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IcedBlades - Modelling of ice accretion on rotor
             blades in a coupled wind turbine tool
             V. Lehtomäki 1, S. Hetmanczyk 2 , M. Durstewitz 2 , A. Baier 2, K. Freudenreich 3 , K. Argyriadis 3
                               1) VTT Technical Research Centre of Finland, Espoo, Finland
        2) Fraunhofer Institute for Wind Energy and Energy System Technology (IWES), Bremerhaven, Germany

                           3) Germanischer Lloyd Renewables Certification, Hamburg, Germany




© Fraunhofer IWES
Outline




•   Project Motivation
•   Project Objectives
•   Cooperation and Partners
•   Work Packages and Schedule
•   Preliminary Study on Icing
•   Summary
Project Motivation
    Northern areas like Scandinavia as well as areas with high altitude feature a
    high potential for large capacity wind farms thanks to favourable wind
    conditions and mostly low populated areas.
•        Expansion of a common European research area by combining different research
         backgrounds
•            WinterWind 2011: R&D Priorities for cold
             climate (Jos Beurskens, ECN)
         •        Impact on loading (aerodynamically and
                  mechanical/aerodynamically induced
                  loads, scale effects)
         •        Impact on performance (how big are
                  “hidden” energy losses)
         •        Field test facilities for problem definition
                  and verification of models
•            Demand for independent technical note on                      Figure 1: Wind energy capacity in the USA [NREL]
             icing (Mike Wöbbeking, GL, WinterWind 2011)



    Motivation    Goals   Partners   Work packages   Preliminary results   Summary
Project Objectives

Within the project scope a new and updated simulation tools for ice accretion on
rotor blades and coupling of this tool to an aero-servo-elastic simulation tool
will be developed.

  1. Predicting the power losses resulting from ice accretion on rotor blades.
  2. Gain a better understanding of dynamic loading effects resulting from ice
     accretion on rotor blades via a validated numerical models.
  3. Developing a new technical note for icing sites to help wind turbine
     designers to take into account icing effects of rotor blades more
     accurately than current guidelines.
  4. Development of icing classes for new edition of IEC 61400-1 Ed3             Ed4
  5. Developing a method to forecast the risk of icing for single wind turbines
     and geographical sites
  6. Forecasting power production in cold climate conditions


 Motivation   Goals   Partners   Work packages   Preliminary results   Summary
Cooperation and Partners


VTT:                             VTT Technical Research Centre of Finland is the biggest
                                 multitechnological applied research organisation in Northern
                                 Europe. VTT provides high-end technology solutions and
                                 innovation services.
Fraunhofer IWES:                 Fraunhofer IWES is the leading German research institute in the
                                 field of wind energy and energy system technologies and offers
                                 a wide research spectrum from material development to grid
                                 optimization.
GL:                              GL Renewables Certification is the leading certification body in
                                 the wind energy sector, offering project and type certifications,
                                 also in the other fields of renewable energy exploitation.
WinWinD:                         WinWinD is an international wind energy solutions provider with
                                 a strong position in the global multi-megawatt market.




 Motivation   Goals   Partners    Work packages   Preliminary results   Summary
Work Packages during 2012-2014
Site Conditions &        Software                   Full-Scale               Software           Forecasting of
Certification            Development &              Measurements             Validation &       Icing Risks
Regulation               Simulation                                          Technical Note
- Assessing              - Adapting of          - Power and load             - Validation &     - Developing a
 appropriate site          TURBICE &              measurements                 improving of       method to
 conditions                OneWind to             from multi-MW                simulation         forecast the risk
- Decision of test         project                WT in icing                  models             of icing for WT
 turbine(s)                requirements           conditions                 - Developing of      outside normal
- Evaluation of          - Creating an iced     - Measuring of                 Ice classes        environmental
 current                   airfoil database       environmental              - Developing of      conditions
 certification             with TURBICE &         conditions and               new ”Technical   - Expanding
 guidelines                CFD                    ice accretion at             Note on Icing”     forecast to local
                         - Dyn. overall WT        FhG IWES met                                    site
                           simulation utilizing   mast
                           iced rotor blades




    Motivation   Goals   Partners   Work packages   Preliminary results   Summary
Work Packages during 2012-2014

  GL Renewables Certification intends to issue a technical note which will include modelling
  criteria for ice aggregation on the rotor blades, design load cases and ice classes for different
  durations of homogeneous and inhomogeneous ice aggregation.
  Therefore, large scale measurements will be used to consider the following issues :
  •   Thickness and local distribution of the ice aggregation along the blade radius and chord line
      resulting in changed mass distributions of the rotor blades.
  •   Changed aerodynamics of the blade profiles due to ice aggregation resulting in altered
      aerodynamic loads on the rotor blade.
  •   Inhomogeneous ice aggregation on the rotor (some blades iced, some not) leading to
      significant mass and aerodynamic imbalances on the rotor and thus high periodic loads.
  •   Temporal distribution of homogeneous and inhomogeneous ice aggregation, depending on
      the climatic conditions.




 Motivation   Goals   Partners   Work packages   Preliminary results   Summary
Preliminary Study on Icing
Overall model                                                    Table 1: Gross Properties Chosen for the NREL 5-MW
                                                                 Baseline Wind Turbine
•      NREL – 5 MW baseline wind turbine
                                                                   Rated power                                   5 MW
•      Widely used in the research community                       Rotor Orientation,                Upwind, 3Blades
Icing Conditions                                                   Configuration
                                                                   Rotor, Hub Diameter                     126 m, 3 m
Table 2: Typical rime ice conditions in Scandinavia

    Temperature                                        -7°C
    Median Volume Diameter (MVD)                      25 m
    Liquid Water Content (LWC)                    25 g/m3
    Icing time                                        3.5 h

Simulation
•      Ice shape from verified VTT code TURBICE and iced airfoil performance CFD results from Fluent
•      Iced airfoil Cl and Cd tables as input for NREL FAST
•      Results focusing on fatigue loads were calculated with NREL MLife
        –   Weibull-Rayleigh distribution of wind, Vave=8.5 m/s


    Motivation   Goals   Partners    Work packages      Preliminary results   Summary
Preliminary Study on Icing
Results: Ice accretion withTurbice & CFD                                                            Turbice result
                                                                                                    2kg/m
Ice on blades causes:
                                                                                                               airfoil
       • Reduction of aerodynamic performance
         (CFD results)                                                                                     3cm


           •     Small effect to airfoil lift coefficient                                 r/R
           •     Larger impact on airfoil drag                                      Accreted ice mass
           •
           Iced Cl and Cd on outer third of the blade                Moderate icing (CFD results)
           r/R = 0.7…1.0
Additional ice mass on blades by GL Guideline
                                                                               =-2…-5%
2010:


•          Only ice mass in the current certification
           design load cases (no aerodynamic effects)!
•          For NREL blade, max ice mass with GL
           formula would be 40kg/m
                                                                            These results are used as input for
•          Simulation with down-scaled GL ice mass                          FAST simulations
           formula according to TURBICE result

    Motivation   Goals   Partners   Work packages   Preliminary results   Summary
Preliminary Study on Icing

Case 1: Air density increase from                                                 = 1.225 to 1.292 kg/m3, 55days/year*
•           Air density of 1.292 kg/m 3 at 0°C and 0 m above sea level
•           No ice accretion on blades
•           Figure below present the components that were mostly effected by air density increase


              Reduced component fatigue
                      design life
             Reference design fatigue life**
    1.000
    0.980                                                                         RootMFlp1        = Blade 1 flapwise moment at the blade root
    0.960                                                                         LSSGagMys        = Nonrotating main bearing tilt moment
    0.940                                                      RootMFlp1          LSShftFys        = Nonrotating low speed shatf shear force
    0.920                                                                         TwrBsMyt         = Tower base fore-aft moment
                                                               LSSGagMys
    0.900
                                                               LSShftFys
    0.880
    0.860                                                      TwrBsMyt
    0.840
                                                                              *    Component Ice class III determined by IEA Task 19, Recommended
    0.820                                                                          Practices for Wind Energy Projects in Cold Climates, Draft, 2011
    0.800
                                                                              ** Reference component Miner cumulative damage             , designed for
                                                                                 20-years of operation



    Motivation    Goals      Partners          Work packages       Preliminary results      Summary
Preliminary Study on Icing
Case 2: Comparison of Rotor ice mass and aerodynamic effects
•            The icing on the rotor is symmetric (all blades have same ice shape) or asymmetric
             (1 blade is ice-free while two other blades are iced)
•            Fatigue loads from aerodynamic effects are bigger than ice mass effect **

    Component                                     Component fatigue loads* vs clean [%]
                                                           Mass effects         Mass + Aero. effects
    RootMzb1                   Sym.                            +2                         +25
                               Asym.                           +1                         +25
    RotThrust                  Sym.                            +1                         +22
                               Asym.                            0                         +22
    TwrBsMyt                   Sym.                             0                         +20
                               Asym.                            0                         +19
    RootMzb1 = Blade 1 pitching moment at the blade root
    RotThrust = Rotor thrust force
    TwrBsMyt = Tower base fore-aft moment

                                                                                                       *:  Fatigue loads represent Damage Equivalent Loads (DELs)
                                                                                                           from load Rainflow Cycle Counting (RCC) method
                                                                                                       **: Assuming that the same ice shape will stay on the blade for
                                                                                                           the whole duration




    Motivation        Goals        Partners         Work packages         Preliminary results   Summary
Preliminary Study on Icing
Case 3: Moderate icing, symmetric icing 30days/year*,
        asymmetric 1day/year,
•         Assumtion: The ice same shape will stay on the blade for the whole duration (31 days/year)
•         -10…-20 % power output loss at low winds AND reduced power output quality


                   Generator power, average                       Generator power, standard deviation




                                                                                                           C1=Clean (no ice)
                                                                                                           Case=Case 3




•         Annual Energy Production (AEP): -13 %
                                                                     *: Component Ice class II determined by IEA Task 19, Recommended
                                                                        Practices for Wind Energy Projects in Cold Climates, Draft, 2011




    Motivation   Goals   Partners     Work packages   Preliminary results    Summary
Preliminary Study on Icing
Case 3: Moderate icing, symmetric icing 30days/year*,
        asymmetric 1day/year,

•      Even a small amount of ice for a short period of time can effect component
       fatigue loads and component design life
                          Blade root design life reduced up to -55 %

     Component                        Component design life
                                      iced vs clean airfoil
     RootMzb1                                          0.45
                                                                                   Increased load level at blade root
                                                                                   (excess vibration levels)
     RotThrust                                         0.76
                                                                                      more stop-start sequences
     TwrBsMyt                                          0.79
     RootMzb1 = Blade 1 pitching moment at the blade root
                                                                                      increased fatigue loads
     RotThrust = Rotor thrust force
     TwrBsMyt = Tower base fore-aft moment




    Motivation         Goals        Partners         Work packages   Preliminary results   Summary
Summary




• Icing of blades causes additional wear and tear on different components
• The aerodynamic effects from iced blades are more significant for the
  fatigue loads than accreted ice mass
• Even small amounts of ice can decrease the wind turbines main
  component’s fatigue design life
• In icing climate sites, a substantial decrease in fatigue design life
  (up to -55 %) is seen if no measures are taken to prevent ice accretion on
  rotor blades




Motivation   Goals   Partners   Work packages   Preliminary results   Summary
Thank you for your attention!




     Ville Lehtomäki
     VTT Technical Research Centre of Finland, Wind Energy
     Address: Vuorimiehentie 5, Espoo, P.O. Box 1000, FI-02044 VTT, Finland
     Phone:     +358 40 176 3147
     Fax:       +358 20 722 5888
     E-Mail:    ville.lehtomaki@vtt.fi


     Sebastian Hetmanczyk
     Fraunhofer Institute for Wind Energy and Energy System Technology, IWES
     Simulation and Assessment of Wind Turbines
     Address: Am Seedeich 45, 27572 Bremerhaven, Germany
     Phone: +49 471 14290-364
     Fax:      +49 471 14290-111
     E-Mail: sebastian.hetmanczyk@iwes.fraunhofer.de




Motivation   Goals   Partners   Work packages   Preliminary results   Summary

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IcedBlades - Modelling of ice accretion on rotor blades in a dynamic overall wind turbine tool V. Lehtomäki (VTT), S. Hetmanczyk, M. Durstewitz, A. Baier (Fraunhofer IWES), K. Freudenreich, K. Argyria

  • 1. IcedBlades - Modelling of ice accretion on rotor blades in a coupled wind turbine tool V. Lehtomäki 1, S. Hetmanczyk 2 , M. Durstewitz 2 , A. Baier 2, K. Freudenreich 3 , K. Argyriadis 3 1) VTT Technical Research Centre of Finland, Espoo, Finland 2) Fraunhofer Institute for Wind Energy and Energy System Technology (IWES), Bremerhaven, Germany 3) Germanischer Lloyd Renewables Certification, Hamburg, Germany © Fraunhofer IWES
  • 2. Outline • Project Motivation • Project Objectives • Cooperation and Partners • Work Packages and Schedule • Preliminary Study on Icing • Summary
  • 3. Project Motivation Northern areas like Scandinavia as well as areas with high altitude feature a high potential for large capacity wind farms thanks to favourable wind conditions and mostly low populated areas. • Expansion of a common European research area by combining different research backgrounds • WinterWind 2011: R&D Priorities for cold climate (Jos Beurskens, ECN) • Impact on loading (aerodynamically and mechanical/aerodynamically induced loads, scale effects) • Impact on performance (how big are “hidden” energy losses) • Field test facilities for problem definition and verification of models • Demand for independent technical note on Figure 1: Wind energy capacity in the USA [NREL] icing (Mike Wöbbeking, GL, WinterWind 2011) Motivation Goals Partners Work packages Preliminary results Summary
  • 4. Project Objectives Within the project scope a new and updated simulation tools for ice accretion on rotor blades and coupling of this tool to an aero-servo-elastic simulation tool will be developed. 1. Predicting the power losses resulting from ice accretion on rotor blades. 2. Gain a better understanding of dynamic loading effects resulting from ice accretion on rotor blades via a validated numerical models. 3. Developing a new technical note for icing sites to help wind turbine designers to take into account icing effects of rotor blades more accurately than current guidelines. 4. Development of icing classes for new edition of IEC 61400-1 Ed3 Ed4 5. Developing a method to forecast the risk of icing for single wind turbines and geographical sites 6. Forecasting power production in cold climate conditions Motivation Goals Partners Work packages Preliminary results Summary
  • 5. Cooperation and Partners VTT: VTT Technical Research Centre of Finland is the biggest multitechnological applied research organisation in Northern Europe. VTT provides high-end technology solutions and innovation services. Fraunhofer IWES: Fraunhofer IWES is the leading German research institute in the field of wind energy and energy system technologies and offers a wide research spectrum from material development to grid optimization. GL: GL Renewables Certification is the leading certification body in the wind energy sector, offering project and type certifications, also in the other fields of renewable energy exploitation. WinWinD: WinWinD is an international wind energy solutions provider with a strong position in the global multi-megawatt market. Motivation Goals Partners Work packages Preliminary results Summary
  • 6. Work Packages during 2012-2014 Site Conditions & Software Full-Scale Software Forecasting of Certification Development & Measurements Validation & Icing Risks Regulation Simulation Technical Note - Assessing - Adapting of - Power and load - Validation & - Developing a appropriate site TURBICE & measurements improving of method to conditions OneWind to from multi-MW simulation forecast the risk - Decision of test project WT in icing models of icing for WT turbine(s) requirements conditions - Developing of outside normal - Evaluation of - Creating an iced - Measuring of Ice classes environmental current airfoil database environmental - Developing of conditions certification with TURBICE & conditions and new ”Technical - Expanding guidelines CFD ice accretion at Note on Icing” forecast to local - Dyn. overall WT FhG IWES met site simulation utilizing mast iced rotor blades Motivation Goals Partners Work packages Preliminary results Summary
  • 7. Work Packages during 2012-2014 GL Renewables Certification intends to issue a technical note which will include modelling criteria for ice aggregation on the rotor blades, design load cases and ice classes for different durations of homogeneous and inhomogeneous ice aggregation. Therefore, large scale measurements will be used to consider the following issues : • Thickness and local distribution of the ice aggregation along the blade radius and chord line resulting in changed mass distributions of the rotor blades. • Changed aerodynamics of the blade profiles due to ice aggregation resulting in altered aerodynamic loads on the rotor blade. • Inhomogeneous ice aggregation on the rotor (some blades iced, some not) leading to significant mass and aerodynamic imbalances on the rotor and thus high periodic loads. • Temporal distribution of homogeneous and inhomogeneous ice aggregation, depending on the climatic conditions. Motivation Goals Partners Work packages Preliminary results Summary
  • 8. Preliminary Study on Icing Overall model Table 1: Gross Properties Chosen for the NREL 5-MW Baseline Wind Turbine • NREL – 5 MW baseline wind turbine Rated power 5 MW • Widely used in the research community Rotor Orientation, Upwind, 3Blades Icing Conditions Configuration Rotor, Hub Diameter 126 m, 3 m Table 2: Typical rime ice conditions in Scandinavia Temperature -7°C Median Volume Diameter (MVD) 25 m Liquid Water Content (LWC) 25 g/m3 Icing time 3.5 h Simulation • Ice shape from verified VTT code TURBICE and iced airfoil performance CFD results from Fluent • Iced airfoil Cl and Cd tables as input for NREL FAST • Results focusing on fatigue loads were calculated with NREL MLife – Weibull-Rayleigh distribution of wind, Vave=8.5 m/s Motivation Goals Partners Work packages Preliminary results Summary
  • 9. Preliminary Study on Icing Results: Ice accretion withTurbice & CFD Turbice result 2kg/m Ice on blades causes: airfoil • Reduction of aerodynamic performance (CFD results) 3cm • Small effect to airfoil lift coefficient r/R • Larger impact on airfoil drag Accreted ice mass • Iced Cl and Cd on outer third of the blade Moderate icing (CFD results) r/R = 0.7…1.0 Additional ice mass on blades by GL Guideline =-2…-5% 2010: • Only ice mass in the current certification design load cases (no aerodynamic effects)! • For NREL blade, max ice mass with GL formula would be 40kg/m These results are used as input for • Simulation with down-scaled GL ice mass FAST simulations formula according to TURBICE result Motivation Goals Partners Work packages Preliminary results Summary
  • 10. Preliminary Study on Icing Case 1: Air density increase from = 1.225 to 1.292 kg/m3, 55days/year* • Air density of 1.292 kg/m 3 at 0°C and 0 m above sea level • No ice accretion on blades • Figure below present the components that were mostly effected by air density increase Reduced component fatigue design life Reference design fatigue life** 1.000 0.980 RootMFlp1 = Blade 1 flapwise moment at the blade root 0.960 LSSGagMys = Nonrotating main bearing tilt moment 0.940 RootMFlp1 LSShftFys = Nonrotating low speed shatf shear force 0.920 TwrBsMyt = Tower base fore-aft moment LSSGagMys 0.900 LSShftFys 0.880 0.860 TwrBsMyt 0.840 * Component Ice class III determined by IEA Task 19, Recommended 0.820 Practices for Wind Energy Projects in Cold Climates, Draft, 2011 0.800 ** Reference component Miner cumulative damage , designed for 20-years of operation Motivation Goals Partners Work packages Preliminary results Summary
  • 11. Preliminary Study on Icing Case 2: Comparison of Rotor ice mass and aerodynamic effects • The icing on the rotor is symmetric (all blades have same ice shape) or asymmetric (1 blade is ice-free while two other blades are iced) • Fatigue loads from aerodynamic effects are bigger than ice mass effect ** Component Component fatigue loads* vs clean [%] Mass effects Mass + Aero. effects RootMzb1 Sym. +2 +25 Asym. +1 +25 RotThrust Sym. +1 +22 Asym. 0 +22 TwrBsMyt Sym. 0 +20 Asym. 0 +19 RootMzb1 = Blade 1 pitching moment at the blade root RotThrust = Rotor thrust force TwrBsMyt = Tower base fore-aft moment *: Fatigue loads represent Damage Equivalent Loads (DELs) from load Rainflow Cycle Counting (RCC) method **: Assuming that the same ice shape will stay on the blade for the whole duration Motivation Goals Partners Work packages Preliminary results Summary
  • 12. Preliminary Study on Icing Case 3: Moderate icing, symmetric icing 30days/year*, asymmetric 1day/year, • Assumtion: The ice same shape will stay on the blade for the whole duration (31 days/year) • -10…-20 % power output loss at low winds AND reduced power output quality Generator power, average Generator power, standard deviation C1=Clean (no ice) Case=Case 3 • Annual Energy Production (AEP): -13 % *: Component Ice class II determined by IEA Task 19, Recommended Practices for Wind Energy Projects in Cold Climates, Draft, 2011 Motivation Goals Partners Work packages Preliminary results Summary
  • 13. Preliminary Study on Icing Case 3: Moderate icing, symmetric icing 30days/year*, asymmetric 1day/year, • Even a small amount of ice for a short period of time can effect component fatigue loads and component design life Blade root design life reduced up to -55 % Component Component design life iced vs clean airfoil RootMzb1 0.45 Increased load level at blade root (excess vibration levels) RotThrust 0.76 more stop-start sequences TwrBsMyt 0.79 RootMzb1 = Blade 1 pitching moment at the blade root increased fatigue loads RotThrust = Rotor thrust force TwrBsMyt = Tower base fore-aft moment Motivation Goals Partners Work packages Preliminary results Summary
  • 14. Summary • Icing of blades causes additional wear and tear on different components • The aerodynamic effects from iced blades are more significant for the fatigue loads than accreted ice mass • Even small amounts of ice can decrease the wind turbines main component’s fatigue design life • In icing climate sites, a substantial decrease in fatigue design life (up to -55 %) is seen if no measures are taken to prevent ice accretion on rotor blades Motivation Goals Partners Work packages Preliminary results Summary
  • 15. Thank you for your attention! Ville Lehtomäki VTT Technical Research Centre of Finland, Wind Energy Address: Vuorimiehentie 5, Espoo, P.O. Box 1000, FI-02044 VTT, Finland Phone: +358 40 176 3147 Fax: +358 20 722 5888 E-Mail: ville.lehtomaki@vtt.fi Sebastian Hetmanczyk Fraunhofer Institute for Wind Energy and Energy System Technology, IWES Simulation and Assessment of Wind Turbines Address: Am Seedeich 45, 27572 Bremerhaven, Germany Phone: +49 471 14290-364 Fax: +49 471 14290-111 E-Mail: sebastian.hetmanczyk@iwes.fraunhofer.de Motivation Goals Partners Work packages Preliminary results Summary