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Natural Gas Turboexpander & NGL Recovery Simulator

Isentropic Cryogenic Expansion • Compander Shaft Power • Booster Recompression • NGL Condensation

1. Feed Gas & Inlet State

2. Expander Stage & Isentropic Dynamics

3. Direct-Coupled Booster Compressor

Turboexpander-Compressor (Compander) & Cold Separator Schematic

🟢 High-Pressure Dry Gas Feed ❄️ Cryogenic Expansion Turbine Wheel 💧 Cold Knock-Out Separator (NGL Dropout) ⚡ Direct-Coupled Booster Compressor Stage
Discharge Temp (T₂)
-- °C
ΔT Drop: -- °C
Shaft Power Extracted
-- kW
-- HP
Booster Pressure Lift
-- bar g
+-- bar boost
NGL Liquid Production
-- bpd
-- tonne/day

Cryogenic Thermodynamics & Mechanical Compander Diagnostics

Mass Flow Rate: -- kg/s (-- t/h)
Expansion Pressure Ratio (P₁/P₂): --
Isentropic Enthalpy Drop (Δh_s): -- kJ/kg
Actual Specific Work Extracted: -- kJ/kg
J-T Valve Equivalent Cooling: -- °C (Expander: -- °C)
Wheel Outlet Liquid Fraction: -- wt%
Shaft Power Transferred to Booster: -- kW
Booster Discharge Temperature: -- °C

Governing Cryogenic Turboexpansion Equations

1. Isentropic Temperature & Enthalpy Drop:

T_{2s} = T_1 × (P_2 / P_1)^{ [ (k-1)/k ] × Z_avg }

Δh_s = [ k / (k - 1) ] × (R / MW) × T_1 × Z_avg × [ 1 - (P_2 / P_1)^{(k-1)/k} ]

2. Actual Shaft Power & Discharge Temperature:

Δh_{actual} = Δh_s × η_{isen} → W_{shaft} = m × Δh_{actual} × η_{mech}

T_2 = T_1 - (Δh_{actual} / Cp)

3. Direct-Coupled Booster Recompression:

P_{boost,out} = P_{boost,in} × [ 1 + (W_{shaft} × η_{comp}) / (m_{residue} × Cp × T_{b,in}) ]^{ [ k / (k-1) ] }

5 Fatal Traps & Engineering Pitfalls

1. High-Velocity Condensate Droplet Impingement Wheel Erosion (>15 wt% liquid)

When expansion cooling condenses more than 12%–15% liquid droplets directly across the rotor blading, supersonic droplet impingement (relative velocities >300 m/s) strips the protective passive oxide film off titanium or 7075-T6 aluminum wheels. Severe micro-pitting develops on blade trailing edges, inducing high-cycle aerodynamic fatigue and explosive catastrophic rotor burst.

2. Trace Moisture Hydrate & Ice Freezing Across Variable Guide Vanes

Even 2 to 5 ppmv of water vapor breakthrough from saturated molecular sieves turns into solid clathrate hydrates and ice needle crystals at -70°C. Hydrates accumulate in the tight clearances of variable inlet guide vanes (IGVs), locking the actuator mechanism. Shards of broken hydrate ice entering the spinning rotor blade throat cause immediate unbalance and trip active magnetic bearings (AMB).

3. Heavy Aromatics (C6+ & Benzene) Solidification in Cold Separator

Feed gas containing trace benzene (>50 ppm) or heavy paraffins (C7–C9) will freeze solid prior to reaching the -80°C demethanizer feed temperature. Solid benzene crystallizes out of liquid ethane/propane onto the cold separator demister mesh pads and liquid level control valves, freezing lines solid and causing sudden liquid carryover into the recompressor stage.

4. Booster Compressor Aerodynamic Surge During Plant Turndown

Because the booster compressor is directly keyed to the expander shaft without a variable-speed coupling, reducing plant feed flow drops the gas volume through the compressor while the expander continues to spin at high RPM (25,000–45,000 RPM). If the anti-surge recycle valve fails to open instantly, the booster enters violent high-frequency surge, slamming the common rotor axially back and forth against its thrust collar.

5. Cryogenic Seal Gas Migration & Lube Oil Freezing

In oil-lubricated bearing companders, dry gas seals prevent -80°C cryogenic process gas from contacting 60°C bearing lube oil. If seal gas differential pressure drops, freezing hydrocarbon gas breaches the labyrinth seal. The bearing oil cools below its pour point, waxing and locking up shaft journal bearings, resulting in complete shaft seizure at 30,000 RPM.

Frequently Asked Questions

What is a turboexpander and how does it achieve cryogenic temperatures for NGL recovery? +
How does the direct-coupled recompressor booster stage work? +
Why is upstream molecular sieve dehydration mandatory prior to turboexpansion? +
What is the limit on liquid condensation inside the turboexpander wheel? +
How does turboexpander temperature drop compare to a Joule-Thomson (J-T) throttling valve? +
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