Grooved Oil Seals: Force Coefficients GT2011-45274 1 A Novel Bulk-Flow Model for Improved Predictions of Force Coefficients in Grooved Oil Seals Operating.

Slides:



Advertisements
Similar presentations
1 XII Congreso y Exposición Latinoamericana de Turbomaquinaria, Queretaro, Mexico, February Dr. Luis San Andres Mast-Childs Tribology Professor.
Advertisements

1 Luis San Andrés Mast-Childs Professor SFD EXPERIMENTAL TESTING & ANALYTICAL METHODS DEVELOPMENT High Load SFD Test Rig Identification of SFD force coefficients.
TRC project TRC 32513/15193S/ME Measurement of leakage in a novel all metal non-contacting annular seal at high temperature Alain Anderson Graduate.
Simple Is Beautiful – Refreshing thinking in engineering modeling and beyond Liming Chang Professor Penn State University Guest Professor National Chung.
TRC Project: Predictions of Force Coefficients in Off-Centered Grooved Oil Seals A novel FE Bulk-Flow Model for Improved Predictions of Force Coefficients.
ASME Turbo Expo June 11-15, 2012, Copenhagen, Denmark
Luis San Andrés Mast-Childs Professor Fellow ASME Identification of Rotordynamic Force Coefficients of a Metal Mesh Foil Bearing using Impact Load Excitations.
Aero-Hydrodynamic Characteristics
Motion of particles trough fluids part 1
33rd Turbomachinery Research Consortium Meeting
1 Luis San Andrés Mast-Childs Professor Identification of SFD force coefficients Large Clearance Open Ends SFD TRC-SFD Linear Nonlinear Force Coefficients.
A test rig for evaluation of thrust foil bearings and/or face seals
This material is based upon work supported by NASA Research Announcement NNH06ZEA001N-SSRW2, Fundamental Aeronautics: Subsonic Rotary Wing Project 2 #
Tutorial 8: Fluid flow Q1. What are the main factors determining air infiltration? In your answer discriminate between factors related to the outdoor environment,
Gas Bearings for Oil-Free Turbomachinery 29th Turbomachinery Consortium Meeting Dynamic Response of a Rotor-Air Bearing System due to Base Induced Periodic.
Tribology Group Year XX Luis San Andres Mast-Childs Professor Turbomachinery Laboratory Mechanical Engineering Department Texas A&M University May 2011.
GT SFD Force Coefficients- Multiple Frequency I DENTIFICATION of SQUEEZE FILM DAMPER FORCE C OEFFICIENTS from MULTIPLE-FREQUENCY NON-CIRCULAR.
1 TRC 2008 The Effect of (Nonlinear) Pivot Stiffness on Tilting Pad Bearing Dynamic Force Coefficients – Analysis Jared Goldsmith Research Assistant Dr.
ASME Turbo Expo 2009: Power for Land, Sea, and Air
Computational Model for Tilting Pad Journal Bearings Yujiao Tao Research Assistant Dr. Luis San Andres Mast-Childs Professor TRC project TRC.
Keun Ryu Research Assistant
1 A Novel Computational Model for Tilting Pad Journal Bearings with Soft Pivot Stiffness Yujiao Tao Research Assistant Dr. Luis San Andrés Mast-Childs.
33rd Turbomachinery Research Consortium Meeting
GT Flexure Pivot Hybrid Gas Bearings Keun Ryu Research Assistant ASME TURBO EXPO 2009, Orlando, Fla Dr. Luis San Andrés Mast-Childs Professor.
33 rd Turbomachinery Research Consortium Meeting Analyses of Pocket Damper Seals and Combined Labyrinth-Brush Seals TRC-SEAL Weilian Shan Graduate.
In the analysis of a tilting pad thrust bearing, the following dimensions were measured: h1 = 10 mm, h2 = 5mm, L = 10 cm, B = 24 cm The shaft rotates.
GT ASME GT Luis San Andrés Mast-Childs Professor, Fellow ASME Texas A&M University Supported by Pratt & Whitney Engines (UTC) 2012.
GT Hybrid Brush Seal Force Coefficients R OTORDYNAMIC F ORCE C OEFFICIENTS OF A HYBRID BRUSH SEAL: M EASUREMENTS AND P REDICTIONS Luis San Andres.
This material is supported by the TAMU Turbomachinery Research Consortium. Parts of the investigation were conducted under NASA NRA on Subsonic Rotary.
FINITE ELEMENT MODELING OF THE EFFECT OF WEAR ON THE LOAD-CARRYING CAPACITY AND MAXIMUM OIL PRESSURE OF A PLAIN JOURNAL BEARING Marc Desjardins and Ernesto.
Iron Loss Calculation in a Claw-pole Structure
Practise questions Answers later.
Tribology Group Luis San Andres Mast-Childs Professor Turbomachinery Laboratory Mechanical Engineering Department Texas A&M University May th TRC.
1 CHAPTER 6 HEAT TRANSFER IN CHANNEL FLOW 6.1 Introduction (1) Laminar vs. turbulent flow transition Reynolds number is where  D tube diameter  u mean.
School of Aerospace Engineering MITE Computational Analysis of Stall and Separation Control in Axial & Centrifugal Compressors Alex Stein Saeid NiaziLakshmi.
Internal pressures Wind loading and structural response Lecture 16 Dr. J.D. Holmes.
CHAPTER 3 EXACT ONE-DIMENSIONAL SOLUTIONS 3.1 Introduction  Temperature solution depends on velocity  Velocity is governed by non-linear Navier-Stokes.
Optimization Of a Viscous Flow Between Parallel Plates Based On The Minimization Of Entropy Generation Presentation By Saeed Ghasemi.
30 th June 20111Enrico Da Riva, V. Rao Parametric study using Empirical Results June 30 th 2011 Bdg 298 Enrico Da Riva,Vinod Singh Rao CFD GTK.
Andrew Spencer Dynamics & Acoustics Engine Development SCANIA :10 Thermal elastohydrodynamic simulation of a slider bearing in a heavy duty.
HEAT TRANSFER FINITE ELEMENT FORMULATION
1 Challenge the future The Lateral Motion of Wafer under the Influence of Thin-film Flow Leilei Hu Solid and Fluid Mechanics
Convection in Flat Plate Boundary Layers P M V Subbarao Associate Professor Mechanical Engineering Department IIT Delhi A Universal Similarity Law ……
1 Estimation of Dynamic Force Coefficients from a Wet (Foamy) Annular Seal Progress Year 1 May rd Turbomachinery Research Consortium Meeting Gary.
Selection of Stator-Rotor Combinations
1 Identification of structural stiffness and material loss factor in a shimmed (generation one) bump type foil bearing Luis San Andrés Mast-Childs Professor.
Rotordynamic Forces Acting on a Centrifugal Open Impeller in Whirling Motion by Using Active Magnetic Bearing July 7, 2011 Eucass 2011 in St Petersburg.
CAD and Finite Element Analysis Most ME CAD applications require a FEA in one or more areas: –Stress Analysis –Thermal Analysis –Structural Dynamics –Computational.
Thermo-aero Dynamic Analysis of Wind Turbines P M V Subbarao Professor Mechanical Engineering Department Development of Characteristic Design Variables.
Chapter 8: Internal Forced Convection
MESF593 Finite Element Methods
HEAT TRANSFER Problems with FEM solution
Michael Rohmer (Former) Graduate Research Assistant Luis San Andrés Mast-Childs Chair Professor TRC-B&C TRC Project May 2016 Year IV.
Date of download: 9/27/2017 Copyright © ASME. All rights reserved.

Automatic Control Theory CSE 322
Gas bearing engineering design Optimization design method
Date of download: 10/19/2017 Copyright © ASME. All rights reserved.
HYDROSTATIC LUBRICATION Applied Fluid Flow
Date of download: 11/6/2017 Copyright © ASME. All rights reserved.
Date of download: 11/14/2017 Copyright © ASME. All rights reserved.
Machine Elements, Luleå University of Technology
Vortex Induced Vibration in Centrifugal pump ( case study)
A CFD ANALYSIS ANCHORED TO TEST DATA
Eulerization of Betz Theory : Wind Turbines
33rd Turbomachinery Research Consortium Meeting
National Chung Cheng University
Dual Induction theory for Wind Turbines
Eulerization of Betz theory: Wind Turbines
3rd Lecture : Integral Equations
Presentation transcript:

Grooved Oil Seals: Force Coefficients GT A Novel Bulk-Flow Model for Improved Predictions of Force Coefficients in Grooved Oil Seals Operating Eccentrically accepted for journal publication ASME GT Luis San Andrés Mast-Childs Professor Texas A&M University Adolfo Delgado Mechanical Engineer GE Global Research Center Supported by TAMU Turbomachinery Research Consortium Presentation available at ASME Turbo Expo 2011 Power for Land, Sea and Air June 6-10, 2011, Vancouver, BC

Grooved Oil Seals: Force Coefficients GT Oil Seals Oil seal in a compressor [1] - Locked oil seal rings can induce instability in compressors. - A common remedy: seals are grooved to reduce cross-coupled stiffness and lower lock-up forces commonly used to prevent leakage of process fluid in centrifugal compressors. Kirk, R., 1986, “Oil Seal Dynamic Considerations for Analysis of Centrifugal Compressors,” Proc. 15th Turbomachinery Symposium, Houston, TX, pp

Grooved Oil Seals: Force Coefficients GT Grooves should reduce force coefficients by a factor of four, i.e. Semanate and San Andrés, (1993) K XY (1 land)= 4 K XY (2 lands) C XX (1 land)= 4 C XX (2 lands) -Fluid inertia effects not predicted (assumed negligible) Predictive Models Baheti and Kirk, (1995) - Reynolds and energy equation (FEM) - Grooves should effectively isolate seal lands - Cross-coupled stiffness and damping coefficients are reduced by ~60 % for grooved configurations - Bulk flow equation model

Grooved Oil Seals: Force Coefficients GT L2L c Journal Constant pressure Short length seal Damping, Cross-coupled Stiffness & Inertia 2-land seal: (deep groove divides lands) L c 30c 5c5c Coeffs are ¼ of original seal

Grooved Oil Seals: Force Coefficients GT [1] Graviss, M., 2005, “The Influence of a Central Groove on Static and Dynamic Characteristics of an Annular Liquid Seal with Laminar Flow,” M.S. Thesis, Texas A&M Univ., College Station, TX. Parallel oil seal configuration [1] 17 mm 76c c 25 mm 136c Oil supply Seal length Journal Parallel seal configuration (balance thrust force due to pressure drop across the seals) Includes ‘deep’ inlet (central) groove to feed seals Parameter identification: F SEAL = 1/2 F Test conf. Predictions do not consider groove or fluid inertia effects ( Zirkelback and San Andrés 1996) Smooth& grooved oil seals: test results Childs et al., (2006, 2007) Results Force coefficients are well predicted (C,K) except added mass coefficients Large added mass coefficients (~15 kg) Added mass predictions using Classical model (Reinhardt & Lund – 1975) (single land- i.e. not including inlet groove) (2.84 kg)

Grooved Oil Seals: Force Coefficients GT Old Predictions Experiments ≠ Inner land groove should reduce crossed-coupled stiffness and direct damping coefficients by a factor of four Groove does not effectively separate seal lands K xy (1 land)= 4 K xy (2 lands) C xx (1 land)= 4 C xx (2 lands) ≠ Null (neglected) added mass coefficients Large added mass coefficients, increasing with increasing groove depth Need for better predictive models Inlet (central) groove not considered (null dynamic pressure). Ignores fluid inertia Large added mass coefficients ≠ At most: K XY (1 land)= 2 K XY (2 lands) C XX (1 land)= 2 C XX (2 lands)

Grooved Oil Seals: Force Coefficients GT P s - P d >0 P d :discharge pressure y z feed plenum groove mid-land groove oil supply, P s Streamlines in axially symmetric grooved annular cavity. PdPd PdPd Fluid flow predictive model Bulk flow for incompressible liquid Qualitative observations of laminar flow field Boundary Conditions Characteristic groove depth Delgado, A., and San Andrés, L., 2010, “A Model for Improved Prediction of Force Coefficients in Grooved Squeeze Film Dampers and Oil Seal Rings,” ASME J. Tribol., 132

Grooved Oil Seals: Force Coefficients GT Linear fluid inertia model n+1 Oil supply zIzI z III z II z IV zNzN n IV N III II I No fluid inertia advection In each flow region: with temporal fluid inertiaReynolds equation

Grooved Oil Seals: Force Coefficients GT Finite Element Solution Off-centered operation x=  R Y X ee  h  R e Film thickness

Grooved Oil Seals: Force Coefficients GT Boundary conditions No generation of dynamic pressure First-order pressures and axial flow rates must be equal Null axial flow rate (axial symmetry) PaPa PaPa P s = supply pressure P a = ambient pressure Laminar flow PsPs

Grooved Oil Seals: Force Coefficients GT Assemble system of equations, impose boundary conditions and solve Finite Element for solution of Reynolds Eqn.

Grooved Oil Seals: Force Coefficients GT Consider small amplitude journal (rotor) motions about a static equilibrium position (SEP) Small amplitude journal motions about an equilibrium position An applied external static load ( W o ) determines the rotor equilibrium position ( e X, e Y ) o with steady pressure field P o and film thickness h o Let the journal whirl with frequency  and small amplitude motions (  e X,  e Y ) about the equilibrium position. Hence Perturbation analysis of flow equations

Grooved Oil Seals: Force Coefficients GT Seal dynamic reaction forces Stiffness coefficients Damping coefficients Force coefficients are independent of excitation frequency for incompressible fluid. Force coefficients depend on rotor speed & static load X Y Z Lateral displacements (X,Y) Inertia coefficients Measure of stability: Whirl frequency ratio WFR = K xy /(C xx 

Grooved Oil Seals: Force Coefficients GT Test Grooved Oil Seal & FE mesh Childs, D. W., Graviss, M., and Rodriguez, L. E., 2007, “The Influence of Groove Size on the Static & Rotordynamic Characteristics of Short, Laminar-Flow Annular Seals,” ASME J. Tribol, 129(2), Clearance = 86  m Journal diameter: 117 mm Parallel oil seals Configuration [Childs et al] 17 mm 76c c (0-15) c 25 mm 136c Oil supply Seal length Discharge plenum Buffer seal Journal 2 mm Outlet plane  z Inlet plane 0 22 Grooves x=R 

Grooved Oil Seals: Force Coefficients GT Boundary conditions P=P exit Zeroth Order Pressure Field Constant static pressure at inlet plane Constant static pressure at exit plane First Order Pressure Field Zeroth and first order pressure and flow fields are periodic in circumferential direction Null dynamic pressure at exit plane Null axial flow rate (axial symmetry) If oil cavitation (P cav =0), the first order dynamic pressure field vanishes Flow continuity is automatically satisfied at boundaries Laminar flow

Grooved Oil Seals: Force Coefficients GT Groove effective depth Test seal CFD simulations show streamline separating flow regions IS a physical boundary delimiting the domain for squeeze film flow due to journal radial motions. Inner land groove close up (CFD -Pressure driven flow) Laminar flow P s = supply pressure P a = ambient pressure 10c 15c PaPa PsPs

Grooved Oil Seals: Force Coefficients GT Test Grooved Oil Seal Childs, D. W., Graviss, M., and Rodriguez, L. E., 2007, “The Influence of Groove Size on the Static & Rotordynamic Characteristics of Short, Laminar-Flow Annular Seals,” ASME J. Tribol, 129(2), x=R  Diameter117 mm Land length24.89 mm Radial land clearance, c85.9 mm Central groove length17 mm Central groove depth136c Inner land groove length2 mm Inner land groove depth0c and 15c Static journal eccentricity (e/c)0-0.7 Shaft speed4,000-10,000 rpm Supply pressure70 bar Oil density850 kg/m 3 Oil viscosity (smooth seal)0.016 Pa.s (54 0 C) Oil viscosity (grooved seal)0.019 Pa.s (49 0 C) Effective depths in model Central groove = 9c Inner land groove = 6c

Grooved Oil Seals: Force Coefficients GT Test oil seal operating conditions Load Journal center locus shows oil seal operates with oil cavitation at the largest test eccentricities (large static load) Journal locus Shaft speed: 10,000 rpm Static eccentricity ratio: 0, 0.3, 0.5, 0.7 Supply pressure: 70 bar Test data Childs, D. W., Graviss, M., and Rodriguez, L. E., 2007, “The Influence of Groove Size on the Static & Rotordynamic Characteristics of Short, Laminar-Flow Annular Seals,” ASME J. Tribol, 129(2),

Grooved Oil Seals: Force Coefficients GT Oil Seal Leakage Predicted leakage correlates very well with tests for both smooth land and grooved seal Smooth Seal Grooved Seal (c g = 15c) (c  = 7c) 10,000 rpm, 70 bar Figure 14

Grooved Oil Seals: Force Coefficients GT Oil Seal Forces At high eccentricity, test data shows larger seal reaction force for smooth & grooved seals Smooth Seal Grooved Seal K XX 10,000 rpm, 70 bar (c g = 15c) (c  = 7c) Figure 7

Grooved Oil Seals: Force Coefficients GT Oil Seal Direct Stiffness Model predicts well direct stiffness for smooth & grooved seals Smooth Seal Grooved Seal Smooth Seal Grooved Seal K YY K XX 10,000 rpm, 70 bar (c g = 15c) (c  = 7c) Figure 8

Grooved Oil Seals: Force Coefficients GT Oil Seal Cross Stiffness Model predicts well decrease in cross- stiffness when adding inner groove Smooth Seal Grooved Seal Smooth Seal Grooved Seal K YX K XY 10,000 rpm, 70 bar (c g = 15c) (c  = 7c) Figure 9

Grooved Oil Seals: Force Coefficients GT Model effectively predicts reduction in cross-coupled stiffness due to mid- land groove. Smooth Seal Grooved Seal K XY Eccentricity=0.3 Eccentricity=0  = 0.0, 0.3 Smooth Seal Grooved Seal (c g = 15c) (c  = 7c) Oil Seal Cross-Stiffnesses 70 bar Figure 10 rotor speed increases

Grooved Oil Seals: Force Coefficients GT Oil Seal Direct Damping Model predicts accurately reduction in direct damping due to inner land groove. Smooth Seal Grooved Seal Smooth Seal Grooved Seal C YY C XX 10,000 rpm, 70 bar (c g = 15c) (c  = 7c) Figure 11

Grooved Oil Seals: Force Coefficients GT Oil Seal Cross Damping Small cross-damping, test data shows larger magnitude than predictions Smooth Seal Grooved Seal Smooth Seal Grooved Seal C YX C XY 10,000 rpm, 70 bar (c g = 15c) (c  = 7c) Figure 12

Grooved Oil Seals: Force Coefficients GT Test data shows large added mass coefficients. Predictions correlate well with experimental results. Added mass coefficients are larger for grooved seal Classical theory (*) predicts ~ 1/10 of test value [1] Reinhardt, F., and Lund, J. W., 1975, “The Influence of Fluid Inertia on the Dynamic Properties of Journal Bearings,” ASME J. Lubr. Technol., 97(1), pp M XX Smooth Seal Grooved Seal (c g = 15c) (c  = 7c) Oil Seal Added Mass 10,000 rpm, 70 bar Figure 13

Grooved Oil Seals: Force Coefficients GT Good correlation for direct force coefficients for the lower journal eccentricities (e/c=0,0.3) and moderate to good correlation for e/c=0.5. Cross-coupled stiffnesses also predicted accurately for the smaller eccentricities. FE model accurately predicts the reduction of the direct stiffness, direct damping, and cross-coupled stiffness coefficients when adding a circumferential groove to the seal land. Added mass coefficients for both seals (smooth and grooved) are also predicted accurately (within 20 %). Both analysis and test results show a grooved seal has larger direct added mass coefficient than a smooth seal. Conclusions:

Grooved Oil Seals: Force Coefficients GT Discrepancies between test results and predictions for large journal eccentricities (e/c)~0.70. Discrepancies due to (unknown) changes in seal clearance and oil viscosity induced by thermal effects. Current model is a significant improvement over prevailing predictive tools to analyze grooved oil seals. Deep grooves do not fully uncouple parallel film lands!! Model applied successfully to grooved SFDs (+ additional experimental verifications) Conclusions:

Grooved Oil Seals: Force Coefficients GT Thanks to TAMU Turbomachinery Research Consortium Acknowledgments Questions (?) Learn more at © 2011 Luis San Andres

Grooved Oil Seals: Force Coefficients GT Prediction: pressure fields for oil seal without inner groove Journal whirl motion with r=5  m,  =200 Hz) (b) Current – central groove interacts with film lands (a) Classical: central groove dyn. pressure = 0

Grooved Oil Seals: Force Coefficients GT Journal whirl motions with r=5  m,  =200 Hz) Prediction: pressure fields for oil seal with inner groove (a) Classical: central groove dyn. pressure = 0 inner land dyn. pressure = 0 (b) Current – central groove and inner groove interacts with film lands