CN108303256A - Three-point mount formula circumference radial loaded and test device - Google Patents

Three-point mount formula circumference radial loaded and test device Download PDF

Info

Publication number
CN108303256A
CN108303256A CN201810092760.8A CN201810092760A CN108303256A CN 108303256 A CN108303256 A CN 108303256A CN 201810092760 A CN201810092760 A CN 201810092760A CN 108303256 A CN108303256 A CN 108303256A
Authority
CN
China
Prior art keywords
test device
load
air bearing
force adjustment
air
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.)
Pending
Application number
CN201810092760.8A
Other languages
Chinese (zh)
Inventor
刘波
卢志伟
张君安
方舟
董皓
王永振
陈登弟
李子昂
王月娇
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.)
Xian Technological University
Original Assignee
Xian Technological University
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 Xian Technological University filed Critical Xian Technological University
Priority to CN201810092760.8A priority Critical patent/CN108303256A/en
Publication of CN108303256A publication Critical patent/CN108303256A/en
Pending legal-status Critical Current

Links

Classifications

    • 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

Three-point mount formula circumference radial loaded and test device of the present invention, including support base, in support base upper surface, the supporting rack that one section is equilateral triangle is set, it is respectively provided with a direction load test device in three vertex of supporting rack, the front end of three direction load test devices is connect with air bearing, tested load main shaft is worn in air bearing, load test device in direction to the load of air bearing vitality and can carry out the monitoring of loading force, the central shaft extended line of three direction load test devices meets at the central axis of support frame as described above, vee-block is fixedly installed on bottom surface in supporting rack, air bearing is arranged by the vee-block in supporting rack.Three-point mount circumference radial loaded and test device of the present invention, it can realize dynamic and static separation, air-floating main shaft static state can be simulated under static and current intelligence, its week is tested and recorded to three direction sustained continuous reinforcings, to meet air supporting hydrostatic spindle testing requirements.

Description

Three-point mount formula circumference radial loaded and test device
Technical field
The invention belongs to field of mechanical technique, and in particular to a kind of three-point mount formula circumference radial loaded and test device.
Background technology
With the development of science and technology, it is the bearing of lubricant with its minimum friction coefficient, high revolution using gas Precision and it is pollution-free the advantages that be more and more widely used with instrument in precision machinery.Air supporting hydrostatic spindle concentrates body High speed, efficient and high-accuracy processing performance are showed, have been one of the main direction of development of precision machine tool main shaft.To air supporting hydrostatic spindle Nature static and the test of bearing capacity of dynamic need one kind that can continuously load, in the case that static and dynamically can be into Row force, the displacement of institute's loaded load and vibration do not influence air supporting hydrostatic spindle, and can circumference any direction into Row loads and added load can be tested and be recorded.
There are some air supporting hydrostatic spindle test experiments platforms in the country, these platforms some air-floating main shaft static state can only be carried out The displacement and vibration of load, load main shaft can be passed in dynamic by accurate load;Some are loaded using counterweight, loaded load It is very accurate, but can not realize continuous load and counterweight load sometimes can seem very heavy and can not find suitable weight Code;Some can realize continuous load using pneumatically loading, due to the compressibility of gas and the unstability of supply gas pressure, can make Loaded load is unstable and consistency is bad.
Invention content
The object of the present invention is to provide a kind of three-point mount formula circumference radial loaded and test devices, solve in the prior art The problem of air supporting hydrostatic spindle test experiments platform.
The technical scheme is that:
Three-point mount formula circumference radial loaded and test device, including support base are arranged one in the support base upper surface A section is the supporting rack of equilateral triangle, and a direction load test device is respectively provided in three vertex of support frame as described above, three The front end of a direction load test device is connect with air bearing, and tested load main shaft, the side are worn in air bearing To the load of air bearing vitality and the monitoring of loading force, three direction load test devices can be carried out to load test device Central shaft extended line meet at the central axis of support frame as described above, vee-block, air bearing is fixedly installed on support frame as described above bottom surface It is arranged in supporting rack by the vee-block, the central shaft of the air bearing and the center overlapping of axles of support frame as described above.
Further, the direction load test device includes force adjustment screw rod, force adjustment screw sleeve, thrust bearing, stayed mast, drawing Force snesor and tension spring;The force adjustment screw sleeve is fixed at the vertex of support frame as described above, and force adjustment screw rod passes through spiral shell Line connection is threaded through in force adjustment screw sleeve, and the lower end of the force adjustment screw rod is described to push away by positioning thrust bearing described in pin connection The lower end of power bearing connects the stayed mast, and the lower end of the stayed mast connects the pulling force sensor, the pulling force sensor Lower end connects the tension spring, and the tension spring lower end is connect by threaded with the outer wall of the air bearing.
Further, the upper end of the force adjustment screw rod is provided with force adjustment knob.
Further, real-time pulling force display screen is provided on the pulling force sensor.
Further, the vee-block, which is bolted, is arranged on the bottom surface of supporting rack, and air bearing is arranged in V-arrangement It is gripped in the V-shaped groove of block and by the pressing plate of the upper end.
Further, it is provided with thrust bearing set outside the thrust bearing.
Beneficial effects of the present invention:
1, three-point mount circumference radial loaded and test device of the present invention, can realize dynamic and static separation, can simulate air-floating main shaft Static state is tested and is recorded to three direction sustained continuous reinforcings under static and current intelligence, to its week, to meet gas Floating hydrostatic spindle testing requirements;
2, load is directly applied in air bearing by apparatus of the present invention, to which loading force is loaded on tested load main shaft, Displacement, vibration and the other outer disturbances generated in loading procedure is certain by having between air bearing and tested load main shaft The air film of pressure is kept apart, and ensure that the measuring accuracy and test accuracy of tested load main shaft.
Description of the drawings
Fig. 1 is the overall structure diagram of apparatus of the present invention;
Fig. 2 is the schematic diagram of the single direction load test device of the present invention and tested load main shaft;
Fig. 3 is air bearing Internal and external cycle structural schematic diagram of the present invention;
Fig. 4 is the A-A sectional views of Fig. 3;
Fig. 5 is the B-B sectional views of Fig. 4;
In figure, 1- support bases, 2- supporting racks, 3- load test devices, 4- air bearing, 5-V shape blocks, 6- force adjustment screw rods, 7- tune Power screw sleeve, 8- thrust bearings, 9- stayed masts, 10- pulling force sensors, 11- tension springs, 12- positioning pins, 13- threadeds, 14- pressing plates, 15- thrust axis bearing sleeves, the tested load main shafts of 16-, 4-1 flow controllers, 4-2 load bearings inner rings, 4-3 loading axis Bearing outer-ring, 4-4 screw thread pin holes, 4-5 suction nozzles, 4-6 air channels, 4-7 seal grooves.
Specific implementation mode
Below by specific implementation mode combination attached drawing, invention is further described in detail.Wherein different embodiments Middle similar component uses associated similar element numbers.In the following embodiments, many datail descriptions be in order to The application is better understood.However, those skilled in the art can be without lifting an eyebrow recognize, which part feature It is dispensed, or can be substituted by other elements, material, method in varied situations.In some cases, this Shen Please it is relevant some operation there is no in the description show or describe, this is the core in order to avoid the application by mistake More descriptions are flooded, and to those skilled in the art, these relevant operations, which are described in detail, not to be necessary, they It can completely understand relevant operation according to the general technology knowledge of description and this field in specification.
Referring to the three-point mount circumference radial loaded and test device described in Fig. 1-Fig. 2, including support base 1, described The supporting rack 2 that a section is equilateral triangle is arranged in 1 upper surface of support base, and one is respectively provided in three vertex of supporting rack 2 A direction load test device 3, the front end of three direction load test devices 3 are connect with air bearing 4, worn in air bearing 4 by Test load main shaft 16, direction load test device 3 to the load of 4 vitality of air bearing and can carry out the monitoring of loading force, and three The central shaft extended line of a direction load test device 3 meets at the central axis of support frame as described above 2, fixes and sets on 2 bottom surface of supporting rack Vee-block 5 is set, vee-block 5, which is bolted, to be arranged on the bottom surface of supporting rack, and air bearing 4 is arranged in the V-shaped groove of vee-block And it is gripped by the pressing plate of the upper end 14, the central shaft of air bearing 4 and the center overlapping of axles of support frame as described above 2.
Direction load test device 3 includes force adjustment screw rod 6, force adjustment screw sleeve 7, thrust bearing 8, stayed mast 9, pulling force sensor 10 and tension spring 11;Force adjustment screw sleeve 7 is fixed at the vertex of supporting rack 2, and force adjustment screw rod 6, which is connected through a screw thread, to be worn In force adjustment screw sleeve 7, the upper end of force adjustment screw rod 7 is provided with force adjustment knob, and by rotating force adjustment knob, force adjustment screw rod 6 can be It is accurately moved forward and backward in force adjustment screw sleeve 7, the lower end of force adjustment screw rod 6 connects thrust bearing 8, thrust bearing by positioning pin 12 Thrust bearing set 15 is provided with outside 8, the lower end of thrust bearing 8 connects stayed mast 9, and thrust bearing 8 can realize force adjustment screw rod 6 and draw Dynamic and static separation of the power bar 9 during force;The lower end of stayed mast 9 connects pulling force sensor 10, the pulling force sensor 10 On be provided with real-time pulling force display screen, may be implemented real-time tensile test and display, 10 lower end of pulling force sensor connection described 11 Tension spring, 11 lower end of tension spring are connect by threaded 13 with the screw thread pin hole 4-4 of the outer wall of air bearing 4.
Referring to Fig. 3-Fig. 5, air bearing 4 is by portions such as load bearings outer ring 4-3, load bearings inner ring 4-2, flow controller 4-1 It is grouped as, tested load main shaft 16 acts on load bearings inner ring 4-2;Gas with certain steady pressure is passed through into air inlet Mouth 4-5 enters in air channel 4-6, in order to avoid in load bearings outer ring 4-3 and load bearings inner ring 4-2 gas leakage, in-between It is provided with seal groove 4-7, being sealed by painting fluid sealant prevents gas leakage;High pressure gas enters load bearings by air channel 4-6 The uniformly distributed flow controller 4-1 in the surfaces inner ring 4-2 is loaded subsequently into load bearings inner ring 4-2 and test in 16 air film gap of main shaft, The unilateral gap general warranty of air film realizes the displacement and vibration of load added by tension spring 11, and energy between 0.02-0.01mm It is enough to realize that tested load main shaft 16 realizes static and dynamic load in the air film of friction free certain pressure.
Apparatus of the present invention are loaded by adjusting the size of the loading force of three direction load test devices 3 by three directions The different synthesis modes of 3 power of tester realize quiet, dynamic circle any direction the load load of tested load main shaft 16. And the size of loading force is transferred to by pulling force sensor in computer and shows and stores.
A detection process example is described below:
Quiet, dynamic circle any direction the load load of tested load main shaft 16 is determined first.And by the big of loading force It is small to pass through static state(Tested main shaft is static)Load or dynamic(Tested main shaft rotation)Load determines tested according to test request The direction θ for loading the size F and loading force of 16 loaded load power of main shaft loads software analysis by experiment and calculates three directions The loading force F of the tension spring 11 of load test device 31、F2、F3;It is 0.4MPa-0.7MPa's to be passed through pressure value to air bearing 4 Stabilizing gas makes the load of three pulling force sensors 10 respectively by rotating the force adjustment screw rod 6 of three direction load test devices 3 Value is adjusted to F in sequence1、F2、F3, reach big according to load in any direction of required resultant force to tested load main shaft 16 The continuous load of small needs, and real-time display and storage are carried out to load;The load of tested load main shaft 16 is loaded and is completed Afterwards, according to the motion state of tested load main shaft 16, in the size F of the loaded load power and direction θ of loading force Carry out test and the record of other correlation test data of tested load main shaft 16.
Present disclosure is not limited to cited by embodiment, and those of ordinary skill in the art are by reading description of the invention And to any equivalent transformation that technical solution of the present invention is taken, it is that claim of the invention is covered.

Claims (6)

1. three-point mount formula circumference radial loaded and test device, which is characterized in that including support base(1), in the support Pedestal(1)The supporting rack that a section is equilateral triangle is arranged in upper surface(2), in support frame as described above(2)Three vertex it is equal One direction load test device is set(3), three direction load test devices(3)Front end and air bearing(4)Connection, it is empty Gas bearing(4)Inside wear tested load main shaft(16), the direction load test device(3)It can be to air bearing(4)Vitality Load and carry out the monitoring of loading force, three direction load test devices(3)Central shaft extended line meet at the support Frame(2)Central axis, support frame as described above(2)Vee-block is fixedly installed on bottom surface(5), air bearing(4)Pass through the vee-block (5)It is arranged in supporting rack(2)It is interior, the air bearing(4)Central shaft and support frame as described above(2)Center overlapping of axles.
2. the apparatus according to claim 1, which is characterized in that the direction load test device(3)Including force adjustment screw rod (6), force adjustment screw sleeve(7), thrust bearing(8), stayed mast(9), pulling force sensor(10)And tension spring(11);The force adjustment Screw sleeve(7)It is fixed at support frame as described above(2)Vertex, force adjustment screw rod(6)It is connected through a screw thread and is threaded through force adjustment spiral shell Rod set(7)It is interior, the force adjustment screw rod(6)Lower end pass through positioning pin(12)Connect the thrust bearing(8), the thrust bearing (8)Lower end connect the stayed mast(9), the stayed mast(9)Lower end connect the pulling force sensor(10), the pulling force Sensor(10)Described in the connection of lower end(11)Tension spring, the tension spring(11)Lower end passes through threaded(13)With the sky Gas bearing(4)Outer wall connection.
3. the three-point mount formula circumference radial loaded and test device of air supporting hydrostatic spindle according to claim 1 or 2, It is characterized in that, the force adjustment screw rod(7)Upper end be provided with force adjustment knob.
4. device according to claim 3, which is characterized in that the pulling force sensor(10)On to be provided with real-time pulling force aobvious Display screen.
5. device according to claim 4, which is characterized in that the vee-block(5)It is bolted and is arranged in supporting rack Bottom surface on, air bearing(4)The pressing plate for being arranged in the V-shaped groove of vee-block and passing through the upper end(14)It grips.
6. device according to claim 5, which is characterized in that the thrust bearing(8)It is provided with thrust bearing set outside (15).
CN201810092760.8A 2018-01-31 2018-01-31 Three-point mount formula circumference radial loaded and test device Pending CN108303256A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810092760.8A CN108303256A (en) 2018-01-31 2018-01-31 Three-point mount formula circumference radial loaded and test device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810092760.8A CN108303256A (en) 2018-01-31 2018-01-31 Three-point mount formula circumference radial loaded and test device

Publications (1)

Publication Number Publication Date
CN108303256A true CN108303256A (en) 2018-07-20

Family

ID=62867139

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810092760.8A Pending CN108303256A (en) 2018-01-31 2018-01-31 Three-point mount formula circumference radial loaded and test device

Country Status (1)

Country Link
CN (1) CN108303256A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110017987A (en) * 2019-04-09 2019-07-16 深圳市骁阳工程咨询有限公司 High speed roller bearing testing stand
CN110108404A (en) * 2019-02-11 2019-08-09 哈尔滨工业大学 A kind of shaft-radial force test device of bearing
WO2020073578A1 (en) * 2018-10-10 2020-04-16 中国矿业大学 Device for testing bearing performance of vertical shaft lifting spindle device
CN111238811A (en) * 2020-01-17 2020-06-05 人本集团有限公司 Detection device for detecting radial bearing capacity of roller bearing
CN114838678A (en) * 2022-07-04 2022-08-02 河北亿泰克轴承有限公司 Pneumatic measuring device for outer diameter of thin-wall bearing ring
CN114877828A (en) * 2022-06-14 2022-08-09 中国航天标准化研究所 Testing machine and testing method for testing aerospace bearing

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06213771A (en) * 1993-01-13 1994-08-05 Sugawara Kenkyusho:Kk Radial loader for measuring vibration/sound of rolling bearing
CN201152812Y (en) * 2008-01-02 2008-11-19 西安工业大学 Radial directional hydrodynamic-hydrostatic gas bearing experiment bench
CN202770631U (en) * 2012-09-25 2013-03-06 上海大学 Radial sliding bearing static load loading device
CN103115774A (en) * 2013-01-21 2013-05-22 中国航天科技集团公司第五研究院第五一〇研究所 Axial and radial combined loading bearing test device
CN103543013A (en) * 2013-10-17 2014-01-29 华中科技大学 Static-pressure axial-radial loading mechanism
CN207881939U (en) * 2018-01-31 2018-09-18 西安工业大学 A kind of circumferentially fixed loading test device of air supporting hydrostatic spindle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06213771A (en) * 1993-01-13 1994-08-05 Sugawara Kenkyusho:Kk Radial loader for measuring vibration/sound of rolling bearing
CN201152812Y (en) * 2008-01-02 2008-11-19 西安工业大学 Radial directional hydrodynamic-hydrostatic gas bearing experiment bench
CN202770631U (en) * 2012-09-25 2013-03-06 上海大学 Radial sliding bearing static load loading device
CN103115774A (en) * 2013-01-21 2013-05-22 中国航天科技集团公司第五研究院第五一〇研究所 Axial and radial combined loading bearing test device
CN103543013A (en) * 2013-10-17 2014-01-29 华中科技大学 Static-pressure axial-radial loading mechanism
CN207881939U (en) * 2018-01-31 2018-09-18 西安工业大学 A kind of circumferentially fixed loading test device of air supporting hydrostatic spindle

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
张君安等: "气体动静压径向轴承试验台研制及实现" *
魏明明等: "空气动静压径向轴承实验台加载装置误差分析" *

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020073578A1 (en) * 2018-10-10 2020-04-16 中国矿业大学 Device for testing bearing performance of vertical shaft lifting spindle device
CN110108404A (en) * 2019-02-11 2019-08-09 哈尔滨工业大学 A kind of shaft-radial force test device of bearing
CN110108404B (en) * 2019-02-11 2021-07-20 哈尔滨工业大学 Axial-radial force testing device for bearing
CN110017987A (en) * 2019-04-09 2019-07-16 深圳市骁阳工程咨询有限公司 High speed roller bearing testing stand
CN110017987B (en) * 2019-04-09 2022-04-12 深圳市骁阳工程咨询有限公司 High-speed rolling bearing test bed
CN111238811A (en) * 2020-01-17 2020-06-05 人本集团有限公司 Detection device for detecting radial bearing capacity of roller bearing
CN114877828A (en) * 2022-06-14 2022-08-09 中国航天标准化研究所 Testing machine and testing method for testing aerospace bearing
CN114877828B (en) * 2022-06-14 2023-12-05 中国航天标准化研究所 Testing machine and testing method for space bearing test
CN114838678A (en) * 2022-07-04 2022-08-02 河北亿泰克轴承有限公司 Pneumatic measuring device for outer diameter of thin-wall bearing ring
CN114838678B (en) * 2022-07-04 2022-09-02 河北亿泰克轴承有限公司 Pneumatic measuring device for outer diameter of thin-wall bearing ring

Similar Documents

Publication Publication Date Title
CN108303256A (en) Three-point mount formula circumference radial loaded and test device
CN207881939U (en) A kind of circumferentially fixed loading test device of air supporting hydrostatic spindle
CN108426712A (en) Wholecircle circumferentially slides radial test and loading device
CN108627344B (en) Device and method for detecting performance of air floatation ball bearing
US20220056954A1 (en) Split-type swing angle adjustable aerostatic bearing device for rotor static balance, and air flotation support device for static balance of rotating ring-shaped parts
CN104880308B (en) A kind of main shaft axial force isostatic pressed loading device
CN106404400B (en) A kind of monoblock type high rigidity gas thrust bearing dynamic performance testing experimental bench
Wang et al. Study on the dynamic and static characteristics of gas static thrust bearing with micro-hole restrictors
CN105424361B (en) A kind of liquid closed type static pressure turntable experimental provision of modifiable flow controller
CN205748914U (en) Bearing rotary torsional moment test device
GB2417564A (en) Determining angular and radial position of a rotor
CN207881946U (en) A kind of circumferential sliding loading test device of air supporting hydrostatic spindle
CN107478365A (en) A kind of ultrasound electric machine power measurement arrangement for loading continuously adjustabe
CN101839791A (en) Uncompleted spherical superconducting rotor air floatation balance measurement method
CN105865787A (en) Dynamic performance tester for high-speed precise bearings
CN110823573A (en) Foil gas bearing comprehensive experiment table device and experiment method
CN106441898B (en) A kind of test device of rolling bearing rotating accuracy
CN106248482A (en) A kind of Triaxial tester being applicable to soft rock and method
CN105547923B (en) A kind of double pulling force source formula magnetorheological fluid yield stress measuring systems
CN206339381U (en) A kind of axial rigidity measurement apparatus of aerostatic bearing
CN111426599B (en) Dynamic diamagnetic suspension multi-dimensional density measuring device and method
CN206074254U (en) A kind of device for testing dynamic stiffness of ball-screw
CN106950137A (en) Tangential fretting abrasion test device and test method
CN104535312B (en) Environmental simulation testing device for magnetic liquid dynamic sealing components
GB2612437A (en) Aging test device for multiple batteries in extruded state and test method

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