Wind Turbine Rotor Blade Extreme Load Envelope Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing wind turbines face challenges in effectively controlling extreme loads on rotor blades due to fluctuating environmental conditions, which can lead to component damage and failure, and current sensor systems are complex, expensive, and prone to inaccuracies.

Innovation Solution

A method and system utilizing a processor to calculate flapwise and edgewise bending moments, along with an average and overall load envelope, to implement control actions when loads exceed a threshold, including pitching the rotor blades, through an envelope-based control algorithm that filters unwanted frequencies and predicts future loads.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional sensor systems are used to measure loads on wind turbine components, then measurement accuracy may be improved, but device complexity and cost increase significantly

Engineering Contradiction:
Improveload measurement accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent uses a computational model (copy) of the load calculation based on thrust measurements and aerodynamic relationships, rather than directly installing complex sensor systems on the blade roots. The model replicates the load measurement function using existing sensors and mathematical relationships, thereby avoiding the complexity and cost of direct measurement sensors while maintaining measurement capability

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent replaces the mechanical sensor system (strain gauges, load cells) with a computational approach using aerodynamic models and thrust measurements. The mechanical measurement system is substituted with an information-processing system that calculates loads from readily available operational parameters, reducing device complexity while providing load information

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If more sensors are installed to improve load measurement reliability, then measurement accuracy improves, but device complexity and failure risk increase

Engineering Contradiction:
Improveload measurement reliabilityVSAvoidsensor system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent makes the existing thrust measurement system serve multiple functions: it provides both the primary control feedback for pitch regulation and the basis for calculating blade root loads. This multi-functionality eliminates the need for separate dedicated load sensors, maintaining reliability while reducing system complexity and the number of potential failure points

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

Solution Approach 2:

The control system uses its own existing measurements (thrust, pitch angle, power output) to calculate loads autonomously without requiring external sensor systems. The system serves its own measurement needs by processing data already collected for control purposes, thereby improving reliability without adding vulnerable external components

Inventive Principle:
Principle #25Self-service

3Reliability

If control actions are taken to reduce extreme loads on rotor blades, then component reliability improves, but energy production may be reduced

Engineering Contradiction:
Improvecomponent reliabilityVSAvoidenergy production
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent calculates and predicts future load envelopes in advance, allowing the control system to prepare for upcoming extreme loads before they occur. By using look-ahead prediction based on wind speed forecasts and aerodynamic models, the system can proactively adjust pitch angles to prevent load exceedances rather than reacting after damage occurs, thereby maintaining reliability while minimizing production losses

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The control system dynamically adjusts pitch angles based on real-time thrust measurements and predicted load envelopes, rather than using fixed conservative limits. This dynamic control allows the system to operate at optimal pitch angles during normal conditions (maximizing energy production) and automatically reduce loads only when and where extreme conditions are predicted, thereby balancing productivity and reliability

Inventive Principle:
Principle #15Dynamics

4Device complexity

If thrust-based control strategies are used to estimate loads, then device complexity is reduced, but measurement precision and reliability may be compromised

Engineering Contradiction:
Improvecontrol system complexityVSAvoidload estimation accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The patent implements a feedback mechanism where the calculated load estimates are continuously compared against predicted load envelopes, and the pitch control is adjusted based on the difference. This closed-loop feedback ensures that even though the load estimation uses simplified thrust-based calculations rather than direct measurements, the control system compensates by actively regulating pitch to maintain loads within acceptable limits, thereby achieving both simplicity and accuracy

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS12392323B2System and method for improved extreme load control for wind turbine rotor blades
Publication Date: 2025.08.19 GENERAL ELECTRIC RENOVABLES ESPANA SL
  • US12392323B2 patent drawing
  • US12392323B2 patent drawing
  • US12392323B2 patent drawing

AI summary

A method for reducing extreme loads acting on at least one rotor blade of a wind turbine includes calculating, via a processor, a flapwise bending moment of the rotor blade(s). Further, the method includes calculating, via the processor, an edgewise bending moment of the rotor blade(s). The method also includes calculating, via the processor, an average load envelope of a blade root bending moment of the rotor blade(s) as a function of the flapwise bending moment and the edgewise bending moment of the rotor blade(s). Moreover, the method includes calculating, via the processor, an overall load envelope of the blade root bending moment of the rotor blade(s) as a function of the average load envelope and a future load estimation of the blade root bending moment of the rotor blade(s). As such, the method also includes implementing, via the processor, a control action when the overall load envelope is above a certain threshold.