Rotor blade of a wind turbine and method for designing same
US-2020248671-A1 · Aug 6, 2020 · US
US11828262B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11828262-B2 |
| Application number | US-202017626384-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 8, 2020 |
| Priority date | Jul 12, 2019 |
| Publication date | Nov 28, 2023 |
| Grant date | Nov 28, 2023 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A rotor blade of a wind turbine, to an associated wind turbine and to an associated method. A rotor blade for a wind turbine, which extends in the longitudinal direction with a profile course from a blade connector to a blade tip, wherein the profile course comprises a course of a lift coefficient, comprising a hub portion adjacent to the blade connector and a tip portion adjacent to the blade tip, a middle portion adjacent to the hub portion and to the tip portion, wherein the middle portion substantially comprises those profile sections which have a relative profile thickness, which is defined as the ratio of maximum profile thickness to profile depth, of between 20% and 30%, and wherein the middle portion comprises a local minimum of the course of the lift coefficient.
Opening claim text (preview).
The invention claimed is: 1. A rotor blade for a wind turbine, comprising: a rotor blade body comprising: a blade connector; a blade tip; and a profile including a plurality of profile sections extending in a longitudinal direction from the blade connector to the blade tip, each profile section including a respective lift coefficient, a relative profile thickness, and a thickness setback, wherein at each profile section, the relative profile thickness is defined as a ratio of a maximum cross-sectional thickness to a chord length, wherein at each profile section, the thickness setback is defined as a ratio of (i) a distance along the chord length from a leading edge of the profile to the maximum cross-sectional thickness to (ii) the chord length, wherein the plurality of profile sections is divided into groups of profile sections including a hub portion adjacent to the blade connector, a tip portion adjacent to the blade tip, and a middle portion between the hub portion and the tip portion, wherein the profile sections in the middle portion include a relative profile thickness between 20% and 30%, wherein the profile further includes a local minimum lift coefficient and a local maximum thickness setback each arranged in the middle portion, and wherein a minimum thickness setback of the profile is arranged between 0% and 40% of a rotor blade length measured from the blade connector toward the blade tip. 2. The rotor blade as claimed in claim 1 , wherein the thickness setback of each profile section is arranged along the profile so as to collectively form an S-shape including a local minimum thickness setback and the local maximum thickness setback. 3. The rotor blade as claimed in claim 2 , wherein the S-shape includes first, second, and third turning points, wherein: the first turning point is arranged between 10% and 25% of the rotor blade length measured from the blade connector toward the blade tip, and/or the second turning point is arranged between 40% and 50% of the rotor blade length measured from the blade connector toward the blade tip, and/or the third turning point is arranged between 65% and 90% of the rotor blade length measured from the blade connector toward the blade tip. 4. The rotor blade as claimed in claim 2 , wherein the local minimum thickness setback is greater than 35%. 5. The rotor blade as claimed in claim 4 , wherein the local minimum thickness setback is greater than 40%. 6. The rotor blade as claimed in claim 1 , wherein the middle portion extends between 30% and 80% of the rotor blade length measured from the blade connector toward the blade tip, and wherein the profile sections in the middle portion include a thickness setback between 35% and 40%. 7. The rotor blade as claimed in claim 1 , wherein the hub portion extends between 0% and 30% of the rotor blade length measured from the blade connector toward the blade tip, and wherein the profile sections in the hub portion include a thickness setback between 25% and 50%. 8. The rotor blade as claimed in claim 7 , wherein the profile sections in the hub portion are arranged such that the thickness setbacks decrease in a direction from the blade connector toward the blade tip. 9. The rotor blade as claimed in claim 1 , wherein the tip portion extends between 80% and 100% of the rotor blade length measured from the blade connector toward the blade tip, wherein the profile sections in the tip portion include a thickness setback between 25% and 35%, and wherein the profile further includes a local minimum thickness setback arranged in the tip portion. 10. The rotor blade as claimed in claim 1 , wherein: the hub portion extends between 0% and 30% of the rotor blade length measured from the blade connector toward the blade tip, and/or the middle portion extends between 30% and 80% of the rotor blade length measured from the blade connector toward the blade tip, and/or the tip portion extends between 80% and 100% of the rotor blade length measured from the blade connector toward the blade tip. 11. The rotor blade as claimed in claim 1 , wherein the relative profile thickness of each profile section is between 15% and 100%. 12. The rotor blade as claimed in claim 1 , wherein at least a portion of the plurality of profile sections includes a flatback profile. 13. The rotor blade as claimed in claim 12 , wherein the flatback profile is arranged in the hub portion. 14. The rotor blade as claimed in claim 1 , wherein the minimum thickness setback is less than 35%. 15. The rotor blade as claimed in claim 14 , wherein the minimum thickness setback is less than 30%. 16. A wind turbine comprising a tower, a rotor, and at least one rotor blade as claimed in claim 1 coupled to the rotor. 17. A windfarm comprising at least two wind turbines as claimed in the claim 16 .
of the section profile of the blades, i.e. aerofoil profile · CPC title
of the blades · CPC title
Cross-section characteristics · CPC title
of the blades · CPC title
Wind turbines with rotation axis in wind direction · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.