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AI Infra Atlas

On-site generation · gas

Gas turbine, cut open

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Every component, inlet to stack

Air path

  • Inlet filter houseCleans and quiets a river of air before the compressor.+

    A turbine this size swallows several hundred kilograms of air every second. The filter house strips dust and salt, a silencer cuts noise, and optional evaporative coolers or chillers cool the air on hot days to recover power.

    Airflow
    ≈600–1,000 kg/s
    Filtration
    Multi-stage, up to EPA/HEPA (E12)
    Pressure drop
    ≈0.5–1 kPa
    Options
    Inlet chilling or fogging, anti-icing
  • Axial compressorRows of spinning blades squeeze air about 20 times.+

    Alternating rows of rotating blades and fixed vanes each raise pressure a little. Variable inlet guide vanes at the front adjust airflow for part load. The compressor absorbs roughly half of the power the turbine makes.

    Stages
    ≈14–21
    Pressure ratio
    ≈20–24 : 1
    Exit temperature
    ≈450–500 °C
    Speed
    3,600 rpm (60 Hz, direct drive)
    Power absorbed
    ≈50% of turbine output

Hot section

  • Combustion systemA ring of cans where natural gas burns in compressed air.+

    Compressed air and fuel mix in a ring of combustor cans. Dry low-NOx designs premix lean so the flame stays cooler and makes less nitrogen oxide. Newer units can burn hydrogen blends.

    Layout
    Can-annular, ≈12–16 cans
    Firing temperature
    ≈1,400–1,600 °C
    NOx
    ≈9–25 ppm (DLN), lower with SCR
    Fuel
    Natural gas; ≈30–50% H₂ blends offered
    Fuel flow
    ≈15–20 kg/s at full load
  • Turbine sectionHot gas spins four stages of superalloy blades.+

    The hot gas expands through four stages, spinning the shaft. First-stage blades run in gas hotter than their own melting point, survived only by internal air cooling channels, film cooling holes and ceramic thermal-barrier coatings.

    Stages
    4
    Blade material
    Single-crystal nickel superalloy
    Coatings
    Ceramic thermal barrier (YSZ)
    Cooling
    Internal passages + film holes
    Inspection
    Hot gas path ≈every 24,000–32,000 h
  • Exhaust diffuser and stackStill about 600 °C, carrying roughly 60% of the fuel energy out.+

    The diffuser slows the exhaust to recover pressure. In simple cycle it leaves through a stack; in combined cycle a heat recovery steam generator turns that heat into steam for a second turbine, lifting efficiency from about 43% to over 63%.

    Exhaust temperature
    ≈600–650 °C
    Simple-cycle efficiency
    ≈41–44% (LHV)
    Combined-cycle efficiency
    ≈63–64% (LHV)
    Stack height
    ≈20–40 m

Generator and grid

  • Rotor and bearingsOne solid shaft from compressor to turbine to generator.+

    A bolted stack of forged discs forms a single rotor weighing on the order of 100 tonnes, riding on oil-film journal bearings and a thrust bearing that holds it in place axially.

    Speed
    3,600 rpm
    Rotor mass
    ≈80–120 t
    Bearings
    Tilting-pad journal + thrust
    Monitoring
    Vibration, temperature, axial position
  • GeneratorTurns shaft power into 60 Hz electricity at about 20 kV.+

    A two-pole synchronous generator spins with the turbine at grid frequency. Large units are hydrogen-cooled because hydrogen carries heat far better than air with less drag.

    Output
    ≈300–550 MW (H-class simple cycle)
    Voltage
    ≈18–24 kV
    Cooling
    Hydrogen (large units) or air
    Efficiency
    ≈98.8–99%
    Start
    Static frequency converter spins it up
  • Generator step-up transformerLifts ≈20 kV to transmission voltage.+

    Connects the generator through isolated-phase bus to the grid or straight to a campus substation. At a behind-the-meter AI campus this may step to 34.5 kV for site distribution instead.

    Rating
    ≈350–600 MVA
    Ratio
    ≈20 kV → 230–500 kV (or 34.5 kV on site)
    Cooling
    ONAN/ONAF/ODAF

Auxiliaries

  • Fuel gas skidFilters, heats and meters gas to the right pressure.+

    Pipeline gas is filtered, heated to stay above its dew point and controlled through stop and control valves. H-class units need high fuel pressure, often requiring a compressor at the site.

    Supply pressure
    ≈3–4.5 MPa (≈450–650 psig)
    Flow
    ≈2–3 million m³ per day at full load
    Safety
    Double block-and-bleed valves
  • Lube oil systemKeeps every bearing floating on a film of oil.+

    A reservoir, pumps, coolers and filters feed oil to every bearing. An emergency DC pump keeps oil flowing while the rotor coasts down if all AC power is lost.

    Reservoir
    ≈15,000–30,000 L
    Pumps
    AC main, AC standby, DC emergency
    Turning gear
    Rotates the shaft slowly while cooling
  • Control and starting packageBrains, fire protection and the starting system.+

    The control system manages start, load and protection. A static starter runs the generator as a motor to bring the shaft up to speed; the unit can reach full load in about 10–30 minutes. A CO₂ system protects the enclosure.

    Start to full load
    ≈10–30 min (aeroderivatives ≈5–10)
    Ramp rate
    ≈50–90 MW/min
    Fire protection
    CO₂ or water mist in enclosure

Typical ranges for heavy-duty F/H-class units from published OEM data (GE 7HA, Siemens Energy SGT6-9000HL, Mitsubishi M501J class) and EPRI/DOE references. A specific machine differs. Not an engineering document.