Wind turbine with pitch control arranged to reduce life shortening loads on components thereof
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F03D-007/04
출원번호
US-0570846
(2009-09-30)
등록번호
US-8096762
(2012-01-17)
우선권정보
DK-2007 00504 (2007-03-30)
발명자
/ 주소
Risager, Lars
Svendsen, Rasmus
Miranda, Erik Carl
출원인 / 주소
Vestas Wind Systems A/S
대리인 / 주소
Wood, Herron & Evans, L.L.P.
인용정보
피인용 횟수 :
7인용 특허 :
17
초록▼
A wind turbine is presented where the operation lifetime of the main bearing is extended by relieving the main bearing by reducing the mean bending moment on the bearing by means of individual pitch control of the blades of the rotor so as to create an aerodynamic mean tilt moment on the rotor by me
A wind turbine is presented where the operation lifetime of the main bearing is extended by relieving the main bearing by reducing the mean bending moment on the bearing by means of individual pitch control of the blades of the rotor so as to create an aerodynamic mean tilt moment on the rotor by means of aerodynamic forces on the blades, the tilt moment at least partly counteracting the bending moment caused by the overhang load forces on the main bearing from the gravitational pull on the rotor mass.
대표청구항▼
1. A wind turbine, comprising: a rotor having a hub and at least two blades,a main bearing providing a rotational support of the rotor on a non-rotating part of the wind turbine,a blade pitching mechanism for individual adjustment of an angle of each of the blades about their longitudinal axes, anda
1. A wind turbine, comprising: a rotor having a hub and at least two blades,a main bearing providing a rotational support of the rotor on a non-rotating part of the wind turbine,a blade pitching mechanism for individual adjustment of an angle of each of the blades about their longitudinal axes, anda control system for controlling operation of the blade pitching mechanism during ordinary operation of the wind turbine in order to reduce a bending moment on the main bearing caused by overhang load forces from a gravitational pull on the rotor mass. 2. The wind turbine according to claim 1, wherein the control system controls the blade pitching mechanism in response to a predetermined value of a counteracting aerodynamic mean tilt moment so that the aerodynamic mean tilt moment on the rotor counteracts the bending moment on the main bearing caused by overhang load forces from the gravitational pull on the rotor mass. 3. The wind turbine according to claim 2, wherein the mean tilt moment on the rotor counteracts at least 20% of the bending moment on the main bearing caused by the overhang load forces from the gravitational pull on the rotor mass. 4. The wind turbine according to claim 1, wherein ordinary operation of the wind turbine includes operation of the wind turbine at average wind speeds between 12 m/s and 18 m/s. 5. The wind turbine according to claim 1, further comprising measurement means arranged to detect load data of the rotor, the load data being a measure of an instantaneous mechanical load on the rotor, and to provide an output accordingly of said load data to the control system, wherein the control system is further arranged to operate the blade pitching mechanism to perform adjustment of the angle of each of the blades in response to the load data output from the measurement means. 6. The wind turbine according to claim 5, wherein the control system determines a common cyclic pitch function and operates the blade pitching mechanism according to the cyclic pitch function depending on an instantaneous azimuth angle of an individual blade. 7. The wind turbine according to claim 5, wherein said measurement means is arranged to provide a measure of blade root bending moments. 8. The wind turbine according to claim 5, wherein said measurement means is arranged to provide a measure of an angle of attack for the blades. 9. The wind turbine according to claim 5, wherein the control system comprises data collection and storage devices for repeatedly collecting and storing the load data of the rotor, and a data processor for processing the collected load data of the rotor of the wind turbine and determining a load distribution function for the rotor from the load data, wherein the control system is arranged to operate the blade pitching mechanism in response to the determined load distribution function. 10. A method of reducing a mean bending moment on a main bearing of a wind turbine, a rotor being rotationally supported by the main bearing, the method comprising: operating a blade pitching mechanism of the wind turbine to individually pitch the rotor blades of the wind turbine in response to a predetermined value of a counteracting aerodynamic mean tilt moment, so that the aerodynamic mean tilt moment on the rotor counteracts the bending moment on the main bearing caused by overhang load forces from gravitational pull on the rotor mass substantially corresponding with the predetermined value. 11. The method according to claim 10, wherein the predetermined mean tilt moment on the rotor corresponds to a counteracting of at least 20% of the bending moment on the main bearing caused by the overhang load forces from the gravitational pull on the rotor mass. 12. The method according to claim 10, wherein ordinary operation of the wind turbine includes operation of the wind turbine at average wind speeds between 12 m/s and 18 m/s. 13. The method according to claim 10, further comprising: repeatedly collecting and storing load data of the rotor,determining a load distribution function for the rotor from the stored data, andoperating a blade pitching mechanism of the wind turbine to individually pitch the rotor blades of the wind turbine in response to the determined load distribution function. 14. The method according to claim 13, wherein the load data of the rotor is obtained by means of measurement means arranged to provide a measure of blade root bending moments. 15. The method according to claim 13, wherein the load data of the rotor is obtained by means of measurement means arranged to provide a measure of an angle of attack for the blades. 16. The method according to claim 13, wherein the load distribution function for the rotor comprises a measure of a tilt moment function of the rotor. 17. A wind turbine, comprising: a rotor having a hub and at least two blades,a main bearing providing a rotational support of the rotor on a non-rotating part of the wind turbine,a blade pitching mechanism for individual adjustment of an angle of each of the blades about their longitudinal axes, anda control system for controlling operation of the blade pitching mechanism during ordinary operation of the wind turbine to perform adjustment of the angle of each of the blades in response to a predetermined value of a counteracting aerodynamic mean tilt moment so that the aerodynamic mean tilt moment on the rotor counteracts a bending moment on the main bearing caused by overhang load forces from a gravitational pull on the rotor mass.
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이 특허에 인용된 특허 (17)
Quynn Allen G. (Bellevue WA), Blade pitch control of a wind turbine.
Larsen,Torben Juul; Madsen,Helge Aagaard; Thomsen,Kenneth, Method of controlling aerodynamic load of a wind turbine based on local blade flow measurement.
Jeppesen, Ole Mølgaard; Bengtson, John; Hansen, Torben Møller, Method of controlling the pitch velocity of a wind turbine blade and control system therefore.
DeLeonardo,Guy Wayne; Finn,Scott Roger; Finnigan,Peter Michael; Kasperski,Donald Joseph, System and method for passive load attenuation in a wind turbine.
Avagliano,Aaron; Lyons,James Patrick Francis; Barbu,Corneliu; Suryanarayanan,Shashikanth, System and method for upwind speed based control of a wind turbine.
Shibata,Masaaki; Hayashi,Yoshiyuki; Furukawa,Toyoaki; Yatomi,Yuuji; Kato,Eiji; Teramoto,Yoshinari; Miyake,Hisao; Hayakawa,Koshi, Wind turbine provided with a controller for adjusting active annular plane area and the operating method thereof.
Shibata,Masaaki; Hayashi,Yoshiyuki; Furukawa,Toyoaki; Yatomi,Yuuji; Kato,Eiji; Teramoto,Yoshinari; Miyake,Hisao; Hayakawa,Koshi, Wind turbine provided with a controller for adjusting active annular plane area and the operating method thereof.
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