Rotordynamics and Machinery Dynamics: Critical Speeds, Rotor Stability and Balancing – Dubai, 20–24 Sep 2027
DestinationDubai
Dates20 – 24 September 2027
Reference636_18239
This session
20–24 Sep 2027
This Rotordynamics and Machinery Dynamics: Critical Speeds, Rotor Stability and Balancing session in Dubai runs from Monday 20 September to Friday 24 September 2027 (week 38, Q3 2027). It is the 2nd of 2 dates in Dubai in 2027, at a fee of 19,500 SAR, the same for each of them. Registration is open for this date. It is held in person at Five-star CBD venue.
DatesMonday 20 Sep – Friday 24 Sep 2027
Week38 of 2027
Duration5 days
Fee19,500 SAR
StatusOpen for registration
FormatIn person
VenueFive-star CBD venue
Programme overview
Introduction:
Rotordynamics and machinery dynamics decide whether a high-speed compressor, turbine or pump train can run through its speed range without resonance, rubs or self-excited whirl, yet many design audits accept vendor critical speed and stability reports without challenge, and field teams chase recurring high vibration without a rotor-bearing model. This Core Concept course trains engineers to model rotor-bearing systems, read Campbell diagrams and unbalance response plots, judge separation margins and logarithmic decrement, check torsional trains and plan multi-plane balancing. Participants produce a Rotordynamic Design Review Report for a case compressor train.
Course Objectives:
Build and validate a lateral rotor-bearing model from shaft geometry, mass-elastic data, bearing coefficients and support stiffness
Interpret undamped critical speed maps, Campbell diagrams and unbalance response plots to confirm amplification factors and separation margins
Assess rotor stability using logarithmic decrement, cross-coupled stiffness and fluid-film bearing and seal coefficients
Review torsional natural frequencies, interference diagrams and coupling selection for motor-, turbine- and gear-driven trains
Plan shop and field balancing using influence coefficient and modal methods for rigid and flexible rotors
Diagnose high-speed rotor problems from orbit, Bode, polar and shaft centreline data and recommend design or operating corrections
Target Audience:
Rotating equipment engineers who approve vendor rotordynamic reports for compressors, turbines and high-speed pumps
Machinery reliability engineers who investigate recurring high vibration, rubs and bearing failures on critical trains
Machine design and project engineers who specify bearings, seals, couplings and rotor geometry for new trains
Turbomachinery field service engineers who carry out run-up tests and field balancing on flexible rotors
Technical authority and asset integrity engineers who sign off rerates, overspeed changes and driver replacements
Course Outline:
Day 1: Rotor-Bearing System Modelling and Natural Frequencies
Rotordynamic Vocabulary: Rigid and Flexible Rotors, Forward and Backward Whirl, Mode Shapes
Jeffcott Rotor Model for Resonance, Phase Shift and Amplification Factor
Rayleigh-Ritz and Dunkerley Estimates of First Lateral Natural Frequency
Finite Element Beam Model Build: Stations, Shaft Sections, Impellers and Added Mass
Gyroscopic Stiffening, Support Stiffness and Pedestal Flexibility Effects on Mode Frequencies
Day 2: Critical Speed Maps, Campbell Diagrams and API 684 Analysis Principles
Undamped Critical Speed Map Versus Bearing Stiffness Range
Campbell Diagram Construction with Excitation Orders and Interference Checks
Unbalance Response Analysis: Unbalance Placement, Probe Locations and Bode Plots
Separation Margin and Amplification Factor Criteria per API 684 Tutorial Principles
Seal Clearance Check Against Predicted Rotor Deflection at Maximum Continuous Speed
Day 3: Fluid-Film Bearings, Seal Forces and Rotor Stability
Plain, Lemon-Bore, Pressure-Dam and Tilting-Pad Journal Bearing Characteristics
Eight Dynamic Coefficients: Direct and Cross-Coupled Stiffness and Damping Versus Sommerfeld Number
Oil Whirl and Oil Whip Mechanisms with Subsynchronous Frequency Signatures
Aerodynamic Cross-Coupling, Labyrinth and Damper Seal Coefficients and Swirl Brakes
Logarithmic Decrement, Level I Screening and Level II Stability Analysis Workflow
Day 4: Torsional Train Analysis, Rotor Balancing and Troubleshooting Cases
Torsional Mass-Elastic Model: Inertias, Shaft Stiffness, Couplings and Gear Ratios
Torsional Interference Diagram, Motor Start-Up Transients and Variable Speed Drive Excitation
Influence Coefficient Method for Single-Plane and Multi-Plane Field Balancing
Modal Balancing of Flexible Rotors and High-Speed Shop Balancing Acceptance
Orbit, Polar, Bode and Shaft Centreline Plot Reading for Rub, Thermal Bow and Instability Cases
Day 5: Case Compressor Train Rotordynamic Review
Case Compressor Train Data Pack: Rotor Drawings, Bearing Data and Vendor Analysis Report
Lateral Critical Speed and Unbalance Response Review Worksheet with Margin Findings
Stability and Torsional Results Challenge Using Logarithmic Decrement and Interference Checks
Run-Up and Coast-Down Test Data Comparison Against Predicted Response
Rotordynamic Design Review Report Assembly and Peer Challenge
Skills You Will Gain:
Rotor-Bearing Modelling
Critical Speed Analysis
Campbell Diagram Interpretation
Bearing Coefficient Evaluation
Rotor Stability Assessment
Torsional Train Analysis
Flexible Rotor Balancing
Transient Vibration Data Interpretation
Why Attend This Course:
Return with a Rotordynamic Design Review Report built on a case compressor train
Challenge vendor rotordynamic reports with clear questions on margins, stability and model assumptions
Resolve subsynchronous vibration, rubs and repeat balancing problems on high-speed machines with a model-based approach
Compare design review and troubleshooting practice with peers from oil and gas, petrochemicals, power generation and process industries
Conclusion:
High-speed machine trains run reliably when their rotor-bearing systems are modelled correctly, their critical speeds are kept clear of the operating range, their bearings and seals leave enough damping and their torsional and balancing behaviour is checked. The course moves from rotor models and natural frequencies, through critical speed maps and Campbell diagrams, to bearing and seal coefficients, stability, torsional analysis and balancing. The final day applies these methods to a case compressor train and produces a Rotordynamic Design Review Report.
Rotordynamics and Machinery Dynamics: Critical Speeds, Rotor Stability and Balancing runs in Dubai over 5 days, with 2 upcoming dates in Dubai. The course fee is 19,500 SAR.
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