Control circuit and method for qualifying a fault for a synchronous machine

Patent metadata

Field	Value
Publication number	US-10429216-B2
Application number	US-201615737392-A
Country	US
Kind code	B2
Filing date	Jun 13, 2016
Priority date	Jun 18, 2015
Publication date	Oct 1, 2019
Grant date	Oct 1, 2019

Abstract

The invention provides a control circuit and a method for qualifying a fault for a synchronous machine. The control circuit ( 10; 110; 210 ) is designed with: a rotor position angle range determination device ( 12; 112; 212 ) which is designed to determine at least one rotor position angle range covered by a rotor of the synchronous machine; a diagnostic signal determination device ( 14; 114; 214 ) which is designed to determine at least one diagnostic signal value of a diagnostic signal which indicates a fault; a comparison device ( 16; 116; 216 ) which is designed to determine whether a predetermined diagnostic threshold ( 56 ) is exceeded by the at least one determined diagnostic signal value or a diagnostic signal value derived from the at least one diagnostic signal value; and a qualification device ( 18; 118; 218 ) which is designed to qualify the fault, which is indicated by the diagnostic signal, on the basis of the at least one covered rotor position angle range and the exceeding of the predetermined diagnostic threshold ( 56 ) by the diagnostic signal value or the derived diagnostic signal value.

First claim

The invention claimed is:

1. A control circuit for qualifying a fault for a synchronous machine, comprising:
a rotor position angle range determination device which is designed to determine at least one rotor position angle range covered by a rotor of the synchronous machine;
a diagnostic signal determination device which is designed to determine at least one diagnostic signal value of a diagnostic signal which indicates a fault, wherein the diagnostic signal determination device is designed to continually determine the diagnostic signal value while the rotor covers the at least one rotor position angle range;
a comparison device which is designed to determine whether a predetermined diagnostic threshold is exceeded by the at least one determined diagnostic signal value or a derived diagnostic signal value derived from the at least one diagnostic signal value;
a qualification device which is designed to qualify the fault, which is indicated by the diagnostic signal, on the basis of the at least one covered rotor position angle range and the exceeding of the predetermined diagnostic threshold by the diagnostic signal value or the derived diagnostic signal value; and
an integration device configured to calculate an integral over a covered rotor position angle within the at least one rotor position angle range with one as the integrand as long as the continually determined diagnostic signal value exceeds the predetermined diagnostic threshold.

2. The control circuit according to claim 1 ,
wherein the qualification device is designed to qualify the fault in the event that the integral exceeds a predetermined value.

3. The control circuit according to claim 1 ,
wherein the integration device is configured to set the integral to zero as soon as the diagnostic signal value no longer exceeds the predetermined diagnostic threshold.

4. The control circuit according to claim 1 ,
wherein the integration device is configured to set the integral to zero as soon as the diagnostic signal value has not exceeded the predetermined diagnostic threshold over a predetermined rotor position angle difference.

5. The control circuit according to claim 1 ,
wherein the diagnostic signal determination device is designed to determine at least one diagnostic signal value of the diagnostic signal for each covered rotor position angle range; the covered rotor position angle ranges being the same size;
wherein the control circuit comprises a computing device, which is designed, on the basis of the at least one diagnostic signal value determined for the respective covered rotor position angle range, to generate a derived diagnostic signal value for the respective rotor position angle range;
wherein the qualification device is designed to qualify the fault in the event that the derived diagnostic signal value exceeds the predetermined diagnostic threshold for a predetermined number of rotor position angle ranges in succession.

6. A method for qualifying a fault for a synchronous machine comprising the following steps:
determining at least one rotor position angle range covered by a rotor of the synchronous machine;
determining at least one diagnostic signal value of a diagnostic signal which indicates a fault, while the rotor passes through the rotor position angle distance, wherein the diagnostic signal value is continually determined while the rotor covers the at least one rotor position angle range;
determining whether a predetermined diagnostic threshold is exceeded by the at least one determined diagnostic signal value or a diagnostic signal value derived from the at least one diagnostic signal value, wherein an integral is calculated over a covered rotor position angle within the at least one rotor position angle range with one as the integrand as long as the continually determined diagnostic signal value exceeds the predetermined diagnostic threshold; and
qualification of the fault, which is indicated by the diagnostic signal, on the basis of the at least one covered rotor position angle range and the exceeding of the predetermined diagnostic threshold by the diagnostic signal value or the derived diagnostic signal value.

7. The method according to claim 6 ,
wherein the fault is qualified in the event that the integral exceeds a predetermined value.

8. The method according to claim 6 ,
wherein the integral is set to zero as soon as the diagnostic signal value no longer exceeds the predetermined diagnostic threshold.

9. The method according to claim 6 ,
wherein the integral is set to zero, as soon as the diagnostic signal value has not exceeded the predetermined diagnostic threshold over a predetermined rotor position angle distance.

10. The method according to claim 6 ,
wherein at least one diagnostic signal value of the diagnostic signal is determined for each covered rotor position angle range; the covered rotor position angle ranges being the same size;
wherein on the basis of the at least one diagnostic signal value determined for the respective covered rotor position angle range, a derived diagnostic signal value is generated for the respective rotor position angle range;
wherein the fault is qualified in the event that the derived diagnostic signal value exceeds the predetermined diagnostic threshold for a predetermined number of rotor position angle ranges in succession.

Assignees

• Bosch Gmbh Robert

Inventors

• Lechner Benjamin
• Raichle Daniel
• Zirkel Daniel
• Ungermann Michael

Classifications

• G01D3/08 Primary

  with provision for safeguarding the apparatus, e.g. against abnormal operation, against breakdown · CPC title

• G01D18/00 Primary

  Testing or calibrating apparatus or arrangements provided for in groups G01D1/00 - G01D15/00 · CPC title

• G01D18/008 Primary

  with calibration coefficients stored in memory · CPC title

• H02P2207/05

  Synchronous machines, e.g. with permanent magnets or DC excitation · CPC title

• G01D5/14

  influencing the magnitude of a current or voltage · CPC title