TORQUE RIPPLE REDUCTION FOR A GENERATOR
20190081583 ยท 2019-03-14
Inventors
Cpc classification
F05B2220/7068
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02P21/05
ELECTRICITY
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/72
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
H02P21/05
ELECTRICITY
F03D9/25
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
It is provided a method of controlling a generator to reduce a harmonic torque ripple, the method including: measuring a first value of an acceleration using a first accelerometer mounted at a first position of the generator; measuring a second value of an acceleration using a second accelerometer mounted at a second position of the generator; deriving a vibration signal based on a combination of the first value and the second value of the acceleration; deriving, based on the vibration signal, an amplitude and a phase of a reference harmonic current; injecting a current into the generator based on the reference harmonic current.
Claims
1. A method of controlling a generator to reduce a harmonic torque ripple, the method comprising: measuring a first value of an acceleration using a first accelerometer mounted at a first position of the generator; measuring a second value of an acceleration using a second accelerometer mounted at a second position of the generator; deriving a vibration signal based on a combination of the first value and the second value of the acceleration; deriving, based on the vibration signal, an amplitude and a phase of a reference harmonic current; and injecting a current into the generator) based on the reference harmonic current.
2. The method according to claim 1, wherein the vibration signal is based on a sum of the first value and the second value of the acceleration.
3. The method according to claim 1, wherein the first value of the acceleration and the second value of the acceleration relate to an acceleration in a circumferential direction of the generator.
4. The method according to claim 1, wherein the first position and the second position have a same radial position and a same circumferential position, but different axial positions, such that the first position and the second position are mirror symmetrically arranged.
5. The method according to claim 1, wherein the first accelerometer is mounted at a first stator plate and the second accelerometer is mounted at a second stator plate, the first stator plate and the second stator plate delimiting a stator towards an environment, further wherein the first stator plate and the second stator plate are annular flat plates.
6. The method according to claim 1, wherein the generator comprises a rotor having permanent magnets mounted thereon arranged in at least two rings in different axial positions being skewed relative to each other in a circumferential direction.
7. The method according to claim 1, further comprising: determining a value of an operating point of the generator; deriving, based on the vibration signal and the value of the operating point, the amplitude and the phase of the reference harmonic current;
8. The method according to claim 7, wherein the value of the operating point is determined based on a measured fundamental torque and a measured rotational speed of the generator or other measurements.
9. The method according to claim 1, wherein deriving the amplitude and the phase of the reference harmonic current comprises: filtering the vibration signal thereby reducing components of the vibration signal other than a particular harmonic to obtain a filtered vibration signal; time averaging an RMS value of the filtered vibration signal; looking up an initial amplitude and an initial phase associated with the value of the operating point from a storage; performing an optimization of the amplitude and phase based on the initial amplitude and the initial phase so that the vibration signal is reduced; and storing, associated with the value of the operating point, the optimized amplitude and optimized phase in a storage.
10. The method according to claim 1, wherein injecting the current into the generator comprises: determining a reference harmonic voltage based on the reference harmonic current and an actual current in at least one stator winding, each of the reference harmonic current and the actual current being represented by components in a dq-coordinate system; forming a sum of the reference harmonic voltage and a reference fundamental voltage; and supplying the sum as reference voltage to a control input of a converter having power input terminals connected to power output terminals of the generator.
11. The method according to claim 1, further comprising: determining the reference fundamental voltage based on the actual current in at least one stator winding of the generator and a reference fundamental current.
12. An arrangement for controlling a generator to reduce a harmonic torque ripple, the arrangement comprising: a first accelerometer mountable at a first position of the generator and adapted to measure a first value of an acceleration; a second accelerometer mountable at a second position of the generator and adapted to measure a second value of an acceleration; a processor adapted: to derive a vibration signal based on a combination of the first value and the second value of the acceleration, and to derive, based on the vibration signal, an amplitude and a phase of a reference harmonic current; and a driver adapted to inject a current into the generator based on the reference harmonic current.
13. A wind turbine, comprising: a shaft with rotor blades connected thereto; a generator mechanically coupled with the shaft; and an arrangement according to claim 1, the driver being configured as a converter that is controlled based on the reference harmonic current.
Description
BRIEF DESCRIPTION
[0046] Some of the embodiments will be described in detail, with references to the following Figures, wherein like designations denote like members, wherein:
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DETAILED DESCRIPTION
[0059] The illustration in the drawings is in schematic form. It is noted that in different figures, similar or identical elements are provided with the same reference signs or with reference signs, which are different from the corresponding reference signs only within the first digit.
[0060]
[0061] The converter 119 is controlled via a converter command 135 (Vdref, Vqref) which is derived and supplied from a control arrangement 150 according to an embodiment of the present invention, which receives at least one input signal 137, such as including at least a vibration signal and optionally including stator winding currents and/or one or more reference values and/or one or more quantities indicative of the operation of the generator 111 or any component of the wind turbine 100.
[0062] The generator in
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[0064] The arrangement 250 illustrated in
[0065] Furthermore, the arrangement 250 comprises a processor 245 which is adapted to determine a value 247 of an operating point of the generator, for example represented by the two values (T.sub.n, .sub.m), one of a plurality of predetermined fundamental torques and one of a plurality of predetermined rotational speeds of the generator.
[0066] The processor 245 is further adapted to derive, based on the vibration signal 243 and optionally also based on the value 247 of the operating point, an amplitude 251 (e.g. A.sub.q6f for a 6.sup.th harmonic of the basic or fundamental frequency 0 and a phase 253 (for example .sub.q6f, for the 6.sup.th harmonic of the fundamental frequency) of a reference harmonic current (for example I.sub.q6f for a reference current of a 6.sup.th harmonic), wherein the harmonic current is also indicated by reference sign 255.
[0067] Further, the arrangement 250 comprises a driver 257 (e.g. configured as converter 119 in
[0068] For performing these functions, the arrangement 250 comprises an auto-tuning controller 259 which receives the vibration signal 243 as well as the value 247 of the load point and further receives an enable signal 249 which is derived by a load point detection module 261 which derives the value of the load point 247 based on the torque T.sub.g of the generator and the electrical frequency .sub.e of the electric generator.
[0069] The reference harmonic current is labelled in
[0070] The arrangement 250 further comprises a harmonic current regulator 263 which receives (e.g. a representation of) the reference harmonic current (Iqref) as well as the d-component Idref of the reference harmonic current which is usually zero. Furthermore, the harmonic current regulator 263 receives the harmonic currents Id, Iq (derived e.g. from Ia, Ib, Ic by Transformation into the dq-system) of at least one set of stator windings of the generator, such as generator 111. The d-component and the q-component of the stator current are for example derived based on the three phase currents Ia, Ib, Ic by performing a park transformation.
[0071] The harmonic current regulator 263 comprises circuitry to derive from the input values a reference harmonic voltage Vdac, Vqac, i.e. components in the d/q-coordinate system which are supplied to addition elements 265. Using the addition elements 265, a sum of a reference fundamental voltage Vddc, Vqdc with the reference harmonic voltage Vdac, Vqac is calculated and output as a reference voltage Vdref, Vqref which is supplied to the driver 257, which may for example be configured as a converter.
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[0073] In
[0074] The arrangement 250 comprises the harmonic current reference calculation module or processor 242 which harbours the auto-tuning controller 259 and the limitation element 252.
[0075] The arrangement 250 further comprises a fundamental current regulator 267 which receives the stator winding currents Id, Iq as well as fundamental current references Iddcref, Iqdcref based on which the fundamental voltage references Vddc, Vqdc are calculated.
[0076] The vibration signal 243 illustrated in
[0077] Thereby,
[0078] At axial end faces, the generator 275 is covered with a first stator plate 281 and a second stator plate 283, respectively, which represent end plates of a generator housing. The first accelerometer 271 is fixed and mounted at the first stator plate 281 at a radial position r1 and a circumferential direction 1, while the second accelerometer 273 is mounted at the second stator plate 283 at a radial position r2 and at a circumferential position 2, wherein r1=r2 and 1=2. However, the two accelerometers 271, 273 are mounted at two different axial positions a1 and a2 which are measured along the axial direction x or 277.
[0079] According to this embodiment of the present invention, the acoustic noise signal for some specific harmonics (e.g. 6f, 12f) is represented by using vibration sensors (for example accelerometers) on the generator stator plates 281 and 283. At least two accelerometers 271, 273 are needed and mounted on two stator plates, respectively. The accelerometers need to be mounted on each stator plate 281, 283 in a mirror-symmetric manner, wherein a mirror plane 285 is perpendicular to the axial direction x or 277 and is arranged in the center (e.g. at (a2-a1)/2) between the stator plates 281 and 283.
[0080] It is in particular useful to employ at least two accelerometers in the case, that a direct drive permanent magnet generator employs a rotor-skewing design, as is exemplary illustrated in
[0081] According to the design illustrated in
[0082] Embodiments of the present invention may provide an accurate and reliable feedback solution for the wind generator torque ripple and noise control. No turbine individually tuning for the torque ripple controller may be required.
[0083] The accelerometer may give a faster and more stable signal response compared to a microphone sound detection signal. The accelerometer signal may be friendlier to the turbine controller.
[0084] Two accelerometers in a symmetrical position may describe an overall torque direction vibration which may cause the noise. Varying torque ripple due to the rotor-skewing design may properly be solved.
[0085] IEC position acoustic noise may be monitored in a real-time by using embodiments of the present invention.
[0086] The
[0087] The trace 19 in
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[0089] Further, also
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[0093] As can be taken from
[0094] Although the present invention has been disclosed in the form of preferred embodiments and variations thereon, it will be understood that numerous additional modifications and variations could be made thereto without departing from the scope of the invention.
[0095] For the sake of clarity, it is to be understood that the use of a or an throughout this application does not exclude a plurality, and comprising does not exclude other steps or elements.