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Day2 Sessioniii 2 Geartech Errichello

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1 Wind Turbine Gearbox Failures Robert Errichello GEARTECH
Transcript
  • 1

    Wind Turbine Gearbox Failures

    Robert Errichello GEARTECH

  • 2

    WIND TURBINE TYPICAL GEAR FAILURES

    BENDING FATIGUE

    HERTZIAN FATIGUE

    WEAR

    SCUFFING

    CRACKING

  • 3

    BENDING FATIGUE OCCURS IN 3 STAGES

    Load

    Crack Initiation Ratchet Marks

    Crack Propagation Beach Marks

    Fracture Ductile / Brittle

  • 4 Bending Fatigue/High-Cycle/Root Fillet Cracks

    Classic bending fatigue with crack initiation at critical point of maximum bending stress. Curved trajectory of crack growth is typical as shown by adjacent fracture. Failure was caused by incomplete flame hardening.

    Copyright 2000 by GEARTECH, Townsend, MT 59644 All rights are reserved.

  • 5 Bending Fatigue/High-Cycle/Tooth End Cracks

    Bending fatigue cracks initiated in root fillets at left ends of teeth due to incomplete hardening on tooth ends.

    Copyright 2000 by GEARTECH, Townsend, MT 59644 All rights are reserved.

    Scuffing in slide direction

    Crack origins

    Beach marks

  • 6

    FATIGUE SURFACE MORPHOLOGY RATCHET MARK

    ORIGIN

    BEACH MARK FRETTING CORROSION

    ORIGIN

    FRACTURE

  • 7

    DEPTH BELOW SURFACE

    TENSILE STRESS NEAR CASE/CORE BOUNDARY

    CASE/CORE BOUNDARY IS CRITICAL

  • 8

    Case History of Bending Fatigue Failure of INT Pinion

    Courtesy of Rainer Eckert, NW Labs

  • 9

    A

    B C

    D D

    E

    F

    Bending Fatigue on INT Pinion

    B

    MnS inclusions

  • 10

    A

    B C

    D D

    E

    F

    Inclusion Origin on Tooth Fragment

    B

    MnS inclusions

  • 11

    A

    B C

    D D

    E

    F

    Close-up of Origin

    B

    MnS inclusions

  • 12

    A

    B C

    D D

    E

    F

    SEM Close-up of Inclusion 100X

    B

    MnS inclusions

  • 13

    A

    B C

    D D

    E

    F

    SEM Close-up of Inclusion 550X

    B

    MnS inclusions

  • 14

    A

    B C

    D D

    E

    F

    SEM Close-up of Inclusion 35X

    B

    MnS inclusions

  • 15

    A

    B C

    D D

    E

    F

    SEM/BSE Close-up of Inclusion 50X

    B

    MnS inclusions

  • 16

    A

    B C

    D D

    E

    F

    SEM/BSE Close-up of Inclusion 100X

    B

    MnS inclusions

  • 17

    A

    B C

    D D

    E

    F

    EDS Analysis (fingerprint) of Inclusion (SEM microscope)

    B

    MnS inclusions

  • 18

    A

    B C

    D D

    E

    F

    EDS Analysis (fingerprint) of Matrix (SEM microscope)

    B

    MnS inclusions

  • 19

    A

    B C

    D D

    E

    F

    Conclusions

    B

    MnS inclusions

    1. Bending fatigue is primary failure mode 2. No surface defects were found at tooth surface 3. No material defects due to heat treatment were found 4. Fatigue crack initiated subsurface 5. Alumina inclusion was found at the crack origin 6. Root cause of bending fatigue is inadequate material cleanliness

  • 20

    HOW TO PREVENT BENDING FATIGUE

    USE STEEL THAT IS: CLEAN, HARDENABLE CARBURIZED SHOT PEENED FINE GRAINED REDUCE: BAINITE, PEARLITE NETWORK CARBIDES MICROCRACKS FLAWS BENDING STRESS

  • 21

    HERTZIAN FATIGUE

  • 22

    HERTZIAN FATIGUE - 3 GENERAL MODES

    MACROPITTING

    MICROPITTING

    SUBCASE FATIGUE

  • 23 Hertzian Fatigue/Macropitting

    Macropitting on a wind turbine pinion caused by misalignment due to excessive bearing clearance. Micropitting surrounding macropits is secondary failure. Note similar damage on each tooth including wear step at end of contact.

    Copyright 2000 by GEARTECH, Townsend, MT 59644 All rights are reserved.

    Macropitting

    Micropitting

  • 24

    HOW TO PREVENT MACROPITTING

    Reduce contact stress

    Use clean steel

    Use carburized steel

    Grind / hone gear teeth

    Keep lube cool, clean, dry

    Use high viscosity lube

  • 25

    MICROPITTING

  • 26 Hertzian Fatigue/Micropitting

    Micropitted gear teeth appear dull, etched, or stained with patches of gray. It attacks high points on gear tooth surfaces such as crests of undulations, peaks of cutter scallops, and ridges of grinding lay.

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

  • 27

    HOW TO PREVENT MICROPITTING

    Grind / hone / polish gear teeth Avoid shot-peened flanks Make hardest gear as smooth as possible Make pinion 2 HRC points harder than gear Use oil with high micropitting resistance Keep lube cool, clean, dry Use high viscosity lube Use high speeds Coat teeth with phosphate, Cu, or Ag Run-in with special lube and controlled loads

  • 28

    SUBCASE FATIGUE

  • 29 Hertzian Fatigue/Subcase Fatigue

    Subcase fatigue may be caused by inadequate case depth, inclusions near case/core boundary, or grind temper. In the helical gear shown, it was caused by grind temper. Fine, longitudinal cracks and sharp edged craters are typical.

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

  • 30

    HOW TO PREVENT SUBCASE FATIGUE

    Reduce contact stress

    Use hardenable steel

    Use optimum case / core properties

    Avoid overheating & grind temper

    Keep subsurface stress < subsurface strength

  • 31

    WEAR

  • 32

  • 33 Wear/Adhesion

    Adhesion is due to microwelding and tearing of asperities. Typically, mild adhesion occurs during running-in and subsides after it removes local asperities. The photo shows some local scuffs (severe adhesion).

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

    Scuffing

  • 34

    HOW TO PREVENT ADHESIVE WEAR

    Use smooth tooth surfaces

    Run-in new gearsets at reduced loads

    Keep lube cool, clean, dry

    Use high speeds

    If low speed, use nitrided gears & high-viscosity lube

    If very low speed, avoid S-P additives

  • 35

    FRETTING CORROSION

  • 36 Wear/Fretting Corrosion

    Fretting corrosion on teeth of a wind turbine pinion. It occurred because the turbine was parked for three months and the drive train vibrated when wind buffeted the rotor.

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

  • 37

    SCUFFING

  • 38 Scuffing (severe adhesion)

    Scuffing on teeth of a wind turbine pinion. It occurred because the oil supply was interrupted. Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

  • 39

    SPECIFIC FILM THICKNESS DEFINES LUBE REGIME

    hmin 1

    2 = (12 + 22)1/2 = hmin /

    Lube Regime< 1 Boundary

    1 2 Mixed Film> 2 Full EHD

  • 40

    GEAR LIFE DEPENDS ON

    Gear Life

    Micropitting Adhesion Scuffing

    Macropitting

  • 41

    HOW TO PREVENT SCUFFING

    OPTIMIZE GEAR GEOMETRY / ACCURACY

    USE NITRIDED STEEL

    GRIND / HONE GEAR TEETH

    COAT GEAR TEETH w/ PHOSPHATE, Cu, Ag

    USE HIGH-VISC, ANTISCUFF LUBE

    COOL GEAR TEETH WITH LUBE

    RUN-IN NEW GEARSETS AT REDUCED LOADS

  • 42

    GRINDING CRACKS

  • 43 Cracking/Grinding Cracks

    Grinding cracks occur on ground flanks usually perpendicular to the grind direction. They are relatively shallow and parallel or in a crazed pattern. Nital etch may show grind temper as in the above photo.

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

  • 44

    HOW TO PREVENT GRINDING CRACKS

    Use proper wheel, feed, speed, & coolant

    Keep retained austenite < 20%

    Keep case free of carbide networks

    Keep surface hardness < 60 HRC

    Inspect for temper w/ acid etch

    Inspect for cracks w/ magnetic particle

  • 45

    CASE / CORE SEPARATION

  • 46 Cracking/Case-Core Separation

    Case-Core separation is brittle fracture that usually occurs because case depth is too deep. Chevron marks on the fracture surface point to the crack origin.

    Copyright 2000 by GEARTECH, Townsend, MT 59644. All rights are reserved.

    Chevron marks

  • 47

    HOW TO PREVENT CASE / CORE SEPARATION

    Control case depth at tooth tips

    Avoid narrow toplands

    Mask toplands to restrict carbon penetration

    Chamfer all edges of teeth

    Use clean steel with high fracture toughness

    Do not refrigerate

    Temper immediately after quenching

    Do not shot peen flanks

    Wind Turbine Gearbox FailuresWIND TURBINE TYPICAL GEAR FAILURESBENDING FATIGUE OCCURS IN 3 STAGESBending Fatigue/High-Cycle/Root Fillet CracksBending Fatigue/High-Cycle/Tooth End CracksFATIGUE SURFACE MORPHOLOGYCASE/CORE BOUNDARY IS CRITICALCase History of Bending Fatigue Failure of INT PinionBending Fatigue on INT PinionInclusion Origin on Tooth FragmentClose-up of OriginSEM Close-up of Inclusion 100XSEM Close-up of Inclusion 550XSEM Close-up of Inclusion 35XSEM/BSE Close-up of Inclusion 50XSEM/BSE Close-up of Inclusion 100XEDS Analysis (fingerprint) of Inclusion (SEM microscope)EDS Analysis (fingerprint) of Matrix (SEM microscope)Slide Number 19HOW TO PREVENT BENDING FATIGUEHERTZIAN FATIGUEHERTZIAN FATIGUE - 3 GENERAL MODESHertzian Fatigue/MacropittingHOW TO PREVENT MACROPITTINGMICROPITTINGHertzian Fatigue/MicropittingHOW TO PREVENT MICROPITTINGSUBCASE FATIGUEHertzian Fatigue/Subcase FatigueHOW TO PREVENT SUBCASE FATIGUEWEARSlide Number 32Wear/AdhesionHOW TO PREVENT ADHESIVE WEARFRETTING CORROSIONWear/Fretting CorrosionSCUFFINGScuffing (severe adhesion)SPECIFIC FILM THICKNESS DEFINES LUBE REGIMEGEAR LIFE DEPENDS ON HOW TO PREVENT SCUFFINGGRINDING CRACKSCracking/Grinding CracksHOW TO PREVENT GRINDING CRACKSCASE / CORE SEPARATIONCracking/Case-Core SeparationHOW TO PREVENT CASE / CORE SEPARATION


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