Method of determining a rotor displacement angle

US9594091B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9594091-B2
Application numberUS-201414197743-A
CountryUS
Kind codeB2
Filing dateMar 5, 2014
Priority dateMar 8, 2013
Publication dateMar 14, 2017
Grant dateMar 14, 2017

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A method of determining a rotor displacement angle of a synchronous generator having a rotor and electrically connected to a power supply network uses at least one rotary speed measuring device. During a revolution of the rotor, in particular during each revolution of the rotor, the measuring device communicates at least one rotary speed signal to an evaluation unit. A frequency measuring device communicates a frequency signal to the evaluation unit for each period duration of a voltage signal of the power supply network. A time duration between communication of the rotary speed signal and communication of the frequency signal is determined by the evaluation unit, and the rotor displacement angle is inferred in dependence on the determined time duration.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of determining a rotor displacement angle of a synchronous generator having a rotor and electrically connected to a power supply network, the method comprising: during a revolution of the rotor, communicating at least one rotary speed signal to an evaluation unit using at least one rotary speed measuring device; communicating a frequency signal to the evaluation unit for each period duration of a voltage signal of the power supply network using a frequency measuring device; determining a time duration between the communication of the rotary speed signal and the communication of the frequency signal using the evaluation unit; inferring the rotor displacement angle based on the determined time duration; determining a no-load time duration; storing, for calibration, the determined time duration as the no-load time duration in the evaluation unit, after synchronisation of the synchronous generator with the power supply network has been effected and substantially without load application to the synchronous generator; determining the rotor displacement angle, using a differential time formed from the determined time duration less the no-load time duration; and inferring the rotor displacement angle based on the differential time. 2. A method as set forth in claim 1 , further comprising: mechanically rigidly connecting the rotor to an engine shaft of an internal combustion engine; and communicating, using the at least one rotary speed measuring device, the at least one rotary speed signal to the evaluation unit for each revolution of the engine shaft or a camshaft of the internal combustion engine. 3. A method as set forth in claim 2 , wherein the at least one rotary speed measuring device includes a sensor, and the method further comprises arranging the sensor along a periphery of the rotor or along a periphery of the engine shaft. 4. A method as set forth in claim 3 , wherein the at least one rotary speed measuring device includes a signalling device co-operating with the sensor, and the method further comprises arranging the signalling device along a periphery of a stator of the synchronous generator or at a housing of the internal combustion engine. 5. A method as set forth in claim 2 , wherein the internal combustion engine comprises a gas engine. 6. A method as set forth in claim 1 , further comprising: proportionally converting the differential time into degrees of the rotor displacement angle, wherein a value of the differential time of substantially zero seconds corresponds to a rotor displacement angle of 0 degrees and a value of the differential time of substantially a quarter of the period duration of the voltage signal of the power supply network corresponds to a rotor displacement angle of 90 degrees. 7. A method as set forth in claim 1 , further comprising: outputting, using the evaluation unit, a warning signal to signal a threatening pole slippage when the rotor displacement angle is determined to be of more than 5 degrees. 8. A method as set forth in claim 7 , wherein the rotor displacement angle of more than 5 degrees comprises a rotor displacement angle of more than 7 degrees. 9. A method as set forth in claim 1 , further comprising: determining an actual period duration of the voltage signal, so as to take account of a network frequency fluctuation with respect to the voltage signal of the power supply network upon or during the operation of determining the time duration between the communication of the rotary speed signal and the communication of the frequency signal; and determining at least one correction factor formed from a predeterminable theoretical period duration fractionised by the actual period duration, wherein the determined time duration is multiplied by the at least one correction factor. 10. A method as set forth in claim 9 , further comprising: determining the actual period duration of the voltage signal by measurement of a time difference between two successive frequency signals. 11. A method as set forth in claim 9 , further comprising: forming a correction factor upon or during the operation of determining the no-load time duration; multiplying the no-load time duration by the correction factor; and storing, in the evaluation unit, the multiplied no-load time duration as a standardised no-load time duration. 12. A method as set forth in claim 9 , further comprising: forming a correction factor upon or during the operation of determining the differential time; forming a standardised time duration by multiplication of the determined time duration by the correction factor; determining the rotor displacement angle by forming a standardised differential time from a standardised time duration less a standardised no-load time duration; and inferring the rotor displacement angle based on the standardised differential time. 13. A method as set forth in claim 1 , wherein the revolution of the rotor comprises each revolution of the rotor.

Assignees

Inventors

Classifications

  • G01P3/48Primary

    by measuring frequency of generated current or voltage {(in general G01R23/00)} · CPC title

  • G01D5/14Primary

    influencing the magnitude of a current or voltage · CPC title

  • and for generating speed information · CPC title

  • for measuring, monitoring, testing, protecting or switching (rectifiers H02K11/04; power electronics H02K11/33) · CPC title

  • using hard-stored calibration data · CPC title

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What does patent US9594091B2 cover?
A method of determining a rotor displacement angle of a synchronous generator having a rotor and electrically connected to a power supply network uses at least one rotary speed measuring device. During a revolution of the rotor, in particular during each revolution of the rotor, the measuring device communicates at least one rotary speed signal to an evaluation unit. A frequency measuring devic…
Who is the assignee on this patent?
Ge Jenbacher Gmbh & Co Og
What technology area does this patent fall under?
Primary CPC classification G01P3/48. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Mar 14 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).