Wind Turbine Boundary Layer Control for Blade Stability

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Longer, more complex wind turbine blades face challenges in pitch control systems, particularly in extreme wind conditions, where negative stall can occur due to blade twist features, leading to turbulence, noise, and instability, and existing boundary layer control systems are difficult to integrate into wind turbine control systems.

Innovation Solution

A wind turbine system with a boundary layer control system that monitors operational speed, tower motion, and aerodynamic loads to activate airflow control through blade surface openings, reducing the need for aggressive pitch adjustments and minimizing mechanical degradation by regulating lift without extensive pitch control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If blade twist features are used to compensate for changing apparent wind angle, then aerodynamic efficiency is improved, but negative stall occurs leading to turbulence, noise and instability

Engineering Contradiction:
Improveaerodynamic efficiencyVSAvoidblade stability
Core Design Contradiction:
ProductivityVSStability of the object's composition

Solution Approach 1:

The boundary layer control system applies local airflow disruption at the mid-portion of the blade through spanwise vents, creating different flow conditions in different blade sections. This localized intervention maintains the beneficial twist geometry while preventing negative stall in the critical mid-section where it occurs most severely.

Inventive Principle:
Principle #3Local quality

2Force

If basic pitch control techniques are used to reduce torque in high wind conditions, then torque control is achieved, but integration with newer longer blade designs becomes problematic

Engineering Contradiction:
Improvetorque controlVSAvoidcontrol system integration complexity
Core Design Contradiction:
ForceVSDevice complexity

Solution Approach 1:

The boundary layer control system acts as an intermediary mechanism between the pitch control system and the aerodynamic loads. By introducing airflow disruption through blade vents, it provides an additional degree of freedom for torque control that works complementarily with pitch control, making the system more adaptable to longer blade designs without requiring complete redesign of the pitch control architecture.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Force

If blade pitch angle is adjusted to reduce overall lift, then torque reduction is achieved, but tip-ward part of the blade goes into negative stall

Engineering Contradiction:
Improvelift reductionVSAvoidblade airflow stability
Core Design Contradiction:
ForceVSStability of the object's composition

Solution Approach 1:

The boundary layer control system performs preliminary action by disrupting the boundary layer airflow before the pitch adjustment would cause negative stall at the blade tip. By pre-conditioning the airflow in the mid-portion of the blade, it prevents the adverse effects of pitch-induced negative angle of attack from propagating to the tip region.

Inventive Principle:
Principle #10Preliminary action

4Adaptability or versatility

If airflow vents are used to disrupt airflow and reduce lift, then torque control flexibility is improved, but system integration complexity increases

Engineering Contradiction:
Improvetorque control flexibilityVSAvoidboundary layer control integration
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The boundary layer control system with spanwise vents is designed to perform multiple functions: torque control, negative stall prevention, and complementarity with pitch control. This multi-functionality justifies the integration complexity by providing a versatile control mechanism that addresses multiple aerodynamic challenges simultaneously, particularly for longer blade designs where single-function controls are insufficient.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system effectively reduces operational risks in extreme wind conditions by providing a robust approach to detect and mitigate damage, reducing pitch control system wear and maintaining stability through controlled airflow disruptions.

Implementation Method 1

a boundary layer control system configured to control airflow through blade surface openings in each of the blades

Methodology Applied
Scientific EffectBoundary layer control: Boundary Layer

Implementation Method 2

Blowing air through the vents disrupts the airflow around the blade, which therefore reduces the generated lift along the corresponding section of the blade

Methodology Applied
Scientific EffectFlow disruption: Flow Separation

Data Source

PatentUS11248584B2Relating to wind turbines having blades equipped with boundary layer control system
Publication Date: 2022.02.15 VESTAS WIND SYSTEMS AS
  • US11248584B2 patent drawing
  • US11248584B2 patent drawing
  • US11248584B2 patent drawing

AI summary

A wind turbine system comprising a nacelle mounted on a tower, a rotor having a plurality of blades and a boundary layer control system configured to control airflow through blade surface openings in each of the blades. The wind turbine system includes a control system configured to perform at least one of the following: to monitor an operational speed parameter of the wind turbine, and to activate the boundary layer control system if it is determined that the 1 operational speed parameter exceeds a predetermined speed parameter threshold; to monitor tower motion and to activate the boundary layer control system based on a determination of excessive tower motion; to monitor for a wind turbine shutdown condition, and to activate the boundary layer control system if it is determined that a wind turbine shutdown condition has been identified; and to monitor the aerodynamic loads on the blades, and to activate the boundary layer control system also based on a determination of excessive blade loads. The system thereby provides an approach to activating and deactivating the boundary layer control system to reduce operational risk to the wind turbine.