1. Overview
CCUS systems must compress captured CO₂ from low-pressure capture conditions (typically 1.2–2.0 bara at 30–60 °C) to pipeline transport conditions (100–200 bara, 30–50 °C dense phase). The compression train is one of the largest parasitic loads on the capture plant — typically 80–130 kWh per tonne of CO₂ captured, equivalent to 4–7% of net plant output for a coal-fired power station with 90% capture.
Three engineering challenges dominate CO₂ compressor design:
- Pressure ratio: 75–150× compression from capture to pipeline — requires 4–6 stages with aerodynamic and mechanical limits per stage.
- Critical-point transition: at ~75 bara the fluid becomes liquid-like; the last stage is properly a centrifugal pump, not a compressor.
- Heat management: compression generates substantial heat that must be rejected via intercoolers to keep materials in range and reduce subsequent-stage power.
| Standard / Reference | Scope |
|---|---|
| GPSA Engineering Data Book §13 | Polytropic head, Schultz method, multi-stage design |
| ASME PTC-10 (2007) | Compressor performance test code — polytropic basis |
| API STD 617 (2014) | Axial and Centrifugal Compressors and Expander-Compressors |
| API STD 618 (2007) | Reciprocating Compressors for Petroleum, Chemical, and Gas Industry Services |
| DOE NETL Cost & Performance Baseline (2022) | Reference compression energy for CCUS power-plant integration |
| ISO 27913:2016 | CO₂ pipeline transport — compression to dense phase |
2. Polytropic Thermodynamics
The Schultz polytropic head equation (GPSA §13, ASME PTC-10) gives the work input per unit mass for a single compression stage:
Polytropic exponent
The polytropic exponent relates to the isentropic exponent (k = Cp/Cv) through the polytropic efficiency ηp:
For CO₂ with k = 1.30 and ηp = 0.75: n = 1 / [1 − 0.30/(1.30 × 0.75)] = 1 / [1 − 0.308] = 1.444.
Discharge temperature
The polytropic discharge temperature is:
Shaft power
Total shaft power accounts for polytropic efficiency (gas-side losses) and mechanical efficiency (gearbox/coupling losses):
3. Multi-Stage Design
The total pressure ratio from capture to pipeline is typically 75–150 (e.g., 1.5 → 150 bara = 100×). This must be split into multiple stages, each within mechanical/aerodynamic limits.
Stage count
For a target maximum pressure ratio per stage (PRmax):
| Compressor type | PRmax/stage | Stages for 100× total | Notes |
|---|---|---|---|
| Centrifugal (CCUS standard) | 3.0 | 5 | Aerodynamic limit at high tip Mach number |
| Centrifugal (conservative) | 2.5 | 6 | Margin for off-design and inlet variations |
| Axial | 1.4 | 14 | Multi-stage in single casing; rare for CO₂ |
| Reciprocating | 3.0–4.0 | 4 | Used for low flow / EOR applications |
Compressibility factor variation
CO₂ Z-factor varies substantially across the train — from ~0.95 at low P to 0.6 near the critical point and back to ~0.85 at supercritical. Industry practice is to use stage-specific Z-averages:
| Stage suction P (bara) | Typical Zavg |
|---|---|
| 1–10 | 0.97–0.99 |
| 10–30 | 0.92–0.96 |
| 30–50 | 0.85–0.92 |
| 50–75 (near critical) | 0.60–0.85 (steep) |
| > 75 (supercritical) | 0.85–1.00 |
For final design, Z is computed from PR-EOS or Span-Wagner at each stage's actual conditions.
4. Intercooling
Inter-stage cooling brings the gas back to a low temperature (typically 35–45 °C, set by cooling water or ambient air) before the next compression stage. The benefits are substantial:
- Polytropic head reduction: Hp ∝ Tin — cooling from 175 °C to 40 °C reduces next-stage head by ~30%.
- Material limits: uncooled compression to 150 bara would produce discharge T > 300 °C — beyond ASME B31.3 carbon-steel piping limits (typically 425 °C max for short term, but cyclic limits much lower).
- Water and acid removal: intercoolers also condense water vapor and trace contaminants, simplifying downstream dehydration.
Intercooler duty
Heat removed per stage is roughly:
Total intercooler duty is summed across all stages except the final (which discharges directly to the pipeline). For the worked example below (4 intercoolers between 5 stages), the total heat removed is ~1.3× the shaft power — significant cooling water demand.
Aftercooler
An aftercooler downstream of the final stage cools the high-pressure dense-phase CO₂ to pipeline operating temperature (usually ambient + 5–10 °C). This is critical because:
- Pipeline operating T is typically 35–40 °C (above CO₂ critical point) — feed must match.
- Hot pipeline operation reduces CO₂ density and increases ΔP per unit mass.
- Pipeline expansion joints and bends are designed for the operating T range.
5. Pump Transition Near Critical
The CO₂ critical point (304.13 K = 30.98 °C, 73.77 bara) sits in the middle of typical CCUS compression trains. Below the critical pressure, CO₂ is a compressible gas; above it, dense liquid (or supercritical fluid). At the typical intercooler temperature of 35–40 °C, conditions immediately below Tc with enough cooling can produce a phase transition.
Industry practice exploits this by switching from compression to liquid pumping for the final 1–2 stages:
| Train segment | P range (bara) | Equipment | Energy (kWh/tCO₂) |
|---|---|---|---|
| Stages 1–4 (gas compression) | 1.5 → 75 | Centrifugal compressor | ~80–100 |
| Knockout + cooler @ 75 bara, 30 °C | ~75 | Surface condenser | ~ −20 (heat removal) |
| Final stage (liquid pumping) | 75 → 150 | Centrifugal pump | ~5 |
| Total compression + pumping | 1.5 → 150 | Hybrid train | ~85–105 |
The liquid pumping segment is dramatically more efficient than gas compression at the same pressure ratio — ~5 kWh/t to lift from 75 to 150 bara via pump, vs ~25 kWh/t to compress the same step as gas. This is the basis for the lower end of the DOE NETL specific-energy range.
6. Worked Example
Problem: Size a CO₂ compression train for 100,000 kg/h captured CO₂. Suction 1.5 bara at 35 °C. Discharge 150 bara dense-phase. Centrifugal, intercooler outlet 40 °C, ηp 75%, ηmech 98%, max PR/stage 3.0.
Step 1: Total ratio and stage count.
Step 2: Polytropic exponent.
Step 3: Stage 1 head and power.
Step 4: Repeat for stages 2–5 with intercooled Tin = 313 K (40 °C). Z drops as P rises, so head per stage actually drops slightly:
| Stage | P_in (bara) | T_in (°C) | T_out (°C) | Z_avg | Hp (kJ/kg) | Shaft kW | Intercool kW |
|---|---|---|---|---|---|---|---|
| 1 | 1.5 | 35 | 174 | 0.95 | 57.2 | 2161 | 3170 |
| 2 | 3.77 | 40 | 184 | 0.95 | 58.1 | 2196 | 3404 |
| 3 | 9.46 | 40 | 184 | 0.92 | 56.3 | 2127 | 3404 |
| 4 | 23.78 | 40 | 184 | 0.75 | 45.9 | 1735 | 3404 |
| 5 | 59.78 | 40 | 184 | 0.60 | 36.7 | 1387 | 0 |
| Total | 9606 kW | 13,382 kW | |||||
Step 5: Specific energy and cooling load.
Run this calculation with your inputs
→ A5: CO₂ Compression Power Calculator7. Standards & References
- GPSA Engineering Data Book, 14th Ed. (2017), §13 Compressors
- ASME PTC-10 (2007), Performance Test Code on Compressors and Exhausters
- API Standard 617, 8th Ed. (2014), Axial and Centrifugal Compressors and Expander-Compressors
- API Standard 618, 5th Ed. (2007), Reciprocating Compressors for Petroleum, Chemical, and Gas Industry Services
- DOE NETL Cost and Performance Baseline for Fossil Energy (2022) — Volume 1: Bituminous Coal & Natural Gas to Electricity
- ISO 27913:2016, CO₂ capture, transportation, and geological storage — Pipeline transportation systems
- Schultz, J.M. (1962). "The Polytropic Analysis of Centrifugal Compressors," J. Eng. Power 84(1), 69–82.
- IEAGHG Technical Report 2014/04, "CO₂ Pipeline Infrastructure"
- NIST REFPROP, NIST Standard Reference Database 23, Version 10.0