Destabilizing Magnetic Forces in Aerodynamic Bearings - UMP Analysis

Destabilizing Magnetic Forces in Aerodynamic Bearings

Unbalanced Magnetic Pull (UMP) - Linear to Quadratic Transition
⚠️ Critical Design Consideration: UMP behavior transitions from linear (F∝e) at small eccentricities to quadratic (F∝e²) at larger eccentricities. Increased rotor weight causes static deflection, increasing initial eccentricity. The quadratic regime creates a severe positive feedback loop, rapidly destabilizing the rotor.

Magnetic Force Analysis

F_UMP = K₁·e + K₂·e²
Current Force Regime:
LINEAR (F∝e)
Linear Component (K₁·e): 0 N
0%
Quadratic Component (K₂·e²): 0 N
0%
Total UMP Force
0 N
Eccentricity Ratio (e/g₀)
0.00
Total Resultant Force
0 N
System Status: RUNNING - Normal Operation
Rotation Speed
30,000 RPM
Air Gap Min
100%
Stability Margin
High
Force Growth Rate
Linear
Stator (Motor)
Rotor (Journal)
Air Film
UMP Force
Weight (mg)
Total Force

Rotor Position

System Parameters

Demonstration Scenarios