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Technische Universität München Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures Smart Wind Turbine Rotor Blades Luiz da Rocha-Schmidt, Felix Stroscher, Bin Wei, Horst Baier 03.07.2012

Smart Wind Turbine Rotor Bladesmediatum.ub.tum.de/doc/1110011/837095.pdf · 2013. 5. 6. · • Smart Rotor Blades are able to reduce peak loads • Aerodynamically efficient control

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  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Smart Wind Turbine Rotor Blades

    Luiz da Rocha-Schmidt, Felix Stroscher, Bin Wei, Horst Baier

    03.07.2012

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Contents

    • Motivation: Reduce peak (gust) loads on wind turbines

    • Smart / Adaptive Wings: Aircraft, Helicopter

    • Morphing Control Surfaces

    • Gust Load Alleviation on Wind Turbines

    • Conclusion

    03.07.2012 2 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Motivation

    • Wind Power is a well established, clean energy source

    • Efficiency aim: build larger wind turbines

    – Largest to date: Enercon E-126, d=126m, P=7,5MW

    • Size limitation (among others):

    – Structural loads due to gravity and wind

    – Lifespan impact: instationary gust loads

    03.07.2012 3 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Smart / Adaptive Structures

    Sensor Controller Actuator

    03.07.2012 4

    • Sensor: observe a disturbance – e.g. wind, acceleration, strain sensor

    • Controller: determine reaction to achieve desired result – e.g. feedback / feedforward controller

    • Actuator: execute controller command – e.g. blade pitch axis rotation, control surface

    Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    • Structural wing model

    – Finite Element Method

    • Aerodynamic Wing Model

    – Doublet Lattice Method

    • Coupled Aero-Elastic analysis

    – time domain

    Trailing edge devices for

    flight- and load control

    Dynamic Load Alleviation (aircraft)

    03.07.2012 5 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Dynamic Load Alleviation (aircraft)

    • Feedforward controller

    – „Gust sniffer“ in front of the wing

    – Control command on the flaps

    • Structural response

    – 30 % peak load reduction

    03.07.2012 6 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Dynamic Load Alleviation / Noise Reduction (Helicopter Blade)

    • „Smart“ Helicopter rotor blade

    – Piezo-actuated Trailing edge

    • +/- 6°deflection

    – Reduced Blade loads

    – Reduced Noise Level

    03.07.2012 7 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Morphing Control Surfaces

    • Plain flaps vs. Morphing Flaps

    • Benefits:

    – Reduced Drag, increased Lift

    – More generated power with same structural loads

    03.07.2012 8 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Airfoil morphing

    9

    S814 Airfoil S812 Airfoil S813 Airfoil

    Sample reference rotor: AOC 15/50 – Layout and airfoils:

    Adaptation using a generic elastoflexible airfoil

    03.07.2012 Luiz da Rocha-Schmidt

    See Poster by Institute of Aerodynamics and Fluid Mechanics!

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Transient Wind Loads (Video)

    NREL 5 MW reference turbine

    hub height: 90 m, rotor diameter: 126 m, mean wind speed: 12 m/s

    03.07.2012 10 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Transient Wind Loads (Video)

    NREL 5 MW reference turbine

    hub height: 90 m, rotor diameter: 126 m, mean wind speed: 12 m/s

    03.07.2012 11 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Effects of gust load alleviation on a wind turbine blade

    • NREL 5 MW reference turbine, Lee et. al., KAIST, Daejeon, Korea

    03.07.2012 12 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Challenges

    • Reliability

    – If the control system fails, the turbine can not be operated without the risk of damage

    • Cost

    – Additional hard- and software is needed

    • Power Requirements

    – Energy consumption of the controller and the actuators must be kept low

    03.07.2012 13 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Conclusion

    • Smart Rotor Blades are able to reduce peak loads

    • Aerodynamically efficient control surfaces: Morphing Flaps

    • Combined: Larger and more efficient wind turbines

    03.07.2012 14 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Thank you – Questions?

    03.07.2012 15 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    BACKUP SLIDES

    03.07.2012 16 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Passive Solution: Elastoflexible wing

    17

    Concept • Internal Support Structure

    • Elastic membrane skin as aerodynamic surface

    Reasoning • Large shape variations are possible with low effort

    • passive flow control through load-dependent

    membrane deflection

    Source: TUM Institute of Aerodynamics and Fluid Mechanics & TUM Institute for Computational Mechanics

    03.07.2012 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Feedforward adaptive filtering → Learning capabilities for specific input signal

    → Response on discrete gust triplet with adaptive filtering

    → Peak reduction increases with time, as filter parameters are adapted

    → ~ 50% Peak reduction

    Dynamic Load Alleviation (aircraft)

    03.07.2012 18 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    19

    Windenergieanlagen: morphing / adaptive rotors

    Membrane wing – “Morphing“ (Airfoil adaptation; passive load control)

    03.07.2012 Luiz da Rocha-Schmidt

  • Technische Universität München

    Lehrstuhl für Leichtbau (LLB) Institute of Lightweight Structures

    Dynamic Load Alleviation of wing-like structures in unsteady flow fields

    → Feedback controller

    • Feedback of acceleration sensor

    signal at the wingtip

    • 2nd order transfer function for

    damping of the 1st bending mode

    • Control Command on Trailing Edge

    Devices

    → Structural response:

    • ~10% reduction of first peak in

    bending moment, but very strong

    reduction of following peaks

    • Highly efficient damping of a steady

    vibration

    • Low efficiency of highly transient

    response

    03.07.2012 20 Luiz da Rocha-Schmidt