Integrated component repair for industrial, aeroderivative and aviation gas turbines. The portfolio combines inspection, powder-metallurgy rebuilding, alloy rejuvenation, coatings and welding; laser blade-tip repair has a separate published materials evidence base. The appropriate route depends on damage, substrate and approved repair scope.
Technical detail
Core features
Blade, vane, nozzle and hot-section repair
LPM rebuilding of missing material
FSR alloy rejuvenation
Protective coatings
Laser blade-tip restoration
Turbine repair
Component restoration
Materials engineering
Use & integration
Recorded applications
Component repair-versus-replacement assessment
Propulsion and power-generation sustainment
These describe the reviewed application scope, not confirmed deployments, released requirements or procurement eligibility.
Evidence of maturity
Industrial delivery is documented in the NCEMC FT8-3 nozzle case, attributed to Mooresville. Specific laser materials are supported by published testing and reported practice; no universal fleet qualification is inferred.
Commercial availability
Current company repair offering. Contracting entity, executing site, part eligibility and acceptance package must be agreed for the work.
Integration and verification
Readiness
A technology readiness level is not established by the reviewed public sources.
Reviewed connections
No reviewed Mission area or released Defence need connection is currently published.
Original sources 8 linked records
These records support this capability and its published Mission area and Defence need connections. A source count is not a count of independent confirmations.
Critical-component repair This bounded statement is retained for reviewer verification.
Supports: Capability · core features
Coatings and welding This bounded statement is retained for reviewer verification.
Supports: Capability · commercial availability
Liburdi Turbine Services currently presents Gas-turbine repair and additive restoration through its official public capability surface.
Supports: Capability · defence applications
Gas-turbine sustainment This bounded statement is retained for reviewer verification.
Supports: Capability · core features
Directed-energy deposition This bounded statement is retained for reviewer verification.
Supports: Capability · technical tags
True North Map applies the hot section tag from Liburdi Turbine Services's documented capability functions.
Supports: Capability · technicaldomainslugs
True North Map maps Gas-turbine repair and additive restoration to test training and sustainment from its documented technology functions.
Supports: Capability · summary
Liburdi provides hot-section repair, coatings, directed-energy-deposition restoration, welding, non-destructive testing, heat treatment and brazing for gas-turbine components.
Supports: Capability · core features
Hot-section repair This bounded statement is retained for reviewer verification.
Supports: Capability · core features
LPM uses engineered nickel/cobalt superalloy deposits to rebuild missing material and damaged blade tips, airfoils, vanes and nozzles. Liburdi describes putty or tape placement and metallurgical bonding without melting the base metal; it is distinct from laser directed-energy deposition.
Supports: Capability · core features
NDT, heat treatment and brazing
Supports: Capability · defence applications
Propulsion life extension This bounded statement is retained for reviewer verification.
Supports: Capability · summary
LPM uses engineered nickel/cobalt superalloy deposits to rebuild missing material and damaged blade tips, airfoils, vanes and nozzles. Liburdi describes putty or tape placement and metallurgical bonding without melting the base metal; it is distinct from laser directed-energy deposition.
Supports: Capability · technical tags
True North Map applies the directed energy deposition tag from Liburdi Turbine Services's documented capability functions.
Supports: Capability · technical tags
True North Map applies the turbine repair tag from Liburdi Turbine Services's documented capability functions.
Supports: Capability · capability type
Propulsion-component repair and advanced restoration
Aerospace Industries Association of Canada's public evidence confirms a company-specific project, award, program or operating context, while configuration-specific acceptance and scale remain bounded by the reviewer warning.
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · commercial availability
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · defence applications
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Liburdi Turbine Services Inc. Dundas co-authors with McGill and University of Toronto studied a Rene 142–MERL 72 powder blend on Haynes 230 using a Liburdi LAWS1000 laser system. Tests found higher tensile/creep performance than Rene 80 with lower elevated-temperature elongation; authors report practising squealer-tip, tip-cap and full-tip repairs at Liburdi. This is not a fleet approval or current commercial qualification list. The paper acknowledges NSERC CRDPJ 539429-19 research support, with no company funding amount.
Supports: Capability · summary
Liburdi Turbine Services Inc. Dundas co-authors with McGill and University of Toronto studied a Rene 142–MERL 72 powder blend on Haynes 230 using a Liburdi LAWS1000 laser system. Tests found higher tensile/creep performance than Rene 80 with lower elevated-temperature elongation; authors report practising squealer-tip, tip-cap and full-tip repairs at Liburdi. This is not a fleet approval or current commercial qualification list. The paper acknowledges NSERC CRDPJ 539429-19 research support, with no company funding amount.
Liburdi describes CT fan-beam X-ray inspection using a linear diode array for internal turbine-blade geometry, wall thinning and defects missed between discrete ultrasonic thickness points; it illustrates a 501-K34 blade. This supports repair disposition, not unlimited resolution or automatic acceptance.
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · capability type
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · technology readiness level
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · technical tags
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · technical tags
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · summary
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · technical tags
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · name
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · defence applications
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · technicaldomainslugs
Liburdi offers blade, vane, nozzle, combustor and hot-section repairs for industrial, aeroderivative and flight-aero gas turbines; its public examples include SGT-A35/RB211, LM2500, LM6000 and PW2000.
Supports: Capability · maturity
Liburdi Turbine Services Inc. Dundas co-authors with McGill and University of Toronto studied a Rene 142–MERL 72 powder blend on Haynes 230 using a Liburdi LAWS1000 laser system. Tests found higher tensile/creep performance than Rene 80 with lower elevated-temperature elongation; authors report practising squealer-tip, tip-cap and full-tip repairs at Liburdi. This is not a fleet approval or current commercial qualification list. The paper acknowledges NSERC CRDPJ 539429-19 research support, with no company funding amount.
FSR uses alloy-specific heat treatments to restore degraded turbine-blade microstructure, with HIP used to close creep cavities. Liburdi states batches are checked metallographically and mechanically, including ASTM E139 stress-rupture testing. It reports more than 500,000 blades treated and commonly two to three additional intervals; outcomes depend on alloy and condition.
Supports: Capability · summary
FSR uses alloy-specific heat treatments to restore degraded turbine-blade microstructure, with HIP used to close creep cavities. Liburdi states batches are checked metallographically and mechanically, including ASTM E139 stress-rupture testing. It reports more than 500,000 blades treated and commonly two to three additional intervals; outcomes depend on alloy and condition.
The NCEMC Anson and Hamlet operator case identifies Liburdi Turbine Services in Mooresville as repair provider, with sister company Dimetrics building a startup simulator. New, service-run and repaired nozzles were tested; pressure and fluorescent penetrant checks followed 250 cycles. NCEMC installed repaired nozzles and reported normal operation. It covers 24 FT8-3 engines and does not establish Canadian delivery.
Liburdi offers LSR aluminide diffusion coatings, APS/HVOF thermal and environmental protection, and RIC compressor erosion-resistant ceramic coatings. LSR internal/external application depends on alloy, furnace size and heat-treatment compatibility; RIC stripping from titanium is not recommended on the company page.
Supports: Capability · summary
Liburdi offers LSR aluminide diffusion coatings, APS/HVOF thermal and environmental protection, and RIC compressor erosion-resistant ceramic coatings. LSR internal/external application depends on alloy, furnace size and heat-treatment compatibility; RIC stripping from titanium is not recommended on the company page.
