Submit the non-sensitive project information through the project review form; do not upload export-controlled, classified or otherwise restricted technical data through the public website.

For laser work-area planning, see OSHA laser hazard standards. Review site conditions and the agreed controls before scheduling.