Method of balancing turbine blades

US11499529B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11499529-B2
Application numberUS-201917261236-A
CountryUS
Kind codeB2
Filing dateJul 19, 2019
Priority dateJul 20, 2018
Publication dateNov 15, 2022
Grant dateNov 15, 2022

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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.

There is disclosed a method of balancing a set of first and second modular blade sections for a set of blades of a rotor of a wind turbine. The method comprises determining a mass moment of the first and second blade sections, the mass moment being determined about an axis equivalent to an axis of rotation of a hub of the turbine when the blade section is assembled onto the hub. A plurality of blade section groups 10 are defined, each comprising a first blade section of the set and at least one second blade section of the set, each blade section group having a blade section group mass moment about the axis. The first blade section and the at least one second blade section in each group are selected so as to satisfy a minimised total ballast condition, to minimise balancing ballast to be added to the set as a whole, or a minimised 15 ballasting difference condition, to minimise the difference in balancing ballast added to different blades, or both.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of balancing a set of modular blade sections for a set of blades of a rotor of a wind turbine, the method comprising the steps of: providing the set of modular blade sections, the set comprising a plurality of first blade sections and a plurality of second blade sections; determining a mass moment of each first blade section and of each second blade section, the mass moment being determined about an axis equivalent to an axis of rotation of a hub of the turbine when the blade section is assembled onto the hub; and defining a plurality of blade section groups, each comprising a first blade section of the set and at least one second blade section of the set, each blade section group having a blade section group mass moment about the axis, the first blade section and the at least one second blade section in each group being selected so as to: minimise a sum of differences between: the group mass moment of the blade section group having the highest group mass moment of the plurality of blade section groups; and the group mass moment of each of the remaining blade section groups; or minimise a difference in mass moment between: the group mass moment of the blade section group or groups having the highest group mass moment of the plurality of blade section groups; and the group mass moment of the blade section group or groups having the lowest group mass moment of the plurality of blade section groups. 2. The method according to claim 1 , wherein each modular blade section in the set of modular blade sections is provided with identifying means, and wherein the method further comprises identifying each first blade section and each second blade section of the set of modular blade sections as belonging to its respective blade section group using the identifying means. 3. The method according to claim 1 , further comprising the step of providing ballast to at least one of the plurality of blade section groups to provide a mass moment equal to the blade section group having the highest mass moment. 4. The method according to claim 3 , wherein no ballast is added to the blade section group having the highest group mass moment of the plurality of blade section groups. 5. The method according to claim 1 , wherein the step of defining a plurality of blade section groups includes providing a blade section group comprising: a first blade section having the highest mass moment of the first blade sections; and a second blade section having the lowest mass moment of the second blade sections. 6. The method according to claim 1 , wherein determining the mass moment of a first or second blade section comprises weighing the first or second blade section. 7. The method according to claim 3 , wherein the ballast is provided at or adjacent: an outer end of one or more inner blade sections; and/or an inner end of one or more outer blade sections. 8. The method according to claim 3 , wherein the ballast is added to a shear web portion of one or more of the first or second blade sections. 9. The method according to claim 3 , wherein providing the ballast to the at least one blade section groups comprises adding one or more of: a granular material; a solid material; a liquid; and a curable fluid. 10. The method according to claim 1 , further comprising the step of assembling the first blade section and the at least one second blade section within each blade section group to one another to form a set of blades for a rotor of a wind turbine. 11. The method according to claim 1 , further comprising the step of assembling the plurality of blade section groups onto a wind turbine hub, such that each blade section group forms a wind turbine blade, the wind turbine blades having an equivalent mass moment, about an axis of rotation of a hub of the turbine, to one another. 12. A set of blades for a rotor of a wind turbine, wherein each blade comprises a blade section group comprising a first blade section and at least one second blade section, each blade section group having a blade section group mass moment about an axis equivalent to an axis of rotation of a hub of the turbine when the blade section is assembled onto the hub; wherein, excluding any supplementary balancing mass added to the blades, the first blade section and the at least one second blade section in each group are selected so as to: minimise a sum of the differences between: the group mass moment of the blade section group having the highest group mass moment of the plurality of blade section groups; and the group mass moment of each of the remaining blade section groups; or minimise a difference in mass moment between: the group mass moment of the blade section group or groups having the highest group mass moment of the plurality of blade section groups; and the group mass moment of the blade section group or groups having the lowest group mass moment of the plurality of blade section groups. 13. The set of blades according to claim 12 , further comprising ballast provided to at least one of the plurality of blade section groups, to provide a mass moment equal to the blade section group having the highest mass moment. 14. The set of blades according to claim 13 , wherein the ballast comprises one or more of the following: a granular material, a block or plate of material, and a liquid. 15. The method according to claim 9 , wherein adding the granular material further comprises adding sand. 16. The method according to claim 9 , wherein adding the solid material further comprises adding metal. 17. The method according to claim 9 , wherein adding the curable fluid further comprises adding a curable polymer. 18. The set of blades according to claim 14 , wherein the granular material comprises sand. 19. The set of blades according to claim 14 , wherein the block or plate of material comprises a steel block or plate. 20. The set of blades according to claim 14 , wherein the liquid comprises a curable polymer.

Assignees

Inventors

Classifications

  • Assembly methods · CPC title

  • by correcting static or dynamic imbalance · CPC title

  • F03D13/35Primary

    Balancing static or dynamic imbalances · CPC title

  • Wind turbines with rotation axis in wind direction · CPC title

  • of the blades · CPC title

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What does patent US11499529B2 cover?
There is disclosed a method of balancing a set of first and second modular blade sections for a set of blades of a rotor of a wind turbine. The method comprises determining a mass moment of the first and second blade sections, the mass moment being determined about an axis equivalent to an axis of rotation of a hub of the turbine when the blade section is assembled onto the hub. A plurality of …
Who is the assignee on this patent?
Vestas Wind Sys As
What technology area does this patent fall under?
Primary CPC classification F03D13/35. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 15 2022 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).