CN109921381B - Chopper protection action criterion method for double-fed motor - Google Patents

Chopper protection action criterion method for double-fed motor Download PDF

Info

Publication number
CN109921381B
CN109921381B CN201910248078.8A CN201910248078A CN109921381B CN 109921381 B CN109921381 B CN 109921381B CN 201910248078 A CN201910248078 A CN 201910248078A CN 109921381 B CN109921381 B CN 109921381B
Authority
CN
China
Prior art keywords
rotor
fault
stator
double
terminal voltage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201910248078.8A
Other languages
Chinese (zh)
Other versions
CN109921381A (en
Inventor
潘文霞
刘明洋
赵坤
张艺博
郭家圣
杨刚
李建成
陈昕
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hohai University HHU
Original Assignee
Hohai University HHU
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hohai University HHU filed Critical Hohai University HHU
Priority to CN201910248078.8A priority Critical patent/CN109921381B/en
Publication of CN109921381A publication Critical patent/CN109921381A/en
Application granted granted Critical
Publication of CN109921381B publication Critical patent/CN109921381B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Control Of Eletrric Generators (AREA)

Abstract

The invention discloses a Chopper protection action criterion method for a double-fed motor, which is characterized in that when the double-fed motor has a short-circuit fault, the terminal voltage after the fault is taken as a Chopper protection action criterion.

Description

Chopper protection action criterion method for double-fed motor
Technical Field
The invention relates to the field of wind power plant safety, in particular to a judgment method for a protection action of a doubly-fed motor Chopper.
Background art:
at present, Chopper protection is added to most double-fed wind turbine generators, the low-voltage ride through capability of a double-fed motor is improved, and the safe and stable operation of a wind power plant is guaranteed. The protection action criterion refers to the basis for judging whether Chopper protection acts after disturbance occurs. After a fault occurs, Chopper protection is usually put into use when the voltage of a direct-current bus is set to be larger than a certain value in order to avoid damage to a converter, but researchers are difficult to judge whether Chopper protection acts from external data, so that parameters which are easy to obtain are needed to serve as criteria for Chopper protection action of a double-fed motor at present.
Disclosure of Invention
The invention aims to provide a Chopper protection action criterion method for a double-fed motor, so as to solve the defects in the prior art.
A Chopper protection action criterion method for a double-fed motor specifically comprises the following steps:
step 1, analyzing a double-fed wind driven generator mathematical model and transient characteristics thereof after a fault;
step 2, deducing a rotor voltage expression of the doubly-fed motor when Chopper protection is not put into operation according to the mathematical model of the doubly-fed wind generator and the transient characteristic of the doubly-fed wind generator;
step 3, making the rotor voltage equal to the direct current bus voltage limiting threshold value, and obtaining a set of terminal voltage and time { (K)di,ti) Get K in the setdThe minimum value of (2) is the limit value of the calculated terminal voltage drop coefficient;
step 4, obtaining a limit value of Chopper protection action fault post-terminal voltage according to the coefficient, wherein the limit value is a Chopper protection action criterion of the doubly-fed wind driven generator disclosed by the invention,
the expression for the rotor voltage is:
Figure BDA0002011593720000021
where t is time, t0For the occurrence of short-circuit fault, RrAs rotor resistance, ωp=ωs–ωrIs the slip angular velocity, omegarIs the angular speed, omega, of the rotorsFor synchronizing the rotational speeds, s ═ ωpsIn order to obtain a slip ratio,
Figure BDA0002011593720000022
is rotor transient equivalent inductance, LsIs equivalent inductance of stator winding, LrIs equivalent inductance of rotor winding, LmIs an excitation inductor;
Figure BDA0002011593720000023
is a rotor current space vector under a dq synchronous rotation coordinate system,
Figure BDA0002011593720000024
is a rotor current reference value, Ps,refAnd Qs,refRespectively an active power reference value and a reactive power reference value, KdFor the terminal voltage drop coefficient, psi, of the dual-feed machinesmAs the amplitude of the stator flux linkage,
Figure BDA0002011593720000025
the attenuation time constant of the direct-current component of the induced electromotive force e of the rotor after the fault;
Figure BDA0002011593720000026
the direct current component of the electromotive force e is induced by the rotor after the fault; u. ofs0For the pre-fault terminal voltage magnitude, μ ═ Rr+kp+jωpL'r)/L'rAnd λ ═ ki/L'rAs a parameter variable, kpAnd kiRespectively is a proportional coefficient and an integral time constant of the rotor current inner loop PI controller;
Figure BDA0002011593720000027
Figure BDA0002011593720000031
is a characteristic root of a certain ordinary differential equation;
Figure BDA0002011593720000032
is the initial value of the current of the rotor,
Figure BDA0002011593720000033
and
Figure BDA0002011593720000034
respectively represent the inductive coupling coefficients of the stator and the rotor,
Figure BDA0002011593720000035
is an initial value of the magnetic linkage of the stator,
Figure BDA0002011593720000036
the initial value of the rotor flux linkage is obtained.
Making the rotor voltage equal to a defined threshold value of the DC bus voltage, i.e.
Figure BDA0002011593720000037
Get { (K)di,ti) K in the setdiMinimum value of (K)dminI.e. the calculated terminal voltage drop coefficient Kd
Therefore, the Chopper protection action criterion of the doubly-fed wind generator disclosed by the invention is as follows:
us1=(1-Kd)us0
us1the voltage at the end of the fault is the Chopper protection action criterion of the doubly-fed wind generator, and if the actual voltage after the fault is less than or equal to us1The Chopper protection is put in, otherwise, the Chopper protection is not put in.
The invention has the advantages that: compared with the Chopper protection action criterion method of the existing double-fed wind generating set, on one hand, the criterion belongs to an external easy-to-observe parameter and is easy to obtain; on the other hand, the criterion is simple and clear, so that researchers can very easily judge whether Chopper protection acts or not, and the method has important significance for deeply developing fault current analysis of the wind power plant.
Drawings
Fig. 1 is an equivalent circuit diagram of the present invention.
Fig. 2 is a transient equivalent circuit diagram of the doubly-fed motor of the present invention.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.
As shown in fig. 1 and fig. 2, a method for determining Chopper protection action of a doubly-fed motor includes the following steps:
step 1, suppose when t0When a three-phase short circuit fault occurs on the stator side, analyzing the transient characteristic after the fault according to the electromagnetic transient equation of the doubly-fed wind generator under the space rotating coordinate system;
the classical voltage flux linkage equation is:
Figure BDA0002011593720000041
the voltage expression of the rotor of the doubly-fed motor when Chopper protection is not put into operation can be deduced from the equation set;
step 2, according to an electromagnetic transient equation of the doubly-fed wind generator under a space rotating coordinate system, deducing a voltage expression of a rotor of the doubly-fed motor when Chopper protection is not put into operation:
Figure BDA0002011593720000042
where t is time, t0For the occurrence of short-circuit fault, RrAs rotor resistance, ωp=ωs–ωrIs the slip angular velocity, omegarIs the angular speed, omega, of the rotorsFor synchronizing the rotational speeds, s ═ ωpsIn order to obtain a slip ratio,
Figure BDA0002011593720000051
is rotor transient equivalent inductance, LsIs equivalent inductance of stator winding, LrIs equivalent inductance of rotor winding, LmIs an excitation inductor;
Figure BDA0002011593720000052
the rotor current space vector under dq synchronous rotation coordinate system is shown, dq represents the coordinate system, d represents a straight axis, q represents a quadrature axis (transient analysis of electric power system, the third edition of Li Photoc, p33-p45),
Figure BDA0002011593720000053
is a rotor current reference value, Ps,refAnd Qs,refRespectively an active power reference value and a reactive power reference value, KdFor the terminal voltage drop coefficient, psi, of the dual-feed machinesmAs the amplitude of the stator flux linkage,
Figure BDA0002011593720000054
the attenuation time constant of the direct-current component of the induced electromotive force e of the rotor after the fault;
Figure BDA0002011593720000055
the direct current component of the electromotive force e is induced by the rotor after the fault; u. ofs0For the pre-fault terminal voltage magnitude, μ ═ Rr+kp+jωpL'r)/L'rAnd λ ═ ki/L'rAs a parameter variable, kpAnd kiRespectively is a proportional coefficient and an integral time constant of the rotor current inner loop PI controller;
Figure BDA0002011593720000056
is a characteristic root of a certain ordinary differential equation; ordinary differential equation of
Figure BDA0002011593720000057
Is the initial value of the current of the rotor,
Figure BDA0002011593720000058
and
Figure BDA0002011593720000059
respectively represent the inductive coupling coefficients of the stator and the rotor,
Figure BDA00020115937200000510
is an initial value of the magnetic linkage of the stator,
Figure BDA00020115937200000511
is an initial value of rotor flux linkage, RsAs the impedance of the stator,
Figure BDA00020115937200000512
is stator equivalent transient inductance, Is0Is the initial value of the stator current before the fault.
Step 3, making the rotor voltage equal to the direct current bus voltage limiting threshold value, namely
Figure BDA0002011593720000061
Get { (K)di,ti) K in the setdiMinimum value of (K)dminI.e. the calculated terminal voltage drop coefficient Kd
Step 4, obtaining a limit value of Chopper protection action fault post-terminal voltage according to the coefficient, wherein the limit value is a Chopper protection action criterion of the doubly-fed wind driven generator disclosed by the invention, namely
us1=(1-Kd)us0
us1The voltage at the end of the fault is the Chopper protection action criterion of the doubly-fed wind generator, and if the actual voltage after the fault is less than or equal to us1The Chopper protection is put in, otherwise, the Chopper protection is not put in.
During research, the Chopper protection action condition is obtained through the method, and then subsequent short-circuit current calculation or related research is carried out.
Based on the above, when judging whether Chopper protection acts, the terminal voltage after the fault is used as Chopper protection action criterion, compared with the Chopper protection action criterion method of the existing double-fed wind generating set, on one hand, the new criterion belongs to an external easy-to-observe parameter and is easy to obtain; on the other hand, the criterion disclosed by the invention is simple and clear, so that a researcher can very easily judge whether Chopper protection acts or not, and the method has important significance for deeply developing fault current analysis of the wind power plant.
It will be appreciated by those skilled in the art that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The embodiments disclosed above are therefore to be considered in all respects as illustrative and not restrictive. All changes which come within the scope of or equivalence to the invention are intended to be embraced therein.

Claims (2)

1. A Chopper protection action criterion method for a double-fed motor is characterized by comprising the following steps:
analyzing a double-fed motor mathematical model and transient characteristics thereof after a fault;
obtaining a double-fed motor rotor voltage expression when Chopper protection is not put into operation according to the mathematical model and the transient characteristic;
calculating to obtain a machine terminal voltage drop coefficient through a rotor voltage expression;
obtaining a fault post-machine terminal voltage value of Chopper protection action according to the machine terminal voltage drop coefficient, namely a criterion of the Chopper protection action of the double-fed motor;
the Chopper protection action criterion method for the double-fed motor comprises the following formula:
us1=(1-Kd)us0 (3)
us1for fault backend voltage, KdIs the terminal voltage drop coefficient u of the dual-feeder machines0For the voltage amplitude at the end of the fault, if the actual voltage after the fault is less than or equal to us1If yes, the Chopper protection is put into the device, otherwise, the Chopper protection is not put into the device;
the rotor voltage expression is:
Figure FDA0002717427270000011
where t is time, t0For the occurrence of a short-circuit fault, j denotes the imaginary part in the complex domain, RrAs rotor resistance, ωp=ωs–ωrIs the slip angular velocity, omegarIs the angular speed, omega, of the rotorsFor synchronizing the rotational speeds, s ═ ωpsIs slip ratio, L'rFor rotor transient equivalent inductance, irIs a rotor current space vector under dq synchronous rotation coordinate system, dq represents the coordinate system, d represents a direct axis, q represents a quadrature axis, KdIs the terminal voltage drop coefficient of the dual-feeder machine, e2For the direct-current component of the rotor-induced electromotive force e after a fault, us0For the voltage amplitude of the machine terminal before the fault, ksRepresenting the stator inductive coupling coefficient;
l 'in the rotor voltage expression'rThe equivalent formula of (a) is:
Figure FDA0002717427270000021
wherein L issIs equivalent inductance of stator winding, LrIs equivalent inductance of rotor winding, LmIs an excitation inductor;
i in the rotor voltage expressionrThe calculation formula of (2) is as follows:
Figure FDA0002717427270000022
wherein,
Figure FDA0002717427270000023
is a rotor current reference value, Ps,refAnd Qs,refRespectively an active power reference value and a reactive power reference value, KdFor the terminal voltage drop coefficient, psi, of the dual-feed machinesmAs the amplitude of the stator flux linkage,
Figure FDA0002717427270000024
is the decay time constant of the dc component of the rotor induced electromotive force e after the fault,
Figure FDA0002717427270000025
for the direct-current component of the rotor-induced electromotive force e after a fault, us0For the pre-fault terminal voltage magnitude, μ ═ Rr+kp+jωpL'r)/L'rAnd λ ═ ki/L'rAs a parameter variable, kpAnd kiRespectively are a proportionality coefficient and an integral time constant of the rotor current inner loop PI controller,
Figure FDA0002717427270000026
which is the characteristic root of some ordinary differential equation,
Figure FDA0002717427270000027
is the initial value of the current of the rotor,
Figure FDA0002717427270000028
and
Figure FDA0002717427270000029
respectively represent the inductive coupling coefficients of the stator and the rotor,
Figure FDA00027174272700000210
is an initial value of the magnetic linkage of the stator,
Figure FDA00027174272700000211
is an initial value of rotor flux linkage, RsAs the impedance of the stator,
Figure FDA00027174272700000212
is stator equivalent transient inductance, Is0Is the initial value of the stator current before the fault.
2. The Chopper protection action criterion method of the double-fed motor according to claim 1, characterized in that: the method for calculating the terminal voltage drop coefficient comprises the following steps:
when the rotor voltage amplitude is equal to the direct-current bus voltage limiting threshold value, obtaining a set of terminal voltage drop coefficients and time t at the moment, namely { (K)di,ti) The formula is:
Figure FDA0002717427270000031
get { (K)di,ti) K in the setdiMinimum value of (K)dminI.e. the calculated terminal voltage drop coefficient Kd,Udc.thA threshold value is defined for the dc bus voltage.
CN201910248078.8A 2019-03-29 2019-03-29 Chopper protection action criterion method for double-fed motor Active CN109921381B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910248078.8A CN109921381B (en) 2019-03-29 2019-03-29 Chopper protection action criterion method for double-fed motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910248078.8A CN109921381B (en) 2019-03-29 2019-03-29 Chopper protection action criterion method for double-fed motor

Publications (2)

Publication Number Publication Date
CN109921381A CN109921381A (en) 2019-06-21
CN109921381B true CN109921381B (en) 2020-12-01

Family

ID=66967644

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910248078.8A Active CN109921381B (en) 2019-03-29 2019-03-29 Chopper protection action criterion method for double-fed motor

Country Status (1)

Country Link
CN (1) CN109921381B (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105356520A (en) * 2015-11-24 2016-02-24 上海电力学院 Control method for improving low voltage ride through capability of wind power plant
CN106777600A (en) * 2016-12-02 2017-05-31 河海大学 Consider the double feedback electric engine short-circuit current calculation method of Chopper protections
CN109444737A (en) * 2018-09-11 2019-03-08 昆明理工大学 It is a kind of meter and crow bar operating time of protection double-fed blower three short circuit current analytic method

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2338224B1 (en) * 2008-10-20 2019-10-02 Woodward Kempen GmbH Protection system of a doubly-fed induction machine
CN105259462B (en) * 2015-11-06 2018-01-19 河海大学 A kind of double feedback electric engine Calculation Method of Three-phase Short-circuit Current

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105356520A (en) * 2015-11-24 2016-02-24 上海电力学院 Control method for improving low voltage ride through capability of wind power plant
CN106777600A (en) * 2016-12-02 2017-05-31 河海大学 Consider the double feedback electric engine short-circuit current calculation method of Chopper protections
CN109444737A (en) * 2018-09-11 2019-03-08 昆明理工大学 It is a kind of meter and crow bar operating time of protection double-fed blower three short circuit current analytic method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
综合Crowbar和Choppe保护的双馈风机低电压穿越仿真研究;曹鹏飞;《华北电力技术》;20170225(第2期);第49-54页,图7-9 *

Also Published As

Publication number Publication date
CN109921381A (en) 2019-06-21

Similar Documents

Publication Publication Date Title
CN104836503B (en) Double-fed aerogenerator stator short-circuit current calculation method under unbalanced fault
CN108599256B (en) Low voltage ride through control method of direct drive type wind turbine generator based on rotation speed regulation
CN107425539B (en) Enhanced low-voltage ride-through control method of doubly-fed wind turbine generator under asymmetric power grid fault
WO2015035892A1 (en) Method for calculating transient short circuit current of dfig set
CN105259462B (en) A kind of double feedback electric engine Calculation Method of Three-phase Short-circuit Current
WO2013118370A1 (en) Control device for wind turbine generator, wind turbine generator, and control method for wind turbine generator
CN102570957B (en) Control method for doubly-fed electric generator
CN106777600B (en) Consider the double feedback electric engine short-circuit current calculation method of Chopper protection
CN107732969B (en) Double-fed wind turbine generator short-circuit current calculation method considering low-voltage ride through overall process
CN106452234B (en) A kind of double-fed aerogenerator stator turn-to-turn short circuit negative-sequence current suppressing method
CN104809265B (en) Meter and the double-fed generator analogue system and method for crow bar protection
CN108462207B (en) Doubly-fed motor short-circuit current calculation method considering transient regulation and control of converter
CN107918695B (en) Doubly-fed wind turbine generator short-circuit current calculation method considering crowbar action
CN110034578B (en) Double-fed motor crowbar protection action criterion method
CN104865523A (en) Doubly-fed generator simulation system and method
CN105938515A (en) Doubly-fed motor three-phase short-circuit current practical calculation method
CN109888837B (en) Wind power plant short-circuit current calculation method based on double-fed motor crowbar protection new criterion
CN109921381B (en) Chopper protection action criterion method for double-fed motor
CN105846459B (en) The adaptive distance protection method combined based on intrinsic frequency with characteristic frequency
CN117081066A (en) Method and system for analyzing transient voltage instability of load of induction motor by considering large disturbance
CN115603306A (en) Rotor transient current-based doubly-fed wind turbine generator rotor voltage compensation method
CN113285639B (en) Method and system for determining negative sequence impedance of base frequency of double-fed induction generator system
CN107069802A (en) Double-fed fan motor unit net side current transformer current calculation method under generator terminal symmetric fault
CN107480406A (en) A kind of dynamic vector method for establishing model of double-fed fan motor unit calculation of short-circuit current
CN107681940B (en) Rotating speed monitoring method based on synchronous generator terminal electrical signal extraction

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant