Abstract

This article presents the consolidated results of a comprehensive validation campaign of a pneumatic active flap system (AFS) developed within the scope of the Induflap2 project [1] in a collaboration effort between Siemens Gamesa Renewable Energy A/S (SGRE), the Technical University of Denmark (DTU), and Rehau GmbH. The validation results presented herein include wind tunnel measurements, measurements in a rotating test rig under free atmospheric conditions, as well as the validation at full scale on a 4MW wind turbine with 130m rotor diameter (SWT-4.0-130). This article is of a summarizing character and the reader is referred to further literature where applicable. During the course of the project, several revisions of the AFS were developed and tested at different levels of fidelity. Along with the different variations of the AFS, the impact of variations of the geometric and material related design parameters were studied. Two of the latest revisions of the AFS were tested at full scale on a wind turbine. The measurements presented herein focus solely on the latest revision of the AFS (internally referred to as the FT008rev10 concept). The different tests and measurements were performed in the period from 2016 to 2019. During the full scale measurements, a wind speed dependent load impact between 5% and 10% was measured for the blade root flapwise bending moments, demonstrating thus a large potential for turbine loading adjustments to perform active load control on modern wind turbines.

Highlights

  • This article presents the consolidated results of a comprehensive validation campaign of a pneumatic active flap system (AFS) developed within the scope of the Induflap2 project [1] in a collaboration effort between Siemens Gamesa Renewable Energy A/S (SGRE), the Technical University of Denmark (DTU), and Rehau GmbH

  • The design of the active flap system shall comply with industrial requirements and be characterized at full scale level striving for a high technology readiness level. It has been an objective of the project to perform the characterization of the AFS in a stepwise approach, increasing the fidelity level of validation in a systematic manner starting with tests under controlled conditions in a wind tunnel, continuing to testing under atmospheric flow in a rotating test rig and on a full scale wind turbine

  • Wind tunnel measurements performed for the latest revision of the AFS show a lift impact levels of approx. 0.4 and provided

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Summary

Introduction

The validation results presented include wind tunnel measurements, measurements in a rotating test rig under free atmospheric conditions, as well as the validation at full scale on a 4MW wind turbine with 130m rotor diameter (SWT-4.0-130). It has been an objective of the project to perform the characterization of the AFS in a stepwise approach, increasing the fidelity level of validation in a systematic manner starting with tests under controlled conditions in a wind tunnel, continuing to testing under atmospheric flow in a rotating test rig and on a full scale wind turbine.

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