CN113671369B - Method for testing minimum starting voltage of gyro motor - Google Patents

Method for testing minimum starting voltage of gyro motor Download PDF

Info

Publication number
CN113671369B
CN113671369B CN202110861546.6A CN202110861546A CN113671369B CN 113671369 B CN113671369 B CN 113671369B CN 202110861546 A CN202110861546 A CN 202110861546A CN 113671369 B CN113671369 B CN 113671369B
Authority
CN
China
Prior art keywords
motor
power supply
gyro
supply voltage
motor shaft
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
CN202110861546.6A
Other languages
Chinese (zh)
Other versions
CN113671369A (en
Inventor
李毓杰
武丽花
赵新宇
刘志宏
张俊
盘海东
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.)
707th Research Institute of CSIC
Original Assignee
707th Research Institute of CSIC
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 707th Research Institute of CSIC filed Critical 707th Research Institute of CSIC
Priority to CN202110861546.6A priority Critical patent/CN113671369B/en
Publication of CN113671369A publication Critical patent/CN113671369A/en
Application granted granted Critical
Publication of CN113671369B publication Critical patent/CN113671369B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/34Testing dynamo-electric machines
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/04Bearings

Abstract

The invention relates to a method for testing minimum starting voltage of a gyro motor, which comprises the following steps: step 1, testing the minimum starting voltage of a motor shaft under different postures at four stages of motor assembly completion, motor installation on a gyro float frame, gyro float encapsulation and gyro integration; and step 2, checking whether the motor has counter potential voltage output after power failure, if so, indicating that the motor can be started under the power supply voltage, recording corresponding power supply voltage values and counter potential voltage values, and if not, indicating that the motor cannot be started under the power supply voltage, continuously increasing the power supply voltage, and electrifying the motor again for checking until the motor counter potential voltage output is seen. The invention can provide a quantitative control means for the quality control in the production process of the gyro motor and ensure the motor starting reliability of the whole life cycle of gyro products.

Description

Method for testing minimum starting voltage of gyro motor
Technical Field
The invention belongs to the technical field of bearing performance test, relates to a voltage test method of a rotor type gyro motor of a liquid floating machine, and particularly relates to a minimum starting voltage test method of a gyro motor.
Background
The dynamic pressure air bearing is a sliding bearing which uses gas as a lubricant and forms a gas film with a certain pressure in the bearing when the rotor rotates at a high speed. There are bearings in the form of cylindrical, opposed conical, opposed hemispherical, spherical, etc. structures, depending on the geometry. Taking a cylindrical H-shaped dynamic pressure air bearing motor structure as an example, spiral grooves are processed on a left thrust plate, a right thrust plate and a motor shaft; the end faces (thrust faces) of the left thrust plate and the left end cover form a left axial bearing, the end faces (thrust faces) of the right thrust plate and the right end cover form a right axial bearing, and the shaft holes of the motor shaft and the left end cover and the right end cover form radial bearings; the axial and radial bearing double-sided clearance is typically (3-5) microns.
Axial bearing theory of operation: the rotor is dragged by the stator magnetic field to start rotating, the gas at the outer edge of the thrust plate is driven to rotate and pumped into the bearing along the spiral groove, and when the gas enters the root of the groove, the gas is blocked by the step of the groove, so that the pressure rise occurs; as the rotation speed of the rotor increases, the pressure continues to increase, when the pressure increases to a certain value, the rotor is supported, and a dynamic pressure supporting air film without mechanical contact is formed between the thrust surface of the rotor and the thrust plate, so that a thrust bearing is formed.
Radial bearing theory of operation: assuming that the motor shaft is in a horizontal position, theoretically, the shaft hole of the rotor end cover is in line contact with the motor shaft when the rotor is stationary; after the motor is electrified, the rotor overcomes the static friction force between the shaft hole of the end cover and the motor shaft, and enters a contact friction stage with the motor shaft, when the rotating speed of the rotor is continuously increased, the rotor drives gas in the gap to move together, and when a moving gas medium approaches to a gap which is smaller, the gas is compressed to form a wedge-shaped gas film and a corresponding high-pressure area. The rotor rotates in an accelerated manner, and the air film supports the rotor, so that the rotor and the shaft form a dynamic pressure supporting air film without mechanical contact, and a radial bearing is formed.
From the above, the contact points of the axial and radial bearings are different when the motor is in different positions and attitudes. For example, in the horizontal state of the motor shaft, due to the influence of acceleration inertia in different directions during carrying, the thrust surface of the rotor end cover is likely to be attached to a thrust plate, and when the next power-on starting is performed, the rotor overcomes the static friction force between the thrust surface and the thrust plate besides the static friction force between the shaft and the shaft hole; for another example, when the motor shaft is vertical, the rotor has a thrust surface against the thrust plate under the force of gravity, and the static friction between the shaft and the shaft hole may become small due to the positional relationship; when the motor shaft is inclined, the radial bearings and the axial bearings are contacted, and static friction force applied to the rotor is more complex.
Therefore, when the motor is in different positions and postures, the resistance of the motor is different, and the starting performance is also different. Limited by the motor bearing structure, it is inconvenient to directly measure the static friction force between the bearings. In order to be able to evaluate the starting performance of the motor at different production stages, it is necessary to find a quantized method for testing the minimum starting voltage of the gyro motor.
Disclosure of Invention
The invention aims to overcome the defects of the prior art, and provides a method for testing the minimum starting voltage of a gyro motor, which can provide a quantitative control means for quality control in the production process of the gyro motor and ensure the motor starting reliability of the whole life cycle of a gyro product.
The invention solves the practical problems by adopting the following technical scheme:
a method for testing minimum starting voltage of a gyro motor comprises the following steps:
step 1, testing the minimum starting voltage of a motor shaft under different postures at four stages of motor assembly completion, motor installation on a gyro float frame, gyro float encapsulation and gyro integration;
and step 2, checking whether the motor has counter potential voltage output after power failure, if so, indicating that the motor can be started under the power supply voltage, recording corresponding power supply voltage values and counter potential voltage values, and if not, indicating that the motor cannot be started under the power supply voltage, continuously increasing the power supply voltage, and electrifying the motor again for checking until the motor counter potential voltage output is seen.
Moreover, the different postures of the motor shaft in the step 1 include: the motor shaft is horizontal, the included angle between the motor shaft rotation direction H and the horizontal is 45 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 90 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 135 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 225 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 270 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 315 degrees, and the included angle between the motor shaft rotation direction H and the horizontal is 360 degrees.
The specific method for checking whether the motor has counter potential voltage output in the step 2 is as follows:
and under each gesture, the power supply voltage is regulated down to any value which can not be started by the motor, the power supply voltage is increased by a fixed step length, the motor is supplied with power for a fixed time, and whether the motor has counter potential voltage output is checked after power failure.
The step size determination method for increasing the power supply voltage comprises the following steps:
λ=rated supply voltage of motor x (1% -2%)
The invention has the advantages and beneficial effects that:
the minimum starting voltage value obtained through the test of the invention represents the magnitude of the static friction moment of the bearing in the current production stage and the current motor shaft gesture, and is an important basis for judging the assembly quality of the bearing. And the change of counter potential voltage obtained by multiple tests under the same starting voltage is measured and can be used as supplement, so that the static friction moment vector sum of different contact parts of the bearing is represented. The invention can provide a quantitative control means for the quality control in the production process of the gyro motor and ensure the motor starting reliability of the whole life cycle of gyro products.
Detailed Description
The following further details examples of the invention:
a method for testing minimum starting voltage of a gyro motor comprises the following steps:
step 1, testing the minimum starting voltage of a motor shaft under different postures at four stages of motor assembly completion, motor installation on a gyro float frame, gyro float encapsulation and gyro integration;
the different postures of the motor shaft in the step 1 include but are not limited to: the motor shaft is horizontal, the included angle between the motor shaft rotation direction H and the horizontal is 45 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 90 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 135 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 225 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 270 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 315 degrees, and the included angle between the motor shaft rotation direction H and the horizontal is 360 degrees.
And step 2, checking whether the motor has counter potential voltage output after power failure, if so, indicating that the motor can be started under the power supply voltage, recording corresponding power supply voltage values and counter potential voltage values, and if not, indicating that the motor cannot be started under the power supply voltage, continuously increasing the power supply voltage, and electrifying the motor again for checking until the motor counter potential voltage output is seen.
The specific method for checking whether the motor has counter potential voltage output in the step 2 is as follows:
and under each gesture, the power supply voltage is regulated down to any value which can not be started by the motor, the power supply voltage is increased by a fixed step length, the motor is supplied with power for a fixed time, and whether the motor has counter potential voltage output is checked after power failure.
Step size determination method for raising power supply voltage:
λ=rated supply voltage of motor x (1% -2%)
In the embodiment, after the motor is assembled, the motor is mounted on the gyro float frame, the gyro float is packaged, and the gyro is integrated, the motor is placed at various positions through the tool, so that the H-shaped bearing can traverse various postures.
In this embodiment, a set of gesture positions is given for reference, as shown in table 1.
Table 1 minimum starting voltage test for a set of motor shafts at different poses
In each gesture, the power supply voltage is regulated down to any value which can not be started by the motor, the power supply voltage is increased by a fixed step length, the motor is supplied with power for a fixed time (the rated voltage power supply time of the motor can be referred to, and the rated voltage power supply time is generally several seconds), and whether the motor has counter potential voltage output is checked after the power is cut off.
Step size determination method for raising power supply voltage:
λ=rated supply voltage of motor x (1% -2%)
If the counter potential voltage exists, the motor can be started under the power supply voltage, the corresponding power supply voltage value and the counter potential voltage value are filled into the table, if the counter potential voltage does not exist, the motor cannot be started under the power supply voltage, the power supply voltage is continuously increased, and the motor is powered on again for checking until the output of the counter potential voltage of the motor can be seen.
In each production stage before the motor is not packaged in the floater, whether the motor is started or not can be judged by visually and actually observing whether the motor rotor rotates or not.
The minimum start-up voltage and back-emf voltage measured at each production stage are reported in table 2.
TABLE 2 minimum Start Voltage test at different stages in the same pose
The method can formulate a control index which accords with reality according to the starting characteristics of the motor, the current motor processing and assembling capability, and compare the control index with measured data to make qualification judgment.
The working principle of the invention is as follows:
the minimum starting voltage value of the invention represents the magnitude of static friction moment of the bearing contact surface in the current production stage and the current motor shaft gesture, and is an important basis for judging the assembly quality of the bearing surface.
The increase amplitude of the static friction moment of the bearing caused by the restraint of the motor in different production stages can be seen from the longitudinal direction of the minimum starting voltage values obtained in different production stages, and a reference is provided for the suppression of the stress in the gyro assembly process.
The change of counter potential voltage obtained by multiple tests under the same starting voltage can be used as supplement, and the static friction moment vector sum of different contact parts of the bearing is represented. Because the resistance force suffered by the motor bearing is mainly the static friction force between the bearings in the starting process, and the radial and axial bearing contact positions are random positions when the motor stops last time, the change of the counter potential voltage can reflect the difference of the static friction force of the bearings.
It should be emphasized that the embodiments described herein are illustrative rather than limiting, and that this invention encompasses other embodiments which may be made by those skilled in the art based on the teachings herein and which fall within the scope of this invention.

Claims (2)

1. A method for testing minimum starting voltage of a gyro motor is characterized by comprising the following steps of: the method comprises the following steps:
step 1, testing the minimum starting voltage of a motor shaft under different postures at four stages of motor assembly completion, motor installation on a gyro float frame, gyro float encapsulation and gyro integration;
step 2, checking whether the motor has counter potential voltage output after power failure, if so, indicating that the motor can be started under the power supply voltage, recording corresponding power supply voltage values and counter potential voltage values, and if not, indicating that the motor cannot be started under the power supply voltage, continuously increasing the power supply voltage, and electrifying the motor again for checking until the motor counter potential voltage output is seen;
the specific method for checking whether the motor has counter potential voltage output in the step 2 is as follows:
under each gesture, the power supply voltage is regulated down to any value which can not be started by the motor, the power supply voltage is increased by a fixed step length, the motor is supplied with power for a fixed time, and whether the motor has counter potential voltage output is checked after power failure;
the step size determination method for increasing the power supply voltage comprises the following steps:
λ=motor rated supply voltage× (1% -2%).
2. The method for testing the minimum starting voltage of the gyro motor according to claim 1, wherein the method comprises the following steps of: the different postures of the motor shaft in the step 1 comprise: the motor shaft is horizontal, the included angle between the motor shaft rotation direction H and the horizontal is 45 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 90 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 135 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 225 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 270 degrees, the included angle between the motor shaft rotation direction H and the horizontal is 315 degrees, and the included angle between the motor shaft rotation direction H and the horizontal is 360 degrees.
CN202110861546.6A 2021-07-29 2021-07-29 Method for testing minimum starting voltage of gyro motor Active CN113671369B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110861546.6A CN113671369B (en) 2021-07-29 2021-07-29 Method for testing minimum starting voltage of gyro motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110861546.6A CN113671369B (en) 2021-07-29 2021-07-29 Method for testing minimum starting voltage of gyro motor

Publications (2)

Publication Number Publication Date
CN113671369A CN113671369A (en) 2021-11-19
CN113671369B true CN113671369B (en) 2023-09-08

Family

ID=78540616

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110861546.6A Active CN113671369B (en) 2021-07-29 2021-07-29 Method for testing minimum starting voltage of gyro motor

Country Status (1)

Country Link
CN (1) CN113671369B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113514180B (en) * 2021-06-07 2023-04-14 北京控制工程研究所 Monitoring, screening and controlling system and method for surface friction torque of bearing of permanent magnet gyro motor
CN115655250A (en) * 2022-12-14 2023-01-31 西安航天精密机电研究所 Gyroscope and processing and assembling method thereof
CN115615594B (en) * 2022-12-19 2023-03-31 西安航天精密机电研究所 Method for testing starting torque margin of H-shaped dynamic pressure bearing motor

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004364473A (en) * 2003-06-09 2004-12-24 Nippon Densan Corp Starting method and device for motor
EP2410651A1 (en) * 2010-07-23 2012-01-25 Askoll Holding S.r.l. Method for starting a permanent magnet single-phase synchronous electric motor and electronic device for implementing said method
CN104483535A (en) * 2014-12-08 2015-04-01 河北汉光重工有限责任公司 Starting voltage testing method for all-digital follow-up system
CN105915130A (en) * 2016-06-14 2016-08-31 浙江钱江摩托股份有限公司 Control method and device of sensorless permanent magnet motor used for pump
CN106664042A (en) * 2014-08-14 2017-05-10 皮尔伯格泵技术有限责任公司 Method for starting a drive motor of an auxiliary assembly of a motor vehicle, and drive motor of an auxiliary assembly of a motor vehicle
CN107733300A (en) * 2017-10-30 2018-02-23 北京航空航天大学 A kind of safe and reliable brushless DC motor without sensor starts control method
CN109617462A (en) * 2018-12-11 2019-04-12 上海肖可雷电子科技有限公司 A kind of recognition methods of electric motor starting state

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004364473A (en) * 2003-06-09 2004-12-24 Nippon Densan Corp Starting method and device for motor
EP2410651A1 (en) * 2010-07-23 2012-01-25 Askoll Holding S.r.l. Method for starting a permanent magnet single-phase synchronous electric motor and electronic device for implementing said method
CN102347723A (en) * 2010-07-23 2012-02-08 阿思科尔控股责任有限公司 Method for starting a permanent magnet single-phase synchronous electric motor and electronic device for implementing said method
CN106664042A (en) * 2014-08-14 2017-05-10 皮尔伯格泵技术有限责任公司 Method for starting a drive motor of an auxiliary assembly of a motor vehicle, and drive motor of an auxiliary assembly of a motor vehicle
CN104483535A (en) * 2014-12-08 2015-04-01 河北汉光重工有限责任公司 Starting voltage testing method for all-digital follow-up system
CN105915130A (en) * 2016-06-14 2016-08-31 浙江钱江摩托股份有限公司 Control method and device of sensorless permanent magnet motor used for pump
CN107733300A (en) * 2017-10-30 2018-02-23 北京航空航天大学 A kind of safe and reliable brushless DC motor without sensor starts control method
CN109617462A (en) * 2018-12-11 2019-04-12 上海肖可雷电子科技有限公司 A kind of recognition methods of electric motor starting state

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
惠欣等.轴承表面状态对动压气浮电机启动的可靠性影响分析.《惯性传感器技术与应用研讨会文集》.2020,81-86. *

Also Published As

Publication number Publication date
CN113671369A (en) 2021-11-19

Similar Documents

Publication Publication Date Title
CN113671369B (en) Method for testing minimum starting voltage of gyro motor
CN207487971U (en) A kind of electro spindle-bearing characteristics experimental rig
Isomura et al. Development of high-speed micro-gas bearings for three-dimensional micro-turbo machines
CN109959514B (en) Paired angular contact ball bearing dynamic friction performance online testing device
CN113432789B (en) Online testing device and method for dynamic balance weight of rotary machine
CN114167280B (en) Screening test method and system for dynamic pressure motor working margin in gyroscope
Jung et al. Monitoring of journal bearing faults based on motor current signature analysis for induction motors
CN103759942B (en) Water lubriucated bearing testing table
Guan et al. Vibration control for rotor mounted on a novel active bump type foil bearing with controllable mechanical preloads
US6804987B2 (en) Apparatus and method for air-contamination detection in disc drive hydrodynamic bearings
CN113864341A (en) Static and dynamic mixed air-bearing rotor system and operation method
US6173234B1 (en) Axial bearing fly-height measurement to detect oil deficiency
Prasad et al. Bearing selection for high-speed electrical machine
US6907769B2 (en) Apparatus and method for detecting air contamination in fluid dynamic bearings
JP3912675B2 (en) Inspection method for hydrodynamic bearings
Lubell et al. Identification and correction of rotor instability in an oil-free gas turbine
JP2007192369A (en) Performance determining method of dynamic pressure bearing and dynamic pressure bearing
JPH10184302A (en) Fluid machine
Olszewski et al. Experimental investigation of prototype water-lubricated compliant foil bearings
US7908737B2 (en) Production method of fluid dynamic-pressure bearing in spindle motor
Cuesta et al. Non-linear behaviors in the motion of a magnetically supported rotor on the catcher bearing during levitation loss: An experimental description
JP2001323893A (en) High speed rotation instrument
CN116222941B (en) Nuclear main pump mechanical seal test bed sealing surface radial vibration simulation device
CN220120376U (en) Main shaft bearing testing machine based on internal force method
Ravikovich et al. Test procedure and test rig for determining the load capacity of axial gas foil bearings

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