CN102374924A - Measurement method of moment of inertia of separately excited DC (Direct Current) motor - Google Patents

Measurement method of moment of inertia of separately excited DC (Direct Current) motor Download PDF

Info

Publication number
CN102374924A
CN102374924A CN2010102623189A CN201010262318A CN102374924A CN 102374924 A CN102374924 A CN 102374924A CN 2010102623189 A CN2010102623189 A CN 2010102623189A CN 201010262318 A CN201010262318 A CN 201010262318A CN 102374924 A CN102374924 A CN 102374924A
Authority
CN
China
Prior art keywords
motor
inertia
moment
direct current
rated
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.)
Granted
Application number
CN2010102623189A
Other languages
Chinese (zh)
Other versions
CN102374924B (en
Inventor
闫小卫
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.)
AVIATION POWER CONTROL SYSTEM RESEARCH INSTITUTE OF AVIATION INDUSTRY Corp OF CHINA
Original Assignee
AVIATION POWER CONTROL SYSTEM RESEARCH INSTITUTE OF AVIATION INDUSTRY Corp OF CHINA
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 AVIATION POWER CONTROL SYSTEM RESEARCH INSTITUTE OF AVIATION INDUSTRY Corp OF CHINA filed Critical AVIATION POWER CONTROL SYSTEM RESEARCH INSTITUTE OF AVIATION INDUSTRY Corp OF CHINA
Priority to CN201010262318.9A priority Critical patent/CN102374924B/en
Publication of CN102374924A publication Critical patent/CN102374924A/en
Application granted granted Critical
Publication of CN102374924B publication Critical patent/CN102374924B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Tests Of Circuit Breakers, Generators, And Electric Motors (AREA)

Abstract

The invention belongs to the motor parameter measurement technology, and relates to an improvement of a measurement method of the moment of inertia of a separately excited DC (Direct Current) motor based on a Siemens 6RA70 series all-digital DC speed control device. The measurement method is characterized by comprising the following steps that: a measured motor is connected; an acceleration time Ta is measured; and the moment of inertia J is calculated. The measurement method provided by the invention is simple and convenient to operate, is suitable for being used in engineering application sites, has strong engineering practicality, and meets the need of debugging of a DC transmission system.

Description

A kind of measuring method of separately excited DC machine moment of inertia
Technical field
The invention belongs to parameter of electric machine measuring technique, relate to improvement the separately excited DC machine method for measuring rotary inertia.
Background technology
In the DC electrical driving control system, the moment of inertia of direct current motor and gear case is very big to the influence of system dynamics response time, in quick response system, requires moment of inertia more little good more.Direct current generator manufacturer is not owing to test the specialized equipment of moment of inertia, and the data of often can not giving actual rotation inertia can only provide the Design Theory data.Some producer even couple very much in love opinion data do not provide yet.In the direct current fax system debug process, whether the actual inertia that need know motor and gear case within the designing requirement scope, if excessive, need add the moment of inertia compensation in controlling unit.GB1311 " direct current generator test method " provides three kinds of assay methods of motor moment of inertia J: from retardation method, rock method and auxiliary pendulum method.
1) be the free parking method from retardation method, at first will measure open-circuit core loss and the mechanical loss of motor when rated speed, rated exciting current be higher than rated speed n NUnder do no-load running, treat that the motor back of operating steadily cuts off rapidly the armature power supply, slow down naturally by its inertia, use the oscillograph recording deceleration curve, analytic curve substitution formula calculating J.
2) method of rocking is the method that compares by the moment of inertia of the moment of inertia of examination rotor and cylindrical standard rotor.Need rotor taken out and hang on the support, measure hunting period, but also will make the false rotor that a quality, diameter that diameter is close with true rotor are calculated inertia, test the false rotor swing cycle under the same conditions, again substitution calculating J.
3) auxiliary pendulum method is fixed in tested machine shaft end face center with a known auxiliary pendulum of quality with the as far as possible little armed lever of quality, asks mean value hunting period, and the substitution formula calculates J.
These three kinds of methods are all cumbersome, and only suitable motor performance detects unit or research unit uses, and are not suitable for the on-the-spot use of practical applications.
Summary of the invention
The objective of the invention is: propose the on-the-spot separately excited DC machine method for measuring rotary inertia that uses of a kind of practical applications easy and simple to handle, suitable, to satisfy the needs of direct current fax system debug.
Technical scheme of the present invention is: a kind of measuring method of separately excited DC machine moment of inertia based on Siemens 6RA70 series digital direct current speeder, is characterized in that the step of measurement is following:
1, connects by measured motor: will be fixed on the measuring table by measured motor, and when needs are measured the total moment of inertia under the motor bringing onto load state, also need and to be connected with load by measured motor; Be connected with armature, the excitation output terminal of Siemens 6RA70 series digital direct current speeder through armature, the excitation terminals of cable then motor;
2, measure acceleration time Ta: give the energising of Siemens 6RA70 series digital direct current speeder; The method of operation is set to " friction and moment of inertia compensation optimizing " method of operation, measures the acceleration time Ta that is accelerated to rated speed by measured motor with rated current and rated exciting current from zero-speed;
3, calculate moment of inertia J: according to computes by the moment of inertia J of measured motor:
J = 91358 kPTa N 2 - - - [ 1 ]
In the formula, P is a direct current generator rated power, and unit is kW; Ta unit is s; N is the motor rated speed, and unit is r/min; K is a correction factor, and definite method of coefficient k is:
k = Ib Ia - - - [ 2 ]
In the formula, Ib is the actual output-current rating of Siemens 6RA70 series digital direct current speeder, and Ia is the armature rated current of tested motor nameplate mark, and unit is A.
Advantage of the present invention is: easy and simple to handle, be fit to the on-the-spot use of practical applications, and engineering practicability is strong, has satisfied the needs of direct current fax system debug.
Description of drawings
Fig. 1 instrumentation plan of the present invention.
Embodiment
Explain further details in the face of the present invention down.Referring to Fig. 1, a kind of measuring method of separately excited DC machine moment of inertia, is characterized in that the concrete steps of measurement are following based on Siemens 6RA70 series digital direct current speeder (hereinafter to be referred as arrangements for speed regulation):
1, connects by measured motor: will be fixed on the measuring table by measured motor, and when needs are measured the total moment of inertia under the motor bringing onto load state, also need and to be connected with load by measured motor; Be connected with armature, the excitation output terminal of arrangements for speed regulation through armature, the excitation terminals of cable then motor;
2, measure acceleration time Ta: switch on to arrangements for speed regulation; The method of operation is set to " friction and moment of inertia compensation optimizing " method of operation; Measure the acceleration time Ta that is accelerated to rated speed by measured motor with rated current and rated exciting current from zero-speed; The Ta respective value is an arrangements for speed regulation inner parameter P540 video data, and unit is s;
3, calculate moment of inertia J: according to computes by the moment of inertia J of measured motor:
J = 91358 kPTa N 2 - - - [ 1 ]
In the formula, P is a direct current generator rated power, and unit is kW; Ta unit is s; N is the motor rated speed, and unit is r/min; K is a correction factor, and definite method of coefficient k is:
k = Ib Ia - - - [ 2 ]
In the formula, Ib is the actual output-current rating of arrangements for speed regulation, and Ia is the armature rated current of tested motor nameplate mark, and unit is A.
Principle of work of the present invention is: the calculating formula process is following:
Acceleration time Ta:
Ta = 4 gJΔN 375 ΔM - - - [ 3 ]
In the formula, g is a constant 9.8; J is a moment of inertia, and unit is kgm 2Δ N is an acceleration range, and unit is r/min; Δ M is the motor acceleration torque, and unit is Nm.
Motor nominal torque M:
M = 9550 P N - - - [ 4 ]
In the formula, P is a motor rated power, and unit is kW; N is the motor rated speed, and unit is r/min.
Introduce correction factor k, derive the calculating formula of moment of inertia J by [3] formula, [4] formula:
J = k 375 MTa 4 gN = 91358 kPTa N 2 - - - [ 1 ]
In the formula, P is tested motor rated power, and unit is kW; Ta is the acceleration time, and unit is s; N is the motor rated speed, and unit is r/min; K is a correction factor, and value is the actual output-current rating of tested motor speed control device and the ratio of tested armature rated current.
Embodiments of the invention: in certain aeroengine control system semi-physical simulation device; The supporting arrangements for speed regulation of separately excited DC machine are Siemens 6RA70 series direct current speeder in the electric drive system; Through the measurement to direct current generator acceleration time (Ta=P540) of many different capacities, rotating speed, result of calculation is seen table 1.
Separately excited DC machine in the table 1 is varied; The miniwatt high speed DC slotless motor that customization is arranged; Have Nan Yang, Shanghai motor in high-power Z4 direct current generator; According to the national standard that motor is made, the moment of inertia design load that producer provides has ± 10% error, and the moment of inertia value of measuring according to the inventive method and the gap of motor producer design load are all in ± 10% scope; Check motor actual rotation inertia to satisfy user demand, embodied easy, effective, the practical advantage of this method.
The rotation inerttia result of 4 embodiment of table 1 the present invention
Figure BSA00000243119800041
Error in the table 1 is meant the measured value of employing the inventive method and the gap of electrical machinery plant's design load.

Claims (1)

1. the measuring method of a separately excited DC machine moment of inertia based on Siemens 6RA70 series digital direct current speeder, is characterized in that the step of measurement is following:
1.1, connect by measured motor: will be fixed on the measuring table by measured motor, when needs are measured the following total moment of inertia of motor bringing onto load state, also needs will be connected with load by measured motor; Be connected with armature, the excitation output terminal of Siemens 6RA70 series digital direct current speeder through armature, the excitation terminals of cable then motor;
1.2, measure acceleration time Ta: give the energising of Siemens 6RA70 series digital direct current speeder; The method of operation is set to " friction and moment of inertia compensation optimizing " method of operation, measures the acceleration time Ta that is accelerated to rated speed by measured motor with rated current and rated exciting current from zero-speed;
1.3, calculate moment of inertia J: according to computes by the moment of inertia J of measured motor:
J = 91358 kPTa N 2 - - - [ 1 ]
In the formula, P is a direct current generator rated power, and unit is kW; Ta unit is s; N is the motor rated speed, and unit is r/min; K is a correction factor, and definite method of coefficient k is:
k = Ib Ia - - - [ 2 ]
In the formula, Ib is the actual output-current rating of Siemens 6RA70 series digital direct current speeder, and Ia is the armature rated current of tested motor nameplate mark, and unit is A.
CN201010262318.9A 2010-08-23 2010-08-23 Measurement method of moment of inertia of separately excited DC (Direct Current) motor Expired - Fee Related CN102374924B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201010262318.9A CN102374924B (en) 2010-08-23 2010-08-23 Measurement method of moment of inertia of separately excited DC (Direct Current) motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201010262318.9A CN102374924B (en) 2010-08-23 2010-08-23 Measurement method of moment of inertia of separately excited DC (Direct Current) motor

Publications (2)

Publication Number Publication Date
CN102374924A true CN102374924A (en) 2012-03-14
CN102374924B CN102374924B (en) 2014-02-05

Family

ID=45793853

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201010262318.9A Expired - Fee Related CN102374924B (en) 2010-08-23 2010-08-23 Measurement method of moment of inertia of separately excited DC (Direct Current) motor

Country Status (1)

Country Link
CN (1) CN102374924B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103595327A (en) * 2013-11-04 2014-02-19 朱淼 Experiment estimation method of motor rotational inertia in electrical drive system
CN105424277A (en) * 2015-12-16 2016-03-23 四川长虹电器股份有限公司 Method and device for obtaining rotational inertia of motor
CN107782498A (en) * 2017-10-10 2018-03-09 中国石油集团川庆钻探工程有限公司 System and method for measuring equivalent rotational inertia of diesel engine
CN113447201A (en) * 2021-06-01 2021-09-28 中国航空工业集团公司沈阳飞机设计研究所 Method for measuring rotational inertia of aero-engine under loading condition

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000111436A (en) * 1998-08-03 2000-04-21 Chinkaku Higashijima Method and device for measuring inertia moment
RU2172936C1 (en) * 2000-01-17 2001-08-27 Копейкин Анатолий Иванович Method for measurement of body moment of inertia
RU2172938C1 (en) * 2000-08-01 2001-08-27 Государственное унитарное предприятие Всероссийский научно-исследовательский институт тепловозов и путевых машин Test bench for experimental studies of flexible couplings
CN1354558A (en) * 2001-12-05 2002-06-19 深圳安圣电气有限公司 Non-synchronous motor rotary inertia identification method
CN101266183A (en) * 2008-05-09 2008-09-17 山东电力研究院 Test method for moment of inertia of pumped storage power station generator/motor rotor
JP2008286608A (en) * 2007-05-16 2008-11-27 Asmo Co Ltd Method and apparatus for measuring motor torque
CN101566526A (en) * 2009-05-15 2009-10-28 重庆长安汽车股份有限公司 Three-Line pendulum torsional pendulum period meter capable of measuring the engine moment inertia

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000111436A (en) * 1998-08-03 2000-04-21 Chinkaku Higashijima Method and device for measuring inertia moment
RU2172936C1 (en) * 2000-01-17 2001-08-27 Копейкин Анатолий Иванович Method for measurement of body moment of inertia
RU2172938C1 (en) * 2000-08-01 2001-08-27 Государственное унитарное предприятие Всероссийский научно-исследовательский институт тепловозов и путевых машин Test bench for experimental studies of flexible couplings
CN1354558A (en) * 2001-12-05 2002-06-19 深圳安圣电气有限公司 Non-synchronous motor rotary inertia identification method
JP2008286608A (en) * 2007-05-16 2008-11-27 Asmo Co Ltd Method and apparatus for measuring motor torque
CN101266183A (en) * 2008-05-09 2008-09-17 山东电力研究院 Test method for moment of inertia of pumped storage power station generator/motor rotor
CN101566526A (en) * 2009-05-15 2009-10-28 重庆长安汽车股份有限公司 Three-Line pendulum torsional pendulum period meter capable of measuring the engine moment inertia

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
中华人民共和国国家质量监督检验检疫总局: "直流电机试验方法", 《中华人民共和国国家标准GB/T1311-2008》, 16 July 2008 (2008-07-16), pages 1 - 34 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103595327A (en) * 2013-11-04 2014-02-19 朱淼 Experiment estimation method of motor rotational inertia in electrical drive system
CN103595327B (en) * 2013-11-04 2016-01-20 朱淼 The experiment estimation method of motor moment of inertia in electric drive system
CN105424277A (en) * 2015-12-16 2016-03-23 四川长虹电器股份有限公司 Method and device for obtaining rotational inertia of motor
CN105424277B (en) * 2015-12-16 2018-02-16 四川长虹电器股份有限公司 A kind of method and apparatus for obtaining motor rotary inertia
CN107782498A (en) * 2017-10-10 2018-03-09 中国石油集团川庆钻探工程有限公司 System and method for measuring equivalent rotational inertia of diesel engine
CN113447201A (en) * 2021-06-01 2021-09-28 中国航空工业集团公司沈阳飞机设计研究所 Method for measuring rotational inertia of aero-engine under loading condition
CN113447201B (en) * 2021-06-01 2023-11-03 中国航空工业集团公司沈阳飞机设计研究所 Aeroengine rotational inertia measurement method under loading condition

Also Published As

Publication number Publication date
CN102374924B (en) 2014-02-05

Similar Documents

Publication Publication Date Title
CN201110888Y (en) Self-starting rare-earth permanent magnet rotor type electric motor microcomputer integrated test apparatus
Lu et al. A nonintrusive and in-service motor-efficiency estimation method using air-gap torque with considerations of condition monitoring
CN104487678B (en) Twin-shaft turbine electricity generation system, the control device of gas turbine engine systems and control method
CN102507120B (en) A test bench for unbalanced magnetic tension test of generator rotor supported by sliding bearings
Ferreira et al. Method for in-field evaluation of the stator winding connection of three-phase induction motors to maximize efficiency and power factor
CN102374924B (en) Measurement method of moment of inertia of separately excited DC (Direct Current) motor
CN101629860A (en) Method for testing partial performances of three-phase asynchronous motors
CN102183705A (en) Method for on line diagnosing turn-to-turn short circuit fault of large-size generator rotor
CN105467223A (en) System and method for testing losses of iron core of electrical steel material in motor environment
CN101915623A (en) Method for measuring temperature of rotor of brushless exciting generator
CN101655400A (en) Method and device for testing shellless motor
JP2016065789A (en) Efficiency measurement method of motor
CN106053054A (en) Gear box characteristic parameter real-time on-line detection device
CN108225696B (en) Energy feedback type shafting torsional vibration testing system
KR102253855B1 (en) Diagnosis method and system of component loss for motor
CN109031124A (en) A kind of motor rotation blockage test method
Zhang et al. A low-intrusion load and efficiency evaluation method for in-service motors using vibration tests with an accelerometer
Božić et al. Efficiency classes of three-phase, cage-induction motors (IE-code) software
Hamatwi et al. Development of a Test Rig for Fault Studies on a scaled-down DFIG
CN213516336U (en) Torque detection experiment table for permanent magnet coupler
CN111766396B (en) Device and method for measuring time constant of rotating speed probe and preamplifier
CN205403687U (en) Iron core plane degree straightness pick -up plate that hangs down
Machado et al. Stray load losses calculation routine based on the Eh-star method
CN112414702A (en) An experimental bench for torque detection of a permanent magnet coupler
CN112152534A (en) Synchronous motor transient torque measuring device and method based on static measurement

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140205