Here are three accessible, high-quality PDFs on turbomachinery rotordynamics (including case studies) you can download or search for:
The compressor rotor model was updated using FEA to simulate alternative seal architectures. The OEM replaced the labyrinth balance piston seal with a hole-pattern swirl-brake damper seal. This modification reduced the circumferential fluid velocity, shifted the log decrement from -0.12 to +0.35, and successfully stabilized the machine across its entire operational envelope.
The oil whip phenomenon was completely eliminated, and the turbine resumed reliable, vibration-free operation across its entire speed envelope.
Perform a full damped eigenvalue analysis to ensure stability, particularly for high-pressure, high-speed machinery. Conclusion turbomachinery rotordynamics with case studies pdf
Hydrodynamic Bearing instability, Seal Aerodynamic cross-coupling
Verification of lateral critical speed separation margins per API standards.
Instability occurs when the forces generated within the machine feed energy into a vibration mode rather than dissipating it. Oil Whirl and Oil Whip The oil whip phenomenon was completely eliminated, and
The seal design was modified to include honeycomb inserts, which reduced the destabilizing cross-coupled stiffness, increasing the stability margin and eliminating the vibration. Case Study 2: Critical Speed Shift in a Steam Turbine
Case Study 2: Torsional Resonance Failure in a Motor-Driven Compressor Train
A generator failed due to fatigue, with fractures appearing in the shaft. Instability occurs when the forces generated within the
Instability occurs when the system absorbs energy from its surroundings, causing vibrations to increase exponentially. This is often caused by:
). A positive log decrement indicates a stable system where vibrations decay over time, whereas a negative log decrement signifies dynamic instability, leading to self-excited subsynchronous whirl or whip. 3. Industrial Case Studies