Fault ride-through system
US-2019288624-A1 · Sep 19, 2019 · US
US10770997B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10770997-B2 |
| Application number | US-201916401570-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 2, 2019 |
| Priority date | May 30, 2018 |
| Publication date | Sep 8, 2020 |
| Grant date | Sep 8, 2020 |
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A power system includes a synchronous electrical generator having a rotor driven by a shaft; a permanent magnet signaling generator, coupled to the shaft; and an angle computation unit configured to calculate a rotor angle or load angle based on a voltage from the permanent magnet signaling generator and a voltage from the synchronous electrical generator.
Opening claim text (preview).
The invention claimed is: 1. A power system, comprising: a synchronous electrical generator having a rotor driven by a shaft; a permanent magnet signalling generator, coupled to the shaft; and an angle computation unit configured to calculate a rotor angle and/or load angle based on a voltage from the permanent magnet signalling generator and a voltage from the synchronous electrical generator. 2. A power system ( 10 ) according to claim 1 , wherein a number of magnetic poles in the permanent magnet signalling generator ( 21 ) is the same as a pole number of the rotor of the synchronous electrical generator ( 11 ). 3. A power system according to claim 1 , wherein a number of phases of the permanent magnet signalling generator is the same as a number of phases in a stator of the synchronous electrical generator. 4. A power system according to claim 1 , wherein magnetic poles of the permanent magnet signalling generator are aligned with magnetic poles of the synchronous electrical generator. 5. A power system according to claim 1 , wherein the angle computation unit is configured to calculate the rotor angle or load angle in one or both of steady state and transient conditions. 6. A power system according to claim 1 , wherein the angle computation unit is configured to: receive the voltage from the permanent magnet signal generator at a first resistor via a variable resistor, receive the voltage from the synchronous electrical generator at a second resistor, first ends of each of the first and second resistors being connected to each other and ground, adjust the value of the variable resistor until the voltages over the first resistor and over the second resistor are equal, and calculate an angle (δ) using the equation: δ = cos - 1 ( V a , snl 2 + V a , pcc / t 2 - V ag 2 2 · V a , nsl V a , pcc / t ) wherein V ag is the voltage between the un-earthed ends of the first and second resistors. 7. A power system according to claim 1 , wherein the angle computation unit comprises a digital signal processor. 8. A power system according to claim 7 , wherein the digital signal processor is configured to: receive a three phase voltage from the permanent magnet signal generator, and determine a voltage angle for the permanent magnet signal generator; receive a three phase voltage from the synchronous electrical generator, and determine a voltage angle for the synchronous electrical generator; and calculate an angle as the difference between the voltage angle for the permanent magnet signal generator and the voltage angle for the synchronous electrical generator. 9. A power system according to claim 1 , wherein the electrical power output from the synchronous electrical generator is less than 30 MW. 10. A power system according to claim 1 , wherein the voltage from the synchronous electrical generator is the voltage at the point of common coupling to a load attached to the synchronous electrical generator or the voltage at an output terminal of the synchronous electrical generator. 11. A method of determining a rotor angle or load angle in a power system comprising synchronous electrical generator, the method comprising calculating the rotor angle or load angle based upon a voltage from a permanent magnet signalling generator coupled to a rotor shaft of the synchronous electrical generator. 12. A method of determining a rotor angle or load angle according to claim 11 , wherein the power system is a power system. 13. A method of determining whether or not an out-of-step condition has occurred, the method comprising: determining a load angle and/or rotor angle of a generator system according to the method of claim 11 ; and determining whether or not an out-of-step condition has occurred depending upon the determined load angle and/or rotor angle. 14. A computer program that, when executed by a computing device, causes the computing device to determine a load angle and/or rotor angle in a power system according to the method of claim 11 and/or an out-of-step condition. 15. A computing device configured to determine a rotor angle in a power system and/or an out-of-step condition by executing the computing program of claim 14 .
Structural association of synchronous generators with auxiliary electric devices influencing the characteristic of the generator or controlling the generator, e.g. with impedances or switches · CPC title
Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices · CPC title
with automatic parallel connection when synchronisation is achieved · CPC title
Means for protecting the generator by using control (control effected upon generator excitation circuit to reduce harmful effects of overloads or transients H02P9/10) · CPC title
for limiting effects of transients · CPC title
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