Liburdi Turbine Services is a Dundas, Ontario gas-turbine component repair and materials-engineering business. It restores blades, vanes, nozzles and other hot-section components through powder-metallurgy rebuilding, alloy rejuvenation, protective coatings, inspection and welding. Its published technical work includes laser-deposited superalloy blade-tip repairs. The Canadian company is wholly owned by Liburdi Engineering Limited; the turbine-services business also operates from Mooresville, North Carolina.
Operating context
Liburdi’s practical entry point is a damaged or life-limited turbine component and its operating history. Inspection helps determine whether material loss, cracks or internal wall thinning permit repair; LPM rebuilds lost geometry, FSR addresses alloy degradation, and coatings restore protection. Buyers are turbine owners, overhaul organizations and engineering teams comparing repair, replacement and remaining service life. The NCEMC FT8-3 case addresses startup thermal-shock cracking and fuel crossflow: Liburdi and Dimetrics tested new, service-run and repaired nozzles before the operator installed repaired units. Combined Cycle Journal identifies Mooresville as the provider. A later FT8 user-group report quotes repair costs around 25–30% of replacement and use of new/repaired nozzles in 16 of 24 engines at an unnamed site; these are reported case economics, not a standard quote. Canadian work scope should be specified separately from US delivery.
Canadian footprint
The Canadian turbine-services facility is at 400 Highway 6 North, Dundas, Ontario. Liburdi dates the business to 1979. Its 2026 statutory report identifies Liburdi Engineering Limited as the Ontario parent of Liburdi Turbine Services Inc. and Dimetrics. The reported workforce of more than 375 in Canada is group-wide and is not a turbine-services headcount. Dundas-affiliated authors co-authored a 2021 laser blade-tip repair paper with McGill and University of Toronto researchers; the paper acknowledges NSERC project CRDPJ 539429-19 without disclosing a company funding amount.
Dundas, Ontario is the published city-level context for Liburdi Turbine Services. It does not imply a street address or exact facility location.
Liburdi Turbine Services merits assessment when a turbine owner or sustainment team needs to determine whether high-value components can be restored rather than replaced. Its combination of geometry rebuilding, alloy rejuvenation, coatings and inspection is backed by specific industrial cases and Canadian laser-repair research. The next useful conversation should start with a part, damage history and acceptance requirement, then establish which Canadian or US entity will execute and release the repair.
Interpretation of the public record. Not qualification, endorsement or evidence of buyer interest.
Liburdi describes fan-beam X-ray CT with a linear diode array to reconstruct internal blade geometry and identify wall thinning between discrete ultrasonic measurement points. Its technical example uses a 501-K34 blade and supports informed repair disposition.
Evidence of maturity
Company technical example demonstrates the inspection approach on a 501-K34 blade; public detection limits and part-specific acceptance thresholds are not provided.
Commercial availability
Presented as an advanced inspection method; confirm available geometry, resolution and inspection acceptance for the part.
FSR addresses turbine-blade alloy degradation through alloy-specific heat treatment, with hot isostatic pressing used to close creep cavities. Liburdi describes metallographic and mechanical verification, including stress-rupture testing, to support further service.
Evidence of maturity
Liburdi reports treating more than 500,000 blades and commonly obtaining two to three additional intervals. These are company-reported aggregate outcomes, not guarantees for an individual blade.
Commercial availability
Commercially presented rejuvenation process, dependent on alloy, condition and agreed acceptance criteria.
Core features
Alloy-specific restoration of degraded microstructure
Hot isostatic pressing for creep cavities
Batch metallographic and mechanical checks
ASTM E139 stress-rupture testing
Recorded applications
Life-extension assessment for service-exposed blades
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.
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.
Liburdi researchers with McGill and University of Toronto studied laser deposition of a Rene 142–MERL 72 superalloy blend using the Liburdi LAWS1000 system. The 2021 paper reports practising squealer-tip, tip-cap and full-tip repair at Liburdi and compares deposited material with conventional repair alloys.
Evidence of maturity
Peer-reviewed 2021 material testing and reported repair practice. Tensile/creep performance exceeded Rene 80 under studied conditions, with lower elevated-temperature elongation. Component interfaces and broader creep studies remained follow-up work.
Commercial availability
Published repair practice establishes more than a concept; the paper does not identify a current fleet-qualified parts list or general delivery approval.
Core features
Laser directed-energy deposition with coaxial powder delivery
Published testing on Haynes 230 substrates
Tensile, stress-rupture and cyclic oxidation characterization
Reported squealer-tip, tip-cap and full-tip repair practice
Recorded applications
Turbine blade-tip restoration
Qualification of repair materials for hot-section components
Liburdi Powder Metallurgy rebuilds lost material in nickel- and cobalt-superalloy turbine components. Putty or tape deposits bond without melting the base metal, addressing cracks, airfoil loss and blade-tip or vane geometry. It is distinct from laser directed-energy deposition.
Evidence of maturity
Liburdi reports intact SGT-A35/RB211 nozzle-guide-vane reconstruction after 24,281 service hours and USD 374,000 savings versus replacement. The operator is unnamed and the outcome is case-specific.
Commercial availability
Offered as a repair service; material compatibility and approved work scope determine applicability.
Core features
Engineered superalloy deposits applied as putty or tape
Rebuilding of blade tips, airfoils, vanes and nozzles
Liburdi’s coating portfolio covers LSR aluminide diffusion protection, APS/HVOF thermal and environmental coatings, and RIC ceramic erosion protection for compressor parts. Selection depends on substrate, exposure and the repair route.
Evidence of maturity
Company technical descriptions establish the offered coating families and process constraints; coating acceptance remains application-specific.
Commercial availability
Offered in the turbine repair portfolio; substrate compatibility and stripping/recoating limits must be specified.
Core features
LSR internal and external diffusion-coating options
APS and HVOF coating processes
RIC compressor erosion protection
LSR depends on alloy, furnace and heat-treatment compatibility
On September 14, 2026, AP4 announced a partnership between Hughes Technical Services and Liburdi Turbine Services combining HTS field services, controls, parts and commissioning with Liburdi hot-gas-path repair. The partners plan additional shop capacity, field support and dedicated engineering associated with Mooresville, North Carolina. No investment value is disclosed, and the announcement does not quantify added Canadian capacity.
Commercial component-repair services with documented industrial operating cases. A 2023 Combined Cycle Journal case reports NCEMC installing repaired FT8-3 nozzles supplied by the Mooresville operation. Laser-alloy research supplies additional technical evidence, with acceptance still specific to part and application.
Ownership and entity scope
Wholly owned by Ontario-incorporated Liburdi Engineering Limited, according to the group’s 2026 statutory supply-chain report.
Ecosystem relationships
Turbine repair and field-service partnership
Hughes Technical Services
AP4’s September 14, 2026 announcement combines HTS field services and commissioning with Liburdi hot-gas-path repair, supported by planned shop, field-service and engineering investment associated with Mooresville, North Carolina. The value is not disclosed.
Questions for a first conversation
01
Which current approvals and repair specifications cover the proposed part, process and repair site?
Transport Canada AMO 42-08 has manual-defined ratings. The linked AS9100 certificate expired June 30, 2025 and the Siemens SGT-A20/SGT-A35 authority expired December 20, 2023; obtain current documents rather than infer present status from these copies.
02
For the proposed alloy and damage condition, what inspection, restoration route and post-repair test determine the next service interval?
LPM rebuilds lost geometry, while FSR addresses degraded microstructure. Liburdi’s SGT-A35/RB211 case reports 24,281 service hours after LPM repair, but that result does not define acceptance or remaining life for a different component.
03
Which legal entity will contract and release the work, and which operations will take place in Dundas versus Mooresville?
The Canadian subsidiary is owned by Liburdi Engineering Limited, while the original NCEMC repair case identifies Mooresville. US military references name the US LLC; group qualifications must be checked against the delivering division.
04
Which blade-tip configurations now use the published laser-deposited alloy, and what component-level qualification supports delivery?
The 2021 paper reports practical tip repairs at Liburdi and material tests, with lower elevated-temperature elongation than Rene 80. It leaves more comprehensive creep and interface studies to future work and provides no fleet-qualified parts list.
Original sources 19 linked records
These records support the organization, its owned capabilities and their reviewed connections. A source count is not a count of independent confirmations.
True North Map derives a first-conversation question about Gas-turbine repair and additive restoration configuration and accepted outcomes from the documented maturity boundary.
Supports: Profile · defence posture
The service can support defence propulsion sustainment, but public evidence does not identify a deep-strike engine, current defence contract or accepted repair configuration.
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Liburdi may help teams evaluate Canadian options for turbine-component repair and life extension. A useful next conversation would establish approved part families, process qualifications, turnaround capacity and independently accepted defence or aerospace repairs for the intended engine.
Supports: Profile · organization categories
True North Map applies the commercial company category to Liburdi Turbine Services from its documented mandate and source-bounded operating evidence.
Supports: Profile · dual use posture
Gas-turbine repair and additive restoration has documented civilian or industrial applications and a bounded potential relevance to Canadian defence, security or strategic-infrastructure needs.
Public sources do not establish a deep-strike engine program, approved part list, current defence customer, available capacity or configuration-specific repair acceptance. The first conversation should therefore separate current offer, development evidence and accepted operational use.
Supports: Profile · description
True North Map derives this executive description for Liburdi Turbine Services from the official identity and technical records together with Aerospace Industries Association of Canada's corroborating evidence.
Supports: Profile · canadian footprint
Liburdi and AIAC identify a Dundas, Ontario operating base and Canadian turbine-services role.
Supports: Profile · organization categories
True North Map applies the dual use category to Liburdi Turbine Services from its documented mandate and source-bounded operating evidence.
Supports: Gas-turbine repair and additive restoration · maturity
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 reports an SGT-A35/RB211 nozzle-guide-vane repair using LPM, machining and recoating: after 24,281 service hours the reconstruction was intact and ready for a second interval, with USD 374,000 claimed savings versus replacement. The operator is unnamed.
Liburdi reports an SGT-A35/RB211 nozzle-guide-vane repair using LPM, machining and recoating: after 24,281 service hours the reconstruction was intact and ready for a second interval, with USD 374,000 claimed savings versus replacement. The operator is unnamed.
Liburdi reports an SGT-A35/RB211 nozzle-guide-vane repair using LPM, machining and recoating: after 24,281 service hours the reconstruction was intact and ready for a second interval, with USD 374,000 claimed savings versus replacement. The operator is unnamed.
Liburdi reports an SGT-A35/RB211 nozzle-guide-vane repair using LPM, machining and recoating: after 24,281 service hours the reconstruction was intact and ready for a second interval, with USD 374,000 claimed savings versus replacement. The operator is unnamed.
Liburdi reports an SGT-A35/RB211 nozzle-guide-vane repair using LPM, machining and recoating: after 24,281 service hours the reconstruction was intact and ready for a second interval, with USD 374,000 claimed savings versus replacement. The operator is unnamed.
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: Profile · website url
https://www.liburditurbineservices.com/ is the canonical official website used by Liburdi Turbine Services.
Liburdi Turbine Services publishes Ontario as its Canadian province or territory.
Supports: Profile · dual use posture
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: Profile · name
Liburdi Turbine Services is the public name used by the organization's official website.
Supports: Profile · entity kind
True North Map classifies Liburdi Turbine Services as a company from its documented legal or institutional role.
Supports: Profile · commercial status
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: Profile · description
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: Profile · primary location.longitude
True North Map uses the Dundas city centroid longitude -79.9566 for a city-level map location.
Supports: Profile · aliases
Liburdi is a documented operating, former or alternate name for Liburdi Turbine Services.
Supports: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · core features
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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · 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.
Bureau Veritas certificate US017135 names Liburdi Engineering Ltd and Liburdi Turbine Services Inc., 400 Highway 6 North, Dundas. Its repair, manufacture and coating scope was certified under ISO 9001:2015 and AS9100D; issue July 1, 2022 and expiry June 30, 2025. This copy does not establish current certification.
Bureau Veritas certificate US017135 names Liburdi Engineering Ltd and Liburdi Turbine Services Inc., 400 Highway 6 North, Dundas. Its repair, manufacture and coating scope was certified under ISO 9001:2015 and AS9100D; issue July 1, 2022 and expiry June 30, 2025. This copy does not establish current certification.
Bureau Veritas certificate US017135 names Liburdi Engineering Ltd and Liburdi Turbine Services Inc., 400 Highway 6 North, Dundas. Its repair, manufacture and coating scope was certified under ISO 9001:2015 and AS9100D; issue July 1, 2022 and expiry June 30, 2025. This copy does not establish current certification.
Bureau Veritas certificate US017135 names Liburdi Engineering Ltd and Liburdi Turbine Services Inc., 400 Highway 6 North, Dundas. Its repair, manufacture and coating scope was certified under ISO 9001:2015 and AS9100D; issue July 1, 2022 and expiry June 30, 2025. This copy does not establish current certification.
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Supports: Profile · canadian footprint
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Supports: Profile · ownership
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
Liburdi Engineering Limited is incorporated in Ontario and wholly owns Liburdi Turbine Services Inc. and Liburdi Dimetrics Corporation. The 2026 report states over 375 employees in Canada for the group, not Turbine Services alone.
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.
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.
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: Profile · operating context
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.
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: Profile · profileData.portfolioScope
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.
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: Full Solution Rejuvenation · name
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: Full Solution Rejuvenation · technical tags
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: Full Solution Rejuvenation · core features
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: Full Solution Rejuvenation · core features
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: Full Solution Rejuvenation · commercial availability
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: Full Solution Rejuvenation · defence applications
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: Full Solution Rejuvenation · technical tags
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: Full Solution Rejuvenation · 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.
Supports: Full Solution Rejuvenation · slug
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: Full Solution Rejuvenation · core features
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: Full Solution Rejuvenation · technical tags
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: Full Solution Rejuvenation · maturity
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: Full Solution Rejuvenation · technology readiness level
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: Full Solution Rejuvenation · technicaldomainslugs
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: Full Solution Rejuvenation · capability type
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: Full Solution Rejuvenation · core features
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: Full Solution Rejuvenation · defence applications
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: Full Solution Rejuvenation · technicaldomainslugs
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: Gas-turbine repair and additive restoration · core features
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: Gas-turbine repair and additive restoration · 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.
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
Supports: Profile · description
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
Liburdi states Joseph Liburdi founded the turbine-services business in 1979. Its listed Canadian facility is 400 Highway 6 North, Dundas, Ontario, and its US facility is in Mooresville, North Carolina. The Dundas phone is +1-905-689-0734.
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.
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.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
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.
Supports: Profile · dual use posture
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.
Supports: Profile · operating context
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.
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.
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.
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.
Supports: Gas-turbine repair and additive restoration · maturity
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.
The capability statement identifies Liburdi Turbine Services LLC in Mooresville, North Carolina, CAGE 6KEA8, and lists US Navy and Air Force among past-performance references. Those references belong to the US entity and cannot establish Canadian Inc. contracts or workshare.
The capability statement identifies Liburdi Turbine Services LLC in Mooresville, North Carolina, CAGE 6KEA8, and lists US Navy and Air Force among past-performance references. Those references belong to the US entity and cannot establish Canadian Inc. contracts or workshare.
The capability statement identifies Liburdi Turbine Services LLC in Mooresville, North Carolina, CAGE 6KEA8, and lists US Navy and Air Force among past-performance references. Those references belong to the US entity and cannot establish Canadian Inc. contracts or workshare.
Supports: Profile · defence posture
The capability statement identifies Liburdi Turbine Services LLC in Mooresville, North Carolina, CAGE 6KEA8, and lists US Navy and Air Force among past-performance references. Those references belong to the US entity and cannot establish Canadian Inc. contracts or workshare.
The capability statement identifies Liburdi Turbine Services LLC in Mooresville, North Carolina, CAGE 6KEA8, and lists US Navy and Air Force among past-performance references. Those references belong to the US entity and cannot establish Canadian Inc. contracts or workshare.
Liburdi Group distinguishes Engineering, Turbine Repair Services, Automation and Dimetrics. Its group-level list of certifications explicitly instructs readers to ask the relevant division which qualifications apply. This does not establish all listed qualifications for every repair site or process.
Supports: Profile · profileData.portfolioScope
Liburdi Group distinguishes Engineering, Turbine Repair Services, Automation and Dimetrics. Its group-level list of certifications explicitly instructs readers to ask the relevant division which qualifications apply. This does not establish all listed qualifications for every repair site or process.
Liburdi Group distinguishes Engineering, Turbine Repair Services, Automation and Dimetrics. Its group-level list of certifications explicitly instructs readers to ask the relevant division which qualifications apply. This does not establish all listed qualifications for every repair site or process.
Liburdi Group distinguishes Engineering, Turbine Repair Services, Automation and Dimetrics. Its group-level list of certifications explicitly instructs readers to ask the relevant division which qualifications apply. This does not establish all listed qualifications for every repair site or process.
Liburdi Group distinguishes Engineering, Turbine Repair Services, Automation and Dimetrics. Its group-level list of certifications explicitly instructs readers to ask the relevant division which qualifications apply. This does not establish all listed qualifications for every repair site or process.
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 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: Profile · commercial status
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 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: Profile · profileData.portfolioScope
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 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: Profile · description
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: Profile · canadian footprint
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 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: Gas-turbine repair and additive restoration · core features
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: Gas-turbine repair and additive restoration · 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.
Supports: Gas-turbine repair and additive restoration · 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.
Supports: Laser blade-tip restoration · core features
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 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: Laser blade-tip restoration · capability type
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: Laser blade-tip restoration · core features
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: Laser blade-tip restoration · core features
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: Laser blade-tip restoration · 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 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: Laser blade-tip restoration · name
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 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 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: Laser blade-tip restoration · slug
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 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 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: Laser blade-tip restoration · core features
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: Laser blade-tip restoration · 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.
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 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 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.
Supports: Profile · operating context
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.
Supports: Profile · executive relevance summary
Source location: executiveRelevanceSummary
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.
Supports: CT turbine-component inspection · capability type
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.
Supports: CT turbine-component inspection · name
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.
Supports: CT turbine-component inspection · core features
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 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 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.
Supports: CT turbine-component inspection · core features
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 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.
Supports: CT turbine-component inspection · core features
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 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 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 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 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 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 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 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.
Supports: CT turbine-component inspection · slug
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 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.
Supports: Gas-turbine repair and additive restoration · summary
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 Turbine Services publishes info@liburditurbineservices.com, telephone 1-800-991-2100 and a contact form asking for equipment model and serial number at https://www.liburditurbineservices.com/contact.
Liburdi Turbine Services publishes info@liburditurbineservices.com, telephone 1-800-991-2100 and a contact form asking for equipment model and serial number at https://www.liburditurbineservices.com/contact.
Liburdi Turbine Services publishes info@liburditurbineservices.com, telephone 1-800-991-2100 and a contact form asking for equipment model and serial number at https://www.liburditurbineservices.com/contact.
Liburdi Turbine Services publishes info@liburditurbineservices.com, telephone 1-800-991-2100 and a contact form asking for equipment model and serial number at https://www.liburditurbineservices.com/contact.
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: Profile · commercial status
Liburdi publicly offers turbine-component repair and restoration services from its Canadian operation.
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: Profile · profileData.portfolioScope
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: Profile · executive relevance summary
Source location: executiveRelevanceSummary
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.
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: Profile · operating context
Liburdi provides specialized sustainment and component-restoration capability rather than manufacturing complete engines.
Supports: Profile · profileData.portfolioScope
Liburdi Turbine Services's documented portfolio in this dossier is bounded to Gas-turbine repair and additive restoration and the source-backed functions listed below.
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.
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: Gas-turbine repair and additive restoration · defence applications
Critical-component repair This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · core features
Coatings and welding This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · commercial availability
Liburdi Turbine Services currently presents Gas-turbine repair and additive restoration through its official public capability surface.
Supports: Gas-turbine repair and additive restoration · defence applications
Gas-turbine sustainment This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · core features
Directed-energy deposition This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · technical tags
True North Map applies the hot section tag from Liburdi Turbine Services's documented capability functions.
Supports: Gas-turbine repair and additive restoration · technicaldomainslugs
True North Map maps Gas-turbine repair and additive restoration to test training and sustainment from its documented technology functions.
Supports: Gas-turbine repair and additive restoration · summary
Liburdi provides hot-section repair, coatings, directed-energy-deposition restoration, welding, non-destructive testing, heat treatment and brazing for gas-turbine components.
Supports: Gas-turbine repair and additive restoration · core features
Hot-section repair This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · core features
NDT, heat treatment and brazing
Supports: Gas-turbine repair and additive restoration · defence applications
Propulsion life extension This bounded statement is retained for reviewer verification.
Supports: Gas-turbine repair and additive restoration · 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: Gas-turbine repair and additive restoration · technical tags
True North Map applies the directed energy deposition tag from Liburdi Turbine Services's documented capability functions.
Supports: Gas-turbine repair and additive restoration · technical tags
True North Map applies the turbine repair tag from Liburdi Turbine Services's documented capability functions.
Supports: Gas-turbine repair and additive restoration · capability type
Propulsion-component repair and advanced restoration
Supports: Gas-turbine repair and additive restoration · name
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.
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.
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.
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.
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: LPM powder-metallurgy restoration · name
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.
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.
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: LPM powder-metallurgy restoration · 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: LPM powder-metallurgy restoration · capability type
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.
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.
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.
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: LPM powder-metallurgy restoration · 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: LPM powder-metallurgy restoration · 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.
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.
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Supports: Profile · current activity as of
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Supports: Turbine repair and field-service partnership relationship
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Supports: Turbine repair and field-service partnership relationship
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Supports: Turbine repair and field-service partnership relationship
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Supports: Turbine repair and field-service partnership relationship
AP4 announced a strategic partnership between its Hughes Technical Services business and Liburdi Turbine Services on September 14, 2026. HTS contributes field services, controls, parts and commissioning, while Liburdi contributes hot-gas-path component repair. The partners plan investment in additional shop capacity, field support and dedicated engineering associated with the Mooresville, North Carolina operation. No financial value is disclosed.
Transport Canada AMO 42-08 names Liburdi Turbine Services Inc. in Dundas for components, NDT and welding. Ratings include engine hardware, liquid penetrant and radiographic inspection, arc and resistance welding, limited by its maintenance policy manual. The November 14, 2008 certificate remains valid until surrendered, suspended or cancelled; this historical document does not verify current registry status or authorize every advertised process.
Transport Canada AMO 42-08 names Liburdi Turbine Services Inc. in Dundas for components, NDT and welding. Ratings include engine hardware, liquid penetrant and radiographic inspection, arc and resistance welding, limited by its maintenance policy manual. The November 14, 2008 certificate remains valid until surrendered, suspended or cancelled; this historical document does not verify current registry status or authorize every advertised process.
Supports: Profile · dual use posture
Transport Canada AMO 42-08 names Liburdi Turbine Services Inc. in Dundas for components, NDT and welding. Ratings include engine hardware, liquid penetrant and radiographic inspection, arc and resistance welding, limited by its maintenance policy manual. The November 14, 2008 certificate remains valid until surrendered, suspended or cancelled; this historical document does not verify current registry status or authorize every advertised process.
Transport Canada AMO 42-08 names Liburdi Turbine Services Inc. in Dundas for components, NDT and welding. Ratings include engine hardware, liquid penetrant and radiographic inspection, arc and resistance welding, limited by its maintenance policy manual. The November 14, 2008 certificate remains valid until surrendered, suspended or cancelled; this historical document does not verify current registry status or authorize every advertised process.
Transport Canada AMO 42-08 names Liburdi Turbine Services Inc. in Dundas for components, NDT and welding. Ratings include engine hardware, liquid penetrant and radiographic inspection, arc and resistance welding, limited by its maintenance policy manual. The November 14, 2008 certificate remains valid until surrendered, suspended or cancelled; this historical document does not verify current registry status or authorize every advertised process.
Siemens issued Liburdi Turbine Services Inc. authority for industrial SGT-A20 (Avon) and SGT-A35 (RB211), all types subject to further listed scope, on December 20, 2018. This linked certificate expired December 20, 2023 and does not establish current authority.
Siemens issued Liburdi Turbine Services Inc. authority for industrial SGT-A20 (Avon) and SGT-A35 (RB211), all types subject to further listed scope, on December 20, 2018. This linked certificate expired December 20, 2023 and does not establish current authority.
Siemens issued Liburdi Turbine Services Inc. authority for industrial SGT-A20 (Avon) and SGT-A35 (RB211), all types subject to further listed scope, on December 20, 2018. This linked certificate expired December 20, 2023 and does not establish current authority.
Siemens issued Liburdi Turbine Services Inc. authority for industrial SGT-A20 (Avon) and SGT-A35 (RB211), all types subject to further listed scope, on December 20, 2018. This linked certificate expired December 20, 2023 and does not establish current authority.
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: Profile · executive relevance summary
Source location: executiveRelevanceSummary
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: Gas-turbine repair and additive restoration · core features
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: Gas-turbine repair and additive restoration · 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.
Supports: Protective turbine coatings · name
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.
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: Protective turbine coatings · 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.
Supports: Protective turbine coatings · core features
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: Protective turbine coatings · core features
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: Protective turbine coatings · core features
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.
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: Protective turbine coatings · core features
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.
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: Protective turbine coatings · slug
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: Protective turbine coatings · capability type
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.
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.
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.
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: Protective turbine coatings · core features
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: Protective turbine coatings · maturity
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.
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.
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.
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.
Combined Cycle Journal reports a 2024 FT8 Users Group presentation by Liburdi and a former plant manager describing nozzle repairs, typically 25-30 percent of replacement cost, and implementation of new and repaired nozzles in 16 of 24 engines at one unnamed site. These are presentation-reported results, not an audited fleet-wide cost guarantee.
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