Aerodynamics
Aerodynamics is fundamental to understanding centrifugal compressor behavior. The phenomena of surge and choke define the operational limits of these machines.
Characteristic Curve
Each centrifugal compressor has a characteristic curve relating pressure and flow:
Pressure (bar)
│
9 ┤ ╭────╮
│ ╱ ╲
8 ┤ ╱ ╲
│ ╱ ╲
7 ┤ ●────────────●────────●
│ Surge Design Choke
6 ┤ │ │ │
│ │ │ │
5 ┤ │ │ │
│ │ │ │
└────┴──────────────┴─────────┴──── Flow (CFM)
500 1500 2500
Surge
Surge is the most critical phenomenon in centrifugal compressors. It is an unstable condition that can destroy the compressor.
What is Surge?
When air flow drops below a critical minimum while discharge pressure is high, air flows in reverse momentarily:
Normal Operation: Surge:
Inlet → Impeller → Outlet Inlet ← Impeller ← Outlet
(reverse flow)
Surge Consequences
| Effect | Severity | Consequence |
|---|---|---|
| Violent vibrations | Critical | Structural damage |
| Explosive noise (bang-bang) | High | Hearing damage |
| Bearing damage | Critical | Mechanical failure |
| Impeller fatigue | High | Cracks, rupture |
| Temperature increase | Medium | Seal degradation |
| Total destruction | Extreme | Equipment loss |
The Surge Line
Pressure
│
│ ╔═══════════════╗
│ ╔╝ SURGE ZONE ║
│ ╔╝ (danger) ║
│ ╔╝ ║
│╔╝ Surge ─────────╫────── Design point
│║ Line ║ ●
│║ ║
│║ SAFE ZONE ║
│║ (operation) ║
│╚═══════════════════╝
└────────────────────────── Flow
Low High
- Surge line: The minimum flow limit for each pressure
- Safe zone: To the right of the surge line
- Surge zone: To the left - operation prohibited
Surge Causes
| Cause | Mechanism | Prevention |
|---|---|---|
| Low demand | Little air consumption | Anti-surge control |
| Closed valves | Discharge restriction | Interlock |
| Clogged filters | Suction restriction | Maintenance |
| Sudden changes | Fast transients | Load ramp |
| Control failure | Sensor/actuator | Redundancy |
Choke (Stonewall)
Choke or stonewall is the opposite limit to surge: it occurs when flow is too high.
What is Choke?
When air velocity reaches the speed of sound at some point in the compressor (typically in the diffuser throat), flow becomes "blocked":
Air velocity in diffuser:
Normal: Choke:
▓▓ ▓▓▓▓▓▓▓▓
▓▓ ▓▓▓▓▓▓▓▓ ← Mach 1.0
▓▓ ▓▓▓▓▓▓▓▓
▓▓ ▓▓▓▓▓▓▓▓
──── ────────
Subsonic Sonic (blocked)
Choke Characteristics
| Aspect | Description |
|---|---|
| Maximum flow | Cannot increase further |
| Pressure | Drops drastically |
| Efficiency | Very low |
| Damage | Less than surge, but inefficient |
| Noise | High, whistling |
Surge vs Choke Comparison
| Characteristic | Surge | Choke |
|---|---|---|
| Flow | Very low | Very high |
| Pressure | High | Low (drops) |
| Danger | Extreme | Moderate |
| Potential damage | Destruction | Inefficiency |
| Correction | Immediate required | Reduce demand |
| Indicator | Noise, vibration | Pressure drop |
Operating Map
The complete operating map shows all zones:
Pressure
│
│ SURGE CHOKE
│ ║ ║
10 ┤ ║ 100% speed ────────── ║
│ ║ ╱ ╲ ║
9 ┤ ║ ╱ 90% speed ───────── ╲ ║
│ ║ ╱ ╱ ╲ ╲ ║
8 ┤ ║╱ ╱ 80% speed ─────── ╲ ╲ ║
│ ╳ ╱ ╱ ╲ ╲ ╲ ║
7 ┤ ╱║ ╱ ╱ ╲ ╲ ╲║
│ ╱ ║╱ ╱ SAFE ╲ ╲ ╳
6 ┤ ╱ ╳ ╱ ZONE ╲ ╲╱║
│╱ ╱║ ╱ ╲ ╱ ║
5 ┤ ╱ ║╱ ╳ ║
│ ╱ ╳ ╱║ ║
└────╫──────────────────────────╫───── Flow
500 2500
Surge Margin
Control systems maintain a safety margin from the surge line:
Pressure
│
│ Surge Control
│ Line Line
│ │ │
│ │←── 10% ───→│
│ │ margin │
│ │ │ ● Operation
│ │ │
└───────────────────────────── Flow
| Margin | Application |
|---|---|
| 10% | Well-controlled systems |
| 15% | Typical applications |
| 20% | Highly variable loads |
| 25%+ | Critical processes |
Factors Affecting the Curve
Inlet Conditions
| Factor | Effect on Surge | Effect on Capacity |
|---|---|---|
| High temperature | Surge at lower flow | Lower capacity |
| Altitude | Surge at lower flow | Lower capacity |
| High humidity | Minor effect | Minor effect |
| Dirty filter | Surge at lower flow | Lower capacity |
Altitude Correction
| Altitude (m) | Correction Factor |
|---|---|
| 0 (sea level) | 1.00 |
| 500 | 0.94 |
| 1000 | 0.89 |
| 1500 | 0.83 |
| 2000 | 0.78 |
| 3000 | 0.69 |
At high altitudes, compressor capacity is significantly reduced. A 1000 CFM compressor at sea level only delivers ~780 CFM at 2000 meters.