CN111444645A - Port machine damage positioning method based on residual stress gap state - Google Patents

Port machine damage positioning method based on residual stress gap state Download PDF

Info

Publication number
CN111444645A
CN111444645A CN202010159712.3A CN202010159712A CN111444645A CN 111444645 A CN111444645 A CN 111444645A CN 202010159712 A CN202010159712 A CN 202010159712A CN 111444645 A CN111444645 A CN 111444645A
Authority
CN
China
Prior art keywords
residual stress
value
port machine
damage
vulnerable
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
Application number
CN202010159712.3A
Other languages
Chinese (zh)
Other versions
CN111444645B (en
Inventor
朱林
周萌
王鹏
黄嘉铭
邱建春
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.)
Yangzhou University
Original Assignee
Yangzhou 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 Yangzhou University filed Critical Yangzhou University
Priority to CN202010159712.3A priority Critical patent/CN111444645B/en
Publication of CN111444645A publication Critical patent/CN111444645A/en
Application granted granted Critical
Publication of CN111444645B publication Critical patent/CN111444645B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/25Measuring force or stress, in general using wave or particle radiation, e.g. X-rays, microwaves, neutrons
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/0047Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes measuring forces due to residual stresses
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N23/00Investigating or analysing materials by the use of wave or particle radiation, e.g. X-rays or neutrons, not covered by groups G01N3/00 – G01N17/00, G01N21/00 or G01N22/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/20Recycling

Abstract

The invention discloses a port machine damage positioning method based on a residual stress gap state, which comprises the following steps: s1, determining the position of the port machine structure which is vulnerable to damage; s2, determining a real-time maximum residual stress interval value of a vulnerable position of the port machine; s3, calculating a state value of the real-time residual stress gap of the port machine; s4, determining a clearance state factor of each vulnerable position; and S5, locating the port machine damage based on the residual stress gap state. The method is high in detection precision and has important practical significance for realizing the damage positioning of the port machine.

Description

Port machine damage positioning method based on residual stress gap state
Technical Field
The invention relates to a port machine damage positioning method, in particular to a port machine damage positioning method based on a residual stress gap state.
Background
With the development of society and the deepening of international trade cooperation, port machines have become more and more important tools for deepening the cooperation between ports of two countries. The port crane is an important mechanized tool for lifting cargos at a port, and with the increase of cargo throughput and extreme change of working load, the damage condition of the structure of the port crane becomes a key point of attention of users and detection personnel and is also a key point of research at home and abroad. At present, most damage positioning methods are developed based on sound vibration characteristics collected under working conditions, the influence of the working conditions and the environment is large, and the difference between different sound vibration characteristic indexes cannot fully reflect the damage position of a port machine structure, so that the common problem in the research field is how to accurately position the damage position starting from the internal performance of the port machine structure reflected under the loading effect.
Disclosure of Invention
The purpose of the invention is as follows: the invention aims to provide a port machine damage positioning method based on a residual stress gap state.
The technical scheme is as follows: the invention provides a port machine damage positioning method based on a residual stress gap state, which comprises the following steps of:
s1, determining the position of the port machine structure which is vulnerable to damage;
s2, determining a real-time maximum residual stress interval value of a vulnerable position of the port machine;
s3, calculating a state value of the real-time residual stress gap of the port machine;
s4, determining a clearance state factor of each vulnerable position;
and S5, locating the port machine damage based on the residual stress gap state.
Further, the determining method of step S1 is as follows: the method comprises the steps of importing a finite element analysis model of the whole port machine into finite element analysis software, carrying out gridding division on the finite element analysis model, setting constraint conditions and applying load conditions on the finite element analysis model according to actual working conditions of the port machine, carrying out post-processing on the finite element analysis model of the port machine, determining each vulnerable position of the port machine structure under the actual working conditions, and marking the model according to an analysis result, wherein the marking position is m, m is 1, 2 and 3.
Further, the determining method of step S2 is as follows: combining the vulnerable positions of the port machine structure under the plurality of actual working conditions determined in the S1, finding the positions of the marks on the actual port machine structure, arranging an X-ray residual stress tester at the corresponding positions, and measuring the residual stress value sigma corresponding to each second according to the time interval of 1 minutemtMeasuring, and calculating an equivalent interval value q of the structure residual stress value at the m position at the ith minuteimAnd i represents a mark of the minute,
Figure BDA0002404614650000021
wherein ,qimThe equivalent interval value of the structural residual stress at the ith minute of the m-number damage position; c (sigma)mt)maxThe maximum value of all residual stress values measured in every minute at the mth vulnerable position; c (sigma)mt)minThe minimum value of all residual stress values measured in every minute at the mth vulnerable position;
Figure BDA0002404614650000022
the average value of all residual stress values measured in every minute at the mth vulnerable position; t is a mark of seconds per minute,
Figure BDA0002404614650000023
real-time q-pair under actual working conditionimAnd calculating and recording.
Further, the calculation method of step S3 is: combining the residual stress equivalent interval values q of each damage position calculated in S2imMaximum value of C (q) over monitoring time for each lesion siteim)maxWith a minimum value of C (q)im)minIdentify and record each lesion location as corresponding to C (q)im)maxAt a time point of C (t)m)maxAnd corresponds to C (q)im)minAt a time point of C (t)m)minAnd further calculating the residual stress gap state value J of each vulnerable position on the basism
Figure BDA0002404614650000024
wherein ,tmTotal monitoring time for each injury site; q. q.simThe equivalent interval value of the residual stress of each damage position is obtained; j. the design is a squaremA residual stress gap state value for each vulnerable site; the compound gap homogenization coefficient; gamma is a singularization coefficient of the damage position; c (q)im)maxThe maximum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained; c (q)im)minThe minimum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained,
Figure BDA0002404614650000025
Figure BDA0002404614650000026
further, the method determined in S4 is: on the basis of the port machine real-time residual stress gap state value calculated in S3, the residual stress gap state value J corresponding to each vulnerable position is calculatedmSubstituting the following equation into the value of the gap state factor Y for each positionmThe calculation is carried out in such a way that,
Figure BDA0002404614650000027
wherein ,YmA gap state factor value for each position; j. the design is a squaremA residual stress gap state value for each vulnerable site; c (J)m)maxThe maximum value of the residual stress gap state value of each vulnerable position; c (J)m)minFor the stump of each vulnerable siteMinimum value of residual stress gap state value; γ is a singularization coefficient of the damage location.
Further, the method for positioning in S5 is: on the basis of S4, all gap state factor values Y are extractedmIn excess of 1.73
Figure BDA0002404614650000031
The position of (1), namely the position where the potential damage in the port machine has occurred,
Figure BDA0002404614650000032
wherein ,
Figure BDA0002404614650000033
the average value of the gap state factor values of all vulnerable positions is obtained; y ismA gap state factor value for each position; m is the number of the position which is easy to damage; n is the number of vulnerable positions.
Has the advantages that: the method can realize the acquisition of the residual stress clearance state of the port machinery under the working condition in real time, determine the main damage interval through the cis-position relation of the clearance state factors, further determine the damage extreme value quantity according to the cis-position factors, and is favorable for determining the specific damage position in real time in the working process of the port crane, thereby more effectively improving the positioning precision of the damage position of the port mechanism.
Drawings
FIG. 1 is a flow chart of the method of the present invention.
Detailed Description
As shown in fig. 1, the method for locating a port machine damage based on a residual stress gap state in this embodiment includes the following steps:
s1, determining a position where a port machine structure is easily damaged:
importing a finite element analysis model of the whole port machine into ANSYS finite element analysis software, carrying out gridding division on the finite element analysis model, then setting constraint conditions and applying load conditions on the finite element analysis model according to actual working conditions of the port machine, then carrying out post-processing on the finite element analysis model of the port machine, determining each vulnerable position of the port machine structure under the actual working conditions, and marking the model according to an analysis result, wherein the marking position is m (m 1, 2, 3.).
S2, determining a real-time maximum residual stress interval value of a position where a port machine is easily damaged:
combining the vulnerable positions of the port machine structure under the plurality of actual working conditions determined in the S1, finding the positions of the marks on the actual port machine structure, arranging an X-ray residual stress tester at the corresponding positions, and measuring the residual stress value sigma corresponding to each second according to the time interval of 1 minutemtMeasuring, and calculating an equivalent interval value q of the structure residual stress value at the m position at the ith minuteim(i represents a minute mark).
Figure BDA0002404614650000034
wherein ,qimThe equivalent interval value of the structure residual stress value of the m-number damage position in the ith minute is shown; c (sigma)mt)maxThe maximum value of all residual stress values measured in every minute at the mth vulnerable position; c (sigma)mt)minThe minimum value of all residual stress values measured in every minute at the mth vulnerable position;
Figure BDA0002404614650000041
the average value of all residual stress values measured in every minute at the mth vulnerable position; t is seconds per minute.
Figure BDA0002404614650000042
Real-time q-pair under actual working conditionimAnd calculating and recording.
S3, calculating a state value of the real-time residual stress gap of the port machine:
combining the residual stress equivalent interval values q of each damage position calculated in S2imMaximum value of C (q) over monitoring time for each lesion siteim)maxWith a minimum value of C (q)im)minIdentify and record each lesion location as corresponding to C (q)im)maxAt a time point of C (t)m)maxAnd corresponds to C (q)im)minAt a time point of C (t)m)min
And further calculating the residual stress gap state value J of each vulnerable position on the basism
Figure BDA0002404614650000043
wherein ,tmTotal monitoring time for each injury site; q. q.simThe equivalent interval value of the residual stress of each damage position is obtained; j. the design is a squaremA residual stress gap state value for each vulnerable site; the compound gap homogenization coefficient; gamma is a singularization coefficient of the damage position; c (q)im)maxThe maximum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained; c (q)im)minAnd the minimum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained.
Figure BDA0002404614650000044
Figure BDA0002404614650000045
S4, determining a clearance state factor of each vulnerable position:
on the basis of the port machine real-time residual stress gap state value calculated in S3, the residual stress gap state value J corresponding to each vulnerable position is calculatedmSubstituting the following equation into the value of the gap state factor Y for each positionmAnd (6) performing calculation.
Figure BDA0002404614650000046
wherein ,YmIn the form of gaps for each positionA value of the state factor; j. the design is a squaremA residual stress gap state value for each vulnerable site; c (J)m)maxThe maximum value of the residual stress gap state value of each vulnerable position; c (J)m)minThe minimum value of the residual stress gap state value of each vulnerable position; γ is a singularization coefficient of the damage location.
S5, carrying machine damage positioning based on the residual stress gap state:
on the basis of S4, all gap state factor values Y are extractedmZhongchao (middle surpass)
Figure BDA0002404614650000051
I.e. where potential damage has occurred in the port machinery.
Figure BDA0002404614650000052
wherein ,
Figure BDA0002404614650000053
the average value of the gap state factor values of all vulnerable positions is obtained; y ismA gap state factor value for each position; m is the number of the position which is easy to damage; n is the number of vulnerable positions.

Claims (6)

1. A port machine damage positioning method based on a residual stress gap state is characterized by comprising the following steps: the method comprises the following steps:
s1, determining the position of the port machine structure which is vulnerable to damage;
s2, determining a real-time maximum residual stress interval value of a vulnerable position of the port machine;
s3, calculating a state value of the real-time residual stress gap of the port machine;
s4, determining a clearance state factor of each vulnerable position;
and S5, locating the port machine damage based on the residual stress gap state.
2. The port machine damage positioning method based on the residual stress gap state of claim 1, wherein: the determination method of step S1 includes: the method comprises the steps of importing a finite element analysis model of the whole port machine into finite element analysis software, carrying out gridding division on the finite element analysis model, setting constraint conditions and applying load conditions on the finite element analysis model according to actual working conditions of the port machine, carrying out post-processing on the finite element analysis model of the port machine, determining each vulnerable position of the port machine structure under the actual working conditions, and marking the model according to an analysis result, wherein the marking position is m, m is 1, 2 and 3.
3. The port machine damage positioning method based on the residual stress gap state as claimed in claim 2, characterized in that: the determination method of step S2 includes: combining the vulnerable positions of the port machine structure under the multiple actual working condition conditions determined in the S1, finding the positions of the marks on the actual port machine structure, arranging an X-ray residual stress tester at the corresponding positions, and measuring the residual stress value sigma corresponding to each second in the ith minute according to the time interval of 1 minutemtMeasuring, and calculating an equivalent interval value q of the structure residual stress value at the m position at the ith minuteimAnd i represents a mark of the minute,
Figure FDA0002404614640000011
wherein ,qimThe equivalent interval value of the structural residual stress of the m-number damage position in the ith minute is shown; c (sigma)mt)maxThe maximum value of all residual stress values measured in every minute at the mth vulnerable position; c (sigma)mt)minThe minimum value of all residual stress values measured in every minute at the mth vulnerable position;
Figure FDA0002404614640000012
the average value of all residual stress values measured in every minute at the mth vulnerable position; t is a mark of seconds per minute,
Figure FDA0002404614640000013
real-time q-pair under actual working conditionimAnd calculating and recording.
4. The port machine damage positioning method based on the residual stress gap state of claim 3, characterized in that: the calculation method of step S3 is: combining the residual stress equivalent interval values q of each damage position calculated in S2imMaximum value of C (q) over monitoring time for each lesion siteim)maxWith a minimum value of C (q)im)minIdentify and record each lesion location as corresponding to C (q)im)maxAt a time point of C (t)m)maxAnd corresponds to C (q)im)minAt a time point of C (t)m)minAnd further calculating the residual stress gap state value J of each vulnerable position on the basism
Figure FDA0002404614640000021
wherein ,tmTotal monitoring time for each injury site; q. q.simThe equivalent interval value of the residual stress of each damage position is obtained; j. the design is a squaremA residual stress gap state value for each vulnerable site; the compound gap homogenization coefficient; gamma is a singularization coefficient of the damage position; c (q)im)maxThe maximum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained; c (q)im)minThe minimum value of the residual stress equivalent interval value of each damage position in the monitoring time is obtained,
Figure FDA0002404614640000022
Figure FDA0002404614640000023
5. the port machine damage positioning method based on the residual stress gap state as claimed in claim 4, wherein: the method determined in S4 is: on the basis of the port machine real-time residual stress gap state value calculated in S3, the residual stress gap state value J corresponding to each vulnerable position is calculatedmSubstituting the following equation into the value of the gap state factor Y for each positionmThe calculation is carried out in such a way that,
Figure FDA0002404614640000024
wherein ,YmA gap state factor value for each position; j. the design is a squaremA residual stress gap state value for each vulnerable site; c (J)m)maxThe maximum value of the residual stress gap state value of each vulnerable position; c (J)m)minThe minimum value of the residual stress gap state value of each vulnerable position; γ is a singularization coefficient of the damage location.
6. The port machine damage positioning method based on the residual stress gap state of claim 5, wherein: the method for positioning in S5 is: on the basis of S4, all gap state factor values Y are extractedmZhongchao (middle surpass)
Figure FDA0002404614640000025
The position of (1), namely the position where the potential damage in the port machine has occurred,
Figure FDA0002404614640000026
wherein ,
Figure FDA0002404614640000027
the average value of the gap state factor values of all vulnerable positions is obtained; y ismA gap state factor value for each position; m is the number of the position which is easy to damage; n is the number of vulnerable positions.
CN202010159712.3A 2020-03-09 2020-03-09 Harbor machine damage positioning method based on residual stress gap state Active CN111444645B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010159712.3A CN111444645B (en) 2020-03-09 2020-03-09 Harbor machine damage positioning method based on residual stress gap state

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010159712.3A CN111444645B (en) 2020-03-09 2020-03-09 Harbor machine damage positioning method based on residual stress gap state

Publications (2)

Publication Number Publication Date
CN111444645A true CN111444645A (en) 2020-07-24
CN111444645B CN111444645B (en) 2023-06-20

Family

ID=71657426

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010159712.3A Active CN111444645B (en) 2020-03-09 2020-03-09 Harbor machine damage positioning method based on residual stress gap state

Country Status (1)

Country Link
CN (1) CN111444645B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112378999A (en) * 2020-10-28 2021-02-19 扬州大学 Method for quantitatively detecting port machine rail damage based on centroid guide threshold

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004081491A1 (en) * 2003-03-10 2004-09-23 Agellis Ab Method and device for determination of residual stresses
CN101270459A (en) * 2007-12-29 2008-09-24 大连交通大学 Method for improving welded joint fatigue strength following chilling treatment after weld toe TIG refusion
CN103359622A (en) * 2013-07-19 2013-10-23 中联重科股份有限公司 Crane and safety control system of boom thereof, and method, control device and system for detecting sidewise bending amount of boom
CN103874807A (en) * 2011-09-20 2014-06-18 科技矿业企业有限公司 Stress and/or accumulated damage monitoring system
CN106815419A (en) * 2017-01-03 2017-06-09 东南大学 A kind of crane running status online evaluation method based on crack information prediction
CN107430637A (en) * 2015-03-05 2017-12-01 株式会社神户制钢所 Residual stress estimates method and residual stress estimating device
CN107844622A (en) * 2017-09-04 2018-03-27 湘潭大学 A kind of simply supported beam damage recognition methods based on faulted condition uniform load face curvature
CN109270170A (en) * 2018-11-21 2019-01-25 扬州大学 A kind of sensitivity amendment loading machine Structural Damage Identification considering Jie's scale
CN110133016A (en) * 2019-04-16 2019-08-16 平高集团有限公司 A kind of method of welding value auxiliary X-ray diffraction detection residual stress
CN110741136A (en) * 2017-06-20 2020-01-31 西门子公司 Extended life of power turbine disks exposed to corrosion damage in use

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004081491A1 (en) * 2003-03-10 2004-09-23 Agellis Ab Method and device for determination of residual stresses
CN101270459A (en) * 2007-12-29 2008-09-24 大连交通大学 Method for improving welded joint fatigue strength following chilling treatment after weld toe TIG refusion
CN103874807A (en) * 2011-09-20 2014-06-18 科技矿业企业有限公司 Stress and/or accumulated damage monitoring system
CN103359622A (en) * 2013-07-19 2013-10-23 中联重科股份有限公司 Crane and safety control system of boom thereof, and method, control device and system for detecting sidewise bending amount of boom
CN107430637A (en) * 2015-03-05 2017-12-01 株式会社神户制钢所 Residual stress estimates method and residual stress estimating device
CN106815419A (en) * 2017-01-03 2017-06-09 东南大学 A kind of crane running status online evaluation method based on crack information prediction
CN110741136A (en) * 2017-06-20 2020-01-31 西门子公司 Extended life of power turbine disks exposed to corrosion damage in use
CN107844622A (en) * 2017-09-04 2018-03-27 湘潭大学 A kind of simply supported beam damage recognition methods based on faulted condition uniform load face curvature
CN109270170A (en) * 2018-11-21 2019-01-25 扬州大学 A kind of sensitivity amendment loading machine Structural Damage Identification considering Jie's scale
CN110133016A (en) * 2019-04-16 2019-08-16 平高集团有限公司 A kind of method of welding value auxiliary X-ray diffraction detection residual stress

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
徐高林;: "港口起重机疲劳破坏成因与修复措施分析", 数码世界 *
王旺生\N\N\N,游敏: "港机结构件焊接残余应力的调控与消除", 港口装卸 *
蔡福海;王欣;高顺德;赵福令;: "起重机结构疲劳强度与寿命评估方法分析", 中国工程机械学报 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112378999A (en) * 2020-10-28 2021-02-19 扬州大学 Method for quantitatively detecting port machine rail damage based on centroid guide threshold

Also Published As

Publication number Publication date
CN111444645B (en) 2023-06-20

Similar Documents

Publication Publication Date Title
CN104239681B (en) Axis system operational modal analysis method based on pulse excitation response signal crosspower spectrum function
CN102269655B (en) Method for diagnosing bearing fault
US9310345B2 (en) Sensor system, computer, and machine
CN111460702B (en) Structural member damage identification method based on forward and reverse damage feature fusion
CN113435018A (en) Damage calculation method for road load spectrum of automobile user
CN104236893A (en) Performance parameter test system and performance parameter test method of hydraulic damper
CN111444645A (en) Port machine damage positioning method based on residual stress gap state
CN108645620A (en) A kind of Fault Diagnosis of Rolling Element Bearings method based on comentropy and Multiscale Morphological
CN111597740A (en) Harvester health monitoring method based on mesoscale ultrasonic teratocardio-band
CN107122907B (en) Method for analyzing symbolized quality characteristics of mechanical and electrical products and tracing fault reasons
CN115169401A (en) Cutter abrasion loss prediction method based on multi-scale DenseNet-ResNet-GRU model
CN109323791A (en) The residual stress distribution measurement method of composite board based on incremental cuts method
CN1782672A (en) Method and apparatus for improved fault detection in power generation equipment
CN104889821B (en) Numerically-controlled slide reliability cutting test method under simulated condition
CN115660466A (en) Budget auditing management system for power transmission and transformation project
CN104820399B (en) Based on the Tool Magazine in Machining Centers mechanical arm reliability test method of on-the-spot load characteristic
CN102650263A (en) Method and device for testing a wind turbine assembly
CN112857806B (en) Bearing fault detection method based on moving window time domain feature extraction
CN110489604B (en) Analysis method and system for test measurement data of gas turbine
CN106370419A (en) Vibration response non-linearity based transmission shaft crack positioning and detecting method
CN109540279B (en) Reverse compression perception recovery method for undersampled dynamic signals in high-speed milling process of machine tool
JP3634085B2 (en) Mounting factory diagnostic system
CN110990247A (en) Test system for validity of unattended issuing system
CN115408897A (en) Harbor machine health assessment method based on vibration spectrum discontinuous reverse correction
CN110501464B (en) Method and system for identifying damage degree and damage position of marine riser

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant