CN106217130A - Milling cutter state on_line monitoring and method for early warning during complex surface machining - Google Patents
Milling cutter state on_line monitoring and method for early warning during complex surface machining Download PDFInfo
- Publication number
- CN106217130A CN106217130A CN201610668278.5A CN201610668278A CN106217130A CN 106217130 A CN106217130 A CN 106217130A CN 201610668278 A CN201610668278 A CN 201610668278A CN 106217130 A CN106217130 A CN 106217130A
- Authority
- CN
- China
- Prior art keywords
- signal
- cumulant
- monitoring
- displacement
- vibration
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q17/00—Arrangements for observing, indicating or measuring on machine tools
- B23Q17/09—Arrangements for observing, indicating or measuring on machine tools for indicating or measuring cutting pressure or for determining cutting-tool condition, e.g. cutting ability, load on tool
- B23Q17/0952—Arrangements for observing, indicating or measuring on machine tools for indicating or measuring cutting pressure or for determining cutting-tool condition, e.g. cutting ability, load on tool during machining
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q17/00—Arrangements for observing, indicating or measuring on machine tools
- B23Q17/09—Arrangements for observing, indicating or measuring on machine tools for indicating or measuring cutting pressure or for determining cutting-tool condition, e.g. cutting ability, load on tool
- B23Q17/0995—Tool life management
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Abstract
The invention provides milling cutter state on_line monitoring and method for early warning during a kind of complex surface machining, belong to field of diagnosis about equipment fault.The present invention demonstrate Milling Force and handle of a knife vibration current vortex displacement signal between there is linear relationship on the basis of, using machine tool chief axis end X that three-dimensional acceleration transducer records, the acceleration signal of Y-direction secondary frequency volume integration as handle of a knife vibration displacement signal, extract the fundamental frequency in integral displacement signal and harmonic signal thereof as monitoring signal, on the one hand overcome all drawbacks directly being carried out displacement detecting in Machining of Curved Surface by eddy current displacement sensor, on the other hand can effectively remove the impact of interference signal;Use Synchronous time average cumulant that monitoring signal is further processed, then utilize characteristic quantity quantitatively to portray synchronized averaging cumulant waveform, realize the monitoring to milling cutter state according to eigenvalue change.
Description
Technical field
During Impeller Machining of the present invention, the method for milling cutter state on_line monitoring belongs to field of diagnosis about equipment fault,
Relate to selection three aspects of calculating of the selection monitoring signal kinds and process, the extraction of characteristic information and characteristic quantity.
Background technology
Along with the large-scale precision machinery such as aero-engine, compression is day by day to high load capacity, high efficiency and high reliability side
To development, the suface processing quality of the critical component-impeller in them is required more and more higher.Owing to spoon of blade structure is multiple
Miscellaneous, the reason such as the narrow space between blade, in the course of processing, knife bar needs to use bigger Mold processing, and this easily causes cutter
Milling cutter generation tipping fixing bottom bar, abrasion, disrepair phenomenon.
The suface processing quality of blade and milling cutter state have substantial connection, tipping, abrasion, damaged milling cutter and blade surface
Between frictional force can be increased dramatically, cutting temperature can steeply rise, the crudy of blade surface can be remarkably decreased, therefore blade
In the course of processing, the on-line monitoring of milling cutter state has very important reality meaning to the raising crudy of blade, working (machining) efficiency
Justice.
Good fortune occasion in Japanese scholars village detect based on cutting component than reflection cutter mill at document cutting component ratio injury
Damage situation, but force transducer exists, and installation is inconvenient, loaded area is little, high in cost of production unfavorable factor, it is impossible to it is applied to actual prison
Survey.Document dynamic milling based on vibration cutting displacement force measuring method points out that milling cutter can be by interrupted cut in the course of processing
The excitation of power, driving frequency be cutter tooth by frequency, when the speed of mainshaft is relatively low, driving frequency be far below tooling system first
Rank natural frequency, it is believed that the stiffness characteristics of cutter is essentially identical with time static, i.e. milling cutter are by after Milling Force effect being elasticity
Deformation, the vibration displacement of the dynamic milling force on milling cutter and surveyed handle of a knife meets linear relationship, therefore can by measurement physical quantity from
The measurement of Milling Force is converted to the measurement of handle of a knife vibration displacement, and the present invention is demonstrating Milling Force and handle of a knife swing current vortex displacement
On the basis of there is linear corresponding relation between signal, it is considered to utilize current vortex displacement signal to replace force signal as monitoring letter
Number, but because current vortex sensor there is also, inconvenient problem is installed, then propose to be added by collection lathe spindle nose X, Y-direction
Rate signal, then to acceleration signal secondary frequency volume integration obtain displacement signal, extract integral displacement signal fundamental frequency and
Harmonic signal, as monitoring signal, on the one hand solves sensor and installs the problem of inconvenience, effectively eliminate interference signal simultaneously
Impact.
Summary of the invention
The present invention is demonstrating on the basis of Milling Force and handle of a knife swing and there is linear relationship between current vortex displacement signal,
The machine tool chief axis end X that records with three-dimensional acceleration transducer, the acceleration signal of Y-direction, to its secondary frequency volume integration conduct
Handle of a knife displacement signal, overcomes all drawbacks directly being carried out displacement detecting in Machining of Curved Surface by eddy current displacement sensor,
On the basis of the handle of a knife vibration displacement signal using Synchronous time average the Cumulant Method Using to go out integration goes interference to process, carry
Go out using the fundamental frequency in integral displacement signal and harmonic signal thereof as monitoring signal, solved milling during complex surface machining
Cutter state on_line monitoring and an early warning difficult problem.
Technical scheme:
Milling cutter state on_line monitoring and method for early warning during a kind of complex surface machining, step is as follows:
Step A. obtains the acceleration signal stage online: three-dimensional acceleration transducer is fixed on machine tool chief axis end, mark
Determine to measure direction to three-dimensional acceleration transducer to be completely superposed with milling handle vibration X-direction and Y-direction, three-dimensional acceleration sensing
Device is for measuring milling handle vibration X-direction and the acceleration signal of Y-direction;
Step B. acceleration signal is converted to monitor signal phase: the milling handle that step A obtains vibrates X-direction and Y side
To acceleration signal, monitoring signal be milling handle vibration displacement signal, to step A obtain milling handle vibration X side
Carry out quadratic integral to the acceleration signal with Y-direction and be converted into displacement signal, represent milling handle vibration displacement;Owing to accelerating
Degree signal band wide ranges, the signal component comprised is complex, causes integral displacement signal to be mixed with more interference signal, in order to
Remove the impact of interference signal, after utilizing Fourier transform (FFT, Fast Fourier Transformation) to integration
Displacement signal carries out spectrum analysis, filters other frequency signals and only retains fundamental frequency and harmonic components thereof, and the inverse Fourier of recycling becomes
Change (IFFT, Inverse Fast Fourier Transformation) and become filtered signal again time-domain signal as prison
Survey signal, in order to verify the effectiveness of monitoring signal measurement vibration cutting displacement, to current vortex displacement signal and monitoring signal pair
The cumulant answered carries out cross-correlation analysis, using the fundamental frequency of integral displacement signal and harmonic signal thereof as monitoring signal, on the one hand
Solve sensor and the problem of inconvenience is installed, can effectively remove the impact of interference signal simultaneously.
The step C. monitoring signal online treatment stage: monitoring milling handle vibrated by Synchronous time average the Cumulant Method Using
Signal is further processed, and strengthens the reliability and stability of monitoring signal.
Synchronous time average the Cumulant Method Using principle is as follows: the periodic waveform of vibration cutting displacement signal is close with cutting tool state
Relevant, during Impeller Machining, working conditions change causes monitoring signal waveform amplitude and changes greatly in different time sections, time domain
Synchronized averaging can be with the effective attenuation frequency signal unrelated with gyration period, therefore, monitoring signal is carried out Synchronous time average
Can strengthen the stability of monitoring signal period waveform, this is extremely important to relying on signal waveform to carry out feature extraction;Time domain is same
Step average accumulated amount is the overall summary to signal, in order to describe the integrality of signal and extract signal letter from different perspectives
Breath, uses Synchronous time average cumulant to be described monitoring signal, and compared with primary signal, the periodic waveform of cumulant is more
Add stable, thus monitoring result is relatively reliable.
It is as follows that Synchronous time average the Cumulant Method Using is treated journey to milling handle vibration monitoring signal: sets rotating machinery
Vibration signal be xt, speed is f0, the sampling interval is Δ, and the discrete signal that vibration signal is corresponding is xt=x (n Δ), will
Vibration signal is according to speed f0Extract corresponding vibration signal, if by xnIntercept as P section, then the cycle of each period isAssume that the sampling number of every section is equal and value is N, synchronized averagingJust can represent with following formula:
Algorithm principle based on Synchronous time average, in conjunction with the computing formula of statistics cumulant, derives Domain Synchronous
The computing formula of average accumulated amount, the single order derived, second order Synchronous time average cumulant formula are as follows:
Single order cumulant:
Second-order cumulant:
Step D. cutting tool state judges the stage online: on the basis of step C, is tired out Synchronous time average by characteristic quantity
Accumulated amount waveform is quantitatively described, it is judged that cutting tool state.
Before and after milling cutter breakage, there is the biggest difference in the signal waveform of the Synchronous time average cumulant of handle of a knife vibration displacement,
Utilizing time domain index quantitatively to portray cumulant waveform, the different corresponding time domain index value of waveform certainly exists difference, by time domain index
As characteristic quantity, realize tool condition monitoring according to the difference of desired value before and after tool failure, use variance, degree of skewness, kurtosis
Value, absolute mean and virtual value portray signal waveform as characteristic quantity, and wherein, variance is for describing the discrete journey of signal waveform
Degree, degree of skewness is for describing skew direction and the degree of data, and kurtosis value is especially sensitive to impact signal, and absolute mean embodies whole
Body amplitude size, feature extraction thinking is as shown in flow chart 1, and each time domain index correspondence formula is as follows:
Variance:
Degree of skewness:
Kurtosis value:
Absolute value average:
Virtual value:
Wherein yiRepresent single order, second order sync average accumulated amount,For single order, second order sync average accumulated amount average.
Beneficial effects of the present invention: the present invention utilizes acceleration transducer to gather signal, and acceleration transducer has installation
Freely measure the feature of simplicity, can be used for actual monitoring;Synchronized averaging cumulant is utilized to extract the characteristic information of milling cutter state, then
In conjunction with characteristic quantity the feature extracting method that synchronized averaging cumulant is quantitatively described had monitoring result is good, programming letter
Feature single, that the speed of service is fast, meets the requirement of on-line monitoring real-time.
Accompanying drawing explanation
Fig. 1 is milling cutter status monitoring flow chart.
Fig. 2 a is X-direction force signal and current vortex displacement linearly relation displacement diagram.
Fig. 2 b is Y-direction force signal and current vortex displacement linearly relation displacement diagram.
Fig. 3 is point of a knife to frequency response function figure at displacement measurement.
Fig. 4 a is the 14th group of data current vortex displacement signal single order accumulation spirogram.
Fig. 4 b is the 14th group of data current vortex displacement signal second-order cumulant figure.
Fig. 4 c is the 14th group of data integral displacement signal single order accumulation spirogram.
Fig. 4 d is the 14th group of data integral displacement signal second-order cumulant figure.
Fig. 5 a is that the 14th group of data current vortex displacement signal returns scatterplot with integral displacement signal single order cumulant linearly
Figure.
Fig. 5 b is that the 14th group of data current vortex displacement signal returns scatterplot with integral displacement signal second-order cumulant linearly
Figure.
Fig. 6 a is the 64th group of data current vortex displacement signal single order accumulation spirogram.
Fig. 6 b is the 64th group of data current vortex displacement signal second-order cumulant figure.
Fig. 6 c is the 64th group of data integral displacement signal single order accumulation spirogram.
Fig. 6 d is the 64th group of data integral displacement signal second-order cumulant figure.
Fig. 7 a is that the 64th group of data current vortex displacement signal returns scatterplot with integral displacement signal single order cumulant linearly
Figure.
Fig. 7 b is that the 64th group of data current vortex displacement signal returns scatterplot with integral displacement signal second-order cumulant linearly
Figure.
Fig. 8 a is 1-80 group data single order cumulant absolute value average figure.
Fig. 8 b is 1-80 group data single order cumulant variance yields figure.
Fig. 8 c is 1-80 group data single order cumulant virtual value figure.
Fig. 8 d is 1-80 group data single order cumulant kurtosis value figure.
Fig. 8 e is 1-80 group data single order cumulant deflection angle value figure.
Fig. 9 a is 1-80 group data second-order cumulant absolute value average figure.
Fig. 9 b is 1-80 group data second-order cumulant variance yields figure.
Fig. 9 c is 1-80 group data second-order cumulant virtual value figure.
Fig. 9 d is 1-80 group data second-order cumulant kurtosis value figure.
Fig. 9 e is 1-80 group data second-order cumulant deflection angle value figure.
Detailed description of the invention
Below in conjunction with technical scheme and accompanying drawing, further illustrate the detailed description of the invention of the present invention.
Experimental data totally 80 groups, is collected in certain enterprise's compressor impeller Milling Process production scene domestic, in gatherer process,
Shutting down at interval of a period of time and observe milling cutter state, find the 61st group of milling cutter tipping, experiment parameter is as shown in table 1.
Table 1 experiment parameter
14th group, the 64th group of data be respectively the data before and after milling cutter tipping, the synchronized averaging cycle is 10 speed cycles,
Fig. 4 a, Fig. 4 b the most corresponding 14th group of data current vortex displacement signal single order, the result of calculation of second-order cumulant, Fig. 4 c, Fig. 4 d
The most corresponding 14th group of integral displacement signal single order, the result of calculation of second-order cumulant;The most corresponding 64th group of number of Fig. 6 a, Fig. 6 b
According to current vortex displacement signal single order, the result of calculation of second-order cumulant;The most corresponding 64th group of integral displacement signal of Fig. 6 c, Fig. 6 d
Single order, the result of calculation of second-order cumulant.
In order to describe the wave-form similarity between current vortex displacement signal and integral displacement signal, calculate the 14th group and the 64th
Correlation coefficient between group data current vortex displacement signal cumulant corresponding with integral displacement signal, and draw scatterplot, Fig. 5 a, figure
The most corresponding regression result between the 14th group of data two class displacement signal single order, second-order cumulant of 5b, Fig. 7 a, Fig. 7 b correspondence respectively
Regression result between the 64th group of data two class displacement signal single order, second-order cumulant.
Found out that correlation coefficient all reaches more than 0.9 by Fig. 5 a, Fig. 5 b and Fig. 7 a, Fig. 7 b, show current vortex displacement signal
With integral displacement signal linearly relation highly significant, both have similar monitoring effect, it is possible to use integral displacement signal
Substitute current vortex displacement signal and carry out tool condition monitoring;Corresponding comparison diagram 4a, Fig. 4 b, Fig. 4 c, Fig. 4 d Yu Fig. 6 a, Fig. 6 b, figure
6c, Fig. 6 d finds out, after tool failure, the single order of two class displacement signals, second-order cumulant amplitude all increased, the most all with two
The amplitude of rank cumulant increases notable;Further, it is also possible to find out that the second-order cumulant amplitude of integral displacement signal increases than electric whirlpool
Stream displacement signal becomes apparent from, and this shows the second-order cumulant second-order cumulant than current vortex displacement signal of integral displacement signal
Sensitiveer to cutting tool state reacting condition.
Fig. 8 a, Fig. 8 b, Fig. 8 c, Fig. 8 d, Fig. 8 e and Fig. 9 a, Fig. 9 b, Fig. 9 c, Fig. 9 d, Fig. 9 e represent that integral displacement is believed respectively
Number single order, the feature extraction result of second-order cumulant, found out integral displacement signal by Fig. 8 a, Fig. 8 b, Fig. 8 c, Fig. 8 d, Fig. 8 e
The each characterizing magnitudes of single order cumulant entirety after the 55th group increases, and Fig. 9 a, Fig. 9 b, Fig. 9 c, Fig. 9 d, Fig. 9 e will become apparent from
The each characterizing magnitudes of single order cumulant of integral displacement signal increases notable at the 55th group, and eigenvalue is basicly stable afterwards, Liang Zhejie
Conjunction can be determined that tool failure occurs at the 55th group, and experimental record tool failure occurs at the 61st group, and this monitoring result is in the
Before 61 groups, thus monitoring result meets the requirements.
Claims (1)
1. milling cutter state on_line monitoring and method for early warning during a complex surface machining, it is characterised in that step is as follows:
Step A. obtains the acceleration signal stage online: three-dimensional acceleration transducer is fixed on machine tool chief axis end, demarcates extremely
Three-dimensional acceleration transducer is measured direction and is completely superposed with milling handle vibration X-direction and Y-direction, and three-dimensional acceleration transducer is used
In measuring milling handle vibration X-direction and the acceleration signal of Y-direction;
Step B. acceleration signal is converted to monitor signal phase: milling handle vibration X-direction that step A obtains and Y-direction
Acceleration signal, monitoring signal is the displacement signal of milling handle vibration, the milling handle vibration X-direction obtaining step A and Y
The acceleration signal in direction carries out quadratic integral and is converted into displacement signal, represents milling handle vibration displacement;Fourier is utilized to become
Change FFT and displacement signal is carried out spectrum analysis, filter other frequency signals and only retain fundamental frequency and harmonic components thereof, inverse Fu of recycling
Filtered signal is become again time-domain signal as monitoring signal by vertical leaf transformation IFFT;
The step C. monitoring signal online treatment stage: monitoring signal milling handle vibrated by Synchronous time average the Cumulant Method Using
It is further processed, strengthens the reliability and stability of monitoring signal;
It is as follows that Synchronous time average the Cumulant Method Using is treated journey to milling handle vibration monitoring signal: sets rotating machinery and shakes
Dynamic signal is xt, speed is f0, the sampling interval is Δ, and the discrete signal that vibration signal is corresponding is xt=x (n Δ), will vibration
Signal is according to speed f0Extract corresponding vibration signal, if by xnIntercept as P section, then the cycle of each period is
Assume that the sampling number of every section is equal and value is N, synchronized averagingRepresent with following formula:
Algorithm principle based on Synchronous time average, in conjunction with the computing formula of statistics cumulant, derives Synchronous time average
The computing formula of cumulant, the single order derived, second order Synchronous time average cumulant formula are as follows:
Single order cumulant:
Second-order cumulant:
Step D. cutting tool state judges the stage online: before and after milling cutter breakage, the Synchronous time average cumulant of handle of a knife vibration displacement
Signal waveform there is the biggest difference, utilize time domain index quantitatively to portray cumulant waveform, the different corresponding time domain index value of waveform
There are differences, using time domain index as characteristic quantity, realize tool condition monitoring according to the difference of desired value before and after tool failure, adopt
Portraying signal waveform by variance, degree of skewness, kurtosis value, absolute mean and virtual value as characteristic quantity, wherein, variance is used for describing
The dispersion degree of signal waveform, degree of skewness is for describing skew direction and the degree of data, and kurtosis value is the quickest to impact signal
Sense, absolute mean embodies overall amplitude size, and each time domain index correspondence formula is as follows:
Variance:
Degree of skewness:
Kurtosis value:
Absolute value average:
Virtual value:
Wherein yiRepresent single order, second order sync average accumulated amount,For single order, second order sync average accumulated amount average.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610668278.5A CN106217130B (en) | 2016-08-15 | 2016-08-15 | Milling cutter state on_line monitoring and method for early warning during complex surface machining |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610668278.5A CN106217130B (en) | 2016-08-15 | 2016-08-15 | Milling cutter state on_line monitoring and method for early warning during complex surface machining |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106217130A true CN106217130A (en) | 2016-12-14 |
CN106217130B CN106217130B (en) | 2018-06-15 |
Family
ID=57548182
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610668278.5A Active CN106217130B (en) | 2016-08-15 | 2016-08-15 | Milling cutter state on_line monitoring and method for early warning during complex surface machining |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106217130B (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107705780A (en) * | 2016-08-08 | 2018-02-16 | 发那科株式会社 | Control device and control system |
CN110008784A (en) * | 2018-01-04 | 2019-07-12 | 西安交通大学 | Milling Force recognition methods and identifying system based on conjugate gradient least-squares algorithm |
CN110842648A (en) * | 2019-11-28 | 2020-02-28 | 南京科技职业学院 | Online cutter wear prediction and monitoring method |
CN110877233A (en) * | 2018-09-05 | 2020-03-13 | 日本电产株式会社 | Wear loss estimation system, wear loss estimation method, correction system, abnormality detection system, and life detection system |
CN112710358A (en) * | 2021-03-29 | 2021-04-27 | 南京诚远高新科技有限公司 | Intelligent machine tool state monitoring device and state monitoring method thereof |
WO2021184421A1 (en) * | 2020-03-20 | 2021-09-23 | 苏州森鼎高端装备有限公司 | Combined intelligent measurement method and cutting device |
CN114126792A (en) * | 2019-07-24 | 2022-03-01 | 西铁城时计株式会社 | Machining device, control device used for same, and control method for machining device |
CN114273974A (en) * | 2021-12-14 | 2022-04-05 | 中国科学院合肥物质科学研究院 | Vibration signal-based tool runout parameter online estimation method in high-speed milling |
CN114755007A (en) * | 2022-04-12 | 2022-07-15 | 上海电气风电集团股份有限公司 | Gear fault diagnosis method and device and computer readable storage medium |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4636779A (en) * | 1984-10-24 | 1987-01-13 | General Electric Company | Acoustic detection of tool break events in machine tool operations |
JPH0349850A (en) * | 1989-07-13 | 1991-03-04 | Omron Corp | Tool damage detecting device |
JPH0885047A (en) * | 1994-09-13 | 1996-04-02 | Sumitomo Metal Ind Ltd | Cutter tip abrasion detecting method for cutting tool |
CN102490086A (en) * | 2011-10-28 | 2012-06-13 | 浙江大学 | System for monitoring working state of boring rod in real time |
CN102765010A (en) * | 2012-08-24 | 2012-11-07 | 常州大学 | Cutter damage and abrasion state detecting method and cutter damage and abrasion state detecting system |
CN103941645A (en) * | 2014-04-09 | 2014-07-23 | 南京航空航天大学 | Thin-wall part complex working condition machining state monitoring method |
CN104741638A (en) * | 2015-04-20 | 2015-07-01 | 江苏师范大学 | Turning cutter wear state monitoring system |
CN105171529A (en) * | 2015-10-12 | 2015-12-23 | 四川大学 | Self-adaptive intelligent feeding control device |
-
2016
- 2016-08-15 CN CN201610668278.5A patent/CN106217130B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4636779A (en) * | 1984-10-24 | 1987-01-13 | General Electric Company | Acoustic detection of tool break events in machine tool operations |
JPH0349850A (en) * | 1989-07-13 | 1991-03-04 | Omron Corp | Tool damage detecting device |
JPH0885047A (en) * | 1994-09-13 | 1996-04-02 | Sumitomo Metal Ind Ltd | Cutter tip abrasion detecting method for cutting tool |
CN102490086A (en) * | 2011-10-28 | 2012-06-13 | 浙江大学 | System for monitoring working state of boring rod in real time |
CN102765010A (en) * | 2012-08-24 | 2012-11-07 | 常州大学 | Cutter damage and abrasion state detecting method and cutter damage and abrasion state detecting system |
CN103941645A (en) * | 2014-04-09 | 2014-07-23 | 南京航空航天大学 | Thin-wall part complex working condition machining state monitoring method |
CN104741638A (en) * | 2015-04-20 | 2015-07-01 | 江苏师范大学 | Turning cutter wear state monitoring system |
CN105171529A (en) * | 2015-10-12 | 2015-12-23 | 四川大学 | Self-adaptive intelligent feeding control device |
Non-Patent Citations (2)
Title |
---|
谢厚正 等: "基于振动测试的数控机床刀具磨损监测方法", 《仪表技术与传感器》 * |
黄民 等: "高档数控机床刀具磨损故障监测方法及实验系统", 《北京信息科技大学学报(自然科学版)》 * |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10481596B2 (en) | 2016-08-08 | 2019-11-19 | Fanuc Corporation | Control device and control system |
CN107705780A (en) * | 2016-08-08 | 2018-02-16 | 发那科株式会社 | Control device and control system |
CN107705780B (en) * | 2016-08-08 | 2020-07-14 | 发那科株式会社 | Control device and control system |
CN110008784A (en) * | 2018-01-04 | 2019-07-12 | 西安交通大学 | Milling Force recognition methods and identifying system based on conjugate gradient least-squares algorithm |
CN110008784B (en) * | 2018-01-04 | 2021-02-26 | 西安交通大学 | Milling force identification method and system based on conjugate gradient least square algorithm |
CN110877233A (en) * | 2018-09-05 | 2020-03-13 | 日本电产株式会社 | Wear loss estimation system, wear loss estimation method, correction system, abnormality detection system, and life detection system |
CN114126792A (en) * | 2019-07-24 | 2022-03-01 | 西铁城时计株式会社 | Machining device, control device used for same, and control method for machining device |
CN110842648A (en) * | 2019-11-28 | 2020-02-28 | 南京科技职业学院 | Online cutter wear prediction and monitoring method |
WO2021184421A1 (en) * | 2020-03-20 | 2021-09-23 | 苏州森鼎高端装备有限公司 | Combined intelligent measurement method and cutting device |
CN112710358B (en) * | 2021-03-29 | 2021-06-25 | 南京诚远高新科技有限公司 | Intelligent machine tool state monitoring device and state monitoring method thereof |
CN112710358A (en) * | 2021-03-29 | 2021-04-27 | 南京诚远高新科技有限公司 | Intelligent machine tool state monitoring device and state monitoring method thereof |
CN114273974A (en) * | 2021-12-14 | 2022-04-05 | 中国科学院合肥物质科学研究院 | Vibration signal-based tool runout parameter online estimation method in high-speed milling |
CN114755007A (en) * | 2022-04-12 | 2022-07-15 | 上海电气风电集团股份有限公司 | Gear fault diagnosis method and device and computer readable storage medium |
Also Published As
Publication number | Publication date |
---|---|
CN106217130B (en) | 2018-06-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN106217130A (en) | Milling cutter state on_line monitoring and method for early warning during complex surface machining | |
Elbestawi et al. | In-process monitoring of tool wear in milling using cutting force signature | |
KR101718251B1 (en) | Method and system for monitoring rotating blade health | |
CN103575523B (en) | The rotary machinery fault diagnosis method of kurtosis-envelope spectrum analysis is composed based on FastICA- | |
CN104215323B (en) | Method for determining sensitivity of each sensor in mechanical equipment vibrating sensor network | |
CN102721462B (en) | Method for quickly computing Bode plot and Nyquist plot of rotary mechanical vehicle starting and parking processes | |
EP0762248A1 (en) | Characterising a machine tool system | |
CN106441761A (en) | Engine blade fatigue testing device | |
CN101221066A (en) | Engineering nonlinear vibration detecting method | |
CN106762343B (en) | The diagnostic method of hydraulic generator set thrust bearing failure based on online data | |
Fan et al. | Blade vibration difference-based identification of blade vibration parameters: A novel blade tip timing method | |
CN109641337A (en) | Equipment for inhibiting of vibration | |
CN106141815A (en) | A kind of high-speed milling tremor on-line identification method based on AR model | |
Ali et al. | Observations of changes in acoustic emission parameters for varying corrosion defect in reciprocating compressor valves | |
CN104390697A (en) | C0 complexity and correlation coefficient-based milling chatter detection method | |
CN103884482A (en) | Vibration testing method and system based on compressor | |
CN110434676A (en) | A kind of boring monitoring chatter method of multisensor time-frequency characteristics fusion | |
EP2577241A2 (en) | Machine vibration monitoring | |
CN110133106B (en) | Vibration damage measuring instrument for power transmission line | |
You et al. | Fault diagnosis system of rotating machinery vibration signal | |
Abdelrhman et al. | Application of wavelet analysis in blade faults diagnosis for multi-stages rotor system | |
CN105807716B (en) | Remanufacture lathe health monitoring systems | |
CN101451882B (en) | Short time amplitude frequency spectrum array for single section shaft vibration analysis for mechanical rotor | |
TW201633025A (en) | Diagnostic method for malfunction mode of machine tool main shaft and system thereof | |
CN205644242U (en) | Refabrication lathe health monitoring system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant |