Wind Turbine Rotor Plane Monitoring Using Single-Receiver GNSS

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Solution Overview

Problem

Existing wind turbine rotor plane alignment systems face accuracy and cost issues due to local turbulence, lightning risks from electrical devices, and errors from ionospheric and tropospheric distortions, leading to inefficient energy harvesting and structural loading.

Innovation Solution

A rotor plane monitoring system using a single receiver unit with a switching mechanism and multiple detection nodes to determine orientation accurately, employing GNSS signals corrected by ground-based systems, and a sequencing module to compute direction vectors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If multiple GNSS receivers are mounted on the wind turbine to determine spatial alignment, then the rotor plane orientation can be directly established, but the system cost increases significantly and measurement accuracy is compromised by ionospheric and tropospheric distortions

Engineering Contradiction:
Improverotor plane orientation accuracyVSAvoidnumber of GNSS receivers
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system divides the measurement function into multiple detection nodes distributed on the wind turbine structure, each node containing an antenna. By segmenting the receiver functionality across multiple nodes and using a single centralized receiver to process signals from all nodes sequentially, the system achieves orientation measurement capability equivalent to multiple receivers while reducing device complexity and cost

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A single GNSS receiver unit is designed to perform multiple measurement functions by sequentially connecting to different detection nodes. This universal receiver can determine the spatial positions of multiple nodes and calculate rotor plane orientation, replacing the need for multiple dedicated receivers and reducing system complexity

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

2Measurement precision

If electrical devices are arranged in the rotor blades to establish rotor plane orientation, then direct measurement is achieved, but flashover risk occurs in the event of lightning strike

Engineering Contradiction:
Improverotor plane orientation measurementVSAvoidlightning strike risk
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The active electronic measurement devices (GNSS receivers) are extracted from the rotor blades and relocated to safe positions on the nacelle or tower. The rotor blades retain only passive detection nodes (antennas) that pose no lightning risk, while the active processing equipment is positioned in lightning-protected zones, separating the measurement function from the hazardous environment

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

Detection nodes with antennas are introduced as intermediary elements on the rotor blades to capture GNSS signals without requiring active electronic devices in the blades themselves. These passive nodes serve as signal collection points that can be safely connected to protected receivers through switching mechanisms, eliminating direct exposure of electronic equipment to lightning risks

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of operation

If pressure sensors at the front hub are used to detect misalignment relative to measured wind direction, then rotor plane alignment can be determined, but accuracy is compromised by local turbulence caused by rotating rotor blades

Engineering Contradiction:
Improvealignment determination methodVSAvoidalignment measurement accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The mechanical pressure sensor-based alignment detection system is replaced with an electromagnetic/GNSS-based spatial position measurement system. By using GNSS signals to directly determine the three-dimensional positions of detection nodes and calculate orientation through geometric relationships, the system eliminates the need for pressure sensors and avoids turbulence-related measurement errors while providing more precise orientation data

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

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

Enables accurate and cost-effective rotor plane alignment, optimizing energy harvesting and reducing structural loading by continuously correcting alignment to wind direction changes.

Implementation Method 1

an antenna assembly configured to detect radio-frequency signals at a plurality of distinct detection nodes on the wind turbine

Methodology Applied
Scientific EffectRadio-frequency signal detection: Electromagnetic Induction

Implementation Method 2

a single receiver unit configured to decode positioning signals or GNSS signals broadcast by satellites of a satellite navigation system

Methodology Applied
Scientific EffectGNSS signal reception and decoding: Electromagnetic Induction

Data Source

PatentEP4463626B1Rotor plane monitoring system
Publication Date: 2025.11.05 SIEMENS GAMESA RENEWABLE ENERGY AS
  • EP4463626B1 patent drawingFigure 1
  • EP4463626B1 patent drawingFigure 2~3
  • EP4463626B1 patent drawingFigure 4~5

AI summary

The invention describes a rotor plane monitoring system (1) of a wind turbine (2), comprising a single receiver unit (10) configured to decode positioning signals (10in) originating from a satellite navigation system; an antenna assembly configured to detect radio-frequency signals at a plurality of distinct detection nodes (N1, …, Nn) on the wind turbine (2) and to relay detected signals (10in) to the receiver unit (10); a signal processing module (13) configured to compute a direction vector (V12,..., V45; V54,..., V21) from the signals (10in) relayed to the receiver unit (10); and an evaluation module (14) configured to determine the rotor plane orientation from the direction vector (V12,..., V45; V54,..., V21). The invention further describes a wind turbine (2) comprising such a rotor plane monitoring system (1); and a method of monitoring the orientation of a wind turbine rotor plane.