Power Generation

Gas Turbine Power Plant

Check health score

Gas Turbine Performance: Compare Like With Like

A gas turbine compresses air, adds energy through combustion, and expands hot gas through the turbine. In combined heat and power service, exhaust heat can also supply a useful thermal demand.

Electrical efficiency and combined heat-and-power efficiency describe different outputs. Gross generator output and net site output are also different boundaries. State which one is being used.

Reference: DOE — Guide to Combined Heat and Power Systems for Boiler Owners and Operators.

Worked Example: Efficiency and Heat Rate

Illustrative example: these assumed values demonstrate arithmetic, not actual plant results or recommended operating targets.

Assume fuel input of 10 MW on an LHV basis and net electrical output of 3 MW.

  • Net electrical efficiency = 3 ÷ 10 × 100 = 30% LHV.
  • Net heat rate = 3,600 ÷ 0.30 = 12,000 kJ/kWh LHV.

For the same boundary and fuel basis, a lower heat rate means less fuel energy per unit of electricity.

If the same installation also delivers 4 MW of useful recovered heat, a simplified combined utilization is:

(3 + 4) ÷ 10 × 100 = 70%.

Only count useful heat delivered to a real demand. Heat that is merely available in the exhaust is not automatically useful output. Include additional fuel inputs if supplementary firing is used.

What Makes Comparisons Fair?

Record electrical load, ambient conditions, fuel-flow reference conditions, fuel heating value, auxiliary demand, and relevant inlet and exhaust data. Use the manufacturer's corrections when comparing performance under different conditions.

Keep Investigation Separate From Control Changes

A worsening trend warrants checking data quality, changed operating conditions, and maintenance history. It does not authorize changing combustion settings, protective limits, or turbine controls. These require the equipment-specific procedure and qualified personnel.

Next step: Build a net-output and fuel-energy trend with consistent boundaries before evaluating improvement projects.

Record observations only where it is safe. Inspection inside equipment, electrical testing, chemical work and changes to protective controls require qualified personnel, approved isolation and the installed equipment manual. Never bypass a trip or repeatedly restart unsafe equipment. Engineering disclaimer

Measurements To Record

  • Ambient temperature, pressure and inlet conditions
  • Fuel flow and heating-value basis
  • Electrical output, auxiliaries and heat rate
  • Vibration, exhaust-temperature distribution and trip history

Maintenance Checklist

  • Record inlet conditions, fuel flow and generation.
  • Trend vibration and exhaust-temperature distribution.
  • Maintain fuel and inlet-air filtration.
  • Use OEM start, shutdown and inspection intervals.

Evidence-Based Diagnosis

Output below baseline

Possible Causes
Ambient derating; inlet losses; compressor fouling; load limitation.
Evidence To Collect
Compare corrected performance or matched ambient/load conditions and inlet-filter pressure loss.
Qualified Follow-Up
Use OEM-supported performance assessment and approved inlet or compressor-maintenance procedures.

High vibration alarm

Possible Causes
Sensor issue; mechanical condition; operating disturbance.
Evidence To Collect
Preserve alarm and trend data and follow the operating response for the specific machine.
Qualified Follow-Up
Escalate to qualified turbine personnel. Do not restart after a protective trip without the required clearance.

High heat rate

Possible Causes
Reduced efficiency; low load; changed fuel basis; auxiliary consumption.
Evidence To Collect
Validate metering and heating-value units and compare at similar load and ambient conditions.
Qualified Follow-Up
Investigate inlet, compressor, combustion and auxiliary performance with the specialist team.

Record The Confirmed Result

Keep the asset model, time, load, ambient conditions, alarm code and relevant readings together. Compare with the last healthy baseline. Record the confirmed cause, approved corrective action and readings after restoration; check that the improvement persists before closing the investigation.

Related Guides And Utilities

Problem Solving Videos

How A Gas Turbine Works (GE Vernova)
Watch on YouTube
How A Combined-Cycle Power Plant Works
Watch on YouTube
Gas Turbine Working Principle (3D Animation)
Watch on YouTube
Hot Gas Path Inspection Explained
Watch on YouTube

How It Works

  1. 1

    Ambient air is drawn in and cleaned in the inlet filter house.

    Ambient air enters through a filter house with weather hoods, pre-filters and HEPA/EPA final stages. Every millibar of inlet pressure drop costs output, so filter ΔP is a daily reading. Air density decides capacity — the same machine loses roughly 0.5–0.9 % power per °C rise in ambient temperature, which is why evaporative coolers, foggers or inlet chillers are fitted in hot climates.

  2. 2

    Axial compressor raises the air to 15–30 bar and 350–450 °C.

    The axial compressor — typically 14 to 18 stages of rotating blades and stationary vanes — squeezes the air to 15–30 bar and 350–450 °C. Variable inlet guide vanes control airflow during start-up, part load and combined-cycle exhaust temperature control, and protect the machine from surge. Fouling of the blade surfaces is the single most common cause of silent output and efficiency loss.

  3. 3

    Fuel gas is injected and burned in the combustors at 1100–1500 °C.

    Fuel gas at 25–45 bar, filtered, heated above its dew point and metered by the gas control valves, is burned in annular or can-annular combustors. Dry Low NOx burners pre-mix fuel and air to hold flame temperature down and keep NOx below 25 ppm without water or steam injection. Firing temperature of 1100–1500 °C is possible only because the first-stage parts are film-cooled and coated with thermal barrier ceramics.

  4. 4

    Hot gas expands through the turbine — two-thirds of the power drives the compressor.

    The hot gas expands through the turbine stages. Roughly two-thirds of the power developed is consumed internally by the compressor on the same shaft — the remaining one-third is the useful output. This is why gas turbine performance is so sensitive: a small drop in compressor efficiency eats directly into net output, several times over.

  5. 5

    Exhaust at 500–600 °C leaves via the stack — or feeds an HRSG in combined cycle.

    Exhaust leaves at 500–600 °C. In simple cycle it goes up the stack through a silencer and the plant sits around 32–42 % efficiency. In combined cycle it feeds a multi-pressure HRSG that raises steam for a steam turbine, lifting plant efficiency to 55–62 %; in cogeneration the same heat makes process steam, chilled water via absorption chillers, or hot water.

  6. 6

    Generator output is stepped up by the GSU transformer to the grid.

    The generator, cooled by air or hydrogen and excited through a static or brushless exciter, delivers power at 11–15 kV. The generator step-up transformer raises this to the grid voltage, with synchronising, protection relays, and the DCS/turbine control system governing speed, load, temperature limits and the full sequence of start, load, unload and cooldown.

Key Components

Air Inlet & Filter House
Clean, low-ΔP air supply

Multi-stage filtration with weather louvres, anti-icing bleed, silencers and a trash screen. Watch ΔP trend and differential alarms: a blocked filter starves the machine, while a burst filter sends dust straight into the compressor and destroys blade coatings.

Axial Compressor
Raises air pressure 15–30 bar

Multi-stage rotor and stator assembly with variable inlet guide vanes and inter-stage bleed valves for surge protection during start and shutdown. Online water wash keeps fouling in check; offline crank wash restores what online wash cannot. Track compressor discharge pressure and temperature to judge health.

Combustion Chamber
Fuel burning, DLN NOx control

Can-annular or annular liners with DLN burners, transition pieces, spark igniters and flame detectors. Exhaust temperature spread across the thermocouples is the key diagnostic — a widening spread points to a plugged nozzle, a cracked liner or a faulty thermocouple long before a trip occurs.

Turbine Section
Expands hot gas into shaft power

Three to four stages of nozzles and buckets in nickel-based superalloys, internally air-cooled and coated with thermal barrier ceramics. Life is counted in fired hours and start cycles; combustion inspection, hot gas path inspection and major overhaul intervals are set by whichever counter arrives first.

Generator & GSU
Electrical power export

Air or hydrogen cooled synchronous generator with an exciter/AVR, neutral grounding, differential and loss-of-field protection, synchronised through the breaker to the GSU transformer. Monitor stator and bearing temperatures, hydrogen purity where applicable, and partial discharge on large units.

Lube Oil & Control System
Bearings, protection, governing

Main, auxiliary and emergency DC oil pumps, coolers, duplex filters, an overhead or accumulator supply, plus hydraulic trip oil. The control system handles speed governing, temperature control, DLN mode transfers, overspeed, vibration and flame-out trips. Oil cleanliness and trip-system testing are non-negotiable.

Typical Operating Parameters

These reference ranges are illustrative context, not approved operating limits. Verify the installed model, duty, fuel or water conditions and applicable site requirements before use.

Pressure Ratio
15 : 1 – 30 : 1
Firing Temperature
1100 – 1500 °C
Exhaust Temperature
500 – 600 °C
Simple Cycle Efficiency
32 – 42 %
Heat Rate
8500 – 11000 kJ/kWh
NOx (DLN)
< 25 ppm @ 15 % O₂

Safety Notes

  • •Gas leak detection and ventilation interlocks in the turbine enclosure.
  • •CO₂ / NOVEC fire suppression must be isolated before man-entry.
  • •Never bypass overspeed, vibration or flame-out trips.
  • •Hot surfaces and 100+ dB noise — PPE and permit control mandatory.

Maintenance Schedule

  • •Daily: vibration, bearing temps, lube oil level, filter ΔP, gas pressure.
  • •Weekly: online water wash check, fuel filter drain, battery/UPS test.
  • •Monthly: offline compressor wash as fouling raises heat rate.
  • •Per OEM hours: combustion inspection, hot gas path inspection, major overhaul.

Problem Solving Matrix

Listed causes are hypotheses, not confirmed findings. Any corrective work requires qualified assessment, approved procedures and follow-up measurements.

IssueLikely causeFix
Output drop at same fuelCompressor fouling / high inlet ΔPOffline wash, replace inlet filters
High exhaust spreadFuel nozzle blockage or burner issueCheck nozzles, verify thermocouples
Flame-out on load changeFuel gas pressure/quality swingStabilise gas skid, check dew point & filters
High vibrationRotor unbalance, bearing wear, misalignmentTrend spectrum, inspect bearings, balance rotor
High NOxDLN tuning drift, wrong combustion modeRe-tune DLN, verify mode transfer points

Equipment Running-Cost Estimate

Use measured electrical input, operating hours and your actual electricity tariff to estimate energy costs for gas turbine power plant. Compare replacement options before setting a project budget.

Calculate running costs
Utilities Expert

Problem Solving With Utilities Expert

Discuss every utility — compressors, chillers, boilers, WHRB, ETP and more — on WhatsApp with Engr. Muhammad Aalam, Manager Utilities. Share your symptoms and readings, and we will reply with practical troubleshooting suggestions when available.

+923336533423
Waste Heat Recovery Boiler (WHRB)Air Compressors