CN109283253A - One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method - Google Patents

One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method Download PDF

Info

Publication number
CN109283253A
CN109283253A CN201811433475.4A CN201811433475A CN109283253A CN 109283253 A CN109283253 A CN 109283253A CN 201811433475 A CN201811433475 A CN 201811433475A CN 109283253 A CN109283253 A CN 109283253A
Authority
CN
China
Prior art keywords
ultrasonic
ultrasonic wave
receiving transducer
transmitting probe
wave receiving
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201811433475.4A
Other languages
Chinese (zh)
Inventor
张玉燕
李永保
温银堂
张芝威
潘钊
贾斌
付凯
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.)
Yanshan University
Original Assignee
Yanshan 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 Yanshan University filed Critical Yanshan University
Priority to CN201811433475.4A priority Critical patent/CN109283253A/en
Publication of CN109283253A publication Critical patent/CN109283253A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04Analysing solids
    • G01N29/06Visualisation of the interior, e.g. acoustic microscopy
    • G01N29/0654Imaging
    • G01N29/069Defect imaging, localisation and sizing using, e.g. time of flight diffraction [TOFD], synthetic aperture focusing technique [SAFT], Amplituden-Laufzeit-Ortskurven [ALOK] technique
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04Analysing solids
    • G01N29/06Visualisation of the interior, e.g. acoustic microscopy
    • G01N29/0609Display arrangements, e.g. colour displays
    • G01N29/0645Display representation or displayed parameters, e.g. A-, B- or C-Scan
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/02Indexing codes associated with the analysed material
    • G01N2291/028Material parameters
    • G01N2291/0289Internal structure, e.g. defects, grain size, texture

Landscapes

  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Abstract

The invention discloses one kind to be based on ultrasonic principle light ceramics base porous compound material defect inspection method, ultrasonic wave transmitting probe and ultrasonic wave receiving transducer are immersed in the water simultaneously, ultrasonic wave transmitting probe is with ultrasonic wave receiving transducer perpendicular to the two sides of light porous ceramic based composites to be detected;Ultrasonic wave transmitting probe moves back and forth to be scanned light porous ceramic based composites to be detected with ultrasonic wave receiving transducer in the direction x-y of the two sides of light porous ceramic based composites to be detected, data collecting card acquires the ultrasonic signal that ultrasonic wave receiving transducer receives and is transferred to the computer for being equipped with LabVIEW program, the data of acquisition are carried out maximum value projection and rebuild to obtain ultrasonic C-scan Image by LabVIEW, it may recognize that defect area, also just complete fault in material test experience.Compared with prior art, the present invention may be implemented to ceramic matric composite Hole, be mingled with and the detection of the defect risks such as unsticking.

Description

One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method
Technical field
The present invention relates to light ceramics base porous compound material defect detecting technique fields, especially a kind of former based on ultrasound Manage light ceramics base porous compound material defect inspection method.
Background technique
In all types of novel Composite Material in Space, the ceramic porous composite material of fiber rigidity has lightweight, antioxygen Change, high specific strength, high ratio modulus, high temperature resistant, creep resistant, fatigue limit be good and the excellent properties such as high-wearing feature, thus aviation, Space industry is widely applied.But the detection about the type composite structure bonding defect, it there is no at present perfect Examination criteria and appraisement system, quality of adhesive detection is carried out to such material and assessment not only has a extensive future but also meaning is deep Far.
In recent years, supersonic testing method was because of high sensitivity, harmless, easy to automate, operation easily grasp, experiment The advantages that equipment can simply carry is widely used in the defects detection of Aeronautics and Astronautics field composite material.To being at present Only, Wei Q using empty coupling ultrasonic technique realize the detection to GFRP covering Nomex honeycomb sandwich composite debonding defect and The detection of ceramic matric composite interior laminate layer defect.It is more that WS Ji etc. using ultrasonic pulse-echo method has studied rocket engine The bonding defect of layer bonded structure.For ceramic porous heat-barrier material bonding defect, Y Wen on the basis of ECT detection system, Propose a kind of Landwebe iterative algorithm for improving initial value, the reconstruction quality for improving defect image by a relatively large margin.Mei Hui Elaborate the present Research detected using infrared thermal imaging, industry CT, X-ray, ultrasonic wave and acoustic emission to CMC material, Wherein ultrasound part mainly have studied the stiffness coefficient of CMC material, elastic behavior and derogatory behaviour under tensile load with And lamination defect of material internal etc..GK Sun successfully is detected diameter in CMC material using Laser Ultrasonic Technique and is greater than 5mm's Interior laminate layer phenomenon.DTD Salvo et al. has studied the mechanical property and its characterization of CMC material.S Poges etc. has studied continuously The preparation and characterization of fiber reinforcement CMC material.Luo Ming is surveyed by acoustical parameter of the ultrasonic water immersion impulse method to CMC material It is fixed.The microstructure and fiber orientation and local delamination and hole defect of D Koch combination CMC material, using modeling method come The result of description experiment test.Z Chen studies the metallic matrix performance of ceramic/metal composite armour, has obtained sound wave Dispersion curve in ceramic/metal matrix medium, and analyze influence of the metallic matrix physical parameter variation to dispersion curve.
But above-mentioned detection method experimental facilities is complicated, Meteorological is high, and cumbersome, and detection efficiency is not high.
Summary of the invention
The invention aims to solve the deficiencies in the prior art, provide a kind of based on ultrasonic principle light ceramics Base porous compound material defect inspection method, for being bonded, be mingled with and hole present in light ceramics base porous compound material The detection of the danger such as hole type defect.
In order to achieve the above objectives, the present invention is implemented according to following technical scheme:
One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method, comprising the following steps:
Step 1: will be immersed in the water after light porous ceramic based composites to be detected cladding with preservative film first, simultaneously Ultrasonic wave transmitting probe and ultrasonic wave receiving transducer are immersed in the water simultaneously, the ultrasonic wave transmitting probe and ultrasonic wave are received and visited Two sides of the head perpendicular to light porous ceramic based composites to be detected, and ultrasonic wave transmitting probe and ultrasonic wave receiving transducer In the same horizontal line, ultrasonic signal is sent to ultrasonic wave transmitting probe by ultrasonic signal generator, ultrasonic wave is through water It travels in light porous ceramic based composites to be detected;
Step 2: ultrasonic wave transmitting probe and ultrasonic wave receiving transducer are in light porous ceramic based composites to be detected The direction x-y of two sides moves back and forth to be scanned light porous ceramic based composites to be detected, data collecting card The ultrasonic signal that acquisition ultrasonic wave receiving transducer receives is then delivered to the LabVIEW program in computer.When to be tested When sample bonding layer existing defects, portion of ultrasonic sound wave can be reflected by defect interface, then the signal received can be by different degrees of Decaying.If zero defect in sample to be tested bonding layer, the ultrasonic transmission wave energy comparison that receiving transducer receives is high.In host computer LabVIEW software by the collected ultrasonic transmission wave amplitude information of capture card using maximum value projection algorithm rebuild i.e.: visiting A ultrasonic signal is recorded at each scan position of head, takes the peak-to-peak value of this signal, it is corresponding to be then assigned to this position The array element of reconstruction image matrix, realizes the correspondence of ultrasonic signal maximum amplitude and reconstruction image gray value, to obtain corresponding Plane monitoring-network image, i.e. Ultrasonic C-Scan reconstruction image, are then shown by LabVIEW software interface;It is super because what is received Acoustical signal amplitude is not of uniform size, and the gray value size of each pixel can be different in reconstruction image, is rebuild and is schemed according to Ultrasonic C-Scan The comparison of different zones color, can identify the defects of detection image region as in, and it is real to complete a fault in material detection It tests.
Further, the ultrasonic signal of the ultrasonic signal generator transmitting is defeated after wideband power amplifer amplifies Ultrasonic wave transmitting probe is arrived out.
Further, the ultrasonic wave transmitting probe is driven with ultrasonic wave receiving transducer by three-dimensional machinery scanning means, three-dimensional Mechanical scanner is by two for driving ultrasonic wave transmitting probe and ultrasonic wave receiving transducer in light porous ceramic to be detected The motor and motor driver that the direction x of the two sides of based composites and the direction y move back and forth are constituted, and motor driver passes through DAQ equipment NI USB-6251 is connected with computer, and the LabVIEW program in computer is sent to DAQ equipment NI USB-6251 Control signal makes motor action.
Further, the Scanning step of the ultrasonic wave transmitting probe and ultrasonic wave receiving transducer is 0.125mm/ times.
Compared with prior art, the present invention may be implemented to ceramic matric composite Hole, be mingled with and unsticking etc. is dangerous Property defect detection, wherein hole type and be mingled with type defects detection effect it is more satisfactory, and can detecte the hole of diameter 1mm Hole type defect.The present invention is the defects detection of the light ceramics based composites of strong sound absorbing performance, data analysis and bonding quality Technical foundation has been established in assessment.
Detailed description of the invention
Fig. 1 is C-scan detection system structural block diagram of the invention.
Fig. 2 is scan path and image-forming principle schematic diagram of the invention.
Fig. 3 is sample 1 and reconstruction image;(a) it is sample 1, is (b) image after reconstruction.
Fig. 4 is sample 2 and reconstruction image;(a) it is sample 2, is (b) image after reconstruction.
Fig. 5 is sample 3 and reconstruction image;(a) it is sample 3, is (b) image after reconstruction.
Fig. 6 is sample 4 and reconstruction image;(a) it is sample 4, is (b) image after reconstruction.
Specific embodiment
To make the objectives, technical solutions, and advantages of the present invention more comprehensible, below in conjunction with drawings and examples, to this Invention is described in further detail.Described herein the specific embodiments are only for explaining the present invention, is not used to limit Invention.
As shown in Figure 1, one kind of the present embodiment is based on ultrasonic principle light ceramics base porous compound material defects detection side Method first has to build detection system, the detection system mainly by being equipped with the computer of LabVIEW program, ultrasonic signal is sent out Raw device, three-dimensional machinery scanning means, power amplifier, ultrasonic wave transmitting probe 2, ultrasonic wave receiving transducer 3, data collecting card group At;Three-dimensional machinery scanning means is made of two motors and motor driver, and workpiece 1 is immersed in the water, ultrasonic wave transmitting probe 2 with Ultrasonic wave receiving transducer 3 is immersed in the water, and the ultrasonic wave transmitting probe 2 is with ultrasonic wave receiving transducer 3 perpendicular to the two sides of workpiece 1 Face, and ultrasonic wave transmitting probe 2 and ultrasonic wave receiving transducer 3 are in the same horizontal line, using LabVIEW program in computer to DAQ equipment NI USB-6251, which sends control signal, makes motor driven systems work to drive three-dimensional machinery scanning means mobile, Ultrasonic wave transmitting probe 2, ultrasonic wave receiving transducer 3 are scanned workpiece 1 according to predefined paths, ultrasonic signal by Ultrasonic signal generator generates, and is received after power amplifier amplifies and penetrates workpiece by ultrasonic wave receiving transducer 3, NI PCI-5122 data collecting card acquires ultrasonic signal in real time and sends computer to, and LabVIEW carries out the data of acquisition most Big value backprojection reconstruction (records a ultrasonic signal i.e. at each scan position of probe, takes the peak-to-peak value of this signal (maximum Value), it is then assigned to the array element of the corresponding reconstruction image matrix in this position, realizes ultrasonic signal maximum amplitude and reconstruction image ash The correspondence of angle value) ultimately form Ultrasonic C-Scan reconstruction image.
When being detected using the detection system of above-mentioned building to light ceramics base porous compound material defects detection, specifically Steps are as follows:
Step 1: first water will be immersed after workpiece 1 (light porous ceramic based composites to be detected) cladding with preservative film In, while ultrasonic wave transmitting probe 2 and ultrasonic wave receiving transducer 3 being immersed in the water simultaneously, the ultrasonic wave transmitting probe 2 with it is super Acoustic receiver probe 3 is perpendicular to the two sides of workpiece 1, and ultrasonic wave transmitting probe 2 and ultrasonic wave receiving transducer 3 are in same level On line, ultrasonic signal, ultrasonic wave water-borne transmission to workpiece are sent to ultrasonic wave transmitting probe 2 by ultrasonic signal generator In 1;
Step 2: the LabVIEW program in computer sends control signal to DAQ equipment NI USB-6251 and makes motor Make, the Scanning step of ultrasonic wave transmitting probe 2 and ultrasonic wave receiving transducer 3 is 0.125mm/ times, and then drives ultrasonic wave transmitting Probe 2 is moved back and forth with ultrasonic wave receiving transducer 3 in the direction x of the two sides of workpiece 1 and the direction y to more to lightweight to be detected Hole ceramic matric composite is scanned, scan path 4, and data collecting card acquisition ultrasonic wave receiving transducer 3 receives super Acoustic signals simultaneously send the computer for being equipped with LabVIEW program to, and the data of acquisition are carried out maximum value projection weight by LabVIEW It builds and (records a ultrasonic signal i.e. at each scan position of probe, take the peak-to-peak value (maximum value) of this signal, then assign To the array element of the corresponding reconstruction image matrix in this position, pair of ultrasonic signal maximum amplitude and reconstruction image gray value is realized Answer), to obtain corresponding plane monitoring-network image, i.e. Ultrasonic C-Scan reconstruction image, Ultrasonic C-Scan reconstruction image is in host computer LabVIEW is shown on interface.Because the ultrasonic signal amplitude that receiving transducer receives is not of uniform size, so Ultrasonic C-Scan rebuilds figure The gray value size of each pixel can be different as in, can be found out by the gray value comparison of Ultrasonic C-Scan reconstruction image scarce Trapping spot 5.
Further to verify feasibility of the invention, sensed system parameter is provided that trigger voltage 5V in experiment, sampling Rate 4MHz, sampling number 10000, external edging trigger, actual scanning step pitch is 0.125mm/ times, using special customized water Point focusing probe is soaked, wafer diameter is 6 millimeters, focal length 50mm, frequency 2.5Mhz.When detection composite material hole type lacks When falling into, because material has strong sound absorbing performance, the ultrasonic signal energy that fault location can be made to receive is greater than the energy at non-defective place, Take the ultrasonic amplitude received corresponding with the gray value of reconstruction image, to pass through different scanning field color in reconstruction image Difference identifies defect area;When detecting the unsticking and inclusion defect in composite structure, because in fault location incident medium Different from transmission medium acoustic impedance, portion of ultrasonic sound wave energy can be reflected, and the signal received is caused to be less than the super of non-defective place Acoustic wave energy identifies defect area eventually by the difference of different scanning field color in reconstruction image.
Hole type defects detection
The defective hole of different-diameter is implanted on No. 1 ceramic matric composite plate, as shown in table 1.Sample 1 having a size of 150mm × 150mm × 5mm, as shown in Fig. 3 (a), wherein iris out mark is probe physical scan area.It is using frequency The ultrasonic transducer of 2.5MHz detects composite material, is then filtered using MAT LAB to the ultrasound data received Wave, enhancing, reconstruction obtain the reconstruction image corresponding with scanning area as shown in Fig. 3 (b).
1 hole type defects detection result of table
Serial number Defect type Defect size Testing result
Defect is 1. Through-hole Φ1.0mm Detection
Defect is 2. Through-hole Φ1.5mm Detection
Defect is 3. Through-hole Φ2.0mm Detection
Defect is 4. Through-hole Φ2.5mm Detection
Defect is 5. Through-hole Φ3.0mm Detection
Defect is 6. Through-hole Φ3.5mm Detection
Defect is 7. Through-hole Φ4.5mm Detection
Defect is 8. Through-hole Φ5.0mm Detection
By testing result it is found that the system can detecte in ceramic matric composite when frequency probe is 2.5MHz Diameter is the defective hole of 1.0mm, and can clearly tell the hole defect of different-diameter.
The detection of air debonding defect
It is tested using No. 2 bonding exemplars, for exemplar having a size of 200mm × 200mm × 10mm, lower layer is the thick ceramics of 6mm Based composites, upper layer are 2mm thickness poly (methyl methacrylate) plate, and centre is by epoxy resin glue sticking, with a thickness of 2mm, in glue-line The air debonding defect of pre-buried irregular shape, as shown in Fig. 4 (a), iris out mark is probe physical scan area, scanning area Shown in the corresponding reconstruction image such as Fig. 4 (b) of domain.
Inclusion defect detection
Sample 3 is having a size of 100mm × 100mm × 10mm, and wherein insulation thickness is 6mm, organic glass plate thickness 2mm, Epoxy glue layer thickness 2mm.The pre-buried foamed glue inclusion defect in intermediate gelatine layer, shown in sample such as Fig. 5 (a), centre circle What is marked out is probe physical scan area, shown in the corresponding reconstruction image of scanning area such as Fig. 5 (b).
Sample 4 is having a size of 100mm × 100mm × 10mm, and wherein insulation thickness is 6mm, organic glass plate thickness 2mm, Epoxide-resin glue thickness 2mm.Detected waddy inclusion defect is labelled in Fig. 6 (a), wherein iris out mark is that probe is practical Scanning area.Fig. 6 (b) is the corresponding image reconstruction result of scanning area.
By testing result it is found that when frequency probe is 2.5MHz, system be capable of detecting when hole in material, unsticking and The dangerous type defect such as it is mingled with, it is preferable for the inclusion defects recognition effect such as foamed glue, waddy at glued layer, air unsticking is lacked Sunken accuracy of identification is also relatively low.Next the software and hardware of the system is required further improvement to improve the resolution ratio and inspection of system Precision is surveyed, to complete detection and positioning, the quantitative analysis to aerospace ceramic matric composite bonding defect.
The limitation that technical solution of the present invention is not limited to the above specific embodiments, it is all to do according to the technique and scheme of the present invention Technology deformation out, falls within the scope of protection of the present invention.

Claims (4)

1. one kind is based on ultrasonic principle light ceramics base porous compound material defect inspection method, which is characterized in that including following Step:
Step 1: will be immersed in the water after light porous ceramic based composites to be detected cladding with preservative film first, while will surpass Sound wave transmitting probe is immersed in the water with ultrasonic wave receiving transducer, the ultrasonic wave transmitting probe and ultrasonic wave receiving transducer perpendicular to The two sides of light porous ceramic based composites to be detected, and ultrasonic wave transmitting probe and ultrasonic wave receiving transducer are in same water On horizontal line, by ultrasonic signal generator to ultrasonic wave transmitting probe send ultrasonic signal, ultrasonic wave water-borne transmission to It detects in light porous ceramic based composites;
Step 2: ultrasonic wave transmitting probe and ultrasonic wave receiving transducer are in the two sides of light porous ceramic based composites to be detected Face moves back and forth to be scanned light porous ceramic based composites to be detected according to the direction x-y, and data collecting card is adopted The ultrasonic signal that collection ultrasonic wave receiving transducer receives is then delivered in the LabVIEW program of computer and is handled, when When sample to be tested bonding layer existing defects, portion of ultrasonic sound wave can be reflected by defect interface, then the signal received can be by difference The decaying of degree, if zero defect in sample to be tested bonding layer, the ultrasonic transmission wave energy comparison that receiving transducer receives is high, on LabVIEW software in the machine of position rebuilds the collected ultrasonic transmission wave amplitude information of capture card using maximum value projection algorithm That is: a ultrasonic signal is recorded at each scan position of probe, is taken the peak-to-peak value of this signal, is then assigned to this position The array element of corresponding reconstruction image matrix realizes the correspondence of ultrasonic signal maximum amplitude and reconstruction image gray value, to obtain Corresponding plane monitoring-network image, i.e. Ultrasonic C-Scan reconstruction image, are then shown by LabVIEW software interface;Because receiving The ultrasonic signal amplitude arrived is not of uniform size, and the gray value size of each pixel can be different in reconstruction image, according to Ultrasonic C-Scan The comparison of different zones color in reconstruction image, can identify the defects of detection image region, complete a fault in material Test experience.
2. according to claim 1 be based on ultrasonic principle light ceramics base porous compound material defect inspection method, spy Sign is: the ultrasonic signal of the ultrasonic signal generator transmitting is output to ultrasound after wideband power amplifer amplifies Wave transmitting probe.
3. according to claim 1 be based on ultrasonic principle light ceramics base porous compound material defect inspection method, spy Sign is: the movement of the ultrasonic wave transmitting probe and ultrasonic wave receiving transducer is driven by three-dimensional machinery scanning means, three Dimension mechanical scanner is by two for driving ultrasonic wave transmitting probe and ultrasonic wave receiving transducer in light porous pottery to be detected The motor and motor driver that the direction x of the two sides of porcelain based composites and the direction y move back and forth are constituted, and motor driver is logical It crosses DAQ equipment NI USB-6251 to be connected with computer, the LabVIEW program in computer is sent out to DAQ equipment NI USB-6251 Control signal is sent to make motor action.
4. according to claim 1 be based on ultrasonic principle light ceramics base porous compound material defect inspection method, spy Sign is: the Scanning step of the ultrasonic wave transmitting probe and ultrasonic wave receiving transducer is 0.125mm/ times.
CN201811433475.4A 2018-11-28 2018-11-28 One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method Pending CN109283253A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811433475.4A CN109283253A (en) 2018-11-28 2018-11-28 One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811433475.4A CN109283253A (en) 2018-11-28 2018-11-28 One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method

Publications (1)

Publication Number Publication Date
CN109283253A true CN109283253A (en) 2019-01-29

Family

ID=65173918

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811433475.4A Pending CN109283253A (en) 2018-11-28 2018-11-28 One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method

Country Status (1)

Country Link
CN (1) CN109283253A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112326793A (en) * 2020-11-05 2021-02-05 北京理工大学 Manipulator backtracking movement method based on ultrasonic C-scan projection view defect relocation
CN112816557A (en) * 2019-11-18 2021-05-18 中国商用飞机有限责任公司 Defect detection method, device, equipment and storage medium
CN114076797A (en) * 2021-11-05 2022-02-22 清华大学 Internal damage detection method and device
CN114324599A (en) * 2022-01-05 2022-04-12 天津大学 Honeycomb sandwich plate debonding area ultrasonic C-scan quantitative method based on period reconstruction

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101672634A (en) * 2009-10-16 2010-03-17 中国电子科技集团公司第四十五研究所 Construction method of C-scan peak image of ultrasonic scanning microscope
CN105424810A (en) * 2015-11-11 2016-03-23 南昌航空大学 Evaluation method for uniformity of fiber reinforcement ceramic matrix composite

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101672634A (en) * 2009-10-16 2010-03-17 中国电子科技集团公司第四十五研究所 Construction method of C-scan peak image of ultrasonic scanning microscope
CN105424810A (en) * 2015-11-11 2016-03-23 南昌航空大学 Evaluation method for uniformity of fiber reinforcement ceramic matrix composite

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
刘松平等: "《先进复合材料无损检测技术》", 30 September 2017, 航空工业出版社 *
张国才等: "基于LabVIEW 的超声C 扫成像系统设计", 《无损检测》 *
彭鸽等: "《南京航空航天大学论文集 2006年 第4册》", 31 March 2007 *
杨小强等: "《虚拟仪器系统集成与工程应用》", 31 January 2018, 冶金工业出版社 *
陈积懋等: "《胶接结构与复合材料的无损检测》", 31 July 1984, 国防工业出版社 *
雷振山等: "《LabVIEW高级编程与虚拟仪器工程应用》", 28 February 2012, 中国铁道出版社 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112816557A (en) * 2019-11-18 2021-05-18 中国商用飞机有限责任公司 Defect detection method, device, equipment and storage medium
CN112326793A (en) * 2020-11-05 2021-02-05 北京理工大学 Manipulator backtracking movement method based on ultrasonic C-scan projection view defect relocation
CN114076797A (en) * 2021-11-05 2022-02-22 清华大学 Internal damage detection method and device
CN114076797B (en) * 2021-11-05 2023-04-07 清华大学 Internal damage detection method and device
CN114324599A (en) * 2022-01-05 2022-04-12 天津大学 Honeycomb sandwich plate debonding area ultrasonic C-scan quantitative method based on period reconstruction

Similar Documents

Publication Publication Date Title
CN109283253A (en) One kind being based on ultrasonic principle light ceramics base porous compound material defect inspection method
CN101101277B (en) High-resolution welding seam supersonic image-forming damage-free detection method
CN104990982B (en) Honeycomb sandwich structure ultrasonic imaging detection method based on automatic scanning
David Nondestructive inspection of composite structures: methods and practice
JP2009510393A (en) Inspection system and associated method
Qing et al. A real-time active smart patch system for monitoring the integrity of bonded repair on an aircraft structure
CN106802323A (en) A kind of ultrasonic total focus imaging system based on complete matrix data
US20060053891A1 (en) Apparatus and method for area limited-access through transmission ultrasonic inspection
Wallentine et al. A study on ground truth data for impact damaged polymer matrix composites
Zaiß et al. Use of thermography and ultrasound for the quality control of SMC lightweight material reinforced by carbon fiber tapes
CN114994177B (en) Ultrasonic defect detection method and device for composite board and composite board
Jurek et al. Non-contact excitation and focusing of guided waves in CFRP composite plate by air-coupled transducers for application in damage detection
Bustamante et al. Evaluation of defect detection in aluminium, CFRP and epoxy resin plates using non-contact air-coupled ultrasonic waves
Wang et al. Ultrasonic testing of carbon fiber-reinforced polymer composites
CN101241110B (en) Method for on-line and damage-free detection for low density material defect by thermo-acoustic technology
CN106645416B (en) A kind of thin-walled CFRP inside pipe fitting quality ultrasound phased array on-line testing method
Kim et al. Imaging defects in laminate composite plates using focused shear waves generated by air-coupled transducer
Cramer Research developments in nondestructive evaluation and structural health monitoring for the sustainment of composite aerospace structures at nasa
Hillger et al. Visualisation of guided wave propagation by ultrasonic imaging methods
Liu et al. Research on automatic positioning system of ultrasonic testing of wind turbine blade flaws
Hernandez Crespo Damage sensing in blades
Alcaide et al. Damage detection on Aerospace structures using PAMELA SHM System
Schaal et al. Automated nondestructive testing of composites using air-coupled guided ultrasound
Hillger et al. Lamb-waves for air-coupled ultrasonic testing with one-sided access
Mahmod et al. Fiber glass composite laminates (FGCL) measurement using 3 axis pulse echo scanning unit

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
CB03 Change of inventor or designer information
CB03 Change of inventor or designer information

Inventor after: Zhang Yuyan

Inventor after: Fu Kai

Inventor after: Li Wanda

Inventor after: Wen Yintang

Inventor after: Pan Zhao

Inventor after: Yuan Yi

Inventor after: Liang Xi

Inventor after: Li Yongbao

Inventor after: Zhang Zhiwei

Inventor after: Jia Bin

Inventor before: Zhang Yuyan

Inventor before: Li Yongbao

Inventor before: Wen Yintang

Inventor before: Zhang Zhiwei

Inventor before: Pan Zhao

Inventor before: Jia Bin

Inventor before: Fu Kai

RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20190129