Electromagnetic Force Coupling in Electric Machines. Mark Solveson, Cheta Rathod, Mike Hebbes, Gunjan Verma, Tushar Sambharam ANSYS, Inc.
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1 Electromagnetic Force Coupling in Electric Machines Mark Solveson, Cheta Rathod, Mike Hebbes, Gunjan Verma, Tushar Sambharam ANSYS, Inc. 1
2 Introduction Low noise regulation Aimed at reduction in noise pollution Comfort Criteria Noise causes discomfort and fatigue Noise suppression demonstrates technological/marketing edge Component Failure Sensitivity of structure to acoustic resonances The above Applies to many Industry sectors: Transportation, Power, Environmental, Building services 2
3 Introduction Noise and vibration in electric machines come from many sources. ANSYS provides excellent capabilities for the design and analysis of electric machines: Electromagnetic performance Electric Drive performance Structural analysis Thermal analysis Acoustics analysis ANSYS field coupling technology allows mapping of electromagnetic forces for Mechanical analysis 3
4 Machine Types Different machines may have different considerations depending on their architecture or control strategies. Primary Forces are in plane (radial and tangential) Single and Three Phase Induction Machines. PM Synchronous Machines (Surface Mount, IPM). Switched reluctance machines Primary force are Axial Axial Flux Machines 4
5 Noise Sources [1] Magnetic Mechanical Aerodynamic Electronic Radial Fluid Cooling Phenomena Switching Harmonics Slot Harmonics Self Auxiliaries Load Induced Magnetic Unbalance Stator Rotor Couplings Modes of Vibration Bearings Balancing Static Eccentricity Foundation Audible Frequencies Dynamic Eccentricity Elliptical Rotor Surface Unbalanced Rotor 20 Hz 60 Hz Hz 4.186kHz 5 khz 20 khz 5 [1] P. Vigayraghavan, R. Krishnan, Noise in Electric Machines: A Review, IEEE, 1998
6 ANSYS Machine Model 6
7 Electromagnetic Design and Analysis ANSYS Machine Design Methodology RMxprt: calculate rated performance for machine Maxwell: Calculate detailed magnetic FEA of machine in time domain Simplorer: Calculate detailed drive design with coupled cosimulation with either RMxprt or Maxwell. SINE1 SINE2 SINE3 TRIANG1 E1 IGBT1 D7 IGBT3 D9 IGBT5 D11 RphaseA RphaseB PhaseA_in PhaseA_out + V RphaseC PhaseB_in PhaseB_out VM1 PhaseC_in PhaseC_out E2 IGBT2 D8 IGBT4 D10 IGBT6 D12 MotionSetup1_in 0 MotionSetup1_out + V_ROTB1 7
8 V V V V V V TR TR TR TR Curve Info SINE1.VAL SINE2.VAL SINE3.VAL TRIANG1.VAL ANSOFT Machine Model in Maxwell Simplorer 2D IPM (Interior Permanent Magnet) motor model created from RMxprt and Maxwell UDP (User Defined Primitive) for rotor Model V Model DModel1 SModel1 4 pole, 1500 RPM, 220 Volt DC bus. Two Control Strategies used: 6 step inverter In Maxwell PWM current regulated Cosimulation Maxwell with Simplorer V LabelID=V32 110V LabelID=V33 D40 S_46 D34 D35 D41 S_47 D42 S_48 D36 D37 D43 S_49 D44 S_50 D38 D39 LabelID=VIA H*Kle ohm LPhaseA LA RA LabelID=VIB H*Kle ohm LPhaseB LB RB LabelID=VIC H*Kle ohm LPhaseC LC RC D45 S_51 LabelID=IVc1 LabelID=IVc2 LabelID=IVc3 LabelID=IVc4 LabelID=IVc5 LabelID=IVc6 100ohm 100ohm 100ohm 100ohm 100ohm 100ohm R20 R21 R22 R23 R24 R V 1V 1V 1V 1V 1V LabelID=V14 LabelID=V15 LabelID=V16 LabelID=V17 LabelID=V18 LabelID=V19 0 SINE1 SINE2 SINE3 TRIANG1 E1 IGBT1 D7 IGBT3 D9 IGBT5 D11 RphaseA RphaseB PhaseA_in PhaseA_out + PhaseB_in PhaseB_out E2 IGBT2 D8 VM1 V IGBT4 D10 IGBT6 D12 RphaseC PhaseC_in MotionSetup1_in PhaseC_out 0.88 MotionSetup1_out Sine Triangle Basic_Inverter Y1 V_ROTB Time [ms]
9 ANSOFT ANSOFT Machine Model in Maxwell Simplorer SAS IP, Inc Torque Basic_Inverter1 SAS IP, Inc Currents Basic_Inverter1 Curve Info FEA1.TORQUE TR Curve Info RphaseA.I TR RphaseB.I TR RphaseC.I TR FEA1.TORQUE 7.50 Y1 [A] Time [ms] Time [ms] 9
10 Force Calculations Force calculation using air gap flux density Maxwell Stress Tensor [9] Force calculation at a point on the stator. Force on a line in the airgap Force on a line co linear with the stator tooth This is common method in literature. Edge Force Density Default field quantity available in Maxwell Can be used for creating lumped force calculations on tooth tips Automatic Force mapping from Maxwell to ANSYS Mechanical. (2D 2D, 2D 3D, 3D 3D) 10
11 Edge Force Density in Maxwell Tangential Force on Tooth Tips 02_DC-6step_IPM ANSOFT Force (Newtons) Curve Info ExprCache(ToothTipTangent_Full1) ExprCache(ToothTipTangent_2) ExprCache(ToothTipTangent_3) ExprCache(ToothTipTangent_4) ExprCache(ToothTipTangent_5) ExprCache(ToothTipTangent_6) Time [ms] Radial Force on Tooth Tips 02_DC-6step_IPM ANSOFT Force (Newtons) Curve Info ExprCache(ToothTipRadial_Full1) ExprCache(ToothTipRadial_2) ExprCache(ToothTipRadial_3) ExprCache(ToothTipRadial_4) ExprCache(ToothTipRadial_5) ExprCache(ToothTipRadial_6) Time [ms] 11
12 Eccentricity Model Left Side Tooth Right Side Tooth 12
13 Rotor missaligned 0%, 25%, 50% Parametric Study of Eccentricity Electromagetic Force Solved simultaneously on multi core computer Shown: Radial Force on Right Tooth Tip FFT of Radial Force 13
14 Edge Force Density, 50% Eccentricity 14
15 50% Eccentricity: Radial and Tangential Force on Right Side and Left Side Tooth 0.00 Radial Tooth Tip Forces ANSOFT Tangential Tooth Tip Forces ANSOFT Force (N) Force (N) Curve Info Radial Force Small Gap Radial Force Large Gap Time [ms] Curve Info Tangential Force Small Gap Tangential Force Large Gap Time [ms]
16 ANSYS Force Mapping 16
17 Two Approaches Direct Force Mapping Electromagnetic forces from Maxwell to Mechanical by linking systems in Workbench Maps 2D Edge Force, and 3D Surface force Transient Analysis for Stress prediction Lumped Force Mapping Tooth Tip objects created for mapping calculated lumped force using EdgeForceDensity in Maxwell. Apply these lumped forces manually or through APDL Macro Further harmonic and Noise Analysis 17
18 Approach 1 Direct Force Mapping Scenario: Study the effect of Rotor Eccentricity Case 1: 0% Eccentricity No misalignment Case 2: 50 % Eccentricity Eccentricity amount is set to 50% of gap width Creates unbalanced electromagnetic forces Peak Edge Force Density 1.5e6 N/m 2 18 Peak Edge Force Density 1.9e6 N/m 2
19 This image cannot currently be displayed. This image cannot currently be displayed. Directional Deformation Radial Max Deformation vs time Case 1 0% Eccentricity 19 Case 2 50 % Eccentricity
20 This image cannot currently be displayed. This image cannot currently be displayed. This image cannot currently be displayed. Von Misses Stress Max Stresses vs time Case 1 0% Eccentricity 20 Case 2 50 % Eccentricity
21 Results: Comparison Higher the amount of eccentricity, higher is the variation of electromagnetic forces, causing deformation of stator, vibration and noise Total Deformation Deformation higher for eccentric model Peak Stresses Stresses at time=12 ms Stator Stresses are non symmetric and higher for eccentric model where the air gap is minimum 21
22 Approach 2 Lumped Force Mapping Electromagnetic Forces Export forces Workbench Flow Chart for Noise Prediction ANSYS Maxwell ANSYS Mechanical ANSYS Acoustics Lumped Forces in Time Domain Real/Imaginary Forces In Frequency Domain Harmonic Response Extract Acoustic Pressures Perform FFT in Maxwell APDL in Workbench APDL in Workbench 22
23 ANSYS Harmonic Analysis 23
24 Modal Analysis: Get Resonant Frequencies Mode #1, 8502 Hz Mode #2, 8708 Hz Mode #3, 8708 Hz First four Natural Frequency and corresponding mode shapes 24 Mode #4, 9080 Hz
25 Why Harmonic Analysis To make sure that a given design can withstand sinusoidal loads at different frequencies To detect resonant response and avoid it if necessary (e.g. using mechanical dampers, changing PWM frequency, etc.) To determine Acoustic response Boundary Conditions Input Forces Appling harmonic forces from Maxwell into ANSYS Mechanical 25
26 Harmonic Response Bode plot Frequency response at a selected node location of the model. Helps determine that Max Amplitude (1.7mm) occurs at 8710 Hz on the selected vertex 26
27 Harmonic Response Contour plot Amplitude distribution of the displacements at a specific frequency, Deformation plot at 8710 Hz 27
28 ANSYS Acoustics 28
29 Acoustics Capabilities in ANSYS Acoustics is the study of the generation, propagation, absorption, and reflection of sound pressure waves in an acoustic medium. Acoustic problems can be identified as Vibro Acoustics: Sound generated structurally (ANSYS Mechanical) Aero Acoustics : Sound generated aerodynamically (ANSYS CFD) 29
30 Modeling Aero Acoustics (ANSYS CFD) Free Space Problem with no solid surfaces: sound generated from turbulence, jet noise Free Space Problem with solid surfaces: Fan noise, airframe noise, rotor noise, boundary layer noise, cavity noise Interior problem: Duct noise, mufflers, ducted fan noise Sound pressure fluctuations 30
31 Vibro Acoustics (ANSYS Mechanical) Computing the acoustic field radiated by a vibrating structure Structure modeled in ANSYS Mechanical where vibration patterns are calculated (Modal, Harmonic Analysis). Applied loads are obtained from Maxwell. Vibration patterns used as boundary conditions to compute acoustic field radiated by structure (ANSYS MAPDL, ANSYS Acoustic Structures) 31
32 This image cannot currently be displayed. This image cannot currently be displayed. Acoustic Analysis Pressure Plot 32
33 Acoustic Analysis Pressure Plot 0.5 m Pres_1 Pres_2 Pres_3 Pressure vs Freq Pressure (Pa) 33 Freq(Hz)
34 Summary Investigated different noise sources for electric machines Demonstrated an integrated approach from Electromagnetics to Structural to Acoustics. Showed the effects of static eccentricity on stator tooth forces, deformation and stresses. Performed modal analysis to find the acoustic resonances Future Work: Investigation of different noise scenarios (machine types, drives) Include more mechanical details (windings, housing, etc) Expand harmonic analysis to include higher frequency content of forces Further investigation of Aero acoustics with ANSYS CFD 34
35 References [1] P. Vijayraghavan, R. Krishnan, Noise in electric machines: A Review, IEEE, 1998 [2] K. Shiohata, R. Kusama, S.Ohtsu, T.Iwatsubo, The Study on Electromagnetic Force Induced Vibration and Noise from a Normal and Eccentric Universal Motors, PIERS Proceedings, [3] S. Fink, S. Peters, Ansoft Noise Prediction for Electrical Motors, CADFEM/ANSYS Presentation, [4] Wei Wang, Quanfeng Li, Zhihuan Song, Shenbo Yu, Jian Chen, Renyuan Tang, Three Dimensional Field Calculation and Analysis of Electromagnetic Vibration and Noise for Disk Permanent Magnet Synchronous Machines, Shenyang University of Technology, China. [5] R. Belmans, D. Verdyck, W. Geysen, R. Findlay, Electro Mechanical Analysis of the Audible Noise of an Inverter Fed Squirrel Cage Induction Motor, IEEE, [6] M. Anwar, I. Husain, Design Perspectives of a Low Acoustic Noise Switched Reluctance Machine, IEEE, [7] S. Huang, M. Aydin, T.A. Lipo, Electronmagnetic Vibration and Noise Assessment for Surface Mounted PM Machines, IEEE, [8] Rakib Islam, Iqbal Hussain, Analytical Model for Predicting Noise and Vibration in Permanent Magnet Synchronous Motors, IEEE [9] Pragasen Pillay, William (Wei) Cai, An Investigation into Vibration in Switched Reluctance Motors, IEEE Transactions on Industry Applications, Vol. 35, NO. 3, May/June,
36 Thank You 36
37 ANSYS Acoustics Structure ANSYS Acoustics Structures computes noise radiated by vibrating structures. From Harmonic Vibrations to Noise Estimates. ANSYS Acoustics Structures integrates with your current simulation tools. 37
38 Title and Abstract Electromagnetic Force Coupling in Electric Machines Including Stress, Deformation, and Acoustic Analysis. Understanding the impact of electromagnetic forces on noise generation for electric machines can include many factors. This presentation will review these issues and illustrate electromagnetic forces, stress, deformation, and acoustic coupling in ANSYS Workbench. An example showing automatic mapping of magnetic time domain forces, and a comparison of stresses for different rotor eccentricities will be shown. 38
39 Presentation Outline (Goal 30 total Slides) 1. Introduction 2. Literature review what are the noise comonents for electric machines a. Noise Sources, examples b. Acoustic Definition, examples 3. EM Motor Methodology a. RMxprt to Maxwell, Simplorer b. Force calculations c. Eccentricity Model 4. Mechanical Analysis a. 2D (3D?) transient force mapping results b. Discussion of FFT approaches (by inspection or 3 rd party tools/scripts) c. 2D (3D?) harmonic Analysis 5. Acoustic analysis a. General capabilities (acoustic elements, Actran coupling? ) b. Results for stator lamination 39
40 40 Noise Sources Magnetic The interaction of magnetic fields and currents in the machine cause electromagnetic torque and thus rotation of the rotor. Evaluation of the radial and tangential forces on the tooth tips are important. This can be accomplished through evaluation of the air gap flux density, or using Force Density field calculations available within Maxwell. If one of the radial force frequencies coincides with the natural frequency of the machine, resonance occurs leading to acoustic noise. Mixed product of stator and rotor winding space harmonics. Slot Harmonics Rotor Eccentricity: improper rotor alignment causing unbalanced magnetic forces on the stator. Lamination vibration due to magnetorestrictive forces (worst when not stacked properly) Electronic Switching noise Inverter PWM frequencies can be in audible range. Current through the winding Lorentz forces
41 41 Noise Sources Mechanical Self resonance natural resonance frequencies Closed form equations FEA Load induced Coupling of machine to load, and mounting. Auxiliaries Bearing Vibration Brush commutators Chattering Intra lamination Function of Bolt force Involves 3D Mechanical transient vibration analysis Manufacturing asymmetries of the rotor and stator nonuniform air gap Stator winding which are not installed properly Aero Dynamics CFD
42 Machine Model in Maxwell VB script Fields Calculator to create Radial and Tangential Force Expressions from EdgeForceDensity VB script Calculates Radial and Tangential Force on Tooth Tips Allows only force on edge that neighbors non ferrous objects Half teeth force components added together Add to Expression Cache 42
43 Harmonic Analysis Overview A technique to determine the steady state response of a structure to sinusoidal (harmonic) loads of known frequency. Input: Harmonic loads (forces, pressures, and imposed displacements) of known magnitude and frequency. (Obtained from Maxwell) May be multiple loads all at the same frequency. Output: Harmonic displacements at each DOF, usually out of phase with the applied loads. Other derived quantities, such as stresses and strains. 43
44 ANSYS Acoustics Structural borne noise (one way Vibro Acoustics) ANSYS Acoustics Structures (FFT s ACTRAN Solver) Vibro Acoustics ANSYS Mechanical (APDL Solver) Aero Acoustics ANSYS CFD Nonlinear fluid structure interaction ANSYS CFD + ANSYS Mechanical 44
45 Aero Acoustics ANSYS CFD Approaches Direct calculation: Resolve the acoustic pressure fluctuations as part of the CFD solution Couple CFD with specialized acoustics codes, Boundary Element Methods (BEM), Hybrid zonal methods Acoustic waves are not tracked with CDF solution Calculate wave propagation using specialized codes (ACTRAN, SYSNOISE) 45
46 Aero Acoustic simulation of Automotive Front End Module cooling fans by using FLUENT s Acoustic module Courtesy of Hyundai MOBIS, Korea Geometry of Cooling Fans Computational domain 46 Pressure Contours Flow Pathlines through Sound pressure fluctuations calculated at the receiver position
47 Subwoofer Example (ANSYS CFD) (non linear fluid with structure) Fluid Structure Interaction Solution Transient Pressures 47
48 Acoustic Energy Source Acoustic Structural Example Coupled Target Object: Nested Cylindrical Cans Scattered Acoustic Radiation FEA Model quarter Symmetry Hemispherical Domain Animation of Acoustic Pressure (Pa) 48
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