CN105675276B - A kind of elastic bearing squeeze film damper damping behavior experimental rig - Google Patents

A kind of elastic bearing squeeze film damper damping behavior experimental rig Download PDF

Info

Publication number
CN105675276B
CN105675276B CN201610020546.2A CN201610020546A CN105675276B CN 105675276 B CN105675276 B CN 105675276B CN 201610020546 A CN201610020546 A CN 201610020546A CN 105675276 B CN105675276 B CN 105675276B
Authority
CN
China
Prior art keywords
squeeze film
exciting
force
elastic bearing
film damper
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
CN201610020546.2A
Other languages
Chinese (zh)
Other versions
CN105675276A (en
Inventor
边杰
李彦
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.)
Hunan Aviation Powerplant Research Institute AECC
Original Assignee
China Aircraft Power Machinery Institute
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 China Aircraft Power Machinery Institute filed Critical China Aircraft Power Machinery Institute
Priority to CN201610020546.2A priority Critical patent/CN105675276B/en
Publication of CN105675276A publication Critical patent/CN105675276A/en
Application granted granted Critical
Publication of CN105675276B publication Critical patent/CN105675276B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Support Of The Bearing (AREA)

Abstract

The present invention discloses a kind of elastic bearing squeeze film damper damping behavior experimental rig, and elastic bearing squeeze film damper damping behavior experimental rig includes mounting base, resilient support, squeeze film outer shroud, loaded ring, exciting simulation mechanism and control mechanism.Resilient support includes ontology and bearing block;Squeeze film outer shroud is fixed on mounting base and is set around the periphery of bearing block;One end of loaded ring is sheathed on the inside of bearing block, and loaded ring can be rotated relative to bearing block;Exciting simulation mechanism includes vibrator, exciting rod, force snesor and acceleration transducer.Wherein, under the action of vibrator, exciting rod applies exciting force to loaded ring, so that bearing block generates vibration, it can receive the exciting force signal that force snesor sends out and the vibration response signal that acceleration transducer is sent out to dynamic signal analyzer, and obtain the vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force.

Description

A kind of elastic bearing squeeze film damper damping behavior experimental rig
Technical field
This invention relates generally to elastic bearing squeeze film damper, in particular to aeroengine rotor The damping behavior experiment of elastic bearing squeeze film damper.
Background technology
Elastic bearing squeeze film damper is had been widely used in Small Aeroengine rotor-bearing system. In the course of work, it can effectively absorb rotor vibrational energy caused by unbalance residual content, be substantially reduced the vibration of rotor Displacement and reduce bearing load, improve engine job stability and reliability and extend bearing working life.
Research to elastic bearing squeeze film damper damping behavior, it is domestic to be mainly partial to Analysis on Mechanism, conventional number Learn the foundation and correlation theory derivation, algorithm research or improvement and some confirmatory experimental studies of mechanical model.In theory In analysis, the Reynolds equation based on ideal viscous fluid basic assumption is generally employed at present as squeeze film damper power The fundamental analysis theory of characteristic.In fact, the operation principle, operating condition and motion state equal ten due to squeeze film damper Point complexity, therefore assume by Reynolds equation is related to some merely, it is difficult to comprehensively it is accurate with truly describe squeeze film and hinder Buddhist nun's device possessed dynamic characteristics during the work time.On verification experimental verification, generally formed at present using rotor and damping support Rotation test device implement the analysis of experiments to elastic bearing squeeze film damper dynamic characteristics.Due to testing process master What is reflected is the comprehensive dynamic characteristic of " rotor-bearing system ", it is difficult to therefrom extract elastic bearing squeeze film damper sheet The dynamic characteristics ingredient of body fully and targetedly investigate and analyze relatively.Therefore, result of the test has often been not enough to Disclose the complicated characteristics of motion of elastic bearing squeeze film damping in effect ground, it is impossible to which elastic bearing squeeze film damper is changed More targetedly instruction is provided into design.
In addition, the existing experimental rig for elastic bearing squeeze film damper, there are fluid during experiment The problems such as splashing, oil film pressure is too small, experimental enviroment is very severe, can not only be stained test apparatus and equipment, can also be to experiment The physical and mental health of personnel brings adverse effect.
At present, rarely has the report of the experimental rig for elastic bearing squeeze film damper, the experiment dress having been reported It is complicated to install meter, operating difficulties.
Above- mentioned information is only used for strengthening the understanding of the background to the present invention, therefore it disclosed in the background technology part It can include not forming the information to the prior art known to persons of ordinary skill in the art.
Invention content
A primary object of the present invention is to overcome at least one defect of the above-mentioned prior art, provides a kind of bullet Property bearing squeeze film damper damping behavior experimental rig and method, design simple and effective, convenient for disassembly and assembly, reliable operation, The vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force can be obtained.
For achieving the above object, the present invention adopts the following technical scheme that:
According to an aspect of the invention, there is provided a kind of elastic bearing squeeze film damper damping behavior experiment dress It puts, including mounting base, resilient support, squeeze film outer shroud, loaded ring, exciting simulation mechanism and control mechanism.
Resilient support includes ontology and bearing block, and ontology is fixed in mounting base, and bearing block is fixedly connected simultaneously certainly with ontology The side of ontology protrudes;Squeeze film outer shroud be fixed on mounting base and around bearing block periphery set, squeeze film outer shroud with There are gap between bearing block, open up oil supplying hole on squeeze film outer shroud, connected with gap, lubricating oil can via oil supplying hole into Enter in gap;One end of loaded ring is sheathed on the inside of bearing block, and loaded ring can be rotated relative to bearing block;Exciting analog machine Structure includes vibrator, exciting rod, force snesor and acceleration transducer, and one end of exciting rod is connect with vibrator, exciting rod The other end of the other end and loaded ring connects, and force snesor is fixed on exciting rod, and acceleration transducer is set to loaded ring On the other end, acceleration transducer is located at exciting rod institute on straight line, and is oppositely arranged with exciting rod;Control mechanism includes dynamic Signal analyzer.
Wherein, under the action of vibrator, exciting rod applies exciting force to loaded ring so that bearing block generates vibration, moves State signal analyzer its can receive the exciting force signal that force snesor sends out and the vibratory response letter that acceleration transducer is sent out Number, and obtain the vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force.
According to an aspect of the invention, there is provided a kind of elastic bearing squeeze film damper damping behavior experiment side Method is carried out using above-mentioned elastic bearing squeeze film damper damping behavior experimental rig, included the following steps:
Exciting force is applied to loaded ring with vibrator so that bearing block generates vibration;
Exciting force is sensed by force snesor and is responded by acceleration transducer sense vibrations;And
What the exciting force signal and acceleration transducer sent out by dynamic signal analyzer reception force snesor was sent out shakes Sound of something astir induction signal, and obtain the vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force.
As shown from the above technical solution, the advantages and positive effects of the present invention are:It is filled using experiment of the present invention It puts, carries out the experiment of certain h type engine h elastic bearing squeeze film damper damping behavior, obtain the resistance of elastic bearing squeeze film The related dynamic characteristics data such as Buddhist nun's device and elastic supporting rigidity, oil clearance, lubricating oil pressure, oil viscosity and start into The percent value of elastic support shaft bearing outer wall amplitude and oil clearance when entering inelastic region, hinders elastic bearing squeeze film Application of Buddhist nun's device in aero-engine development has important references value.Also, the present invention experimental rig design it is simple and effective, Convenient for disassembly and assembly, reliable operation, can carry out more physical parameters of elastic bearing squeeze film damper influences to advise on its damping behavior The experimental study of rule.
Description of the drawings
Consider following the following detailed description of the embodiment of the present invention in conjunction with the accompanying drawings, various targets of the invention, Feature and advantage will become apparent.Attached drawing is only the exemplary diagram of the present invention, is not necessarily drawn to scale. In the accompanying drawings, same reference numeral always shows same or similar component.Wherein:
Fig. 1 is a kind of elastic bearing squeeze film damper damping behavior experiment according to an illustrative embodiments System block diagram;
Fig. 2 is a kind of elastic bearing squeeze film damper damping behavior experiment according to an illustrative embodiments The overall structure figure of device;
Fig. 3 is along the transverse sectional view of line A-A in Fig. 2;
Fig. 4 is along the transverse sectional view of line B-B in Fig. 2;And
Fig. 5 is the partial enlarged view in C lines in Fig. 3.
Specific embodiment
Example embodiment is described more fully with reference to the drawings.However, example embodiment can be with a variety of shapes Formula is implemented, and is not understood as limited to embodiment set forth herein;On the contrary, these embodiments are provided so that the present invention will Fully and completely, and by the design of example embodiment comprehensively it is communicated to those skilled in the art.Identical attached drawing in figure Label represents same or similar structure, thus will omit their detailed description.
Described feature, structure or characteristic can be incorporated in one or more embodiments in any suitable manner In.In the following description, many details are provided to fully understand embodiments of the present invention so as to provide.However, It will be appreciated by persons skilled in the art that technical scheme of the present invention can be put into practice without one in the specific detail or more It is more or other methods, component, material etc. may be used.In other cases, be not shown in detail or describe known features, Material or operation are to avoid fuzzy each aspect of the present invention.
As shown in Figures 1 to 5, the present invention provides a kind of elastic bearing squeeze film damper damping behavior experimental rig, Including mounting base 10, resilient support 20, squeeze film outer shroud 30, loaded ring 40, exciting simulation mechanism and control mechanism.
Resilient support 20 includes ontology 21 and bearing block 22, and ontology 21 is fixed in mounting base 10, bearing block 22 and ontology 21 are fixedly connected and are protruded from the side of ontology 21.Squeeze film outer shroud 30 is fixed on mounting base 10 and around the outer of bearing block 22 There are gap between squeeze film outer shroud 30 and bearing block 22, oil supplying hole 31 is opened up on squeeze film outer shroud 30 for week setting, with Gap connects, and lubricating oil can enter via oil supplying hole 31 in gap.One end of loaded ring 40 is sheathed on the inside of bearing block 22, adds Carrying ring 40 can rotate relative to bearing block 22.Exciting simulation mechanism includes vibrator (not shown), exciting rod 51, force snesor 52 and acceleration transducer 53, one end of exciting rod 51 connect with vibrator, the other end of exciting rod 51 is another with loaded ring 40 One end connects, and force snesor 52 is fixed on exciting rod 51, and acceleration transducer 53 is set on the other end of loaded ring 40, is added Velocity sensor 53 is located at 51 institute of exciting rod on straight line, and is oppositely arranged with exciting rod 51.Control mechanism includes Dynamic Signal Analyzer.
Wherein, under the action of vibrator, exciting rod 51 applies exciting force to loaded ring 40 so that the generation of bearing block 21 is shaken It is dynamic, dynamic signal analyzer its can receive exciting force signal that force snesor 52 sends out and what acceleration transducer 53 was sent out shakes Sound of something astir induction signal, and obtain the vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force.
The elastic bearing squeeze film damper damping behavior experimental rig of the present invention is to install existing resilient support In in mounting base, false bearings are simulated with loaded ring, vibrator generates the bearing block of sine excitation power excitation elastic bearing, so as to mould Intend the load applied during rotor rotation to elastic bearing squeeze film damper.When the bearing block of elastic bearing generate it is circumferential into When dynamic, typical squeeze film is formed between squeeze film outer shroud.Elastic bearing squeeze film is measured by acceleration transducer Vibratory response of the damper under vibrator excitation.
Using experimental rig of the present invention, certain h type engine h elastic bearing squeeze film damper damping behavior is carried out Experiment, obtains elastic bearing squeeze film damper and elastic supporting rigidity, oil clearance, lubricating oil pressure, oil viscosity etc. Related dynamic characteristics data and elastic support shaft bearing outer wall amplitude when initially entering inelastic region and oil clearance Percent value has important references value to application of the elastic bearing squeeze film damper in aero-engine development.Also, The experimental rig of the present invention designs simple and effective, convenient for disassembly and assembly, reliable operation, can carry out elastic bearing squeeze film damper Experimental study of more physical parameters to its damping behavior affecting laws.
In the present embodiment, the ontology 21 of elastic bearing is fixed on by 8 stove bolts 23 and small nut 24 in mounting base 10, The outer wall of the bearing block 22 of elastic bearing is towards squeeze film outer shroud 30, and there are small―gap sutures therebetween.Squeeze film outer shroud 30 Upper and lower end face for plane, squeeze film outer shroud 30 is connected by 6 king-bolts 32 with mounting base 10.However, above structure Connection mode is without being limited thereto.
30 inner wall of squeeze film outer shroud is provided with oil groove 33 and two seal grooves 34, and two seal grooves 34 are located at oil groove 33 Both sides.The lubricating oil of oil pump (not shown) supply is delivered to oil supplying hole 31 through fuel feed pump 35, subsequently into oil groove 33, and then It is covered with entire squeeze film chamber D.Sealing ring 36 is equipped in two seal grooves 34, sealing ring 36 and the outer wall of bearing block 21 are close Cooperation, plays sealing function, so that the lubricating oil with certain pressure will not be revealed from the both ends of squeeze film chamber, both favorably In the foundation of squeeze film pressure, while it is also ensured that good test environment and the comfort of tester's operation.
Common exciting force can be analyzed to two orthogonal power, and therefore, in the present embodiment, there is provided two sets of exciting moulds Intend mechanism, the two angle is 90 °, and the same frequency of two vibrators generations, the sine excitation power of 90 ° of phase difference then can synchronization motivationtheories The bearing block 22 of elastic bearing, so as to the load applied during model rotor rotation to elastic bearing squeeze film damper.
Wherein, two sets of exciting simulation mechanisms is are symmetrical arranged relative to elastic bearing, in two orthogonal excitation cycles Under power effect, the vibratory response of the bearing block outer wall of elastic bearing, acceleration transducer measures its corresponding vibratory response respectively, Vibratory response accesses dynamic signal analyzer together with the mutually perpendicular exciting force of both direction.At further analysis Reason, can obtain the relation curve between the vibratory response of elastic bearing squeeze film damper and exciting force.
In the present embodiment, each exciting simulation mechanism further includes force-transmitting seat 54, and the other end of exciting rod 51 passes through power transmission spiral shell Bolt 55 and locking nut 56 are connect with force-transmitting seat 54, and the both ends of force-transmitting seat 54 are fixed on by hold-down bolt 57 on loaded ring 40.
Wherein, one end of loaded ring 40 is annular, and the other end of loaded ring 40 is rectangular, and force-transmitting seat 54 is arch, power transmission The both ends of seat 54 and the other end of loaded ring 40 are fixed.
As shown in Figure 1, in the present embodiment, control mechanism may also include signal generator, power amplifier and controller, letter Number generator is capable of the frequency and amplitude of the exciting force of adjusting vibration exciter, and power amplifier is capable of the power of adjusting vibration exciter, controls Device processed is used to control vibrator.It can be with the big of the out-of-balance force in model rotor real work by the size for changing exciting force Different rotating speeds small, that the frequency for changing exciting force can be in model rotor real work.Further, different bullets can also be studied The parameters such as property support stiffness, oil clearance, oil viscosity, lubricating oil pressure are to elastic bearing squeeze film damper damping behavior It influences to get to the damping behavior of elastic bearing squeeze film damper.
Specially:It is identical with amplitude, 90 ° of phase difference that HIOKI-7075 double-channel signals generator generates two frequencies Sinusoidal signal.This two-way sinusoidal signal controls two B&K-4826 respectively after the amplification of B&K-2721 single channels power amplifier The output parameter of vibrator makes it generate amplitude and the controllable equivalent rotary exciting force of frequency.Exciting force is through two BISE5110 After dynamic force sensor measuring, it is loaded on elastic bearing squeeze film damper.Two B&K-4382V acceleration transducers are surveyed The elastic bearing squeeze film damper vibratory response of amount, through B&K-2692-0S4 four-ways charge amplifier amplification after and two BISE5110 force sensor measurings through the amplified exciting force signal of SK6881 single channel charge amplifiers, access together DEWE-3021 dynamic signal analyzers.At Dewesoft6.6.7 Dynamic Signals record and analysis software further analysis Reason can obtain the relation curve of the vibratory response of elastic bearing squeeze film damper and exciting force and it is firm with elastic bearing The changing rule of the parameters such as degree, oil clearance, oil viscosity, lubricating oil pressure is to get to elastic bearing squeeze film damper Damping behavior.
In in one embodiment, elastic bearing squeeze film damper damping behavior test method is:It is mutual using direction 90 ° of 2 vibrator same frequencys vertically, phase difference excitations are carried out with obtaining rotation field of force exciting in the range of (10-1000) Hz Sweep and vibration is tested.During experiment, the root vibration strains of orthogonal two springs on subject elastic bearing are measured Amount measures the exciting force of exciting rod on this two direction;Measure the acceleration on orthogonal two direction of elastic support shaft bearing Value measures output power and its frequency (being equivalent to speed-frequency) of vibrator etc., the numbers such as record oil viscosity, lubricating oil pressure According to.
Change elastic supporting rigidity, oil clearance, oil viscosity and lubricating oil pressure etc. by design value and carry out above-mentioned experiment. Suitable elastic supporting rigidity, oil clearance, oil viscosity and lubricating oil pressure are selected, classification changes exciting force size, obtains bullet Property bearing strain and amplitude relation curve, find the percent value of the amplitude and oil clearance when initially entering inelastic region, Obtain the damping behavior of elastic bearing squeeze film damper.
Above in relation to elastic bearing squeeze film damper damping behavior experimental rig, only by taking the device as an example, say The specific design and implementation process of the bright present invention, it is not limited to the concrete structure of experimental rig.For those skilled in the art For member, the invention may be variously modified and varied.Any modification for all within the spirits and principles of the present invention, being made, Equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Although exemplary embodiment describing the present invention with reference to several, it is to be understood that, term used is explanation and shows Example property, term and not restrictive.The spirit or reality that can be embodied in a variety of forms without departing from invention due to the present invention Matter, it should therefore be appreciated that above-described embodiment is not limited to any aforementioned details, and should be in the spirit that appended claims are limited With widely explained in range, therefore the whole variations fallen into claim or its equivalent scope and remodeling all should be accompanying power Profit requirement is covered.

Claims (7)

1. a kind of elastic bearing squeeze film damper damping behavior experimental rig, including:
Mounting base;
Resilient support, including ontology and bearing block, ontology is fixed in mounting base, and bearing block is fixedly connected with ontology and from originally The side of body protrudes;
Squeeze film outer shroud is fixed on mounting base and is set around the periphery of bearing block, squeeze film outer shroud and bearing block it Between there are gap, squeeze film outer shroud inner wall is provided with oil groove and two seal grooves, and two seal grooves are located at the both sides of oil groove, Squeeze film outer shroud upper surface opens up oil supplying hole, is connected with oil groove, between lubricating oil can enter via oil supplying hole and oil groove In gap, sealing ring, the outer wall tight fit of sealing ring and bearing block are equipped in two seal grooves;
Loaded ring, one end are sheathed on the inside of bearing block;
Exciting simulation mechanism, including vibrator, exciting rod, force snesor, force-transmitting seat and acceleration transducer, one end of exciting rod It is connect with vibrator, the other end of exciting rod is connected by the other end of force-transmitting seat and loaded ring, and force snesor is fixed on exciting On bar, acceleration transducer is set on the other end of loaded ring, and acceleration transducer is located at exciting rod institute on straight line, and with Exciting rod is oppositely arranged;And
Control mechanism, including dynamic signal analyzer;
Wherein, under the action of vibrator, exciting rod applies exciting force to loaded ring so that bearing block generates vibration, and dynamic is believed It can receive the exciting force signal that force snesor sends out and the vibration response signal that acceleration transducer is sent out for number analyzer, and Obtain the vibratory response of elastic bearing squeeze film damper and the relation curve of exciting force.
2. elastic bearing squeeze film damper damping behavior experimental rig as described in claim 1, wherein, outside squeeze film The oil supplying hole that ring upper surface opens up directly connects oil groove, and lubricating oil is delivered to oil supplying hole through fuel feed pump, and into oil groove, is formed Squeeze film chamber with certain pressure.
3. elastic bearing squeeze film damper damping behavior experimental rig as claimed in claim 2, wherein, exciting analog machine The quantity of structure is two sets, and the angle of two sets of exciting simulation mechanisms is 90 °, and the vibrator of two sets of exciting simulation mechanisms generates together The exciting force of 90 ° of frequency and phase difference.
4. elastic bearing squeeze film damper damping behavior experimental rig as claimed in claim 3, wherein, each exciting mould Intend mechanism and further include force-transmitting seat, the other end of exciting rod is connect by power transmission bolt and lock nut with force-transmitting seat, force-transmitting seat Both ends are fixed on by hold-down bolt on loaded ring.
5. elastic bearing squeeze film damper damping behavior experimental rig as claimed in claim 4, wherein, force-transmitting seat is bow Shape, the both ends of force-transmitting seat and the other end of loaded ring are fixed.
6. elastic bearing squeeze film damper damping behavior experimental rig as described in claim 1, wherein, control mechanism is also Including signal generator, power amplifier and controller, signal generator is capable of the frequency and amplitude of adjusting vibration exciter, and power is put Big device is capable of the power of adjusting vibration exciter, and controller is used to control vibrator.
7. elastic bearing squeeze film damper damping behavior experimental rig as described in claim 1, wherein, elastic bearing squeezes The parameter of film damper is pressed to include elastic supporting rigidity, oil clearance, oil viscosity and lubricating oil pressure.
CN201610020546.2A 2016-01-13 2016-01-13 A kind of elastic bearing squeeze film damper damping behavior experimental rig Active CN105675276B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610020546.2A CN105675276B (en) 2016-01-13 2016-01-13 A kind of elastic bearing squeeze film damper damping behavior experimental rig

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610020546.2A CN105675276B (en) 2016-01-13 2016-01-13 A kind of elastic bearing squeeze film damper damping behavior experimental rig

Publications (2)

Publication Number Publication Date
CN105675276A CN105675276A (en) 2016-06-15
CN105675276B true CN105675276B (en) 2018-07-10

Family

ID=56300323

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610020546.2A Active CN105675276B (en) 2016-01-13 2016-01-13 A kind of elastic bearing squeeze film damper damping behavior experimental rig

Country Status (1)

Country Link
CN (1) CN105675276B (en)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106353076A (en) * 2016-07-07 2017-01-25 大连海事大学 Tester for determining dynamic characteristic coefficient of squeeze film damper
CN106289645B (en) * 2016-11-07 2020-05-01 北京东方振动和噪声技术研究所 Rotor dynamic balance measuring method and device based on steady state excitation method
CN106768986B (en) * 2017-02-22 2018-10-02 大连海事大学 Fluid film lubrication damping test platform
CN106907355B (en) * 2017-04-28 2019-03-05 中国航发湖南动力机械研究所 A kind of elastic bearing squeeze film damper
CN106989917A (en) * 2017-06-01 2017-07-28 中国航发湖南动力机械研究所 Flexibly support the dynamic stiffness measurement device and its measuring method of squeeze film damper
CN108279119B (en) * 2017-12-28 2019-05-21 华中科技大学 A kind of squeeze film damper performance test apparatus of Parameter adjustable
CN108303241B (en) * 2017-12-28 2019-09-27 西安理工大学 A kind of modularization oil-film damping test device and method
FR3087686B1 (en) * 2018-10-31 2020-12-11 Safran Aircraft Engines TOOLS FOR BALANCING A TURBOMACHINE MODULE INCLUDING AN OVERHEAD STATOR
CN109752171B (en) * 2018-12-17 2020-07-28 南京航空航天大学 Bidirectional excitation tester for measuring inner layer oil pressure of floating ring type squeeze film damper
CN109764088B (en) * 2019-01-09 2019-11-08 东南大学 A kind of squeeze film thickness adjusting apparatus
CN109708802B (en) * 2019-02-22 2020-06-30 大连交通大学 Distributed pressure test device and test method for squeeze film damper
CN110261126A (en) * 2019-06-24 2019-09-20 中国航发动力股份有限公司 A kind of gas turbine squeeze film damper gap loads measuring device
CN110553847B (en) * 2019-09-25 2024-07-12 泸州卓远液压有限公司 Buoyancy type thrust adapter
CN112798396B (en) * 2019-10-28 2024-04-02 中国石油化工股份有限公司 Stroke adjusting mechanism and reciprocating test machine with same
CN111397908A (en) * 2020-03-24 2020-07-10 西安航空职业技术学院 Parameter-adjustable performance test device for squeeze film damper
CN113950937B (en) * 2021-09-24 2023-08-18 江苏大学 Threshing cylinder vibration monitoring and slowing system and method and combine harvester
CN114112256B (en) * 2021-10-20 2023-06-13 中国航发四川燃气涡轮研究院 Exciting device and exciting method for rotor dynamics test
CN113984365B (en) * 2021-11-02 2024-06-18 哈尔滨工业大学 Novel extrusion oil film damper dynamic coefficient measurement device
CN114001957B (en) * 2021-11-04 2024-03-29 沈阳智振科技有限公司 Vertical bearing testing machine
CN114414225B (en) * 2021-12-28 2024-01-16 西北工业大学 Device for testing dynamic characteristics of elastic ring type extrusion oil film damper
CN115165276B (en) * 2022-07-25 2024-07-23 中国人民解放军海军工程大学 Vibration isolation element dynamic characteristic testing device and testing method thereof
CN115855356B (en) * 2022-11-24 2024-04-02 中国核动力研究设计院 Experimental device and method for measuring force of supporting cylinder extrusion film
CN116127629B (en) * 2022-12-16 2023-11-28 中国核动力研究设计院 Calculation method and system for small-gap structure extrusion film force based on magnitude analysis
CN116840195A (en) * 2023-05-18 2023-10-03 中国船舶集团有限公司第七〇三研究所 Dynamic transmittance test device for sealing ring of extrusion oil film damper based on machine vision
CN117629873B (en) * 2023-12-19 2024-07-26 深圳大学 Soil body resonance column test device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1657800A (en) * 2004-12-03 2005-08-24 西北工业大学 Method and device for suppression of vibration of rotor system with elastic support
CN102425639A (en) * 2011-11-30 2012-04-25 中国航空动力机械研究所 Elastic supporting structure

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009270612A (en) * 2008-05-07 2009-11-19 Toyota Motor Corp Bearing structure of turbocharger

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1657800A (en) * 2004-12-03 2005-08-24 西北工业大学 Method and device for suppression of vibration of rotor system with elastic support
CN102425639A (en) * 2011-11-30 2012-04-25 中国航空动力机械研究所 Elastic supporting structure

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
弹支挤压油膜阻尼器动力特性分析方法研究;陈钊;《中国优秀硕士学位论文全文数据库工程科技II辑》;20090615(第4期);第三章挤压油膜阻尼器实验台设计以及第四章挤压油膜阻尼器动力特性试验,图3.1-3.10 *

Also Published As

Publication number Publication date
CN105675276A (en) 2016-06-15

Similar Documents

Publication Publication Date Title
CN105675276B (en) A kind of elastic bearing squeeze film damper damping behavior experimental rig
CN105910780A (en) Accurate controllable non-contact test piece rotary magnetic field fatigue excitation and vibration test device
CN102928222B (en) Method for testing and identifying dynamic characteristic coefficients of sliding bearing
CN106989917A (en) Flexibly support the dynamic stiffness measurement device and its measuring method of squeeze film damper
Varney et al. Crack detection in a rotor dynamic system by vibration monitoring—Part II: Extended analysis and experimental results
Kumar et al. Condition monitoring of rotating machinery through vibration analysis
Babu et al. A review on application of dynamic parameters of journal bearing for vibration and condition monitoring
Liu et al. Engine misfire diagnosis based on the torsional vibration of the flexible coupling in a diesel generator set: simulation and experiment
CN108279119A (en) A kind of squeeze film damper performance test apparatus of Parameter adjustable
CN103292958B (en) A kind of rotor based on model is without test mass unbalance parameter discrimination method
Li et al. Experimental and numerical investigations on an unbalance identification method for full-size rotor system based on scaled model
Satyanarayana et al. Investigation of the stresses induced in crank shaft AISI E4340 forged steel
Cheng et al. Non-linear dynamics of a rotor-bearing-seal system
Machorro-López et al. Identification of damaged shafts using active sensing—simulation and experimentation
Iacobellis et al. Experimental investigation of the effects of squeeze film damper design on highspeed rotor system
CN106768986A (en) Fluid film lubrication damping test platform
CN104483067A (en) Measuring method of dynamic unbalance amount of fan
Alsaleh et al. Analysis of the lateral vibrations of an unbalanced Jeffcott rotor
Han et al. Parameter identifications for a rotor system based on its finite element model and with varying speeds
Mohammad et al. Negative Potential Energy Content Analysis in Cracked Rotors Whirl Response
Zhang et al. Experimental identification of fluid-induced force in labyrinth seals
Bielawski Measurement and evaluation of mechanical vibration of reciprocating machines
Subbiah Evaluation of Pedestal Stiffness Variations in Steel Supported Structures for Steam Turbines
Dekys et al. Use of MSC. ADAMS software product in modelling vibration sources
Grządziela et al. The impact estimation of damping foundations in dynamics of the rotor system

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address

Address after: Dong Jiaduan 412002 in Hunan province Zhuzhou city Lusong District

Patentee after: AECC HUNAN AVIATION POWERPLANT Research Institute

Country or region after: China

Address before: Dong Jiaduan 412002 in Hunan province Zhuzhou city Lusong District

Patentee before: CHINA AVIATION POWER MACHINERY INSTITUTE

Country or region before: China

CP03 Change of name, title or address