ASME Turbo Expo 2009: Power for Land, Sea, and Air

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ASME Turbo Expo 2009: Power for Land, Sea, and Air. Thermohydrodynamic Analysis of Bump Type Gas Foil Bearings: A Model Anchored to Test Data. Luis San Andrés Tae Ho Kim Mast-Childs Professor Research Associate. Texas A&M University. ASME GT2009-59919. - PowerPoint PPT Presentation

Transcript of ASME Turbo Expo 2009: Power for Land, Sea, and Air

  • This material is based upon work supported by NASA Research Announcement NNH06ZEA001N-SSRW2, Fundamental Aeronautics: Subsonic Rotary Wing Project 2 # 32525/39600/ME and the Turbomachinery Research ConsortiumASME Turbo Expo 2009: Power for Land, Sea, and AirThermohydrodynamic Analysis of Bump Type Gas Foil Bearings: A Model Anchored to Test DataTexas A&M UniversityLuis San Andrs Tae Ho KimMast-Childs Professor Research AssociateASME GT2009-59919Accepted for J. Eng. Gas Turbines Power (In-Press)

  • Gas Foil Bearings Bump typeSeries of corrugated foil structures (bumps) assembled within a bearing sleeve. Integrate a hydrodynamic gas film in series with one or more structural layers. PROVEN TECHNOLOGY!!Applications: Aircraft ACMs, micro gas turbines, turbo expanders, turbo compressors, Damping from dry-friction and operation with limit cyclesTolerant to misalignment and debris, also high temperatureNeed coatings to reduce friction at start-up & shutdownOften need cooling flow for thermal management of rotor-GFB system

  • Gas Foil Bearings (+/-)Increased reliability: large load capacity (< 100 psi)No lubricant supply system, i.e. reduce weight High & low temperature capability (up to 1,200 F) No scheduled maintenance with increased life Less load capacity than rolling or oil bearingsThermal management (cooling) issuesLittle test data for rotordynamic force coefficientsPredictive models lack validation. Difficulties in accessing full test data geometry and operating conditions

  • Overview GFB computational modelsSalehi et al. (2001): Couette flow approximation to estimate bearing temperatures.Heshmat (1983), Carpino and Talmage (2003, 2006), Kim and San Andrs (2005, 2007), Lee, et al. (2006), Le Lez, et al. (2008): Predict static/dynamic performance of bump-type GFBs with isothermal flow model and simple to complex foil modelsLe Lez et al. (2007): Nonlinear elastic bump model. THD model predicts larger load capacity than isothermal flow model.Peng and Khonsari (2006): Thermal management of GFB from cooling gas stream underneath top foil.Feng and Kaneko (2008), San Andrs and Kim (2009): FE top foil & support structure model. Predicted bearing temperatures in agreement with test data (Radil and Zeszotek, 2006), obtained at room temperature (~21C) without cooling flow.Thermohydrodynamic (THD) model predictions:

  • Overview Rotordynamic measurementsDellaCorte and Valco (2000): Review open literature and estate Rule of Thumb to estimate load capacity of GFBs. Salehi et al. (2001) : Measure temperatures in foil bearing operating with axial cooling stream flow.San Andrs et al. (2006, 2008): Large imbalances cause subsync. whirl motions due to FB structure hardening.Ruscitto et al (1978): Load capacity tests on simple GFB. Full test data & bearing geometryHeshmat (1994): Demonstrates maximum speed of 132 krpm, i.e. 4.61 106 DN. Ultimate specific load (~100 psig). Most designs operate at 10 psig or below. Radil and Zeszotek (2006): Measure temperatures in foil bearing operating with changes in load and rotor speed.

  • Foil Bearing Research at TAMUTest Gas Foil Bearing (Bump-Type)Generation II. Diameter: 38.1 mm25 corrugated bumps (0.38 mm of height)Reference: DellaCorte (2000)Rule of Thumb2003-2009: Funded by NSF, Capstone Turbines, NASA GRC, Turbomachinery Research Consortium

  • THD modelGFB with cooling flows (inner and outer)Outer flow streamBearing housing zxRSoz=0z=LT

  • THD model governing equationsConvection of heat by fluid flow + diffusion to bounding surfaces = compression work + dissipated energyXYX=RSide view of GFB with hollow shaft

  • Configuration of control volume for integration of flow equations ( = Pf or Tf)Subscripts E,W,N,S for east, west, north, and south nodes; and subscripts e,w,n,s for east, west, north, and south faces of control volumeNumerical solution of Reynolds and thermal energy transport equations implement exact advection control volume model (Faria and San Andrs, 2000)Numerical solution procedure

  • Heat flux paths in rotor - GFB system Simple representation in terms of thermal resistances within a GFB supporting a hot hollow shaft

    Heat conducted into the bearing

    Cooling gas streamcarries away heat Heat flow model

  • Equivalent heat transfer coefficients: Heat transfer from film flow to outer bearing cartridgeWithout outer cooling flow stream

  • Thermal energy mixing processAt gap in between trailing and leading edge of top foil. : empirical thermal mixing coefficient enforced. Top foil detachment doest not allow for gas film pressure to fall below ambient pressure. No ingress of fresh gas

  • Width of arrow denotes intensity of energy transportBalance of thermal energy transportExample only

  • Top foil thickness, Bump foil thickness, Bump height, Gas Constant, Viscosity, 1.73Conductivity, Density, GFB model: Generation I GFB with single top foil and bump strip layerModel Validation: geometry & operating conditionsGas viscosity, density & conductivity, foil material props., and clearance change with temperature Ref. [7, 21]: Radil and Zeszotek, 2004Dykas and Howard, 2004

  • Predicted peak film temperatureStatic load (vertical:180)

    Comparison to test data (Radil and Zeszotek, 2004)Peak film temperature grows as static load increases and as rotor speed increases. Peak film temperatures higher than ambient temperature, even for small load of 9 N. TSupply=21 CW/LD= 16 psi= 1.1 barTshaft=Tbearing =Tambient = 21 C

    Load (24)

    741021371685583125190

    771061361686088128186

    821121411817098136192

    9011914919380110148202

    9612616020592124162214

    101134176217104138177228

    30,000 rpm

    40,000 rpm

    50,000 rpm

    20,000 rpm

    Test data (Mid-plane)

    Predictions(Mid-plane)

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (23)

    111

    1.0051.0081.01

    1.0021.0121.017

    1.0011.0181.025

    1.0011.0241.034

    1.0031.0311.043

    1.0051.041.053

    1.0081.0491.065

    1.0121.0591.077

    1.0171.0711.091

    1.0231.0831.107

    1.031.0971.124

    1.0381.1121.142

    1.0461.1281.163

    1.0551.1461.186

    1.0641.1651.212

    1.0741.1861.241

    1.0851.2091.273

    1.0961.2331.309

    1.1071.261.349

    1.121.2891.393

    1.1321.321.442

    1.1451.3541.496

    1.1591.3891.555

    1.1721.4271.619

    1.1861.4671.688

    1.2011.5091.762

    1.2151.5531.839

    1.2291.5981.919

    1.2441.6432.001

    1.2581.6892.083

    1.2711.7342.164

    1.2851.7792.242

    1.2971.8212.317

    1.311.8622.386

    1.3211.8982.448

    1.3311.9312.502

    1.341.962.547

    1.3471.9832.582

    1.35322.607

    1.3582.0122.62

    1.3612.0172.621

    1.3622.0152.61

    1.3612.0062.588

    1.3581.992.553

    1.3531.9672.507

    1.3461.9372.45

    1.3371.9012.382

    1.3261.8582.304

    1.3131.812.218

    1.2981.7562.123

    1.2811.6982.022

    1.2631.6351.915

    1.2431.571.804

    1.2211.5021.692

    1.1991.4331.58

    1.1751.3631.469

    1.1511.2941.361

    1.1271.2251.258

    1.1021.161.164

    1.0781.11.085

    1.0541.0481.027

    1.0321.0121

    1.01311

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    Static load increases

    44 N

    133 N

    222 N

    Circumferential angle [deg]

    Dimensionless pressure, p/pa

    Load (22)

    46.251.24260.112

    46.251.24260.112

    46.25851.460.308

    46.34951.58260.522

    46.46451.78560.755

    46.652.0161.008

    46.7652.2661.285

    46.94552.53761.588

    47.15252.83961.921

    47.3853.16862.287

    47.62753.52662.689

    47.89453.91463.132

    48.17954.33463.622

    48.48154.78964.165

    48.855.28364.768

    49.13655.81965.439

    49.48856.39966.185

    49.85657.02867.017

    50.2457.70867.943

    50.63858.44468.973

    51.05159.23770.117

    51.47960.09271.381

    51.9261.00872.774

    52.37461.98774.299

    52.83963.02875.957

    53.31664.12877.742

    53.80165.28379.646

    54.29566.48781.653

    54.79367.73283.743

    55.29669.00685.891

    55.79970.29988.067

    56.30171.59590.24

    56.79872.8892.377

    57.28774.13794.447

    57.76475.35196.418

    58.22776.50598.262

    58.67277.58399.952

    59.09478.569101.464

    59.49179.45102.778

    59.85980.214103.875

    60.19480.848104.742

    60.49481.344105.365

    60.75581.695105.738

    60.97681.894105.853

    61.15481.939105.709

    61.28881.827105.306

    61.37781.562104.65

    61.41981.144103.749

    61.41680.581102.615

    61.36779.88101.264

    61.27579.0599.717

    61.1478.10597.997

    60.96577.05896.135

    60.75375.92894.168

    60.50774.73392.136

    60.23273.49390.076

    59.93272.22888.026

    59.61470.95986.028

    59.28269.71184.147

    58.94368.52882.488

    58.60767.48481.194

    58.29166.68480.437

    58.02466.30880.26

    57.85466.31680.36

    57.88966.44380.44

    58.06966.55380.505

    58.23966.64880.558

    58.39866.73280.603

    58.54766.80680.641

    58.68766.87280.673

    58.8266.93280.701

    58.94566.98680.725

    59.06467.03680.746

    59.17867.08280.765

    59.28667.12480.782

    59.3967.16480.798

    59.4967.20280.812

    59.58367.23680.824

    59.58367.23680.824

    Static load increases

    44 N

    133 N

    222 N

    Circumferential angle [deg]

    Temperature [ C]

    Load (21)

    111111

    1.0111.0051.0061.0081.0091.01

    1.0081.0021.0071.0121.0151.017

    1.0071.0011.011.0181.0221.025

    1.0081.0011.0141.0241.031.034

    1.0061.0031.0191.0311.0391.043

    1.0061.0051.0251.041.0481.053

    1.0051.0081.0321.0491.0591.065

    1.0061.0121.041.0591.0711.077

    1.0061.0171.0491.0711.0841.091

    1.0071.0231.061.0831.0981.107

    1.0081.031.0711.0971.1131.124

    1.011.0381.0831.1121.131.142

    1.0111.0461.0961.1281.1491.163

    1.0131.0551.111.1461.171.186

    1.0151.0641.1251.1651.1931.212

    1.0181.0741.1411.1861.2181.241

    1.021.0851.1581.2091.2461.273

    1.0231.0961.1761.2331.2761.309

    1.0261.1071.1961.261.311.349

    1.0291.121.2171.2891.3471.393

    1.0321.1321.2391.321.3871.442

    1.0351.1451.2621.3541.4311.496

    1.0381.1591.2871.3891.4781.555

    1.0421.1721.3131.4271.5291.619

    1.0451.1861.3391.4671.5831.688

    1.0481.2011.3671.5091.6411.762

    1.0511.2151.3961.5531.7011.839

    1.0541.2291.4251.5981.7631.919

    1.0571.2441.4541.6431.8262.001

    1.061.2581.4831.6891.892.083

    1.0631.2711.5121.7341.9532.164

    1.0661.2851.5411.7792.0142.242

    1.0681.2971.5681.8212.0732.317

    1.0711.311.5941.8622.1282.386

    1.0731.3211.6181.8982.1782.448

    1.0741.3311.641.9312.2222.502

    1.0761.341.6591.962.2592.547

    1.0771.3471.6761.9832.2882.582

    1.0781.3531.68822.312.607

    1.0791.3581.6972.0122.3222.62

    1.0791.3611.7022.0172.3262.621

    1.0791.3621.7032.0152.322.61

    1.0791.3611.6992.0062.3042.588

    1.0781.3581.6911.992.2792.553

    1.0771.3531.6791.9672.2452.507

    1.0761.3461.6621.9372.2012.45

    1.0741.3371.641.9012.1492.382

    1.0721.3261.6141.8582.0892.304

    1.071.3131.5841.812.0212.218

    1.0671.2981.5511.7561.9462.123

    1.0641.2811.5131.6981.8662.022

    1.0611.2631.4731.6351.7811.915

    1.0571.2431.431.571.6931.804

    1.0541.2211.3851.5021.6031.692

    1.051.1991.3381.4331.5111.58

    1.0451.1751.291.3631.421.469

    1.0411.1511.2421.2941.3311.361

    1.0361.1271.1941.2251.2451.258

    1.0321.1021.1471.161.1641.164

    1.0271.0781.1011.11.0931.085

    1.0221.0541.0591.0481.0371.027

    1.0181.0321.0241.0121.0011

    1.0131.0131.001111

    1.00911111

    1.00511111

    1.00211111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    9 N

    Static load increases

    44 N

    89 N

    133 N

    178 N

    222 N

    Predictions - 40 krpm-20um_0.6_20

    Circumferential angle [deg]

    Dimensionless pressure, p/pa

    Load (20)

    46.45246.248.16151.24255.30860.112

    46.45246.248.16151.24255.30860.112

    46.57446.25848.27351.455.4960.308

    46.7346.34948.41551.58255.69560.522

    46.88346.46448.5851.78555.91860.755

    47.02346.648.7752.0156.16261.008

    47.1746.7648.98652.2656.43161.285

    47.3346.94549.22852.53756.72661.588

    47.49947.15249.49452.83957.04961.921

    47.67747.3849.78553.16857.40162.287

    47.86147.62750.153.52657.78762.689

    48.05147.89450.43953.91458.20863.132

    48.24848.17950.80454.33458.6763.622

    48.45148.48151.19454.78959.17664.165

    48.65948.851.61255.28359.73164.768

    48.87349.13652.05755.81960.34265.439

    49.09349.48852.53356.39961.01466.185

    49.31649.85653.03957.02861.75267.017

    49.54550.2453.57857.70862.56467.943

    49.77750.63854.1558.44463.45568.973

    50.01351.05154.75759.23764.43170.117

    50.25151.47955.39860.09265.49771.381

    50.49351.9256.07561.00866.65672.774

    50.73652.37456.78861.98767.91174.299

    50.98152.83957.53463.02869.26175.957

    51.22753.31658.31364.12870.70377.742

    51.47453.80159.12165.28372.2379.646

    51.72154.29559.95666.48773.83281.653

    51.96854.79360.81367.73275.49583.743

    52.21455.29661.68769.00677.20285.891

    52.45855.79962.5770.29978.93488.067

    52.70156.30163.45671.59580.66890.24

    52.94156.79864.33772.8882.3892.377

    53.17857.28765.20374.13784.04694.447

    53.41257.76466.04675.35185.64396.418

    53.64158.22766.85676.50587.14698.262

    53.86758.67267.62277.58388.53599.952

    54.08759.09468.33778.56989.79101.464

    54.30359.49168.9979.4590.892102.778

    54.51259.85969.57480.21491.825103.875

    54.71660.19470.0880.84892.577104.742

    54.91360.49470.50181.34493.136105.365

    55.10360.75570.83381.69593.495105.738

    55.28660.97671.06981.89493.647105.853

    55.46361.15471.20681.93993.591105.709

    55.63161.28871.24381.82793.325105.306

    55.79361.37771.17881.56292.854104.65

    55.94761.41971.01281.14492.182103.749

    56.09361.41670.74780.58191.32102.615

    56.23361.36770.38779.8890.28101.264

    56.36561.27569.93779.0589.07699.717

    56.4961.1469.40278.10587.72797.997

    56.60860.96568.79277.05886.25796.135

    56.7260.75368.11375.92884.69194.168

    56.82660.50767.37874.73383.05892.136

    56.92660.23266.59873.49381.38990.076

    57.02259.93265.78572.22879.71188.026

    57.11359.61464.95170.95978.05386.028

    57.259.28264.11269.71176.4684.147

    57.28558.94363.28668.52875.00282.488

    57.36758.60762.50967.48473.7981.194

    57.44858.29161.84166.68472.95380.437

    57.5358.02461.36766.30872.69380.26

    57.61457.85461.26366.31672.79780.36

    57.70357.88961.41566.44372.89880.44

    57.80458.06961.55866.55372.98280.505

    57.92858.23961.68766.64873.05380.558

    58.08658.39861.80266.73273.11480.603

    58.26558.54761.90766.80673.16780.641

    58.44158.68762.00266.87273.21380.673

    58.61558.8262.0966.93273.25480.701

    58.78658.94562.1766.98673.29180.725

    58.95459.06462.24567.03673.32480.746

    59.1259.17862.31667.08273.35480.765

    59.28459.28662.38167.12473.38280.782

    59.44659.3962.44467.16473.40780.798

    59.60659.4962.50367.20273.43180.812

    59.75859.58362.55767.23673.45280.824

    59.75859.58362.55767.23673.45280.824

    9 N

    Static load increases

    44 N

    89 N

    133 N

    178 N

    222 N

    Predictions - 40 krpm-20um_0.6_20

    Circumferential angle [deg]

    Temperature [ C]

    Load (19)

    0.4831

    1.932

    4.348

    7.729

    12.08

    Solid shaft

    tS = 10 mm

    tS = 2 mm

    Shaft wall thickness decreases

    Predictions - 40 krpm-20um_0.6_20

    Rotor speed [krpm]

    Centrifugal growth [ C]

    Load (16)

    0.48311.0541.712

    1.9324.2176.846

    4.3489.48815.4

    7.72916.8727.39

    12.0826.3542.79

    Solid shaft

    tS = 10 mm

    tS = 2 mm

    Shaft wall thickness decreases

    Predictions - 40 krpm-20um_0.6_20

    Rotor speed [krpm]

    Centrifugal growth [m]

    Load (18)

    8792000-44560093390097450008752100-36220048330010027000

    9037000-176100726700100700009277100-7409342888010247000

    9465000160800425200104800001017600030090036151010637000

    9893000420900163000108100001079300065758017911011072000

    10320000623700-6547011060000113980008773201332011416000

    10710000784600-24970011260000119840001005200-8609611679000

    Solid lines: THDDash lines: Isothermal

    KXX

    THD

    KYY

    KXY

    KYX

    Isothermal

    Static load [N]

    Stiffness coefficient [MN/m]

    Load (17)

    742.3-193.1235.1529.8622.88-173.95244.72546

    659.9-136.5227.4478.7565.24-157.39218.65498.52

    538.7-74.91215.9409.4509.03-124.49197.16427.97

    435.5-32.93200.1349.3430.7-79.451188.34367.62

    349.9-5.784179.6295.1362.34-45.516172.35325.72

    282.212.23157.2246.9315.66-26.816151.76295.17

    Solid lines: THDDash lines: Isothermal

    CXX

    THD

    CYY

    CXY

    CYX

    Isothermal

    Static load [N]

    Damping coefficient [KN-s/m]

    Load (15)

    26.25965.35316224410.0209260.016951

    18.87729.59449215420.0203940.017041

    14.82118.08433215740.0201110.01746

    12.30114.83343536530.0201620.017994

    9.522712.18104744070.0204370.018771

    8.392210.37674908260.0208540.019711

    THD

    Isothermal

    THD

    Isothermal

    Static load [N]

    Journal attitude angle [deg]

    Drag torque [N-m]

    Load (14)

    0.840951.83145365716.57815.572

    4.22465.434352546513.99812.655

    8.424910.278448659711.4459.3519

    12.27414.61505917069.72967.1382

    16.01318.78185959918.54525.5448

    19.65122.65045624357.70944.4498

    THD

    Isothermal

    THD

    Isothermal

    c' = 17 m

    Static load [N]

    Journal eccentricity [m]

    Minimum film thickness [m]

    Load (10)

    102137168831251907455

    106136168881281867760

    112141181981361928270

    1191491931101482029080

    1261602051241622149692

    134176217138177228101104

    30,000 rpm

    40,000 rpm

    50,000 rpm

    20,000 rpm

    Test data (Mid-plane)

    Predictions(Mid-plane)

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (13)

    13712574551245311164

    136128776012255110.566.5

    14113682701236011571

    14914890801306912277

    160162969214181130.582

    1761771011041559514586

    Test data (Mid-plane)

    40,000 rpm

    Test data (Edge)

    20,000 rpm

    Predictions(Edge)

    Predictions(Mid-plane)

    Test data - 40 krpm

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    AxialT133 (3)

    93.974129.95410212669.37777

    102.168139.62111914975.13990

    105.271143.0949811877.11477

    106.958144.86278.185

    108.082145.99478.92

    108.893146.7979.464

    109.477147.34779.862

    109.878147.71180.141

    110.125147.92180.319

    110.24147.99980.409

    110.116147.88780.314

    109.857147.64580.131

    109.445147.24779.847

    108.848146.65579.442

    108.022145.81878.891

    106.879144.63478.147

    105.167142.79677.062

    102.034139.23875.07

    93.845129.57169.309

    20,000 rpm

    30,000 rpm

    40,000 rpm

    Side edge (rear)

    Side edge (front)- Edges

    Mid-plane

    Test data

    Predictions

    Axial node number

    Temperature [C]

    Sheet2

    50krpm222N30-50krpm89N30-50krpm133N40krpm1.932um

    Side edgeMid-planeSide edgekrpmSide edgeMid-planeSide edgekrpmSide edgeMid-planeSide edgershaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    183217164180degTest data309611292309611292Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg41118401191411114011914111190.8307625.5816.32217.74816.5772.10E-028.88E+06-4.67E+059.55E+059.86E+06755.5-197.1240.6541.6

    207215207311195015417113650154171136444.101417.58313.46716.69314.1562.06E-029.15E+06-2.02E+057.61E+051.02E+07674.9-139.3230.9491.9

    21120898.19214.1510.41215.63311.6652.04E-029.62E+061.28E+054.78E+051.06E+07556.4-75.83215.8425.3

    13311.92312.3628.22614.8339.97122.04E-021.01E+073.80E+052.36E+051.10E+07456.3-31.56195.4368.8

    20.52.0530-50krpm30-50krpm17815.55110.5646.611114.1518.7622.07E-021.06E+075.69E+052.95E+041.13E+07375.4-2.171169.2319.9

    34.54.116.4NSide edgeMid-planeSide edgeEdge-avg30umN30405020umN30405022218.9739.20525.456813.5717.91442.12E-021.10E+077.17E+05-1.29E+051.15E+07312.219.1139.7277.8

    6.5209647464643097409176145

    4467776666.50.844870.74417615540krpm1.932um20krpm0.5um

    50krpm89N89718271718911089167155rshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyyrshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    ReaCenterFront13377907777133132133165163Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/mLoad (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    1788296828217817890.8409526.25916.31117.7816.5782.09E-028.79E+06-4.46E+059.34E+059.75E+06742.3-193.1235.1529.891.430841.57617.11217.74617.2198.82E-038.22E+065.55E+06-2.81E+055.26E+057.17E+061922.1-720.931053.31829.7

    190deg41118222861018686222222444.224618.87713.26316.70613.9982.04E-029.04E+06-1.76E+057.27E+051.01E+07659.9-136.5227.4478.7446.751830.17512.08315.06512.6998.93E-031.31E+076.67E+063244.31.19E+057.80E+061510.7-497.57773.111685.2

    1001091003111930um898.424914.82110.06715.67711.4452.01E-029.47E+061.61E+054.25E+051.05E+07538.7-74.91215.9409.48912.23721.17.775613.0069.10269.44E-031.31E+078.23E+063.91E+05-597518.53E+061202.8-281.5462.951494.9

    21120309861028384.52095420umN30405013312.27412.3017.788414.8939.72962.02E-029.89E+064.21E+051.63E+051.08E+07435.5-32.93200.1349.313316.75515.5475.270511.6237.14471.00E-021.47E+079.47E+066.46E+05-1.28E+059.10E+061085.1-137.47278.271357.8

    44901068788.50.7446820915714517816.0139.52276.101514.2258.54522.04E-021.03E+076.24E+05-6.55E+041.11E+07349.9-5.784179.6295.117820.92612.1393.678510.5475.92781.07E-021.47E+071.05E+078.24E+05-1.79E+059.58E+061053.3-38.164156.41249.8

    8996112929489880.74414122219.6518.39224.840913.6477.70942.09E-021.07E+077.85E+05-2.50E+051.13E+07282.212.23157.2246.9

    30krpm89N1331021199810013310789

    ReaCenterFront178108126103105.5178133ex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyyex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    222113134109111222178mmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/mmmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg4111830um2229.00.0400008.22E+068.75E+06-3.62E+054.83E+051.00E+07622.9-174.0244.7546.09.00.0200008.22E+065.91E+06-4.71E+057.63E+057.24E+062018.9-812.1938.51969.9

    74787431119409114137108111096044.00.0400001.31E+079.28E+06-7.41E+044.29E+051.02E+07565.2-157.4218.7498.544.00.0200001.31E+076.96E+06-4.34E+043.60E+058.14E+061552.9-503.4825.01790.5

    2112044114136107110.50.7447220umN30405089.00.0400001.47E+071.02E+073.01E+053.62E+051.06E+07509.0-124.5197.2428.089.00.0200001.31E+078.72E+064.62E+05-9.27E+038.88E+061245.3-269.7525.71606.7

    89119141111115899220-209141122133.00.0400001.47E+071.08E+076.58E+051.79E+051.11E+07430.7-79.5188.3367.6133.00.0200001.47E+071.02E+077.75E+05-1.26E+059.44E+061159.4-135.6325.81470.9

    70krpm89N1331261491181221330.744141121178.00.0400001.57E+071.14E+078.77E+051.33E+041.14E+07362.3-45.5172.4325.7178.00.0200001.47E+071.13E+079.47E+05-1.82E+059.89E+061178.0-56.5210.21378.7

    ReaCenterFront178134160127130.517889222.00.0400001.57E+071.20E+071.01E+06-8.61E+041.17E+07315.7-26.8151.8295.2

    222149176141145222133139136FOIL Bearing static load performance parameters

    190deg4111825um178150150Load-Xe_structureexeyEccentricityeccentricityAngleMinimum filmFx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR

    12914212931119509146168131138.50997222200.00.0400001.57E+071.17E+079.47E+05-4.50E+041.16E+07337.2-35.0162.3309.3[N]mmmmratiodeg[m]NNNbar[bar]N-m[kW]N/m-

    21120441461681281370.744989.0020.101.231.331.810.1047.1816.72-9.0-0.29.00.041.098.14E-031.70E-026.85E+060.00

    891541811361458911225umN30405044.0023.536.724.207.930.4332.0310.88-44.0-0.344.00.211.398.40E-031.76E-027.57E+060.00

    133162193143152.513312920-209119110FOIL Bearing static load performance parameters89.0027.0112.945.0413.890.7521.266.03-89.2-0.489.20.431.749.11E-031.91E-028.70E+060.03

    Themmal gradient (Deg C/mm)1781722051541631781460.844Load-Xe_structureexeyEccentricityeccentricityAngleMinimum filmMinimum filmMinimum filmFx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR133.0030.0118.005.1018.71.015.813.27-133.98-1.3134.00.652.079.94E-032.08E-029.74E+060.00

    300000.24390243922218321716317322289133133[N]mmmmratiodeg[m][m][m]NNNbar[bar]N-m[kW]N/m-178.0033.1322.474.8022.971.2412.071.78-178.7-0.8178.70.872.391.09E-022.27E-021.06E+070.00

    500000.54878048782.052.051339.0018.630.761.661.830.1165.3515.3316.71915.572-9.0-0.09.00.041.181.70E-027.10E-029.58E+060.00

    700000.79268292684.116.44.116.417817117144.0021.974.732.685.430.3229.5912.0115.18412.655-43.6-0.743.60.211.401.70E-027.14E-029.87E+060.00

    22289.0025.399.773.1910.280.6018.088.0813.3649.3519-89.0-0.389.00.431.711.75E-027.31E-021.04E+070.00

    133.0028.3914.133.7414.60.914.835.3612.1057.1382-133.08-0.9133.10.652.031.80E-027.54E-021.08E+070.00

    50krpm44N50krpm133N20umN304050178.0031.4518.363.9618.781.1012.183.4710.9775.5448-178.2-0.7178.20.862.351.88E-027.86E-021.12E+070.139N : 20 - 100 krpm

    ReaCenterFrontReaCenterFront20-20910790222.0034.2522.284.0822.651.3310.382.2410.0264.4498-222.1-1.0222.11.082.651.97E-028.26E-021.16E+070.28ex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    0.644mmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg41118190deg41118891071009.00.0200008.22E+065.91E+06-4.71E+057.63E+057.24E+062018.9-812.1938.51969.9

    8390833111911912711831119133200.0032.8520.353.9820.731.2111.062.8010.4874.9532-200.1-0.3200.10.972.501.92E-028.05E-021.14E+070.229.00.0400008.22E+068.09E+06-5.19E+056.83E+058.73E+06879.9-263.9276.2742.7

    21120211201781231209.00.0600008.22E+068.88E+06-4.42E+058.83E+059.32E+06572.2-143.3137.3428.6

    2229.00.0800008.22E+069.37E+06-3.76E+058.79E+059.67E+06411.3-91.384.8289.0

    9.00.01000008.22E+069.66E+06-3.33E+058.64E+059.90E+06315.8-64.659.7213.7

    30krpm44N30krpm133N32umN304050

    ReaCenterFrontReaCenterFront20-209117100FOIL Bearing static load performance parameters

    0.644Speede_structureexeyEccentricityeccentricityAngleMinimum filmMinimum film (center)Minimum film (near edge)Fx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR

    190deg41118190deg4111889128128[rpm]mmmmratiodeg[m][m][m]NNNbar[bar]N-m[kW]N/m-

    596359311198891883111913320000.0020.101.231.331.810.1047.1816.7217.26116.81-9.0-0.29.00.041.098.14E-031.70E-026.85E+060.00

    211202112017840000.0020.101.090.711.300.0733.0117.2317.85517.334-9.0-0.19.00.041.091.62E-026.80E-028.64E+060.15

    22260000.0020.101.040.511.160.0626.0517.3918.02317.497-9.0-0.09.00.041.092.43E-021.53E-019.32E+060.19

    70krpm44N70krpm133N80000.0020.101.000.411.10.122.2917.4718.117.583-8.99-0.29.00.041.093.24E-022.71E-019.71E+060.20

    ReaCenterFrontReaCenterFront27umN304050180deg100000.0020.100.980.341.040.0619.0817.5218.14517.642-9.0-0.19.00.041.094.05E-024.24E-019.95E+060.20

    20-209609921486175

    190deg41118190deg411180.644999920krpm0.5um

    11112111131119150164150311198980109214109182rshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    2112021120133Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    17810814019820091.430841.57617.11217.74617.2198.82E-035.55E+06-2.81E+055.26E+057.17E+061922.1-720.931053.31829.7

    222440.9669928.4117.61118.80817.8251.90E-027.61E+06-4.00E+058.27E+058.78E+06876.26-233.34313.41706.46

    Themmal gradient (Deg C/mm)Themmal gradient (Deg C/mm)890.8242517.44217.84619.69218.2743.07E-028.65E+06-2.35E+055.34E+059.56E+06470.46-105.18142.74379.62

    300000.243902439300000.182926829325umN3040501330.770156.163918.07820.33918.8984.38E-029.28E+06-300122.53E+051.01E+07289.36-54.98590.006232.87

    500000.4268292683500000.548780487820-2091171780.8279-4.146717.55321.27319.7595.75E-029.69E+061.61E+05837191.04E+07206.68-32.47373.863153.01

    700000.6097560976700000.85365853660.744

    89137

    themal gradient deg C/mmMid-planeTemperauture Deg CSide edgeTemperauture Deg C133

    300005000070000300005000070000300005000070000178169

    440.2439024390.42682926830.60975609764463901215983111222

    890.2439024390.54878048780.7926829268897810914274100129

    1330.18292682930.54878048780.85365853661339112716488119150Solid shaftRadial growthWall thickness: 10 mmRadial growthWall thickness: 2 mmRadial growth

    2.00E+014.83E-074.83E-012.00E+011.05E-061.05E+002.00E+011.71E-061.71E+00

    Solid journalMax1804.00E+011.93E-061.93E+004.00E+014.22E-064.22E+004.00E+016.85E-066.85E+00

    20umN3040503040506.00E+014.35E-064.35E+006.00E+019.49E-069.49E+006.00E+011.54E-051.54E+01

    20-2098.00E+017.73E-067.73E+008.00E+011.69E-051.69E+018.00E+012.74E-052.74E+01

    0.6441.00E+021.21E-051.21E+011.00E+022.64E-052.64E+011.00E+024.28E-054.28E+01

    898811715988117157

    133

    Axial temp. at 37 node number178114145183114145183

    30K 89N22220 krpm

    63.39783.177106.394019N44N89N133N178N222N

    63.39783.177106.3940.0132Solid journalMax180XPTPTPTPTPTPT

    70.93994.777121.4050.026320umN3040503040500146.452146.2148.161151.242155.308160.112

    73.799.969128.7050.039420-2094.6151.01146.4521.00546.21.00648.1611.00851.2421.00955.3081.0160.112

    75.243103.026133.1230.05250.65449.2311.00846.5741.00246.2581.00748.2731.01251.41.01555.491.01760.308

    76.294105.108136.1440.065689961311879413117613.8461.00746.731.00146.3491.0148.4151.01851.5821.02255.6951.02560.522

    77.058106.616138.3260.078713318.4621.00846.8831.00146.4641.01448.581.02451.7851.0355.9181.03460.755

    77.616107.714139.9120.091817812315920612115920223.0771.00647.0231.00346.61.01948.771.03152.011.03956.1621.04361.008

    78.012108.489141.030.104922227.6921.00647.171.00546.761.02548.9861.0452.261.04856.4311.05361.285

    78.273108.998141.7590.1171032.3081.00547.331.00846.9451.03249.2281.04952.5371.05956.7261.06561.588

    78.426109.29142.170.13111Solid journalMax18036.9231.00647.4991.01247.1521.0449.4941.05952.8391.07157.0491.07761.921

    78.275109.008141.7840.1441220umN30405030405041.5381.00647.6771.01747.381.04949.7851.07153.1681.08457.4011.09162.287

    78.012108.5141.0590.1571320-20946.1541.00747.8611.02347.6271.0650.11.08353.5261.09857.7871.10762.689

    77.616107.724139.9420.17140.74450.7691.00848.0511.0347.8941.07150.4391.09753.9141.11358.2081.12463.132

    77.056106.624138.3550.183158915114755.3851.0148.2481.03848.1791.08350.8041.11254.3341.1358.671.14263.622

    76.289105.116136.1720.19616133601.01148.4511.04648.4811.09651.1941.12854.7891.14959.1761.16364.165

    75.237103.032133.1520.2091717817924217623764.6151.01348.6591.05548.81.1151.6121.14655.2831.1759.7311.18664.768

    73.69299.974128.7360.2221822269.2311.01548.8731.06449.1361.12552.0571.16555.8191.19360.3421.21265.439

    70.93194.785121.4440.2351973.8461.01849.0931.07449.4881.14152.5331.18656.3991.21861.0141.24166.185

    63.3983.185106.4410.24820Solid journalMax18078.4621.0249.3161.08549.8561.15853.0391.20957.0281.24661.7521.27367.017

    63.3983.185106.4410.2612119umN203040502030405020-edge40-edge83.0771.02349.5451.09650.241.17653.5781.23357.7081.27662.5641.30967.943

    20-209609614823055831251905312487.6921.02649.7771.10750.6381.19654.151.2658.4441.3163.4551.34968.973

    0.6544619514823060881281865512292.3081.02950.0131.1251.0511.21754.7571.28959.2371.34764.4311.39370.117

    897111314221770981361926012396.9231.03250.2511.13251.4791.23955.3981.3260.0921.38765.4971.44271.381

    133821131512108011014820269130101.5381.03550.4931.14551.921.26256.0751.35461.0081.43166.6561.49672.774

    178941261652209212416221481141106.1541.03850.7361.15952.3741.28756.7881.38961.9871.47867.9111.55574.299

    22210714018023310413817722895155110.7691.04250.9811.17252.8391.31357.5341.42763.0281.52969.2611.61975.957

    115.3851.04551.2271.18653.3161.33958.3131.46764.1281.58370.7031.68877.742

    1201.04851.4741.20153.8011.36759.1211.50965.2831.64172.231.76279.646

    124.6151.05151.7211.21554.2951.39659.9561.55366.4871.70173.8321.83981.653

    222 NTHDAdiabatic129.2311.05451.9681.22954.7931.42560.8131.59867.7321.76375.4951.91983.743

    20107128133.8461.05752.2141.24455.2961.45461.6871.64369.0061.82677.2022.00185.891

    30140157138.4621.0652.4581.25855.7991.48362.571.68970.2991.8978.9342.08388.067

    40180197143.0771.06352.7011.27156.3011.51263.4561.73471.5951.95380.6682.16490.24

    50233256147.6921.06652.9411.28556.7981.54164.3371.77972.882.01482.382.24292.377

    152.3081.06853.1781.29757.2871.56865.2031.82174.1372.07384.0462.31794.447

    156.9231.07153.4121.3157.7641.59466.0461.86275.3512.12885.6432.38696.418

    161.5381.07353.6411.32158.2271.61866.8561.89876.5052.17887.1462.44898.262

    20krpm30krpm40krpm50krpm166.1541.07453.8671.33158.6721.6467.6221.93177.5832.22288.5352.50299.952

    89133891338913389133170.7691.07654.0871.3459.0941.65968.3371.9678.5692.25989.792.547101.464

    160.30869.37785.65193.974123.254129.954183.102187.618175.3851.07754.3031.34759.4911.67668.991.98379.452.28890.8922.582102.778

    260.30869.37785.6519693.974102123.254119129.954126183.102154187.6181621801.07854.5121.35359.8591.68869.574280.2142.3191.8252.607103.875

    364.20475.13990.94102.168129.362139.621189.318197.386184.6151.07954.7161.35860.1941.69770.082.01280.8482.32292.5772.62104.742

    466.14477.11493.727105.271132.374143.094191.162199.841189.2311.07954.9131.36160.4941.70270.5012.01781.3442.32693.1362.621105.365

    567.32178.18595.374106.958133.993144.862191.793200.697193.8461.07955.1031.36260.7551.70370.8332.01581.6952.3293.4952.61105.738

    668.12678.9296.473108.082135.008145.994192.059201.156198.4621.07955.2861.36160.9761.69971.0692.00681.8942.30493.6472.588105.853

    768.70979.46497.252108.893135.697146.79192.184201.465203.0771.07855.4631.35861.1541.69171.2061.9981.9392.27993.5912.553105.709

    869.13179.86297.806109.477136.168147.347192.227201.657207.6921.07755.6311.35361.2881.67971.2431.96781.8272.24593.3252.507105.306

    969.42580.14198.183109.878136.474147.711192.208201.744212.3081.07655.7931.34661.3771.66271.1781.93781.5622.20192.8542.45104.65

    1069.61180.31998.413110.125136.648147.921192.154201.756216.9231.07455.9471.33761.4191.6471.0121.90181.1442.14992.1822.382103.749

    1169.70180.40998.517112110.24119136.707141147.999149192.066181201.702193221.5381.07256.0931.32661.4161.61470.7471.85880.5812.08991.322.304102.615

    1269.60980.31498.405110.116136.61147.887192.012201.631226.1541.0756.2331.31361.3671.58470.3871.8179.882.02190.282.218101.264

    1369.4280.13198.164109.857136.402147.645191.957201.525230.7691.06756.3651.29861.2751.55169.9371.75679.051.94689.0762.12399.717

    1469.12279.84797.776109.445136.062147.247191.867201.344235.3851.06456.491.28161.141.51369.4021.69878.1051.86687.7272.02297.997

    1568.69579.44297.21108.848135.553146.655191.708201.0482401.06156.6081.26360.9651.47368.7921.63577.0581.78186.2571.91596.135

    1668.10878.89196.418108.022134.82145.818191.448200.613244.6151.05756.721.24360.7531.4368.1131.5775.9281.69384.6911.80494.168

    1767.29678.14795.303106.879133.753144.634191.013199.985249.2311.05456.8261.22160.5071.38567.3781.50274.7331.60383.0581.69292.136

    1866.11377.06293.637105.167132.068142.796190.156198.894253.8461.0556.9261.19960.2321.33866.5981.43373.4931.51181.3891.5890.076

    1964.16575.0790.828102.034128.976139.238188.038196.136258.4621.04557.0221.17559.9321.2965.7851.36372.2281.4279.7111.46988.026

    2060.26969.30985.5399293.84598122.858111129.571118181.798136186.343143263.0771.04157.1131.15159.6141.24264.9511.29470.9591.33178.0531.36186.028

    2160.26969.30985.53993.845122.858129.571181.798186.343267.6921.03657.21.12759.2821.19464.1121.22569.7111.24576.461.25884.147

    272.3081.03257.2851.10258.9431.14763.2861.1668.5281.16475.0021.16482.488

    2717796102119126154162276.9231.02757.3671.07858.6071.10162.5091.167.4841.09373.791.08581.194

    118290112119141149181193281.5381.02257.4481.05458.2911.05961.8411.04866.6841.03772.9531.02780.437

    2071779298111118136143286.1541.01857.531.03258.0241.02461.3671.01266.3081.00172.693180.26

    290.7691.01357.6141.01357.8541.00161.263166.316172.797180.36

    295.3851.00957.703157.889161.415166.443172.898180.44

    3001.00557.804158.069161.558166.553172.982180.505

    304.6151.00257.928158.239161.687166.648173.053180.558

    309.231158.086158.398161.802166.732173.114180.603

    313.846158.265158.547161.907166.806173.167180.641

    318.462158.441158.687162.002166.872173.213180.673

    323.077158.615158.82162.09166.932173.254180.701

    327.692158.786158.945162.17166.986173.291180.725

    332.308158.954159.064162.245167.036173.324180.746

    336.923159.12159.178162.316167.082173.354180.765

    341.538159.284159.286162.381167.124173.382180.782

    346.154159.446159.39162.444167.164173.407180.798

    350.769159.606159.49162.503167.202173.431180.812

    355.385159.758159.583162.557167.236173.452180.824

    360159.758159.583162.557167.236173.452180.824

    Update Curve Fit

    Sheet2

    11111111

    &A

    Page &P

    Kxx

    Kxy

    Kyx

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    Kxx fit

    Kxy fit

    Kyx fit

    Kyy fit

    Load (12)

    11111111

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    Load (11)

    11111111

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    Mxx

    Mxy

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    Myx fit

    Myy fit

    AxialT133 (2)

    11111111

    NOTE to USER: WFR and Keq make sense only for frequency INDEPENDENT force coefficients - GIVEN Here only as a reference

    Journal eccentricity along X-direction.

    Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    Journal eccentricity along Y-direction. Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    External load along X-direction. See typical notation.

    Used only if VERY LOAD=FIND Eccentricity Option is active.

    After execution, check that output reaction force balances load, i.e.Load-X + FX =0

    External load along Y-direction. See typical notation.

    Used only if VARY LOAD= FIND ECCENTRICITY Option is active. After execution, check that output reaction force balances load, i.e.Load-Y + FY =0

    Table of speeds (RPM)rotor or journal speed if Synchronous analysis option selected.orrotor whirl speed if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Table of impedance coefficients (real part): Rij = Kij + w^w Mijw( frequency in rad/s)

    Rotor or journal speed in rpm if Synchronous analysis option selected with varying loads.orBearing load (Load-X) in N if Synchronous analysis option selected with varying speeds.orRotor whirl speed in Hz if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    e_structure, rotor displacement due to lateral force along X-direction at null rotor speed. = radial clearance + max. bump deflection

    e_structure > ex, ey always.

    Journal eccentricity along X-direction, resulting from applied load

    Journal eccentricity along Y-direction, resulting from applied load

    Journal eccentricity = sqrt (ex^2+ey^2).

    Dimensionless journal eccentricity resulting from applied load

    Jounal attitude angle in deg.See FIGURE in TYPICAL NOTATION

    Minimum gas film thickness between top foil and journal.

    Bearing reaction force along X-direction

    Bearing reaction force along Y-direction

    Bearing reaction force = Sqrt (Fx^2 + Fy^2)

    Bearing Specific load= Bearing load (or Force)/Rotor diameter/Axial length

    Maximum gas film pressure

    Bearing torque induced by gas film drag force

    = Bearing torque times rotor speed (rad/s)

    Equivalent stiffness (Keq) and whirl frequency ratio (WFR) make sense only for synchronous excitation.

    Disregard results if asynchronous calculations

    Whril Frequency Ratio

    Minimum gas film thickness between top foil and journal.

    Minimum gas film thickness between top foil and journal.

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Tae Ho Kim:With consideration of foil material degradation

    Tae Ho Kim:Without foil material degradation

    Update Curve Fit

    &A

    Page &P

    Kxx

    Kxy

    Kyx

    Kyy

    Kxx fit

    Kxy fit

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    Kyy fit

    1

    1

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    1

    1

    1

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    Cyy fit

    Load (9)

    11111111

    &A

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    Mxx

    Mxy

    Myx

    Myy

    Mxx fit

    Mxy fit

    Myx fit

    Myy fit

    Load (8)

    11111111

    NOTE to USER: WFR and Keq make sense only for frequency INDEPENDENT force coefficients - GIVEN Here only as a reference

    Journal eccentricity along X-direction.

    Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    Journal eccentricity along Y-direction. Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    External load along X-direction. See typical notation.

    Used only if VERY LOAD=FIND Eccentricity Option is active.

    After execution, check that output reaction force balances load, i.e.Load-X + FX =0

    External load along Y-direction. See typical notation.

    Used only if VARY LOAD= FIND ECCENTRICITY Option is active. After execution, check that output reaction force balances load, i.e.Load-Y + FY =0

    Table of speeds (RPM)rotor or journal speed if Synchronous analysis option selected.orrotor whirl speed if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Table of impedance coefficients (real part): Rij = Kij + w^w Mijw( frequency in rad/s)

    Rotor or journal speed in rpm if Synchronous analysis option selected with varying loads.orBearing load (Load-X) in N if Synchronous analysis option selected with varying speeds.orRotor whirl speed in Hz if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    e_structure, rotor displacement due to lateral force along X-direction at null rotor speed. = radial clearance + max. bump deflection

    e_structure > ex, ey always.

    Journal eccentricity along X-direction, resulting from applied load

    Journal eccentricity along Y-direction, resulting from applied load

    Journal eccentricity = sqrt (ex^2+ey^2).

    Dimensionless journal eccentricity resulting from applied load

    Jounal attitude angle in deg.See FIGURE in TYPICAL NOTATION

    Minimum gas film thickness between top foil and journal.

    Bearing reaction force along X-direction

    Bearing reaction force along Y-direction

    Bearing reaction force = Sqrt (Fx^2 + Fy^2)

    Bearing Specific load= Bearing load (or Force)/Rotor diameter/Axial length

    Maximum gas film pressure

    Bearing torque induced by gas film drag force

    = Bearing torque times rotor speed (rad/s)

    Equivalent stiffness (Keq) and whirl frequency ratio (WFR) make sense only for synchronous excitation.

    Disregard results if asynchronous calculations

    Whril Frequency Ratio

    Tae Ho Kim:With consideration of foil material degradation

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Update Curve Fit

    &A

    Page &P

    Kxx

    Kxy

    Kyx

    Kyy

    Kxx fit

    Kxy fit

    Kyx fit

    Kyy fit

    1

    1

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    Cxy fit

    Cyx fit

    Cyy fit

    AxialT133

    11111111

    &A

    Page &P

    Mxx

    Mxy

    Myx

    Myy

    Mxx fit

    Mxy fit

    Myx fit

    Myy fit

    AxialT89

    107128

    140157

    180197

    233256

    NOTE to USER: WFR and Keq make sense only for frequency INDEPENDENT force coefficients - GIVEN Here only as a reference

    Journal eccentricity along X-direction.

    Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    Journal eccentricity along Y-direction. Used only if VARY ECCENTRICITY= FIND BEARING LOAD Option is active.

    External load along X-direction. See typical notation.

    Used only if VERY LOAD=FIND Eccentricity Option is active.

    After execution, check that output reaction force balances load, i.e.Load-X + FX =0

    External load along Y-direction. See typical notation.

    Used only if VARY LOAD= FIND ECCENTRICITY Option is active. After execution, check that output reaction force balances load, i.e.Load-Y + FY =0

    Table of speeds (RPM)rotor or journal speed if Synchronous analysis option selected.orrotor whirl speed if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Table of impedance coefficients (real part): Rij = Kij + w^w Mijw( frequency in rad/s)

    Rotor or journal speed in rpm if Synchronous analysis option selected with varying loads.orBearing load (Load-X) in N if Synchronous analysis option selected with varying speeds.orRotor whirl speed in Hz if Asynchronous analysis option selected. In this case CONSTANT SHAFT RPM for all cases.

    e_structure, rotor displacement due to lateral force along X-direction at null rotor speed. = radial clearance + max. bump deflection

    e_structure > ex, ey always.

    Journal eccentricity along X-direction, resulting from applied load

    Journal eccentricity along Y-direction, resulting from applied load

    Journal eccentricity = sqrt (ex^2+ey^2).

    Dimensionless journal eccentricity resulting from applied load

    Jounal attitude angle in deg.See FIGURE in TYPICAL NOTATION

    Minimum gas film thickness between top foil and journal.

    Bearing reaction force along X-direction

    Bearing reaction force along Y-direction

    Bearing reaction force = Sqrt (Fx^2 + Fy^2)

    Bearing Specific load= Bearing load (or Force)/Rotor diameter/Axial length

    Maximum gas film pressure

    Bearing torque induced by gas film drag force

    = Bearing torque times rotor speed (rad/s)

    Equivalent stiffness (Keq) and whirl frequency ratio (WFR) make sense only for synchronous excitation.

    Disregard results if asynchronous calculations

    Whril Frequency Ratio

    Minimum gas film thickness between top foil and journal.

    Minimum gas film thickness between top foil and journal.

    Tae Ho Kim:With consideration of foil material degradation

    Structural foil stiffness coefficient (Kstructure)Concept: K = -dFx/dx, change in lateral force due to change in displacement at null rotor speed.Kstructure > Kxx, Kyy always.

    Table of stiffness coefficients (Kxx, Kxy, Kyx, Kyy)Concept: Kij = -dFi/dXj, change in lateral force (i) due to change in displacement (j).

    Table of damping coefficients (Cxx, Cxy, Cyx, Cyy)Concept: Cij = -dFi/dVj, change in lateral force (i) due to change in velocity (j).

    Test data - Mid-plane

    222 N

    THD solution

    Adiabatic wall

    Predictions - 40 krpm-20um_0.6_20

    Rotor speed [krpm]

    Peak temperature [ C]

    Load (7)

    1371257455124531141086464

    1361287760122551141076766

    1411368270123601191117171

    1491489080130691261187777

    1601629692141811341278282

    176177101104155951491418686

    Test data - Mid-plane

    40,000 rpm

    Test data - Edges

    20,000 rpm

    Predictions- Edges

    Predictions- Mid-plane

    Test data - 40 krpm

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (6)

    93.974129.954187.61810212616269.37777

    102.168139.621197.38611914919375.13990

    105.271143.094199.8419811814377.11477

    106.958144.862200.69778.185

    108.082145.994201.15678.92

    108.893146.79201.46579.464

    109.477147.347201.65779.862

    109.878147.711201.74480.141

    110.125147.921201.75680.319

    110.24147.999201.70280.409

    110.116147.887201.63180.314

    109.857147.645201.52580.131

    109.445147.247201.34479.847

    108.848146.655201.04879.442

    108.022145.818200.61378.891

    106.879144.634199.98578.147

    105.167142.796198.89477.062

    102.034139.238196.13675.07

    93.845129.571186.34369.309

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Axial node number

    Temperature [C]

    Load (4)

    10213712517455

    106136128447760

    112141136898270

    1191491481339080

    1261601621789692

    134176177222101104

    20,000 rpm

    30,000 rpm

    40,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (5)

    1021375312574961486055

    1061365512877951486160

    11214160136821131427170

    11914969148901131518280

    12616081162961261659492

    13417695177101140180107104

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (3)

    93.974129.954187.61810212616269.37777

    102.168139.621197.38611914919375.13990

    105.271143.094199.8419811814377.11477

    106.958144.862200.69778.185

    108.082145.994201.15678.92

    108.893146.79201.46579.464

    109.477147.347201.65779.862

    109.878147.711201.74480.141

    110.125147.921201.75680.319

    110.24147.999201.70280.409

    110.116147.887201.63180.314

    109.857147.645201.52580.131

    109.445147.247201.34479.847

    108.848146.655201.04879.442

    108.022145.818200.61378.891

    106.879144.634199.98578.147

    105.167142.796198.89477.062

    102.034139.238196.13675.07

    93.845129.571186.34369.309

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Axial node number

    Temperature [C]

    Load (2)

    85.651123.254183.10296119154160.30871

    90.94129.362189.31811214118164.20482

    93.727132.374191.1629211113666.14471

    95.374133.993191.79367.321

    96.473135.008192.05968.126

    97.252135.697192.18468.709

    97.806136.168192.22769.131

    98.183136.474192.20869.425

    98.413136.648192.15469.611

    98.517136.707192.06669.701

    98.405136.61192.01269.609

    98.164136.402191.95769.42

    97.776136.062191.86769.122

    97.21135.553191.70868.695

    96.418134.82191.44868.108

    95.303133.753191.01367.296

    93.637132.068190.15666.113

    90.828128.976188.03864.165

    85.539122.858181.79860.269

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Axial node number

    Temperature [C]

    Load

    10213716853125124

    10613616855128122

    11214118160136123

    11914919369148130

    12616020581162141

    13417621795177155

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    centri

    1021371685312512474961482306055

    1061361685512812277951482306160

    11214118160136123821131422177170

    11914919369148130901131512108280

    12616020581162141961261652209492

    13417621795177155101140180233107104

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    thermal

    10213716899974

    10613616844444477

    1121411819413117682

    11914919313313313390

    12616020512115920296

    134176217222222222101

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Chart1 (2)

    10213716899974

    10613616844444477

    112141181941478982

    11914919313313313390

    12616020512117623796

    134176217222222222101

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Chart1 (5)

    102137168999

    106136168444444

    11214118188117157

    119149193133133133

    126160205114145183

    134176217222222222

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Chart2

    10213716891756099

    10613616844444499

    1121411818918280109

    119149193133133133133

    126160205178200108140

    134176217222222222222

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.7_0

    Static load [N]

    Peak temperature [ C]

    Chart2 (2)

    1021371687454609791221109017560

    106136168876872984412144444444

    1121411811108892112898913310018280

    119149193132107133129133136133133133133

    126160205178178178146178150171120200108

    134176217222222222222222222222222222222

    30,000 rpm

    40,000 rpm

    50,000 rpm

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-0.8_30

    Predictions - 30 krpm-0.7_20

    Predictions - 30 krpm-0.7_0

    Predictions - 30 krpm-25um_0.7_0

    Predictions - 30 krpm-20um_0.7_0

    Static load [N]

    Peak temperature [ C]

    Sheet3

    000

    0.1210.2590.432

    0.4831.0371.729

    1.0872.3333.891

    1.9324.1486.917

    3.0196.48110.809

    4.3489.33315.564

    5.91812.70321.185

    7.72916.59227.67

    9.78220.99935.02

    12.07725.92543.234

    Solid shaft

    Ri =0.5 Ro

    Ri =0.75 Ro

    22

    Rotor speed [rpm]

    Centrifugal growth [m]

    Chart1 (8)

    0.55250.510.765

    76.37570.5105.75

    166.725153.9230.85

    Inconel X750

    Inconel 718

    AISI 304 (Stainless steel)

    Temperature [ C]

    Thermal expansion [m]

    Chart1 (6)

    0.2439024390.42682926830.6097560976

    0.2439024390.54878048780.7926829268

    0.18292682930.54878048780.8536585366

    30,000 rpm

    50,000 rpm

    70,000 rpm

    Static load [N]

    Axial Thermal gradient [ C/mm]

    Chart1 (9)

    918878746359

    1271191091009083

    164150142129121111

    Mid-plane

    133 N

    89 N

    44 N

    Side edge

    Rotor speed [rpm]

    Peak temperature [ C]

    Sheet3 (2)

    74100129

    78109142

    74100129

    30,000 rpm

    50,000 rpm

    70,000 rpm

    Temperature [C]

    Chart1 (3)

    1830207

    217215

    164207

    Temperature [C]

    http://www.hightempmetals.com/techdata/hitempInconelX750data.php

    InconelX750

    Modulus of Elasticity

    CMPa x 10(6)

    26.7213.7

    260197.9

    538172.4

    732144.8

    816127.6

    Thermal Conductivity

    CW/m-K

    14916.9

    31620.5

    53826.5

    64928.7

    76031.4

    87135.3

    Inconel 718AISI4140 steel test shaftAISI 304 stainless steel bearing housing

    http://www.espimetals.com/tech/inconel718.pdfTheraml expansion coefficientTheraml expansion coefficient

    R0.025m211Gpahttp://www.efunda.com/materials/alloys/alloy_steels/show_alloy.cfm?ID=AISI_4140&prop=all&Page_Title=AISI%204140http://www.goodfellow.com/csp/active/STATIC/A/Stainless_Steel_-_AISI_304.HTML

    alph1.30E-05Kavg

    conductivity11.4W/m.K

    CRgThermal Properties18

    26.70.552516.3

    26076.375

    538166.725Properties

    732229.775TreatmentR0.025m

    816257.07512.320-100moreoil hardened, tempered 600Calph1.20E-05K

    42.7100more

    473150-200moreCRg

    Inconel x75026.70.765

    http://www.hightempmetals.com/techdata/hitempInconelX750data.php260105.75

    R0.025m538230.85

    alph1.20E-05Kat 20 deg C732318.15

    816355.95

    CRg

    26.70.51

    26070.5

    538153.9

    732212.1

    816237.3

    Centrifugal growth

    http://www.hightempmetals.com/techdata/hitempInconel718data.php

    Inconel 718

    http://www.espimetals.com/tech/inconel718.pdf

    R0.025m208Gpa

    rpmsolid0.5 Ro0.75Ro

    0000

    1.00E+040.1210.2590.432

    2.00E+040.4831.0371.729

    3.00E+041.0872.3333.891

    4.00E+041.9324.1486.917

    5.00E+043.0196.48110.809

    6.00E+044.3489.33315.564

    7.00E+045.91812.70321.185

    8.00E+047.72916.59227.67

    9.00E+049.78220.99935.02

    1.00E+0512.07725.92543.234

    http://www.hightempmetals.com/techdata/hitempInconelX750data.php

    http://www.efunda.com/materials/alloys/alloy_steels/show_alloy.cfm?ID=AISI_4140&prop=all&Page_Title=AISI%204140

    12.3

    42.7

    473

    http://www.goodfellow.com/csp/active/STATIC/A/Stainless_Steel_-_AISI_304.HTML

    10678.197146

    11190.684142

    123109.38144

    137127.15151

    152144.91162

    168161.68175

    c=20 m

    c=25 m

    c=32 m

    Static load [N]

    Peak temperature [ C]

    99.55678.197

    112.3690.684

    136.63109.38

    161.32127.15

    187.72144.91

    215.11161.68

    Adiabatic

    Heat transfer convection

    Static load [N]

    Peak temperature [ C]

    2552

    2855

    3359

    4268

    6691

    Peak temperature

    Inlet mixing temperature

    Mixing ratio,

    Temperature [ C]

    50000 rpm

    Peal temp

    Static loadadiabaticheat coeffCalculation of specific heat

    999.55678.197Specific heat

    44112.3690.684

    89136.63109.38

    133161.32127.15Prandtl No.

    178187.72144.91

    222215.11161.68

    Dimensionless spesific heat

    adiabaticRotor speed5000065.4498469498m/s

    Static loadc=32umc=25umc=20umrho1.169kg/m3

    978.197106146cp1080J/kg-degK

    4490.684111142EMU1.85E-05Pa-s

    89109.38123144K0.0257W/m.KFor air

    133127.15137151Pr No.7.77E-01

    178144.91152162Specific heat6.18E+02

    222161.68168175Diml spe heat9.90E-01c/(emu*cp)1.60E-03

    Nu avg4.92E+02

    ReL6.50E+05

    Specific heat8.05E+01492.1050786737

    Mixing

    Lminlet tempPeak

    02552

    0.22855

    0.43359

    0.64268

    0.86691

    6390121

    78109142

    91127164

    30,000 rpm

    50,000 rpm

    70,000 rpm

    Static load [N]

    Peak temperature [ C]

    MBD00553F60.unknown

    MBD005545AE.unknown

    MBD00553C7F.unknown

  • Mid-plane & edge film temperaturesDifference in film temperatures at mid-plane and edge (axial thermal gradient) increases as rotor speed increases. Higher film temperatures at bearing mid-plane evidence absence of axial cooling flow pathStatic load (vertical:180).

    Comparison to test data (Radil and Zeszotek, 2004)TSupply=21 CTshaft=Tbearing =Tambient = 21 C

    Load (25)

    74641371115553125124

    7766.5136110.56055128122

    82711411157060136123

    90771491228069148130

    9682160130.59281162141

    1018617614510495177155

    Test data (Mid-plane)

    40,000 rpm

    Test data (Edge)

    20,000 rpm

    Predictions(Edge)

    Predictions(Mid-plane)

    Test data - 40 krpm

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (24)

    741021371685583125190

    771061361686088128186

    821121411817098136192

    9011914919380110148202

    9612616020592124162214

    101134176217104138177228

    30,000 rpm

    40,000 rpm

    50,000 rpm

    20,000 rpm

    Test data (Mid-plane)

    Predictions(Mid-plane)

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (23)

    111

    1.0051.0081.01

    1.0021.0121.017

    1.0011.0181.025

    1.0011.0241.034

    1.0031.0311.043

    1.0051.041.053

    1.0081.0491.065

    1.0121.0591.077

    1.0171.0711.091

    1.0231.0831.107

    1.031.0971.124

    1.0381.1121.142

    1.0461.1281.163

    1.0551.1461.186

    1.0641.1651.212

    1.0741.1861.241

    1.0851.2091.273

    1.0961.2331.309

    1.1071.261.349

    1.121.2891.393

    1.1321.321.442

    1.1451.3541.496

    1.1591.3891.555

    1.1721.4271.619

    1.1861.4671.688

    1.2011.5091.762

    1.2151.5531.839

    1.2291.5981.919

    1.2441.6432.001

    1.2581.6892.083

    1.2711.7342.164

    1.2851.7792.242

    1.2971.8212.317

    1.311.8622.386

    1.3211.8982.448

    1.3311.9312.502

    1.341.962.547

    1.3471.9832.582

    1.35322.607

    1.3582.0122.62

    1.3612.0172.621

    1.3622.0152.61

    1.3612.0062.588

    1.3581.992.553

    1.3531.9672.507

    1.3461.9372.45

    1.3371.9012.382

    1.3261.8582.304

    1.3131.812.218

    1.2981.7562.123

    1.2811.6982.022

    1.2631.6351.915

    1.2431.571.804

    1.2211.5021.692

    1.1991.4331.58

    1.1751.3631.469

    1.1511.2941.361

    1.1271.2251.258

    1.1021.161.164

    1.0781.11.085

    1.0541.0481.027

    1.0321.0121

    1.01311

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    111

    Static load increases

    44 N

    133 N

    222 N

    Circumferential angle [deg]

    Dimensionless pressure, p/pa

    Load (22)

    46.251.24260.112

    46.251.24260.112

    46.25851.460.308

    46.34951.58260.522

    46.46451.78560.755

    46.652.0161.008

    46.7652.2661.285

    46.94552.53761.588

    47.15252.83961.921

    47.3853.16862.287

    47.62753.52662.689

    47.89453.91463.132

    48.17954.33463.622

    48.48154.78964.165

    48.855.28364.768

    49.13655.81965.439

    49.48856.39966.185

    49.85657.02867.017

    50.2457.70867.943

    50.63858.44468.973

    51.05159.23770.117

    51.47960.09271.381

    51.9261.00872.774

    52.37461.98774.299

    52.83963.02875.957

    53.31664.12877.742

    53.80165.28379.646

    54.29566.48781.653

    54.79367.73283.743

    55.29669.00685.891

    55.79970.29988.067

    56.30171.59590.24

    56.79872.8892.377

    57.28774.13794.447

    57.76475.35196.418

    58.22776.50598.262

    58.67277.58399.952

    59.09478.569101.464

    59.49179.45102.778

    59.85980.214103.875

    60.19480.848104.742

    60.49481.344105.365

    60.75581.695105.738

    60.97681.894105.853

    61.15481.939105.709

    61.28881.827105.306

    61.37781.562104.65

    61.41981.144103.749

    61.41680.581102.615

    61.36779.88101.264

    61.27579.0599.717

    61.1478.10597.997

    60.96577.05896.135

    60.75375.92894.168

    60.50774.73392.136

    60.23273.49390.076

    59.93272.22888.026

    59.61470.95986.028

    59.28269.71184.147

    58.94368.52882.488

    58.60767.48481.194

    58.29166.68480.437

    58.02466.30880.26

    57.85466.31680.36

    57.88966.44380.44

    58.06966.55380.505

    58.23966.64880.558

    58.39866.73280.603

    58.54766.80680.641

    58.68766.87280.673

    58.8266.93280.701

    58.94566.98680.725

    59.06467.03680.746

    59.17867.08280.765

    59.28667.12480.782

    59.3967.16480.798

    59.4967.20280.812

    59.58367.23680.824

    59.58367.23680.824

    Static load increases

    44 N

    133 N

    222 N

    Circumferential angle [deg]

    Temperature [ C]

    Load (21)

    111111

    1.0111.0051.0061.0081.0091.01

    1.0081.0021.0071.0121.0151.017

    1.0071.0011.011.0181.0221.025

    1.0081.0011.0141.0241.031.034

    1.0061.0031.0191.0311.0391.043

    1.0061.0051.0251.041.0481.053

    1.0051.0081.0321.0491.0591.065

    1.0061.0121.041.0591.0711.077

    1.0061.0171.0491.0711.0841.091

    1.0071.0231.061.0831.0981.107

    1.0081.031.0711.0971.1131.124

    1.011.0381.0831.1121.131.142

    1.0111.0461.0961.1281.1491.163

    1.0131.0551.111.1461.171.186

    1.0151.0641.1251.1651.1931.212

    1.0181.0741.1411.1861.2181.241

    1.021.0851.1581.2091.2461.273

    1.0231.0961.1761.2331.2761.309

    1.0261.1071.1961.261.311.349

    1.0291.121.2171.2891.3471.393

    1.0321.1321.2391.321.3871.442

    1.0351.1451.2621.3541.4311.496

    1.0381.1591.2871.3891.4781.555

    1.0421.1721.3131.4271.5291.619

    1.0451.1861.3391.4671.5831.688

    1.0481.2011.3671.5091.6411.762

    1.0511.2151.3961.5531.7011.839

    1.0541.2291.4251.5981.7631.919

    1.0571.2441.4541.6431.8262.001

    1.061.2581.4831.6891.892.083

    1.0631.2711.5121.7341.9532.164

    1.0661.2851.5411.7792.0142.242

    1.0681.2971.5681.8212.0732.317

    1.0711.311.5941.8622.1282.386

    1.0731.3211.6181.8982.1782.448

    1.0741.3311.641.9312.2222.502

    1.0761.341.6591.962.2592.547

    1.0771.3471.6761.9832.2882.582

    1.0781.3531.68822.312.607

    1.0791.3581.6972.0122.3222.62

    1.0791.3611.7022.0172.3262.621

    1.0791.3621.7032.0152.322.61

    1.0791.3611.6992.0062.3042.588

    1.0781.3581.6911.992.2792.553

    1.0771.3531.6791.9672.2452.507

    1.0761.3461.6621.9372.2012.45

    1.0741.3371.641.9012.1492.382

    1.0721.3261.6141.8582.0892.304

    1.071.3131.5841.812.0212.218

    1.0671.2981.5511.7561.9462.123

    1.0641.2811.5131.6981.8662.022

    1.0611.2631.4731.6351.7811.915

    1.0571.2431.431.571.6931.804

    1.0541.2211.3851.5021.6031.692

    1.051.1991.3381.4331.5111.58

    1.0451.1751.291.3631.421.469

    1.0411.1511.2421.2941.3311.361

    1.0361.1271.1941.2251.2451.258

    1.0321.1021.1471.161.1641.164

    1.0271.0781.1011.11.0931.085

    1.0221.0541.0591.0481.0371.027

    1.0181.0321.0241.0121.0011

    1.0131.0131.001111

    1.00911111

    1.00511111

    1.00211111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    111111

    9 N

    Static load increases

    44 N

    89 N

    133 N

    178 N

    222 N

    Predictions - 40 krpm-20um_0.6_20

    Circumferential angle [deg]

    Dimensionless pressure, p/pa

    Load (20)

    46.45246.248.16151.24255.30860.112

    46.45246.248.16151.24255.30860.112

    46.57446.25848.27351.455.4960.308

    46.7346.34948.41551.58255.69560.522

    46.88346.46448.5851.78555.91860.755

    47.02346.648.7752.0156.16261.008

    47.1746.7648.98652.2656.43161.285

    47.3346.94549.22852.53756.72661.588

    47.49947.15249.49452.83957.04961.921

    47.67747.3849.78553.16857.40162.287

    47.86147.62750.153.52657.78762.689

    48.05147.89450.43953.91458.20863.132

    48.24848.17950.80454.33458.6763.622

    48.45148.48151.19454.78959.17664.165

    48.65948.851.61255.28359.73164.768

    48.87349.13652.05755.81960.34265.439

    49.09349.48852.53356.39961.01466.185

    49.31649.85653.03957.02861.75267.017

    49.54550.2453.57857.70862.56467.943

    49.77750.63854.1558.44463.45568.973

    50.01351.05154.75759.23764.43170.117

    50.25151.47955.39860.09265.49771.381

    50.49351.9256.07561.00866.65672.774

    50.73652.37456.78861.98767.91174.299

    50.98152.83957.53463.02869.26175.957

    51.22753.31658.31364.12870.70377.742

    51.47453.80159.12165.28372.2379.646

    51.72154.29559.95666.48773.83281.653

    51.96854.79360.81367.73275.49583.743

    52.21455.29661.68769.00677.20285.891

    52.45855.79962.5770.29978.93488.067

    52.70156.30163.45671.59580.66890.24

    52.94156.79864.33772.8882.3892.377

    53.17857.28765.20374.13784.04694.447

    53.41257.76466.04675.35185.64396.418

    53.64158.22766.85676.50587.14698.262

    53.86758.67267.62277.58388.53599.952

    54.08759.09468.33778.56989.79101.464

    54.30359.49168.9979.4590.892102.778

    54.51259.85969.57480.21491.825103.875

    54.71660.19470.0880.84892.577104.742

    54.91360.49470.50181.34493.136105.365

    55.10360.75570.83381.69593.495105.738

    55.28660.97671.06981.89493.647105.853

    55.46361.15471.20681.93993.591105.709

    55.63161.28871.24381.82793.325105.306

    55.79361.37771.17881.56292.854104.65

    55.94761.41971.01281.14492.182103.749

    56.09361.41670.74780.58191.32102.615

    56.23361.36770.38779.8890.28101.264

    56.36561.27569.93779.0589.07699.717

    56.4961.1469.40278.10587.72797.997

    56.60860.96568.79277.05886.25796.135

    56.7260.75368.11375.92884.69194.168

    56.82660.50767.37874.73383.05892.136

    56.92660.23266.59873.49381.38990.076

    57.02259.93265.78572.22879.71188.026

    57.11359.61464.95170.95978.05386.028

    57.259.28264.11269.71176.4684.147

    57.28558.94363.28668.52875.00282.488

    57.36758.60762.50967.48473.7981.194

    57.44858.29161.84166.68472.95380.437

    57.5358.02461.36766.30872.69380.26

    57.61457.85461.26366.31672.79780.36

    57.70357.88961.41566.44372.89880.44

    57.80458.06961.55866.55372.98280.505

    57.92858.23961.68766.64873.05380.558

    58.08658.39861.80266.73273.11480.603

    58.26558.54761.90766.80673.16780.641

    58.44158.68762.00266.87273.21380.673

    58.61558.8262.0966.93273.25480.701

    58.78658.94562.1766.98673.29180.725

    58.95459.06462.24567.03673.32480.746

    59.1259.17862.31667.08273.35480.765

    59.28459.28662.38167.12473.38280.782

    59.44659.3962.44467.16473.40780.798

    59.60659.4962.50367.20273.43180.812

    59.75859.58362.55767.23673.45280.824

    59.75859.58362.55767.23673.45280.824

    9 N

    Static load increases

    44 N

    89 N

    133 N

    178 N

    222 N

    Predictions - 40 krpm-20um_0.6_20

    Circumferential angle [deg]

    Temperature [ C]

    Load (19)

    0.4831

    1.932

    4.348

    7.729

    12.08

    Solid shaft

    tS = 10 mm

    tS = 2 mm

    Shaft wall thickness decreases

    Predictions - 40 krpm-20um_0.6_20

    Rotor speed [krpm]

    Centrifugal growth [ C]

    Load (16)

    0.48311.0541.712

    1.9324.2176.846

    4.3489.48815.4

    7.72916.8727.39

    12.0826.3542.79

    Solid shaft

    tS = 10 mm

    tS = 2 mm

    Shaft wall thickness decreases

    Predictions - 40 krpm-20um_0.6_20

    Rotor speed [krpm]

    Centrifugal growth [m]

    Load (18)

    8792000-44560093390097450008752100-36220048330010027000

    9037000-176100726700100700009277100-7409342888010247000

    9465000160800425200104800001017600030090036151010637000

    9893000420900163000108100001079300065758017911011072000

    10320000623700-6547011060000113980008773201332011416000

    10710000784600-24970011260000119840001005200-8609611679000

    Solid lines: THDDash lines: Isothermal

    KXX

    THD

    KYY

    KXY

    KYX

    Isothermal

    Static load [N]

    Stiffness coefficient [MN/m]

    Load (17)

    742.3-193.1235.1529.8622.88-173.95244.72546

    659.9-136.5227.4478.7565.24-157.39218.65498.52

    538.7-74.91215.9409.4509.03-124.49197.16427.97

    435.5-32.93200.1349.3430.7-79.451188.34367.62

    349.9-5.784179.6295.1362.34-45.516172.35325.72

    282.212.23157.2246.9315.66-26.816151.76295.17

    Solid lines: THDDash lines: Isothermal

    CXX

    THD

    CYY

    CXY

    CYX

    Isothermal

    Static load [N]

    Damping coefficient [KN-s/m]

    Load (15)

    26.25965.35316224410.0209260.016951

    18.87729.59449215420.0203940.017041

    14.82118.08433215740.0201110.01746

    12.30114.83343536530.0201620.017994

    9.522712.18104744070.0204370.018771

    8.392210.37674908260.0208540.019711

    THD

    Isothermal

    THD

    Isothermal

    Static load [N]

    Journal attitude angle [deg]

    Drag torque [N-m]

    Load (14)

    0.840951.83145365716.57815.572

    4.22465.434352546513.99812.655

    8.424910.278448659711.4459.3519

    12.27414.61505917069.72967.1382

    16.01318.78185959918.54525.5448

    19.65122.65045624357.70944.4498

    THD

    Isothermal

    THD

    Isothermal

    c' = 17 m

    Static load [N]

    Journal eccentricity [m]

    Minimum film thickness [m]

    Load (10)

    102137168831251907455

    106136168881281867760

    112141181981361928270

    1191491931101482029080

    1261602051241622149692

    134176217138177228101104

    30,000 rpm

    40,000 rpm

    50,000 rpm

    20,000 rpm

    Test data (Mid-plane)

    Predictions(Mid-plane)

    Test data - 30 krpm

    Test data - 40 krpm

    Test data - 50 krpm

    Predictions - 30 krpm-20um_0.6_20

    Predictions - 40 krpm-20um_0.6_20

    Predictions - 50 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    Load (13)

    13712574551245311164

    136128776012255110.566.5

    14113682701236011571

    14914890801306912277

    160162969214181130.582

    1761771011041559514586

    Test data (Mid-plane)

    40,000 rpm

    Test data (Edge)

    20,000 rpm

    Predictions(Edge)

    Predictions(Mid-plane)

    Test data - 40 krpm

    Predictions - 40 krpm-20um_0.6_20

    Static load [N]

    Peak temperature [ C]

    AxialT133 (3)

    93.974129.95410212669.37777

    102.168139.62111914975.13990

    105.271143.0949811877.11477

    106.958144.86278.185

    108.082145.99478.92

    108.893146.7979.464

    109.477147.34779.862

    109.878147.71180.141

    110.125147.92180.319

    110.24147.99980.409

    110.116147.88780.314

    109.857147.64580.131

    109.445147.24779.847

    108.848146.65579.442

    108.022145.81878.891

    106.879144.63478.147

    105.167142.79677.062

    102.034139.23875.07

    93.845129.57169.309

    20,000 rpm

    30,000 rpm

    40,000 rpm

    Side edge (rear)

    Side edge (front)- Edges

    Mid-plane

    Test data

    Predictions

    Axial node number

    Temperature [C]

    Sheet2

    50krpm222N30-50krpm89N30-50krpm133N40krpm1.932um

    Side edgeMid-planeSide edgekrpmSide edgeMid-planeSide edgekrpmSide edgeMid-planeSide edgershaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    183217164180degTest data309611292309611292Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg41118401191411114011914111190.8307625.5816.32217.74816.5772.10E-028.88E+06-4.67E+059.55E+059.86E+06755.5-197.1240.6541.6

    207215207311195015417113650154171136444.101417.58313.46716.69314.1562.06E-029.15E+06-2.02E+057.61E+051.02E+07674.9-139.3230.9491.9

    21120898.19214.1510.41215.63311.6652.04E-029.62E+061.28E+054.78E+051.06E+07556.4-75.83215.8425.3

    13311.92312.3628.22614.8339.97122.04E-021.01E+073.80E+052.36E+051.10E+07456.3-31.56195.4368.8

    20.52.0530-50krpm30-50krpm17815.55110.5646.611114.1518.7622.07E-021.06E+075.69E+052.95E+041.13E+07375.4-2.171169.2319.9

    34.54.116.4NSide edgeMid-planeSide edgeEdge-avg30umN30405020umN30405022218.9739.20525.456813.5717.91442.12E-021.10E+077.17E+05-1.29E+051.15E+07312.219.1139.7277.8

    6.5209647464643097409176145

    4467776666.50.844870.74417615540krpm1.932um20krpm0.5um

    50krpm89N89718271718911089167155rshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyyrshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    ReaCenterFront13377907777133132133165163Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/mLoad (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    1788296828217817890.8409526.25916.31117.7816.5782.09E-028.79E+06-4.46E+059.34E+059.75E+06742.3-193.1235.1529.891.430841.57617.11217.74617.2198.82E-038.22E+065.55E+06-2.81E+055.26E+057.17E+061922.1-720.931053.31829.7

    190deg41118222861018686222222444.224618.87713.26316.70613.9982.04E-029.04E+06-1.76E+057.27E+051.01E+07659.9-136.5227.4478.7446.751830.17512.08315.06512.6998.93E-031.31E+076.67E+063244.31.19E+057.80E+061510.7-497.57773.111685.2

    1001091003111930um898.424914.82110.06715.67711.4452.01E-029.47E+061.61E+054.25E+051.05E+07538.7-74.91215.9409.48912.23721.17.775613.0069.10269.44E-031.31E+078.23E+063.91E+05-597518.53E+061202.8-281.5462.951494.9

    21120309861028384.52095420umN30405013312.27412.3017.788414.8939.72962.02E-029.89E+064.21E+051.63E+051.08E+07435.5-32.93200.1349.313316.75515.5475.270511.6237.14471.00E-021.47E+079.47E+066.46E+05-1.28E+059.10E+061085.1-137.47278.271357.8

    44901068788.50.7446820915714517816.0139.52276.101514.2258.54522.04E-021.03E+076.24E+05-6.55E+041.11E+07349.9-5.784179.6295.117820.92612.1393.678510.5475.92781.07E-021.47E+071.05E+078.24E+05-1.79E+059.58E+061053.3-38.164156.41249.8

    8996112929489880.74414122219.6518.39224.840913.6477.70942.09E-021.07E+077.85E+05-2.50E+051.13E+07282.212.23157.2246.9

    30krpm89N1331021199810013310789

    ReaCenterFront178108126103105.5178133ex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyyex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    222113134109111222178mmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/mmmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg4111830um2229.00.0400008.22E+068.75E+06-3.62E+054.83E+051.00E+07622.9-174.0244.7546.09.00.0200008.22E+065.91E+06-4.71E+057.63E+057.24E+062018.9-812.1938.51969.9

    74787431119409114137108111096044.00.0400001.31E+079.28E+06-7.41E+044.29E+051.02E+07565.2-157.4218.7498.544.00.0200001.31E+076.96E+06-4.34E+043.60E+058.14E+061552.9-503.4825.01790.5

    2112044114136107110.50.7447220umN30405089.00.0400001.47E+071.02E+073.01E+053.62E+051.06E+07509.0-124.5197.2428.089.00.0200001.31E+078.72E+064.62E+05-9.27E+038.88E+061245.3-269.7525.71606.7

    89119141111115899220-209141122133.00.0400001.47E+071.08E+076.58E+051.79E+051.11E+07430.7-79.5188.3367.6133.00.0200001.47E+071.02E+077.75E+05-1.26E+059.44E+061159.4-135.6325.81470.9

    70krpm89N1331261491181221330.744141121178.00.0400001.57E+071.14E+078.77E+051.33E+041.14E+07362.3-45.5172.4325.7178.00.0200001.47E+071.13E+079.47E+05-1.82E+059.89E+061178.0-56.5210.21378.7

    ReaCenterFront178134160127130.517889222.00.0400001.57E+071.20E+071.01E+06-8.61E+041.17E+07315.7-26.8151.8295.2

    222149176141145222133139136FOIL Bearing static load performance parameters

    190deg4111825um178150150Load-Xe_structureexeyEccentricityeccentricityAngleMinimum filmFx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR

    12914212931119509146168131138.50997222200.00.0400001.57E+071.17E+079.47E+05-4.50E+041.16E+07337.2-35.0162.3309.3[N]mmmmratiodeg[m]NNNbar[bar]N-m[kW]N/m-

    21120441461681281370.744989.0020.101.231.331.810.1047.1816.72-9.0-0.29.00.041.098.14E-031.70E-026.85E+060.00

    891541811361458911225umN30405044.0023.536.724.207.930.4332.0310.88-44.0-0.344.00.211.398.40E-031.76E-027.57E+060.00

    133162193143152.513312920-209119110FOIL Bearing static load performance parameters89.0027.0112.945.0413.890.7521.266.03-89.2-0.489.20.431.749.11E-031.91E-028.70E+060.03

    Themmal gradient (Deg C/mm)1781722051541631781460.844Load-Xe_structureexeyEccentricityeccentricityAngleMinimum filmMinimum filmMinimum filmFx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR133.0030.0118.005.1018.71.015.813.27-133.98-1.3134.00.652.079.94E-032.08E-029.74E+060.00

    300000.24390243922218321716317322289133133[N]mmmmratiodeg[m][m][m]NNNbar[bar]N-m[kW]N/m-178.0033.1322.474.8022.971.2412.071.78-178.7-0.8178.70.872.391.09E-022.27E-021.06E+070.00

    500000.54878048782.052.051339.0018.630.761.661.830.1165.3515.3316.71915.572-9.0-0.09.00.041.181.70E-027.10E-029.58E+060.00

    700000.79268292684.116.44.116.417817117144.0021.974.732.685.430.3229.5912.0115.18412.655-43.6-0.743.60.211.401.70E-027.14E-029.87E+060.00

    22289.0025.399.773.1910.280.6018.088.0813.3649.3519-89.0-0.389.00.431.711.75E-027.31E-021.04E+070.00

    133.0028.3914.133.7414.60.914.835.3612.1057.1382-133.08-0.9133.10.652.031.80E-027.54E-021.08E+070.00

    50krpm44N50krpm133N20umN304050178.0031.4518.363.9618.781.1012.183.4710.9775.5448-178.2-0.7178.20.862.351.88E-027.86E-021.12E+070.139N : 20 - 100 krpm

    ReaCenterFrontReaCenterFront20-20910790222.0034.2522.284.0822.651.3310.382.2410.0264.4498-222.1-1.0222.11.082.651.97E-028.26E-021.16E+070.28ex_inputey_inputLoad-XLoad-YSpeedKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    0.644mmNNrpmN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    190deg41118190deg41118891071009.00.0200008.22E+065.91E+06-4.71E+057.63E+057.24E+062018.9-812.1938.51969.9

    8390833111911912711831119133200.0032.8520.353.9820.731.2111.062.8010.4874.9532-200.1-0.3200.10.972.501.92E-028.05E-021.14E+070.229.00.0400008.22E+068.09E+06-5.19E+056.83E+058.73E+06879.9-263.9276.2742.7

    21120211201781231209.00.0600008.22E+068.88E+06-4.42E+058.83E+059.32E+06572.2-143.3137.3428.6

    2229.00.0800008.22E+069.37E+06-3.76E+058.79E+059.67E+06411.3-91.384.8289.0

    9.00.01000008.22E+069.66E+06-3.33E+058.64E+059.90E+06315.8-64.659.7213.7

    30krpm44N30krpm133N32umN304050

    ReaCenterFrontReaCenterFront20-209117100FOIL Bearing static load performance parameters

    0.644Speede_structureexeyEccentricityeccentricityAngleMinimum filmMinimum film (center)Minimum film (near edge)Fx ReactionFy ReactionForceSpecific loadMax pressureTorquePower LossKeqWFR

    190deg41118190deg4111889128128[rpm]mmmmratiodeg[m][m][m]NNNbar[bar]N-m[kW]N/m-

    596359311198891883111913320000.0020.101.231.331.810.1047.1816.7217.26116.81-9.0-0.29.00.041.098.14E-031.70E-026.85E+060.00

    211202112017840000.0020.101.090.711.300.0733.0117.2317.85517.334-9.0-0.19.00.041.091.62E-026.80E-028.64E+060.15

    22260000.0020.101.040.511.160.0626.0517.3918.02317.497-9.0-0.09.00.041.092.43E-021.53E-019.32E+060.19

    70krpm44N70krpm133N80000.0020.101.000.411.10.122.2917.4718.117.583-8.99-0.29.00.041.093.24E-022.71E-019.71E+060.20

    ReaCenterFrontReaCenterFront27umN304050180deg100000.0020.100.980.341.040.0619.0817.5218.14517.642-9.0-0.19.00.041.094.05E-024.24E-019.95E+060.20

    20-209609921486175

    190deg41118190deg411180.644999920krpm0.5um

    11112111131119150164150311198980109214109182rshaftKstructureKxxKxyKyxKyyCxxCxyCyxCyy

    2112021120133Load (N)eccenanglehminhminchminneartorN/m[N/m]N/mN/mN/m[N-s/m]N-s/mN-s/mN-s/m

    17810814019820091.430841.57617.11217.74617.2198.82E-035.55E+06-2.81E+055.26E+057.17E+061922.1-720.931053.31829.7

    222440.9669928.4117.61118.80817.8251.90E-027.61E+06-4.00E+058.27E+058.78E+06876.26-233.34313.41706.46

    Themmal gradient (Deg C/mm)Themmal gradient (Deg C/mm)890.8242517.44217.84619.69218.2743.07E-028.65E+06-2.35E+055.34E+059.56E+06470.46-105.18142.74379.62

    300000.243902439300000.182926829325umN3040501330.770156.163918.07820.33918.8984.38E-029.28E+06-300122.53E+051.01E+07289.36-54.98590.006232.87

    500000.4268292683500000.548780487820-2091171780.8279-4.146717.55321.27319.7595.75E-029.69E+061.61E+05837191.04E+07206.68-32.47373.863153.01

    700000.6097560976700000.85365853660.744

    89137

    themal gradient deg C/mmMid-planeTemperauture Deg CSide edgeTemperauture Deg C133

    300005000070000300005000070000300005000070000178169

    440.2439024390.42682926830.60975609764463901215983111222

    890.2439024390.54878048780.7926829268897810914274100129

    1330.18292682930.54878048780.85365853661339112716488119150Solid shaftRadial growthWall thickness: 10 mmRadial growthWall thickness: 2 mmRadial growth

    2.00E+014.83E-074.83E-012.00E+011.05E-061.05E+002.00E+011.71E-061.71E+00

    Solid journalMax1804.00E+011.93E-061.93E+004.00E+014.22E-064.22E+004.00E+016.85E-066.85E+00

    20umN3040503040506.00E+014.35E-064.35E+006.00E+019.49E-069.49E+006.00E+011.54E-051.54E+01

    20-2098.00E+017.73E-067.73E+008.00E+011.69E-051.69E+018.00E+012.74E-052.74E+01

    0.6441.00E+021.21E-051.21E+011.00E+022.64E-052.64E+011.00E+024.28E-054.28E+01

    898811715988117157

    133

    Axial temp. at 37 node number178114145183114145183

    30K 89N22220 krpm

    63.39783.177106.394019N44N89N133N178N222N

    63.39783.177106.3940.0132Solid journalMax180XPTPTPTPTPTPT

    70.93994.777121.4050.026320umN3040503040500146.452146.2148.161151.242155.308160.112

    73.799.969128.7050.039420-2094.6151.01146.4521.00546.21.00648.1611.00851.2421.00955.3081.0160.112

    75.243103.026133.1230.05250.65449.2311.00846.5741.00246.2581.00748.2731.01251.41.01555.491.01760.308

    76.294105.108136.1440.065689961311879413117613.8461.00746.731.00146.3491.0148.4151.01851.5821.02255.6951.02560.522

    77.058106.616138.32