This application claims priority to European Patent Application No. 19172847.6, having a filing date of May 6, 2019, the entire contents of which are hereby incorporated by reference.
The following relates to a method and to an arrangement for calculating the position and speed of the rotor of an electric generator. Further, the following relates to a wind turbine comprising an electric generator and the arrangement for calculating the position and speed of the rotor of the electric generator.
A wind turbine typically comprises a wind rotor with blades connected thereto and an electric generator, in particular a high power permanent magnet synchronous machine having a generator rotor which is mechanically connected to the wind rotor. A wind turbine may further include a converter connected to the electric generator.
The knowledge of the rotor speed and position is a requirement for controlling a permanent magnet synchronous machine. Estimation methods are usually adopted to avoid extra sensors and to reduce hardware requirements, which are implemented in the converter control system and require the frequency converter to be in operation. In wind turbines, converter operation is typically started above a given rotor speed, the so-called “cut-in speed”. As a consequence, additional hardware is usually required for the synchronization of the generator with the converter, namely, a speed sensor and/or voltage sensors. In fact, none of these sensors is required during converter operation, but only to ensure a smooth generator start by avoiding a large torque disturbance as a consequence of an erroneous rotor position. Torque disturbances at start up may be audible, being a concern with regards to noise. Moreover, component fatigue may increase and turbine life-time decrease.
As a more cost-effective alternative to the above described solution, the present disclosure proposes to estimate speed and position of the rotor without involving signals outputted by speed/position and voltage sensors.
An aspect relates to a circuit for calculating position and/or speed of a rotor of an electric generator. The circuit comprises:
In the context of embodiments of the present invention, a “circuit” or “module” can be implemented as an hardware circuit and/or a programmable logic circuit configured and arranged for implementing the specified operations/activities. In possible embodiments, a programmable circuit may include one or more computer circuits programmed to execute a set (or sets) of instructions (and/or configuration data). The instructions (and/or configuration data) can be in the form of firmware or software stored in and accessible from a memory (circuit).
Another aspect relates to a method for calculating position and/or speed of a rotor of an electric generator. The method comprises:
The method may be implemented in hardware and/or software and may in particular be performed by a wind turbine controller or in general a generator controller. The generator may in particular be or comprise a permanent magnet synchronous machine, in which plural permanent magnets are attached to a rotor which rotates relative to a stator, the stator having at least one set of stator windings, for example one or more sets of three-phase stator windings. The electric generator may be comprised in a wind turbine.
Advantageously, embodiments of the present invention permit speed estimation by using an accelerometer signal as an alternative to speed and voltage sensors. An accelerometer may be used, which is installed on the wind turbine for providing also other function, which are independent from the estimation of speed and position of the rotor. For example, an accelerometer is normally required for closed-loop control of torque ripple in a direct drive wind turbine. Therefore embodiments of the present invention provide the possibility to a reduction of costs. Embodiments of the present invention permit to avoid the direct measurement of the cogging torque by means of load cells and strain gauges, which may be costly and unreliable.
According to embodiments of the present invention, the accelerometer is fixed with respect to a stator of the electric generator. In particular, the accelerometer may be fixed to a stationary ring of rotary bearing of the electric generator. The accelerometer may measure the acceleration in tangential or radial or other direction of the stationary ring of the main bearing of the generator. The vibration signal may comprise one or more higher harmonics of a fundamental electric frequency of the generator, the fundamental frequency being in particular related to a frequency of revolutions of a generator rotor rotating relative to a fixed stator.
Embodiments of the present invention are now described with reference to the accompanying drawings. Embodiments of the present invention are not restricted to the illustrated or described embodiments.
The aspects defined above and further aspects of embodiments of the present invention are apparent from the examples of embodiment to be described hereinafter and are explained with reference to the examples of embodiment. Embodiments of the present invention will be described in more detail hereinafter with reference to examples of embodiment but to which the invention is not limited.
Some of the embodiments will be described in detail, with reference to the following figures, wherein like designations denote like members, wherein:
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.
The electric generator 100 typically shows a cogging torque Tcog, which varies periodically within a mechanical period:
T
cog
=ΣT
k sin(mkθ)
where m is the least common multiple of the number slots (Ns) and the number of poles (Np) of the stator 105, k is an integer varying between 1 and infinite, Tk a plurality of constants depending on the geometry of the rotor 106 and the stator 105 and θ is the rotor mechanical position. The cogging torque Tcog results from the airgap reluctance variation with rotor position, in other words from the interaction between magnets and stator teeth (when the stator 105 is unexcited). The vibration signal 202 is used according to the embodiment of the present invention as an input signal, which is a good representation of the cogging torque Tcog. This was confirmed by experimental observation.
A comparison of experimental results 322 of the speed of the rotor 106 with the rotor speed signal 222 is shown in the diagram 300 of
The logical circuit 200 may be activated when the electric generator 100 is in open circuit, i.e. when the electric generator 100 is below the so-called “cut-in speed” and the converter is switched off. The logical circuit 200 may be activated at the time when the connection between the electric generator 100 and the converter is required, i.e. at the cut-in speed or immediately before the “cut-in speed” is reached.
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.
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.
Number | Date | Country | Kind |
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19172847.6 | May 2019 | EP | regional |