Device and method of controlling blade instabilities of a wind turbine to avoid blade fluttering

US11905932B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11905932-B2
Application numberUS-202117928017-A
CountryUS
Kind codeB2
Filing dateMay 21, 2021
Priority dateJun 5, 2020
Publication dateFeb 20, 2024
Grant dateFeb 20, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A device and a method of controlling blade instabilities of a wind turbine is provided. The method including the following steps: defining at least one preliminary overspeed threshold value; defining a fluttering rotor speed at and above which a predetermined fluttering of at least one of the blades occurs, the fluttering rotor speed is defined as a function of the pitch angle and/or as a function of the wind speed; setting a final overspeed threshold value to be equal to or smaller than a minimum rotor speed of the at least one preliminary overspeed threshold value and the fluttering rotor speed at the actual pitch angle and/or at the actual wind speed; and controlling the rotor speed to not exceed the final overspeed threshold value.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of controlling blade instabilities of a wind turbine, the wind turbine comprising a rotor having a plurality of rotor blades, the rotor being mounted to a nacelle to rotate about a rotation axis with a rotor speed, wherein each blade is configured to be pitched by a pitch angle about a pitch axis of the blade, the method comprising: defining at least one preliminary overspeed threshold value; defining a fluttering rotor speed at and above which a predetermined fluttering of at least one of the blades occurs, the fluttering rotor speed is defined as a function of the pitch angle and/or as a function of the wind speed; setting a final overspeed threshold value to be equal to or smaller than a minimum rotor speed of the at least one preliminary overspeed threshold value and the fluttering rotor speed at an actual pitch angle and/or at an actual wind speed; and controlling the rotor speed to not exceed the final overspeed threshold value. 2. The method according to claim 1 , wherein the final overspeed threshold value is acquired from a lookup table as a function of the at least one preliminary overspeed threshold value, the actual pitch angle and/or the actual wind speed. 3. The method according to claim 1 , wherein the at least one preliminary overspeed threshold value is dynamically changed based on a predetermined parameter or based on a predetermined event. 4. The method according to claim 1 , wherein the at least one preliminary overspeed threshold value includes: a first preliminary overspeed threshold value which is provided from a hardware outside the wind turbine; and/or a second preliminary overspeed threshold value which is provided from an internal control device of the wind turbine; wherein the final overspeed threshold value is set to be equal to or smaller than a minimum rotor speed of at least one of the first preliminary overspeed threshold value and the second preliminary overspeed threshold value, and of the fluttering rotor speed at the actual pitch angle and/or at the actual wind speed. 5. A control device configured to control blade instabilities of a wind turbine, the wind turbine comprising a rotor having a plurality of rotor blades, the rotor being mounted to a nacelle to rotate about a rotation axis with a rotor speed, wherein each blade is configured to be pitched by a pitch angle about a pitch axis of the blade, wherein, the control device is configured to set a final overspeed threshold value to be equal to or smaller than a minimum rotor speed of at least one preliminary overspeed threshold value and a fluttering rotor speed, at and above which a predetermined fluttering of at least one of the blades occurs, the fluttering rotor speed is defined as a function of the pitch angle and/or as a function of the wind speed; and the control device is configured to control the rotor speed to not exceed the final overspeed threshold value. 6. The control device according to claim 5 , wherein the control device is configured to access a lookup table, where the final overspeed threshold value is defined as a function of the at least one preliminary overspeed threshold value, an actual pitch angle and/or an actual wind speed. 7. The control device according to claim 5 , wherein the at least one preliminary overspeed threshold value dynamically changes based on a predetermined parameter or based on a predetermined event. 8. The control device according to claim 5 , wherein the at least one preliminary overspeed threshold value includes: a first preliminary overspeed threshold value which is provided from a hardware outside the wind turbine; and/or a second preliminary overspeed threshold value which is provided from the control device; wherein the control device is configured to set the final overspeed threshold value to be equal to or smaller than a minimum rotor speed of at least one of the first preliminary overspeed threshold value and the second preliminary overspeed threshold value, and of the fluttering rotor speed at an actual pitch angle and/or at an actual wind speed. 9. A wind turbine comprising the control device according to claim 5 .

Assignees

Inventors

Classifications

  • F03D7/0276Primary

    controlling rotor speed, e.g. variable speed · CPC title

  • Preventing, counteracting or reducing vibration or noise · CPC title

  • to prevent overspeed · CPC title

  • Rotor or generator speeds · CPC title

  • active, predictive, or anticipative · CPC title

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Frequently asked questions

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What does patent US11905932B2 cover?
A device and a method of controlling blade instabilities of a wind turbine is provided. The method including the following steps: defining at least one preliminary overspeed threshold value; defining a fluttering rotor speed at and above which a predetermined fluttering of at least one of the blades occurs, the fluttering rotor speed is defined as a function of the pitch angle and/or as a funct…
Who is the assignee on this patent?
Siemens Gamesa Renewable Energy As
What technology area does this patent fall under?
Primary CPC classification F03D7/0276. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 20 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).