CN112629810A - Air film parameter measuring device and method for integrated shaft type curved surface static pressure restrictor - Google Patents
Air film parameter measuring device and method for integrated shaft type curved surface static pressure restrictor Download PDFInfo
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- CN112629810A CN112629810A CN202011514837.XA CN202011514837A CN112629810A CN 112629810 A CN112629810 A CN 112629810A CN 202011514837 A CN202011514837 A CN 202011514837A CN 112629810 A CN112629810 A CN 112629810A
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- 230000003068 static effect Effects 0.000 title claims abstract description 13
- 238000000034 method Methods 0.000 title claims abstract description 9
- 230000003287 optical effect Effects 0.000 claims abstract description 33
- 238000005259 measurement Methods 0.000 claims abstract description 27
- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 230000002706 hydrostatic effect Effects 0.000 claims 3
- 238000006073 displacement reaction Methods 0.000 claims 1
- 238000009434 installation Methods 0.000 claims 1
- 239000003638 chemical reducing agent Substances 0.000 abstract description 2
- 238000005461 lubrication Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 6
- 230000009471 action Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
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Abstract
The invention discloses an air film parameter measuring device and method of an integrated shaft type curved surface static pressure restrictor, which can automatically perform three-dimensional scanning acquisition on air film microflow field parameters. The invention comprises the following steps: the device comprises a curved surface workbench base, a bearing seat, an optical axis curved surface workbench, a coupler, a curved surface restrictor, a rotating motor, a speed reducer, a temperature sensor, a pressure sensor, a two-dimensional guide rail, a Z-direction feeding mechanism, a base and a support column. The optical axis curved surface workbench is of an integrated structure, a rectangular surface is cut out of the bottom surface, a certain depth is hollowed inwards, and the workbench is provided with two threaded holes, so that a temperature sensor and a pressure sensor can be conveniently mounted. The invention provides an experimental device for realizing measurement of the parameters of the gas film micro-flow field of the curved surface restrictor, and has certain practicability and referential property.
Description
Technical Field
The invention belongs to the field of ultra-precise gas static pressure lubrication, and particularly relates to an integrated shaft type device and method for measuring parameters of a gas film of a curved surface static pressure restrictor.
Background
The gas static pressure lubrication technology has the advantages of high reuse rate, cleanness and no pollution, so the gas static pressure lubrication technology is widely used in lubrication devices in the bearing technology recently, and is applied to the industries of aerospace, medical service, electronic technology, ocean engineering, nuclear energy development and the like. The surface of the bearing sleeve is provided with air supply small holes, and in the running process of the rolling shaft, air passes through the air supply small holes on the bearing sleeve to form high pressure and enters between the bearing sleeve and the rolling shaft to play a role in lubrication. Therefore, the research on the parameters of the air film formed by the curved-surface stripping static-pressure restrictor is necessary for the gas static-pressure lubrication technology.
At present, only few colleges and universities in China have devices capable of measuring static pressure air film parameters, and most of the devices are used for measuring plane air film parameters, and no device equipment capable of realizing global measurement is provided for measuring air film parameters of a curved surface restrictor. The invention provides an integrated shaft type device and a method for measuring air film parameters of a curved surface static pressure restrictor, which are used for automatically measuring the pressure and temperature parameters of an air film micro-flow field of the curved surface restrictor.
Disclosure of Invention
The invention provides an integrated shaft type curved surface static pressure restrictor air film parameter measuring device and method aiming at the current research situation of the air static pressure lubrication technology.
The device comprises a curved surface rotation measuring mechanism, a two-dimensional guide rail, a Z-direction feeding mechanism, a supporting column and a base;
the curved surface rotation measuring mechanism comprises a curved surface workbench base, a bearing seat, an optical axis curved surface workbench, a coupler, a rotating motor, a temperature sensor and a pressure sensor; the curved surface rotation measuring mechanism is fixed on the two-dimensional guide rail through a curved surface workbench base;
the curvature radius of the measuring surface of the optical axis curved surface workbench is matched with the curvature radius of the curved surface throttleer; the central angle of the optical axis curved surface workbench is twice that of the curved surface throttler; the optical axis curved surface workbench is of an integrated axial structure, and a temperature sensor and a pressure sensor are arranged in the optical axis curved surface workbench; the optical axis curved surface workbench is arranged on a curved surface workbench base through a bearing seat, and clockwise and anticlockwise rotation measurement is realized under the action of a rotating motor;
the two-dimensional guide rail comprises a transverse feeding guide rail and a longitudinal adjusting guide rail; during measurement, the transverse feeding guide rail and the curved surface rotation measuring mechanism are matched to jointly complete the measurement path of the air film of the curved surface restrictor. The longitudinal adjusting guide rail is used for adjusting the longitudinal position of the curved surface rotation measuring mechanism;
the Z-direction feeding mechanism is used for adjusting the size of a gap between the curved surface throttler and the optical axis curved surface workbench so as to adjust the thickness of an air film; the supporting column and the base support and bear the whole device.
The working process of the invention is as follows: starting a power supply, sending a pulse signal to a longitudinal adjusting guide rail motor by an upper computer, controlling the guide rail to move, and adjusting the longitudinal position of the curved surface rotation measuring mechanism; the upper computer sends a pulse signal to the transverse feeding guide rail to adjust the initial position; the upper computer sends a pulse signal to the rotating motor to adjust the initial position of the optical axis curved surface workbench. And the thickness of the air film of the curved surface restrictor is adjusted through the Z-direction feeding structure, and the curved surface restrictor is fixed. The upper computer adjusts the air supply pressure through an air source pressure control program. The upper computer sends fixed pulse signals to the rotating motor and the transverse feeding motor, the optical axis curved surface workbench rotates, the upper computer reads data of the pressure sensor and data of the temperature sensor, judges whether the sensor reaches an axial boundary of the air film after reaching the radial boundary of the air film, and moves the transverse feeding guide rail if the sensor does not reach the axial boundary, and the rotation measurement is repeated; and if the air film axial boundary is reached, the upper computer stops sending fixed pulse signals, stops data acquisition, resets all motors and finishes measurement.
The invention has the beneficial effects that: the invention adopts a mode of matching a transverse feeding guide rail and a curved surface rotation measuring mechanism for feeding, and realizes the global measurement of the parameters of the air film micro-flow field of the curved surface static pressure restrictor. The integrated axial design of the rotating optical axis and the curved surface workbench is adopted, the cylindricity and the coaxiality tolerance of the curved surface rotating measuring mechanism during measurement are better guaranteed, meanwhile, the automatic measurement is completed by adopting the software of an upper computer, and the influence of human factors on the measuring result is reduced to the greatest extent.
Drawings
FIG. 1 is an overall perspective view of the present invention;
FIG. 2 is a perspective view of the curved surface rotation measuring mechanism of the present invention;
FIG. 3 is a block diagram of an optical axis curved stage of the present invention;
FIG. 4 is a schematic diagram of the control system of the present invention;
FIG. 5 is a flow chart of the present invention for performing a measurement;
Detailed Description
The invention is further described below with reference to the accompanying drawings.
As shown in fig. 1 and 2, the present invention comprises: the device comprises a curved surface restrictor 1, an optical axis curved surface workbench 2, a support column 3, a bearing seat 4, a curved surface workbench base 5, a longitudinal adjusting guide rail 6, a base 7, a Z-direction feeding mechanism 8, a temperature sensor 9, a pressure sensor 10, a coupler 11, a rotating motor 12, a speed reducer 13 and a transverse feeding structure 14.
As shown in fig. 2, the curved surface rotation measuring mechanism includes a curved surface worktable base, a bearing seat, an optical axis curved surface worktable, a coupling, a curved surface restrictor, a rotation motor, a temperature sensor, a pressure sensor, and a control card; the curved surface rotation measuring mechanism is fixed on the two-dimensional guide rail through the curved surface workbench base.
As shown in fig. 3, the curvature radius of the measuring surface of the optical axis curved surface workbench is matched with the curvature radius of the curved surface restrictor; the central angle of the optical axis curved surface workbench is twice that of the curved surface throttler; the optical axis curved surface workbench is of an integrated axial structure of an optical axis and a curved surface workbench, and a temperature sensor and a pressure sensor are arranged in the optical axis curved surface workbench; the optical axis curved surface workbench is arranged on a curved surface workbench base through a bearing seat, and clockwise and anticlockwise rotation measurement is realized under the action of a motor.
The two-dimensional guide rail comprises a transverse feeding guide rail and a longitudinal adjusting guide rail; during measurement, the transverse feeding guide rail and the curved surface rotation measuring mechanism are matched to jointly complete the measurement path of the air film of the curved surface restrictor. The longitudinal adjusting guide rail is used for adjusting the longitudinal position of the curved surface rotation measuring mechanism.
The Z-direction feeding mechanism is used for adjusting the size of a gap between the curved surface throttler and the optical axis curved surface workbench so as to adjust the thickness of an air film; the supporting column and the base support and bear the whole device.
As shown in fig. 4, the control system of the present invention includes: the device comprises an upper computer, a transverse motor guide rail, a longitudinal motor guide rail, a rotating motor, an air supply pressure control device, a temperature sensor and a pressure sensor;
as shown in fig. 5, the workflow of completing one measurement in the present invention is: starting a power supply, sending a pulse signal to a longitudinal adjusting guide rail motor by an upper computer, controlling the guide rail to move, and adjusting the longitudinal position of the curved surface rotation measuring mechanism; the upper computer sends a pulse signal to the transverse feeding guide rail to adjust the initial position; the upper computer sends a pulse signal to the rotating motor to adjust the initial position of the optical axis curved surface workbench. And the thickness of the air film of the curved surface restrictor is adjusted through the Z-direction feeding structure, and the curved surface restrictor is fixed. The upper computer adjusts the air supply pressure through an air source pressure control program. The upper computer sends fixed pulse signals to the rotating motor and the transverse feeding motor, the optical axis curved surface workbench rotates, the upper computer reads data of the pressure sensor and data of the temperature sensor, judges whether the sensor reaches an axial boundary of the air film after reaching the radial boundary of the air film, and moves the transverse feeding guide rail if the sensor does not reach the axial boundary, and the rotation measurement is repeated; and if the air film axial boundary is reached, the upper computer stops sending fixed pulse signals, stops data acquisition, resets all motors and finishes measurement.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present invention are included in the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (4)
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CN202011514837.XA CN112629810A (en) | 2020-12-21 | 2020-12-21 | Air film parameter measuring device and method for integrated shaft type curved surface static pressure restrictor |
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CN202011514837.XA CN112629810A (en) | 2020-12-21 | 2020-12-21 | Air film parameter measuring device and method for integrated shaft type curved surface static pressure restrictor |
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Citations (11)
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---|---|---|---|---|
US20020088276A1 (en) * | 2001-01-09 | 2002-07-11 | Hideo Omotani | Model for wind tunnel test |
KR20080038541A (en) * | 2006-10-30 | 2008-05-07 | 염충균 | Gas Permeation Membrane Analysis Apparatus and Method |
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JP5634630B1 (en) * | 2014-04-14 | 2014-12-03 | 株式会社湘南貿易 | Uneven thickness adjustment type air ring |
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CN108535413A (en) * | 2018-03-29 | 2018-09-14 | 中国计量大学 | High stability plane air film parameter measuring apparatus |
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CN210051433U (en) * | 2019-07-19 | 2020-02-11 | 中国计量大学 | Measuring device for normal random micro-vibration of throttler |
CN211626881U (en) * | 2020-04-20 | 2020-10-02 | 苏州亮宇光学科技有限公司 | Instrument for detecting free-form surface virtual image distance |
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2020
- 2020-12-21 CN CN202011514837.XA patent/CN112629810A/en active Pending
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US20020088276A1 (en) * | 2001-01-09 | 2002-07-11 | Hideo Omotani | Model for wind tunnel test |
KR20080038541A (en) * | 2006-10-30 | 2008-05-07 | 염충균 | Gas Permeation Membrane Analysis Apparatus and Method |
CN202547863U (en) * | 2012-03-16 | 2012-11-21 | 李宜伦 | High-precision dynamic calibration calibrating apparatus for force sensor |
JP5634630B1 (en) * | 2014-04-14 | 2014-12-03 | 株式会社湘南貿易 | Uneven thickness adjustment type air ring |
CN106768828A (en) * | 2017-03-06 | 2017-05-31 | 浙江工业大学 | A kind of non-contacting gas hydrostatic spindle air film flow field test system |
CN108535413A (en) * | 2018-03-29 | 2018-09-14 | 中国计量大学 | High stability plane air film parameter measuring apparatus |
CN210051433U (en) * | 2019-07-19 | 2020-02-11 | 中国计量大学 | Measuring device for normal random micro-vibration of throttler |
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