Movatterモバイル変換


[0]ホーム

URL:


CN107037185B - Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time - Google Patents

Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time
Download PDF

Info

Publication number
CN107037185B
CN107037185BCN201710443291.5ACN201710443291ACN107037185BCN 107037185 BCN107037185 BCN 107037185BCN 201710443291 ACN201710443291 ACN 201710443291ACN 107037185 BCN107037185 BCN 107037185B
Authority
CN
China
Prior art keywords
sensor
composite material
curing
piezoelectric ceramics
ceramics piece
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.)
Expired - Fee Related
Application number
CN201710443291.5A
Other languages
Chinese (zh)
Other versions
CN107037185A (en
Inventor
王奕首
李煜坤
卿新林
孙虎
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.)
Xiamen University
Original Assignee
Xiamen 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 Xiamen UniversityfiledCriticalXiamen University
Priority to CN201710443291.5ApriorityCriticalpatent/CN107037185B/en
Publication of CN107037185ApublicationCriticalpatent/CN107037185A/en
Application grantedgrantedCritical
Publication of CN107037185BpublicationCriticalpatent/CN107037185B/en
Expired - Fee Relatedlegal-statusCriticalCurrent
Anticipated expirationlegal-statusCritical

Links

Classifications

Landscapes

Abstract

Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time, is related to composite material.Using can packaging ceramic piezoelectric patches and special material form co-curing sensor;The special material is using one of polycaprolactone etc.;Co-curing sensor is fixed on to the type chamber of mold in advance, co-curing sensor is reserved type chamber metallic channel and solidified after sealing;In composite material injection, flow process generates pressure change, and cure sensor generates electric signal to piezoelectric ceramics piece together, obtains composite material flowing advanced position;Composite material is solidified after being full of type chamber, and according to supersonic detection method, by the variation real-time monitoring curing degree of velocity of wave and amplitude, and co-curing sensor will be integrated in composite material surface after solidifying, directly as monitoring structural health conditions.

Description

Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time
Technical field
The present invention relates to composite materials, real-time for composite material life cycle more particularly, to piezoelectric ceramics piece sensorMonitoring method.
Background technique
Advanced composite material has many advantages, such as that specific strength and specific stiffness are high, performance can design, be easy to integrally formed, is lightweightThe ideal material of efficient configuration design is widely used in aerospace, communications and transportation, the latent warship in ocean, petrochemical industry and building and buildsBuild the heavy construction structure in equal fields.However, composite material is in large scale structure due to designing, manufacturing the limitation with detection techniqueThe superior function of upper application is also far from giving full play to, wherein most important reason is the absence of the reality to moulding process solidification processWhen monitor and control, product quality is difficult to ensure.Meanwhile composite material is vulnerable to impact injury, and the most mesh of defect can not be surveyed,Need advanced health monitoring technique ([1] COLPO F, HUMBERT L, BOTSIS J.Characterisation ofresidual st resses in a single fibre compositewith FBG sensor[J].CompositesScience and Technology,2007,67(9):1830-1841).Therefore, to composite material solidification process, processAccurate monitoring in real time is carried out with use process, to improving product quality, reduce cost, ensure that composite structure safety hasHighly important meaning.
Piezoelectric ceramics piece can be achieved on the conversion equipment of positive and negative piezoelectric effect, both can be based on direct piezoelectric effect to dynamicPressure is monitored, and the technologies such as ultrasound detection and supersonic guide-wave monitoring can be realized based on reversed piezoelcetric effect.It is pressed using ceramicsElectric piece is disc structure, radius 4mm, with a thickness of 0.2mm.
The used special material for first packaging ceramic piezoelectric patches, it is desirable that it is low with fusing point, initial strength is highFeature, and be one of resin matrix curing agent and one of modified material, such as polycaprolactone.
Mainly there are ultrasonic method, Fiber Optic Sensor, dielectric method, impedance method and calorifics for composite material solidification monitoring technology at this stageMethod mainly has supersonic guide-wave method, Fiber Optic Sensor, impedance method etc. for composite material structure health monitoring technology.Ultrasonic method is comparedOther monitoring methods have many advantages, such as that precision is high, structure is simple, at low cost.
Monitoring structural health conditions are to be using the distributed sensor networks being permanently integrated in body structure surface or embedded structureBasis is revolutionary innovative technology ([2] CROWLEY D M, WARD C, POTTER K.A status of determining structural intergrityof acceptance criteria and process requirements in advanced compositesmanufacturing,and whether they are fit for purpose[R].SAE Technical Pap-Er.2013), important work can be played in composite structure design, manufacture, military service and the life cycle management of maintenanceWith.
Summary of the invention
The purpose of the present invention is can not carry out life cycle management for existing composite molding and processing monitoring missingThe phenomenon that monitoring, while it being directed to the problems such as complicated for operation, precision is not high, at high cost in existing composite molding monitoring technology,Piezoelectric ceramics piece sensor is provided and is used for composite material life cycle method of real-time.
The present invention the following steps are included:
1) using can packaging ceramic piezoelectric patches and special material formation co-curing sensor;The special material, which uses, gathers oneselfOne of lactone etc.;
2) co-curing sensor is fixed on to the type chamber of mold in advance, co-curing sensor is reserved type chamber metallic channel and sealedAfter solidify;
3) when composite material injects, flow process generates pressure change, and cure sensor generates piezoelectric ceramics piece togetherElectric signal obtains composite material flowing advanced position;
4) composite material, according to supersonic detection method, passes through the variation reality of velocity of wave and amplitude full of being solidified after type chamberWhen monitor curing degree, and co-curing sensor will be integrated in composite material surface after solidifying, directly as monitoring structural health conditions.
In step 2), co-curing sensor and metallic channel are reserved in the mold, the depth of the metallic channel is togetherThe thickness of cure sensor is preferably identical;The sealing can be used identical material and be fixed;The mold can for metal die,One of composite material mould, ceramic material mold, quartz material mold, cement material mold, gypsum material mold etc.;InstituteStating cured temperature can be 60~180 DEG C, keep heating rate uniform, and heating rate is no more than 10 DEG C/min.In the moldSlot should ensure that cavity surface is smooth, sensor arrangement does not influence product surface quality after sensor encapsulation.
In step 3), fiber-reinforced resin matrix compound material is can be used in the composite material or Whisker reinforced resin-base is multipleOne of condensation material etc.;The liquid molding process of the composite material, which can be used, to be vacuumized;The flow front position is to makeResin flow front is incuded with the direct piezoelectric effect of piezoelectric ceramics piece.
In step 4), when the characterization curing degree of the supersonic detection method, velocity of wave V can be usedLThere is sensing in the side=2d/tWhen device and attenuation alpha=(1/d) 20log (A0/ A) characterization curing degree, wherein d is plate thickness, and t is time, A0To emit signal amplitude, ATo receive signal amplitude;When for monitoring structural health conditions, it can be used for supersonic guide-wave technology or acoustic emission;The ultrasound inspectionSurvey method is by co-curing sensor arrangement in composite material work piece side, piezoelectric ceramics piece connection signal capture card is sent outIt penetrates and also receives.
The present invention has technical effect following prominent:
1, easy to operate: the present invention forms co-curing combination sensor using special material and piezoelectric ceramics piece, directly usesSpecial material is encapsulated into mold inside groove again;
2, sensor does not impact composite property: special material be resin curing agent and modified material itOne, if polycaprolactone fusing point is 60 DEG C, technological temperature is more than 60 DEG C and curing reaction is for exothermic reaction, and polycaprolactone energy is completeIt is complete to incorporate resin.
3, sensor does not impact composite gauge: using the heating speed for being no more than 10 DEG C/min, resin existsCan be partially cured when reaching special material fusing point, overall viscosity increases, and special material dosage is seldom, and part can be equal to after thawingCuring agent can ensure that sensor is fixed on composite material surface.
4, system is simple: the reception and transmitting of signal can be carried out with set of system, in life cycle management monitoring allReal-time monitoring can be carried out using only piezoelectric ceramics.
5, the life cycle management monitoring that the present invention is able to achieve composite structure manufacture, is on active service and safeguards, piezoelectric ceramics pieceIt is finally integrated in composite material surface and forms structural healthy monitoring system.Structural healthy monitoring system is present large scale structure, friendshipThe current state-of-the art technological concept of industry, analyzing binding model by Real-time Monitoring Data can be predicted the service life, and ensure the peace of structureFull property and reliability.
Detailed description of the invention
Fig. 1 is the co-curing sensor schematic of the embodiment of the present invention.
Fig. 2 is special material and piezoelectric ceramics piece co-curing sensor schematic of the invention.
Fig. 3 is structural schematic diagram in mold of the invention.
Fig. 4 is the structural schematic diagram after piezoelectric ceramics piece and composite material co-curing of the invention.
Specific embodiment
The present invention is further illustrated with reference to the accompanying drawings and examples.
As shown in figures 1-4.Specific step is as follows for the embodiment of the present invention:
1) using can packaging ceramic piezoelectric patches 3 and the formation co-curing sensor 7 of special material 2;The special material 2 usesOne of polycaprolactone etc.;
2) co-curing sensor 7 is fixed on to the type chamber 6 of mold 10 in advance, co-curing sensor 7 reserves type chamber metallic channel 4And solidify after sealing;Co-curing sensor 7 and metallic channel 8, the depth and co-curing of the metallic channel 8 are reserved in the moldThe thickness of sensor 7 is preferably identical;The sealing can be used identical material and be fixed;The mold 10 can for metal die,One of composite material mould, ceramic material mold, quartz material mold, cement material mold, gypsum material mold etc.;InstituteStating cured temperature can be 60~180 DEG C, keep heating rate uniform, and heating rate is no more than 10 DEG C/min.In the moldSlot should ensure that cavity surface is smooth, sensor arrangement does not influence product surface quality after sensor encapsulation.
3) when composite material 11 injects, flow process generates pressure change, cure sensor 7 together of piezoelectric ceramics piece 3Electric signal is generated, 11 flow front position of composite material is obtained;Fiber-reinforced resin base composite wood can be used in the composite materialOne of material or Whisker Reinforced Polymer Composites etc.;The liquid molding process of the composite material, which can be used, to be vacuumized;The flow front position is that resin flow front is incuded using the direct piezoelectric effect of piezoelectric ceramics piece.
4) composite material 11, according to supersonic detection method, passes through the variation of velocity of wave and amplitude full of being solidified after type chamber 6Real-time monitoring curing degree, and co-curing sensor 7 will be integrated in 11 surface of composite material after solidifying, and supervise directly as structural healthIt surveys.When the characterization curing degree of the supersonic detection method, velocity of wave V can be usedLWhen there is a sensor in the side=2d/t and attenuation alpha=(1/d)20log(A0/ A) characterization curing degree, wherein d is plate thickness, and t is time, A0To emit signal amplitude, A is to receive signal amplitude;When for monitoring structural health conditions, it can be used for supersonic guide-wave technology or acoustic emission;The supersonic detection method, being will be solid altogetherChange sensor 7 and be arranged in composite material work piece side, piezoelectric ceramics piece connection signal capture card is made to emit also to receive.
Special material (such as polycaprolactone) and piezoelectric ceramics piece co-curing sensor are made in advance, and sensor is fixed in advanceIt is sensed in tank 5 and type chamber metallic channel 4 in mold cavity co-curing, groove depth cure sensor consistency of thickness, and reserved type togetherChamber metallic channel 4, is finally sealed using special material, to determine that special material has been fully cured;According to composite wood feed liquidBody formed technique requirement, in resin injection, flow process can generate pressure change, according to direct piezoelectric effect, piezoelectric ceramics pieceCo-curing sensor can generate electric signal, obtain resin flowing advanced position;Resin is solidified after being full of type chamber, according to ultrasoundTesting principle, by the variation of velocity of wave and amplitude come real-time monitoring curing degree;Piezoelectric ceramics piece sensor will integrate after hardeningComposite material surface, and composite material composed structure health monitoring systems, can be used active supersonic guide-wave monitoring technology andPassive type acoustic emission carries out real-time monitoring to composite structure integrality and damage.
In Fig. 1, label 1 is conducting wire, and 9 be seal groove.
The present invention is further illustrated below with composite liquid moulding process, and (special material selection gathers in oneselfEster).
As indicated with 1, the radius of piezoelectric ceramics piece is 4mm to co-curing sensor schematic of the invention, with a thickness of 0.2mm.Piezoelectric ceramics piece is integrally packaged using polycaprolactone, is still wafer type after encapsulation, radius 4.1mm, with a thickness of0.4mm。
The process for producing composite material that the present invention takes is liquid molding process.Mold shape is as shown in Fig. 2, selected moldOuter dimension is 600mm × 600mm × 40mm, and internal cavity is having a size of 400mm × 400mm × 3mm.With the intracavitary arrangement 4 of typeFor piezoelectric ceramics piece sensor, first opening four radiuses in mold cavity inner surface is 4.1mm, the counterbore slot of thickness 0.4mm, holeShoulder radius is 4.2mm, depth 0.1mm.The conducting wire used is the enameled wire of diameter 0.05mm, and 0.1mm length and width are opened in moldHigh metallic channel.Then encapsulation sensor and conducting wire are put into counterbore slot and metallic channel, and encapsulate sensing again with polycaprolactoneDevice removes extra polycaprolactone, guarantees that mould inner surface is smooth and polycaprolactone has been fully cured.Then according to liquid molding workSkill, coating release agent put the carbon fiber unidirectional cloth of 400mm × 400mm size, and 8 layers of cloth of laying are pressed [0/90/ ± 45]sAngle pavingIt puts.Vacuum is extracted after the laying release cloth of the top, borrows vacuum indentation resin can be to polycaprolactone table when resin flows through sensorFace generates a dynamic pressure, is eventually transferred to piezoelectric ceramics piece, generates electric signal, by sensor whether generate electric signal comeJudge whether resin flows through sensitive zones.After resin is full of type chamber, mold is put into insulating box and is heated in 80 DEG C30min, waits completion to be solidified, and when solidification, resin becomes solid from liquid, on the mechanical properties such as modulus and Poisson's ratio are started from scratchRise, and also with the physical-chemical reactions such as crosslinking, heat release, can velocity of wave to ultrasonic signal and amplitude have an impact, pass throughThe velocity of wave V of ultrasonic signalL=2d/t and amplitude α=(1/d) 20log (A0/ A) change to characterize curing degree, pass through following formula:
Use formulaWithCarry out accurate calculating curing degree.ρ is resin density, α in formulaUSTableShow that curing degree, L indicate resin storage volume modulus, L0Indicate initial volume modulus (when solidification does not complete), LfIndicate maximum storageBulk modulus (when solidification is completed).
Finally mold is taken out, opens mold, the co-curing product of sensor and finished product composition is taken out, carries out surface letterSingle processing.Shape is as shown in Figure 3.The sensing network of piezoelectric ceramics piece sensor composition has been permanently integrated at composite structureSurface can be used for the active monitoring based on supersonic guide-wave technology and the passive type monitoring based on acoustic emission.From resinThe monitoring structural health conditions of flow front finally, can in a set of acquisition system data acquisition.
It is monitored from producing to being worked into using whole life cycle in conclusion the present invention can be used for composite material, andWhole process can be monitored using only piezoelectric ceramics piece sensor, is not necessarily to other sensor-based systems.
The present invention provides a kind of methods that piezoelectric ceramics piece sensor is used for composite material life cycle real-time monitoring, mainWanting step includes: that piezoelectric ceramics piece positive and negative anodes are connected conducting wire, first uses special material packaging ceramic piezoelectric patches, which answersComposite property is not influenced, and the material is required to have the characteristics that fusing point is low, initial strength is high, and is the solidification of resin matrixOne of agent or one of modified material, such as polycaprolactone;The special material of molten condition is imported in the mold having had been prepared for andPiezoelectric ceramics piece is formed by curing encapsulation sensor;Then sensor is put into mold preformed groove, will be sensed using identical materialDevice and its fixed encapsulation of conducting wire;Remaining process flow is carried out according to composite liquid moulding process, and resin injection flowing can produceRaw dynamic pressure is transmitted to piezoelectric ceramics sector-meeting and generates electric signal;Material mechanical performance enhances at any time when solidification, can be to ceramicsThe ultrasonic velocity and amplitude size that piezoelectric patches generates have an impact;Workpiece is taken out in demoulding after curing molding and piezoelectric ceramics piece is totalCured article.The present invention not only realizes real-time monitoring composite liquid forming process, but also finally by piezoelectric ceramics piece groupAt sensing network can co-curing in composite material surface, can be used for the health monitoring technique of composite structure, to be compoundMaterial monitors from design, manufacture, military service and the life cycle management of maintenance and provides technical support.

Claims (6)

4) composite material, according to supersonic detection method, is supervised in real time full of being solidified after type chamber by the variation of velocity of wave and amplitudeCuring degree is surveyed, and co-curing sensor will be integrated in composite material surface after solidifying, directly as monitoring structural health conditions;It is described superWhen the characterization curing degree of sound detection method, with velocity of wave VLWhen there is a sensor in the side=2d/t and attenuation alpha=(1/d) 20log (A0/A)Curing degree is characterized, wherein d is plate thickness, and t is time, A0To emit signal amplitude, A is to receive signal amplitude;The ultrasound detectionMethod is by co-curing sensor arrangement in composite material work piece side, piezoelectric ceramics piece connection signal capture card is made to emitAlso it receives.
CN201710443291.5A2017-06-132017-06-13Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-timeExpired - Fee RelatedCN107037185B (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
CN201710443291.5ACN107037185B (en)2017-06-132017-06-13Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201710443291.5ACN107037185B (en)2017-06-132017-06-13Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time

Publications (2)

Publication NumberPublication Date
CN107037185A CN107037185A (en)2017-08-11
CN107037185Btrue CN107037185B (en)2019-04-12

Family

ID=59541810

Family Applications (1)

Application NumberTitlePriority DateFiling Date
CN201710443291.5AExpired - Fee RelatedCN107037185B (en)2017-06-132017-06-13Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time

Country Status (1)

CountryLink
CN (1)CN107037185B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN112649473B (en)*2020-11-022022-12-09湖北三江航天江河化工科技有限公司Method for monitoring curing process of lining layer of solid rocket engine
CN116242510A (en)*2022-12-212023-06-09天津大学 Health monitoring method for the service process of composite laminated connection structures

Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN101561400A (en)*2009-05-132009-10-21沈阳航空工业学院Method for repairing aged aircraft structural damage with optical fiber intelligent composite and monitoring health
CN206114428U (en)*2016-09-082017-04-19中国航空工业集团公司沈阳飞机设计研究所Airborne combined material stiffened plate structural test spare

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN101561400A (en)*2009-05-132009-10-21沈阳航空工业学院Method for repairing aged aircraft structural damage with optical fiber intelligent composite and monitoring health
CN206114428U (en)*2016-09-082017-04-19中国航空工业集团公司沈阳飞机设计研究所Airborne combined material stiffened plate structural test spare

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
复合材料连接结构健康监测技术研究进展;王奕首等;《复合材料学报》;20160131;第33卷(第1期);第3-4页

Also Published As

Publication numberPublication date
CN107037185A (en)2017-08-11

Similar Documents

PublicationPublication DateTitle
CN1090318C (en)Composite structure resin cure monitoring using an optical fiber grating sensor
CN104315990B (en) A test device for thermal molding and curing deformation of resin-based composite materials and its preparation and use method
CN109843557A (en) 3D printing method and equipment
CN107037185B (en)Piezoelectric ceramics piece sensor is used for composite material life cycle method of real-time
Krizsma et al.In-situ monitoring of deformation in rapid prototyped injection molds
CN107367523A (en)A kind of method of the effectively chemical shrinkage factor of same with thermosetting compound material of monitoring in real time
CN103913514A (en)Method for monitoring temperature and gradient cracks of large-volume concrete
CN104634488B (en)Deformation measurement method and device for airplane composite material stringer
CN105588673A (en)Method for monitoring acting force between mold and member by fiber grating sensor
Pasco et al.Characterisation of the thermoset prepreg compression moulding process
Yang et al.Failure mode analysis and prediction model of additively manufactured continuous carbon fiber‐reinforced polylactic acid
CN204625504U (en)PBX explosive shaped device
CN107685497A (en)Smart laminated plate and preparation method with damage real-time perception and warning function
RU2603798C1 (en)Method of forming articles of composite material
Nawab et al.A device to measure the shrinkage and heat transfers during the curing cycle of thermoset composites
JP2008044358A (en)Monitoring method for forming condition of fiber-reinforced plastic
Masmoudi et al.Structural health monitoring by acoustic emission of smart composite laminates embedded with piezoelectric sensor
CN105758793A (en)Curing procedure oriented method for monitoring interfacial force between composite materials and molds
CN102431183B (en) Forming mold and method for manufacturing molded parts using the mold
CN202401395U (en)Intelligent cable for bridge
CN202994738U (en)Mass concrete temperature gradient crack monitoring device
Mulvaney-Johnson et al.Real time diagnostics of gas/water assisted injection moulding using integrated ultrasonic sensors
RU2108910C1 (en)Method of manufacture of multi-ply panel of composite material
Ijaz et al.Vacuum consolidation of commingled thermoplastic matrix composites
Lin et al.Experimental study on forming quality of hat-shaped component based on combined mandrel pressurization method

Legal Events

DateCodeTitleDescription
PB01Publication
PB01Publication
SE01Entry into force of request for substantive examination
SE01Entry into force of request for substantive examination
GR01Patent grant
GR01Patent grant
CF01Termination of patent right due to non-payment of annual fee

Granted publication date:20190412

CF01Termination of patent right due to non-payment of annual fee

[8]ページ先頭

©2009-2025 Movatter.jp