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Gas Turbines with special emphasis on hydrogen combustion

Gas Turbines with special emphasis on hydrogen combustion banner
Preview this course
Self-paced Beginner

Gas Turbines with special emphasis on hydrogen combustion

4(1581)
100 enrolled
2696 views
₹ 199
72 min
Anytime
English
2696 views
Team EveryEng
Team EveryEngMechanical Engineering
  • 7-day money-back guarantee
  • Lifetime access
  • Certificate of completion
Volume pricing for groups of 5+

Why enroll

Expertise in gas turbines with hydrogen combustion can ignite your career in the energy and power generation sectors. You'll be in high demand as a Turbine Engineer, Power Plant Manager, or Energy Consultant, with opportunities to work on cutting-edge projects and contribute to the transition to clean energy. This specialized knowledge will position you for leadership roles, research and development initiatives, and entrepreneurial ventures in the emerging hydrogen economy.

What enrolled engineers say

5 verified reviews
  • Feb 25, 2026

    Initially, I wasn’t sure what to expect from this course. From a senior engineer perspective, the material sits firmly at a beginner level, but it does a decent job laying out the fundamentals behind gas turbine operation and hydrogen combustion. The breakdown of the Brayton cycle and ISO site rating was useful, especially when compared against how turbines are actually derated in oil & gas applications like LNG compression or offshore power generation. The discussion on NOx correlations and adiabatic flame temperature tied in well with real constraints seen in chemical and pharmaceutical utility plants, where emissions limits and permit margins can be tight. One challenge was the limited treatment of edge cases—hydrogen-rich fuels at part load and transient operation were mentioned, but not deeply analyzed, which is often where problems show up in practice. Burner technology comparisons (lean vs fuel-rich) were solid, though more contrast with current dry low NOx systems used in industry would help. A practical takeaway was the structured way to think about ambient conditions, inlet losses, and exhaust impacts when estimating real turbine output. That framework maps directly to early project screening. I can see this being useful in long-term project work.

    Araz J. Verified
  • Feb 25, 2026

    At first glance, the topics looked familiar, but the depth surprised me. Coming from oil & gas projects, gas turbines and the Brayton cycle weren’t new, yet the way site rating and ISO corrections were broken down filled a real gap. Ambient temperature and inlet losses are things usually handled by vendors, so it was useful to finally understand what’s behind those correction curves. The section on NOx emissions and correlations was especially relevant. On a recent brownfield upgrade, emission limits were the main constraint, and the discussion around lean combustion versus fuel‑rich burners helped connect combustion theory to what actually ends up in the stack. Hydrogen combustion was another eye-opener. Flame speed, adiabatic flame temperature, and flashback risks were explained clearly, but the challenge was mentally translating that to existing turbine hardware that was never designed for hydrogen-rich fuels. One practical takeaway was being able to sanity-check OEM performance guarantees and emission numbers instead of taking them at face value. That’s already helped during internal design reviews. Overall, it felt grounded in real engineering practice.

    Abhishek K. Verified
  • Feb 25, 2026

    This course turned out to be more technical than I anticipated. For a beginner label, it went reasonably deep into Brayton cycle behavior and how site rating shifts with ambient temperature and inlet losses, which is very relevant in oil & gas cogeneration projects. The section on NOx correlations and lean vs. fuel‑rich burners lined up with what’s typically seen in refinery gas turbines, although it was useful to see the theory spelled out instead of just relying on OEM curves. One challenge was reconciling the simplified NOx models with real hydrogen combustion edge cases. In practice, once hydrogen content climbs, flashback risk and adiabatic flame temperature effects make those correlations less reliable, something the course only briefly flagged. Still, the discussion helped frame why dry low NOx systems struggle with hydrogen-rich fuels and why SCR is still common in industry. A practical takeaway was how to think about ISO ratings versus actual site conditions. That’s directly applicable when reviewing performance guarantees or doing early feasibility for a turbine package. Some parallels with chemical/pharmaceutical thermal oxidizers also came through, especially around emissions control philosophy. The content felt aligned with practical engineering demands.

    Omkar Z. · Project Manager Verified

Is this course for you?

You should take this if

  • You work in Steam & Gas Turbines or Renewable & New Energy
  • You're a Mechanical Engineering / Power Plant Engineering professional
  • You prefer self-paced learning you can revisit

You should skip if

  • You need a different specialisation outside Mechanical Engineering
  • You need live interaction with an instructor

Course details

This course provides a comprehensive introduction to gas turbines and their working principles. It begins by explaining the different types of gas turbines, including industrial heavy-duty and aeroderivative turbines, and how they are used in power generation and industrial applications. Participants will learn about the Brayton Cycle, which forms the basic thermodynamic cycle for gas turbine operation. The course also explains the concept of site rating of gas turbines based on ISO rating and how environmental factors such as ambient temperature, barometric pressure, inlet losses, and outlet losses affect turbine performance. In addition, the course discusses exhaust gases produced by gas turbines and focuses on the formation and control of NOx emissions. Learners will explore various burner technologies used in turbines, including lean and fuel-rich combustion methods. The concept of adiabatic flame temperature and its importance in combustion will also be covered. Special attention is given to hydrogen combustion and the use of hydrogen-rich fuels, which are gaining importance due to their low carbon footprint. Finally, the course introduces new and advanced burner technologies designed to improve efficiency and reduce emissions in modern gas turbine systems.

Course suitable for

Key topics covered

  • Gas Turbine Introduction

  • Type of Gas Turbines

  • Gas Turbine Thermodynamic Cycle

  • Gas Turbine Performance

  • Emissions of Gas Turbines

  • NOx emissions from gas turbines

  • Factors influencing NOx emissions

  • NOx formation correlations for gas turbines

  • NOx formation for hydrogen-rich gases in turbines

  • NOx reduction methods for gas turbines

  • Gas Turbine combustion technologies

  • Advances in Burner Technology for 100% hydrogen combustion

Course content

The course is readily available, allowing learners to start and complete it at their own pace.

6 lectures1 hr 12 min
  1. Introduction
    5 min
  2. Turbine classifications
    5 min
  3. Gas turbine thermodynamic cycle
    13 min
  4. Performance of gas turbines
    15 min
  5. Factor influencing
    19 min
  6. Combustion Technology
    15 min

Opportunities that await you!

Career opportunities

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Questions and Answers

A: That's the most common mistake — assuming flame arrestors address temperature-driven ignition. They stop a flame front by quenching; they don't change metal skin temperatures or local residence time. Autoignition in hydrogen blends is a thermal problem tied to liner cooling and equivalence ratio excursions, not a flame speed issue. The other cases are exactly why arrestors get specified around premix hardware and skids.

A: You're mixing protection mechanisms. The zoning standard is worried about flammable atmospheres forming at all, not heat removal or exhaust toxicity. Hydrogen's buoyancy and wide flammability range drive the air change logic so a small leak doesn't sit above LFL long enough to find an ignition source. Surface temperature control is handled elsewhere.

A: You're assuming the issue is valve type. It's not. The drawing tells you where leaked gas goes, and hydrogen behaves nothing like NG once released. Permeation and jet velocity make a shared NG vent a bad idea even if MAWP looks fine on paper. The other points either overreach or misread what the P&ID actually implies.

A: That's the trap — looking only at one operating point. Flashback margin is the ratio, and hydrogen eats that margin quickly as you turndown or get boundary layer slowing near walls. Saying 25 is bigger than 2.5 misses how little headroom you actually have compared to methane. Pressure matters, sure, but velocity gradients are the trigger here.