New Tech Global is currently seeking a Senior Gas Turbine Combustion Engineer for a direct hire opportunity in Houston, Texas.
Overview
The Senior Gas Turbine Combustion Engineer is responsible for the design, development, analysis, and optimization of gas turbine combustion systems. This role requires advanced expertise in combustion engineering, combustor hardware design, combustion performance evaluation, emissions mitigation, and thermodynamic analysis. The successful candidate will provide technical leadership across cross-functional engineering teams and support combustion system performance throughout the product lifecycle.
Responsibilities:
Lead the design, development, and modification of gas turbine combustor components including liners, transition pieces, fuel nozzles, swirlers, cooling schemes, and fuel delivery hardware.
Perform advanced combustion analysis including flame stability, emissions (NOx/CO), temperature profile management, pressure oscillations, and combustion dynamics.
Evaluate and optimize combustion system performance for reliability, durability, emissions compliance, operability, and fuel flexibility.
Conduct root cause analysis of combustion hardware failures, performance degradation, and operational issues.
Review engineering documentation including 3D models, detailed drawings, CFD simulations, thermal analyses, and material specifications.
Work closely with mechanical, thermal, materials, and controls engineering teams.
Support validation testing including rig tests, engine tests, and field validation programs.
Provide technical guidance to manufacturing, supply chain, quality, and field service teams.
Participate in design reviews, risk assessments, and reliability evaluations.
Collaborate with customers, field engineers, and service teams to support aftermarket solutions.
Mentor junior engineers and contribute to internal technical development initiatives.
Qualifications
Bachelor's degree in Mechanical Engineering, Aerospace Engineering, or related discipline.
Senior-level experience in gas turbine combustion design and development.
Strong understanding of combustion fundamentals, thermodynamics, heat transfer, fluid mechanics, and gas turbine performance.
Proficiency with combustion modeling tools, CFD analysis, thermal simulations, finite element analysis, and engineering software.
Experience with combustor hardware development, testing, validation, and problem resolution.
Strong analytical, diagnostic, and communication skills.
Master's degree preferred.
Direct experience with GE Frame 6B (6B) gas turbine combustion systems highly preferred.
Experience with Dry Low Emissions (DLE/DLN) combustion technologies preferred.
Familiarity with gas turbine materials, coatings, cooling technologies, and manufacturing processes preferred.
Experience with fuel flexibility studies including natural gas, liquid fuels, and hydrogen blends preferred.
Experience supporting rig testing, engine test campaigns, and field validation programs preferred.