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Air Foil Bearing 2011 Neuros Co., Ltd

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Presentation on airfoil bearings for high speed machinery.

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  • Air Foil Bearing

    2011

    Neuros Co., Ltd

  • 2 Turbo Energy R&D Center

    Air Foil Bearing

    Air film is generated automatically by the hydrodynamic interaction between

    viscous fluid and foil structure in a rotating sleeve.

    Elasto-Hydrodynamics : Elasticity + Reynolds Eqn. for Lubrication

    Running Air Film Thickness : 5 ~ 20 m

    Application : Oil-Free Small & High Speed Rotor

    Principle of Air Bearing Hydrodynamic Pressure Generation

    U

    Pressure Distribution

    Velocity Distribution

  • 3 Turbo Energy R&D Center

    Applied Configuration

    Bump Type : 2 Journal Bearings + 2 Thrust Bearings

    Journal Bearings : Rotor Weight + Unbalance Load + Instability Operability

    Thrust Bearings : Thrust Load + Tip Clearance Control + Power Loss Performance

    Journal Bearing Thrust Bearing

  • 4 Turbo Energy R&D Center

    Principle

    Elasto-Hydrodynamics

    Semi-Empirical Method

    Iterative Solution

    Relaxation Factor

    Hydrodynamics Reynolds Eqn Compressible Viscous Fluid Dynamics FDM : Nonlinear Pressure Distribution Geometry (by Elastic Deformation of Top Foil)

    Elasticity Beam or Plate Theory Linear Elastic Deformation FEM Foil Deflection Force (by Pressure from Hydrodynamics) Journal Bearing Thrust Bearing

  • 5 Turbo Energy R&D Center

    Elasticity of Foil Structure

    Top foils are supported by bump springs

    Top foil : Geometry for hydrodynamics

    Bump foil : Considered as spring with

    Foil structure is designed to be in elastic range of

    material Infinite life with normal operation

    Bk

    Top Foil

    Bk E

    EI

    L

    Bump Foil

    i+1uuiiu' u'i+1

    ff

    m i+1m i

    i+1i

    Strain,

    Stress,

    Limit

    2 (30%)

    1: Rotor Weight

    Limit : Elastic Range

    2 : Max. Value in Running

    1 (10%)

    FEM Analysis of Bump

  • 6 Turbo Energy R&D Center

    Advantages of Air Foil Bearing

    Noncontact Bearing Long Life / No. Scheduled Maintenance

    Improved Performance : Low Power Loss

    Low Noise and Vibration

    Oil-Free Higher Reliability : Simple, No Oil Lub. System

    System Weight Reduction : over 15% of Total Weight

    Soft Failure : Easy to Replace

    High Speed Operation : ~ 4 million DN (Others ~ 1 million DN)

    Environmental Durability Low and High Temp. : Cryogenic ~ 650 C

    Process Fluid Operation : Air, Neon,Helium, Xenon, Refrigerants, Liquid Oxygen, Liquid Nitrogen

    More Stable Rotor Structure Larger Bearing Journal Size : D 40mm at 100,000 RPM

    Increase Stiffness Property of Rotor

    Bigger Critical Speed Margin

  • 7 Turbo Energy R&D Center

    Comparison with Other Bearings

    High DN Number : D (Diameter in mm) x N (RPM)

    Reliable, Long Life, Simple, and Environment-friendly

    Rolling Element Bearing

    Small

    Low Loss

    High Load

    Noisy

    Short Life

    Limited DN

    Aero Engine

    Small Machine

    Fluid Film Bearing

    Long Life

    Low Vibration

    Hydrodynamic

    Complex

    High Loss

    Limited DN

    Industrial Machine

    Air Foil Bearing

    High Speed

    Simple/Oil-less

    Low Loss

    Low Load

    Coating

    Small Rotor

    ACM

    Small Machine

  • 8 Turbo Energy R&D Center

    Rotordynamics using Air Foil Bearing

    106

    107

    108

    0

    10000

    20000

    30000

    40000

    50000

    60000

    Ball Bearing

    Air Foil Bearing

    Ro

    tati

    on

    al S

    peed

    , R

    PM

    Supports Stiffness, N/m

    79%

    7%

    Operating Range

    1st

    2nd

    3rd

    Ball Bearing

    Industrial Turbo Machine : Motor + Compressor + Turbine

    Stable Critical Speed Design with Air Foil Bearing

    Air Foil Bearing

  • 9 Turbo Energy R&D Center

    Application of Air Foil Bearing

    ACM for ECS (Cabin Pressurizing/Avionics Cooling)

    Small / High Speed Rotor :

  • 10 Turbo Energy R&D Center

    Application to Industrial Machines

    Applied to Various Turbo Machines: ~ 100,000 RPM, ~ 600 C

    Turbo Blowers with High Speed Motor : Advanced Application

    20000 40000 60000 80000 100000 1200000

    20

    40

    60

    80

    100

    Potential Region

    Jo

    urn

    al B

    eari

    ng

    Dia

    mete

    r (m

    m)

    Rotor Speed (RPM)

    Turbo Blower

    Turbo Compressor

    Microturbine

    Cryocooler

    Pathfinder

    Region I

    Region II

    Region III

    Region I : Conventional ACM, Turbo Expander Mircroturbine

    Region II : Medium Turbo Compressor Microturbine

    Region III : Advanced Turbo Blower

  • 11 Turbo Energy R&D Center

    Developed Air Foil Bearings

    Group 1 Group 2 Group 3 Group 4 Group 5 Group 6

    Application Turbo Blower Cryocooler Micro Turbine NRL Motor Compressor for PEM FC

    ACM for

    Aircraft

    Power 30 ~ 300 hp 38 kW 65 kW 200 kW 15kW Cooling 2kW

    Motor PMSM PMSM PMSM PMSM PMSM -

    RPM 17,000~60,000 100,000 61,300 70,000 96,000 60,000

    Journal Dia. 40~90 mm 40 mm 50 mm 60 mm 25 mm 25 mm

    Rotor Mass 3~26 kg 2.6 kg 12 kg 8.6 kg 0.9 kg 0.6 kg

    DN 3.6 million 4 million 3 million 4.2 million 2.4 million 1.5 million

    Temp. ~ 200 C ~ 200 C ~ 600C ~ 200 C ~ 200 C ~ 200 C

    Fluid Air, Gas Air, Gas Air Air Air Air

  • 12 Turbo Energy R&D Center

    Features

    Motor : 50 ~ 300 HP

    PD : 0.3 ~ 1.0 kgf/cm2

    TD : 58 ~ 106 C

    High Efficient Compressor

    High Speed Motor/Inverter

    Air Foil Bearing

    Cooled by Itself

    Sewage Treatment

    Pneumatic Conveying

    Air Supply for

    Chemical Process

    Ventilation

    Cooler

    Application 1

  • 13 Turbo Energy R&D Center

    Application 1

  • 14 Turbo Energy R&D Center

    Application 2

    PMSM for Neon Compressor

    38 kW at 100,000 RPM

    Gas Foil Bearing

  • 15 Turbo Energy R&D Center

    Application 3

    Cogeneration System using a Microturbine : 65 kW

    Life : 30,000 hrs (Time Between Overhauls)

    Noise : 65dB @10m

  • 16 Turbo Energy R&D Center

    Application 3

    Vibration Free Rotor System

    Oil Free System Air Foil Bearing

    Flexible Coupling Design

    Critical Speeds

    1st 2nd 3rd 4th 5th

    Analysis 11,760 12,150 15,160 19,387 140,260

    Experiment 10,300 10,650 14,970 17,970

    (RPM)

    Flexible Coupling Mircroturbine Rotor Assembly

  • 17 Turbo Energy R&D Center

    Application 4

    Micro Air Compressor for PEM Fuel Cell

    15 kW @ 96,000 RPM

    Operating temperature : -20C to 50C

  • 18 Turbo Energy R&D Center

    Application 5

    ACM for Aircraft POD

    Cooling Capacity 2 kW

    40,000 ~ 60,000 rpm

  • 19 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 1

    Journal Bearing Test Thrust Bearing Test

    Air Turbine Driven : ~ 30,000 RPM

    Loading by Pneumatic Device : ~ 80 kgf

    Journal & Thrust Bearing Test

  • 20 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 2

    Motor Driven : ~ 120,000 RPM

    Loading by Pneumatic Device : ~ 30 kgf

    Journal & Thrust Bearing Test

    Journal Bearing Test Thrust Bearing Test

  • 21 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 3

    Motor Driven : ~ 42,000 RPM

    Loading by Pneumatic Device : ~ 80 kgf

    High Temperature Environment : ~ 600 C

    High Temp. Test

  • 22 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 4

    On/Off Test for Endurance of Coating : 20,000 Cycles

    Rotor Mass : 2.6 kg

    Motor Driven

    Automation Using LabView

    On/Off Test

  • 23 Turbo Energy R&D Center

    Endurance Test Results

    Vibration (Shaft Disp.)

    Journal Bearing Surface Shaft Surface

    RPM Profile

  • 24 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 5

    Rotor-Bearing Simulator : Air-lubricated, Rotor Mass 13.2 kg

    75kW Motor(PMSM) with Inverter : Accurate Speed Control

    Axial Loading Mechanism : Pressurizing on Rotating Disk

    Power Loss Evaluation by Temperature & Cooling Flow Rate

    Max. 30,000 RPM and 100 kgf

    Air Foil Thrust Bearings

    Cooling Air In

    Pressurizing Chamber

    Cooling Air Out

    High Speed Motor

    Air Foil Journal BearingsLabyrinth Seal

    LM

    Guide

    Pressurinzing Air In

    Load Cell

    Rotor-Bearing Simulator

  • 25 Turbo Energy R&D Center

    Air Foil Bearing Test Rig 6

    Rotor-Bearing Simulator : Air-lubricated, Rotor Mass 26 kg

    223kW Motor(PMSM) with Inverter

    Axial Loading Mechanism

    Max. 25,000 RPM and 100 kgf

    Rotor-Bearing Simulator

  • 26 Turbo Energy R&D Center

    Lift Off Speed of Journal Bearing

    Rotor Mass : 14.7 kg

    Lift Off Speed : 2,000 RPM

  • 27 Turbo Energy R&D Center

    Endurance at Field Operation

    50hp Turbo Blower : Steel Company

    Field Operation : 20,000 On/Off

    Cycles

  • 28 Turbo Energy R&D Center

    Endurance Test of FC Compressor

    20hp Compressor for PEM FC

    1,000,000 On/Off Cycles

  • 29 Turbo Energy R&D Center

    Blower : Low Pressure Compressor

    Pressure Ratio : 1.3 ~ 2.0

    Type

    Positive Displacement Blower : Roots

    Turbo Blower : Gear Box Type / High Speed Motor

    Efficiency, Maintenance, Noise : Roots Type Turbo Type

    Application

    Air Supply : Waste Water Treatment, Power Plant Desulfurization

    Raw Power Transportation : Cement Industry, Petrochemical Industry

    Ventilation / Cooling / Vacuum

    Roots Blower Turbo Blower

  • 30 Turbo Energy R&D Center

    Applications of Blower

    3 ~ 10 m

    Air

    Blower

    Waste Water Treatment

    Aerobic microorganisms dissolve contaminants by blowing air into sewage

  • 31 Turbo Energy R&D Center

    Turbo Blower Gear Driven Turbo Blower

    Low Speed AC Motor

    Coupling + Gear Box + Compressor

    Fluid Film Bearing

    Large & Complex

    Oil System & Cooling System

    Periodical Maintenance (G/B, Coupling,Bearing)

    High Speed Turbo Blower

    High Speed Motor

    Single Rotor : Compressor + Motor

    Air Foil Bearing

    Small & Simple

    Oil Free System

    Maintenance Free

  • 32 Turbo Energy R&D Center

    Dr. Dellacorte(NASA) visit (2007.9 / 2010.9)