CN204514863U - A kind of turbine blade crack detection device - Google Patents
A kind of turbine blade crack detection device Download PDFInfo
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- CN204514863U CN204514863U CN201520175213.8U CN201520175213U CN204514863U CN 204514863 U CN204514863 U CN 204514863U CN 201520175213 U CN201520175213 U CN 201520175213U CN 204514863 U CN204514863 U CN 204514863U
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Abstract
The utility model provides a kind of turbine blade crack detection device, comprises sonac and single-chip microcomputer; Described sonac quantity is three, is respectively connected to single-chip microcomputer by amplifying circuit, bandwidth-limited circuit, comparator circuit successively, and three sonacs are apart 16cm ± 0.5cm between any two; The every road of described amplifying circuit comprises at least a slice instrument amplifier; The every road of described bandwidth-limited circuit at least comprises two panels operational amplifier; Described three sonacs be uniformly distributed be arranged on a circular The Cloud Terrace front edge position on, The Cloud Terrace is rotated by transverse axis motor and longitudinal axis Electric Machine Control; Described bandwidth-limited circuit is the bandwidth-limited circuit of 100kHz ~ 250kHz.The utility model utilizes ultrasonic signal in three level sensor stereoscopic monitoring blade cracks evolutions, adopts phase method and automatically carry out a position in conjunction with monolithic Electric Machine Control to follow the tracks of, and can accurately search crackle approximate range; Can non-contact detection be realized, install and detect all very convenient.
Description
Technical field
The utility model relates to a kind of turbine blade crack detection device, belongs to hydraulic turbine detection technique.
Background technology
The hydraulic turbine be catchment, machine, oil, electricity, gas in the huge nonlinear dynamic system of complexity of one, be equipment very crucial in Hydropower Unit, its health status will directly affect the running status of whole water turbine set.The hydraulic turbine often there will be after operation a period of time that blade loosens, crackle, fracture, cavitation and cavitation erosion and sand erosion; the abnormal vibrations of appearance and water guide turbine is in operation, the wherein safety and economic operation of the generation serious threat hydroelectric power plant of the blade cracks of rotary wheel of water turbine.
Chinese utility model patent ZL201420080423.4 discloses a kind of hydraulic turbine abnormity early warning system based on ultrasound examination, this early warning system adopts hyperacoustic mode, well can detect Abnormal Leaves, accuracy, anti-noise degree is all higher, need not contact and also can complete detection, but this early warning system cannot detect for the crackle of blade, first it detects audio frequency is 20KHz ~ 23KHz, and facts have proved that audio frequency that crackle produces is not at this audio section, secondly it adopts transmitting/receiving ultrasonic sensor, and blade cracks rear own rotation will produce ultrasound wave, the ultrasound wave adopting the words of transmitting/receiving ultrasonic sensor that blade can be caused to produce becomes noise, affect actual Detection results, moreover its ultrasonic sensor three is between two at a distance of 20cm, be unfavorable for that the situation to cracking detects.
Utility model content
For solving the problems of the technologies described above, the utility model provides a kind of turbine blade crack detection device, this turbine blade crack detection device utilizes ultrasonic signal in three level sensor stereoscopic monitoring blade cracks evolutions, adopt phase method and automatically carry out a position in conjunction with monolithic Electric Machine Control and follow the tracks of, can accurately search crackle approximate range.
The utility model is achieved by the following technical programs.
A kind of turbine blade crack detection device that the utility model provides, comprises sonac and single-chip microcomputer; Described sonac quantity is three, is respectively connected to single-chip microcomputer by amplifying circuit, bandwidth-limited circuit, comparator circuit successively, and three sonacs are apart 16cm ± 0.5cm between any two; The every road of described amplifying circuit comprises at least a slice instrument amplifier; The every road of described bandwidth-limited circuit at least comprises two panels operational amplifier; Described three sonacs be uniformly distributed be arranged on a circular The Cloud Terrace front edge position on, The Cloud Terrace is rotated by transverse axis motor and longitudinal axis Electric Machine Control; Described bandwidth-limited circuit is the bandwidth-limited circuit of 100kHz ~ 250kHz.
Described sonac is 400SR160 type sensor; Described single-chip microcomputer is Atmega16 single-chip microcomputer.
Described instrument amplifier is INA128 instrument amplifier; Described operational amplifier is double operational LM833N operational amplifier.
Also comprise acoustic-optic alarm and be connected to single-chip microcomputer.
The driving circuit of transverse axis motor and longitudinal axis motor is connected to single-chip microcomputer, and motor-drive circuit core is L298 driving chip.
Also comprise power converting circuit and be connected to single-chip microcomputer.
The beneficial effects of the utility model are: 1. utilize ultrasonic signal in three level sensor stereoscopic monitoring blade cracks evolutions, adopt phase method and automatically carry out a position in conjunction with monolithic Electric Machine Control to follow the tracks of, and can accurately search crackle approximate range; 2. can realize non-contact detection, install and detect all very convenient.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the side view of Fig. 1;
Fig. 3 is the utility model connection diagram;
Fig. 4 is the connection diagram of signal processing in Fig. 3;
Fig. 5 is the signal isolating amplifier circuit figure that in Fig. 4, sensor 1 processes branch road;
Fig. 6 is the bandwidth-limited circuit figure that in Fig. 4, sensor 1 processes branch road;
Fig. 7 is comparer and the magnitude demodulator circuit diagram that in Fig. 4, sensor 1 processes branch road;
Fig. 8 is The Cloud Terrace mobile tracking and sound light alarming circuit figure in Fig. 3.
In figure: 1-sensor, 2-The Cloud Terrace, 3-transverse axis motor, 4-longitudinal drive shaft, 5-longitudinal axis motor, 6-base.
Embodiment
Further describe the technical solution of the utility model below, but described in claimed scope is not limited to.
A kind of turbine blade crack detection device as shown in Figures 1 to 4, comprises sonac 1 and single-chip microcomputer; Described sonac 1 quantity is three, is respectively connected to single-chip microcomputer by amplifying circuit, bandwidth-limited circuit, comparator circuit successively, and three sonacs 1 are apart 16cm ± 0.5cm between any two; The every road of described amplifying circuit comprises at least a slice instrument amplifier; The every road of described bandwidth-limited circuit at least comprises two panels operational amplifier; Described three sonacs 1 be uniformly distributed be arranged on a circular The Cloud Terrace 2 front edge position on, The Cloud Terrace 2 controls to rotate by transverse axis motor 3 and longitudinal axis motor 5; Described bandwidth-limited circuit is the bandwidth-limited circuit of 100kHz ~ 250kHz.
Thus, by ultrasonic sensor, detect the acoustical signal sent in turbine blade crackle emergence and development process, judged the development degree of crackle by hyperacoustic intensity of detecting and frequency.And adopt three ultrasonic probes in systems in which, form isosceles triangle to ultrasound examination, the position of sound source is judged by phase method, and adopt the central point of two stepper motors formation The Cloud Terraces to three probes to carry out position adjustment, determine the approximate location of sound source, thus judge the roughly local of crackle.
Through detecting, blade cracks production process can send the vibrations of frequency distribution at 100kHz ~ 250kHz, and with ultrasonic signal, belong to the sound that frequency is higher, the sound that its feature rather low-frequency frequency is lower, attenuation amplitude is little, propagation farther, and quality, the early warning reliability of signal are secure.
Because blade cracks can produce ultrasound wave, therefore for ensureing Detection results, described sonac 1 is 400SR160 type sensor; Described single-chip microcomputer is Atmega16 single-chip microcomputer.
Described instrument amplifier is INA128 instrument amplifier; Described operational amplifier is double operational LM833N operational amplifier.
Also comprise acoustic-optic alarm and be connected to single-chip microcomputer.
The driving circuit of transverse axis motor 3 and longitudinal axis motor 5 is connected to single-chip microcomputer, and motor-drive circuit core is L298 driving chip.
Also comprise power converting circuit and be connected to single-chip microcomputer.
As shown in Figure 4, signal processing is first by being divided into 3 independently to process branch road, and the corresponding sensor signal in each road, processing form and the circuit structure on three tunnels are basically identical.Process branch road as explanation using sensor 1, be divided into 5 step process: signal isolation, signal amplification, bandpass filtering, signal are compared, signal amplitude detection.Output signal current signal is delivered in " signal isolation " and is isolated by sensor, reduce the contact of late-class circuit and front stage circuits, then buffer circuit output signal is passed through " signal amplification " circuit again and is amplified, obtain the large-signal facilitating filtering, amplifying signal just can obtain the signal of corresponding frequency band 100kHz ~ 250kHz through " bandpass filtering ", this signal passes through frequency and the amplitude that " comparer " and " magnitude demodulator " obtains signal again, finally delivers in single-chip microcomputer.
As shown in Figure 5, sensor signal isolating amplifier circuit comprises sensor S1, operational amplifier U1 (OP37A), U2 (LM393), resistance R1, R2, R3, electric capacity C1.5V power supply receives the positive pole of S1 by resistance R1, R2, more logical S1 negative pole connecting resistance R3 to GND.After sensor S1 experiences ultrasound wave, ultrasonic signal is converted to the current signal of corresponding frequency.C1 is capacitance, for the DC component in current signal being removed.U1 amplifier is used as buffer circuit, input signal and output signal isolated, and the current signal of sensor is changed into voltage signal.U2 is instrument amplifier INA128, and resistance R3 forms signal amplification circuit, and the major function of this circuit is amplified at U2 No. 6 pin output signals, then sent by port P1:A.
As shown in Figure 6, bandwidth-limited circuit forms active band-pass filter primarily of double operational LM833N operational amplifier and resistance, electric capacity.Element has U3:A, U3:B (LM833N), resistance R4 ~ R10, electric capacity C2 ~ C5.It is 100kHz ~ 250kHz that this circuit band leads to scope, undesired signal in main filtered signal, improves the degree of purity of signal.The input signal of bandwidth-limited circuit is inputted by port P1:B, and the P1:A port in P1:B and Fig. 5 is connected.The signal exported is exported by port P2:A, and port P2:A is connected to P2:B in Fig. 7.
As shown in Figure 7, in comparer and magnitude demodulator circuit, the function of comparer is that signal is changed into square-wave signal, so that single-chip microcomputer counts, this circuit U 5 (OP37A) is formed.Its input signal port is P2:B, and output port is F1, is connected to the PD2 port of U6 in Fig. 8 (Atmega16).The function of magnitude demodulator circuit is that signal is carried out the amplitude that half-wave rectification obtains signal, and by diode D1, electric capacity C6, resistance R12 form, and its output port is AD1, are connected to the PA1 port of U6 in Fig. 8 (Atmega16)
Fig. 8 is that The Cloud Terrace follows the tracks of driving circuit and sound light alarming circuit.Single-chip microcomputer adopts Atmega16 single-chip microcomputer, is mainly used for carrying out AD sampling, external counting, and drives sound light alarming circuit and motor-drive circuit.
Wherein PA1, PA2, PA3 pin of U6 gathers AD1, AD2, AD3 port signal, obtains digital signal, the amplitude signal after AD1, AD2, AD3 port signal difference respective sensor 1,2,3 processes.
The square-wave signal of F1 is wherein accepted by the external interrupt INT0 of the PD2 pin of U6, external interrupt is produced with rising edge, in INT0 interrupt function, accept F2,3 signal rising edges by external interrupt INT1, the INT2 of PD3, PB2 pin of U6, and counted by inside and calculate the phase differential of F2, F3 signal relative to F1; Square-wave signal after F1, F2, F3 port square wave difference respective sensor 1,2,3 processes.
Acoustooptic alarm system is realized by Single-chip Controlling LED and hummer, and sound light alarming circuit includes resistance R13, R14, R15, R16, D2 red LED, NPN triode Q1, Q2, hummer BUZ1.By PC0, PC of U6 1 pin produce low and high level time, drive conducting and the closedown of triode Q1, Q2, thus make hummer and LED start and stop.
The Cloud Terrace follows the tracks of the realization being carried out movement by motor, and the driving circuit of motor comprises motor drive ic L298, electric capacity C7, C8, diode D3 ~ D10, two direct current generators motor1, motor2.IN1 ~ IN4 pin of L298 is connected with single-chip microcomputer PC4 ~ PC7 pin, and ENA, ENB are connected with single-chip microcomputer PD4, PD5.IN1, IN2 for controlling turning to of motor motor1, when IN1 for the flat INT2 of high point be low level time, motor rotates forward, on the contrary reversion, INT3, INT4 turn to for control motor2's.ENA, ENA, by accepting the PWM drive singal of single-chip microcomputer, can control the rotating speed of two motors.Electric capacity C1, C2 are power filter and voltage stabilizing.8 diodes protect for over current of motor.
Claims (6)
1. a turbine blade crack detection device, comprise sonac (1) and single-chip microcomputer, it is characterized in that: described sonac (1) quantity is three, respectively be connected to single-chip microcomputer by amplifying circuit, bandwidth-limited circuit, comparator circuit successively, three sonacs (1) are apart 16cm ± 0.5cm between any two; The every road of described amplifying circuit comprises at least a slice instrument amplifier; The every road of described bandwidth-limited circuit at least comprises two panels operational amplifier; Described three sonacs (1) be uniformly distributed be arranged on a circular The Cloud Terrace (2) front edge position on, The Cloud Terrace (2) controls to rotate by transverse axis motor (3) and longitudinal axis motor (5); Described bandwidth-limited circuit is the bandwidth-limited circuit of 100kHz ~ 250kHz.
2. turbine blade crack detection device as claimed in claim 1, is characterized in that: described sonac (1) is 400SR160 type sensor; Described single-chip microcomputer is Atmega16 single-chip microcomputer.
3. turbine blade crack detection device as claimed in claim 1, is characterized in that: described instrument amplifier is INA128 instrument amplifier; Described operational amplifier is double operational LM833N operational amplifier.
4. turbine blade crack detection device as claimed in claim 1, is characterized in that: also comprise acoustic-optic alarm and be connected to single-chip microcomputer.
5. turbine blade crack detection device as claimed in claim 1, it is characterized in that: the driving circuit of transverse axis motor (3) and longitudinal axis motor (5) is connected to single-chip microcomputer, motor-drive circuit core is L298 driving chip.
6. turbine blade crack detection device as claimed in claim 1, is characterized in that: also comprise power converting circuit and be connected to single-chip microcomputer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520175213.8U CN204514863U (en) | 2015-03-26 | 2015-03-26 | A kind of turbine blade crack detection device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520175213.8U CN204514863U (en) | 2015-03-26 | 2015-03-26 | A kind of turbine blade crack detection device |
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| CN204514863U true CN204514863U (en) | 2015-07-29 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104730149A (en) * | 2015-03-26 | 2015-06-24 | 中国电建集团贵阳勘测设计研究院有限公司 | Hydraulic turbine blade crack detection device |
| CN111595274A (en) * | 2019-02-21 | 2020-08-28 | 宝山钢铁股份有限公司 | Testing device and testing method for rapidly detecting depth of full circumferential cracks at bottom of V-shaped groove of profile steel roller |
-
2015
- 2015-03-26 CN CN201520175213.8U patent/CN204514863U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104730149A (en) * | 2015-03-26 | 2015-06-24 | 中国电建集团贵阳勘测设计研究院有限公司 | Hydraulic turbine blade crack detection device |
| CN111595274A (en) * | 2019-02-21 | 2020-08-28 | 宝山钢铁股份有限公司 | Testing device and testing method for rapidly detecting depth of full circumferential cracks at bottom of V-shaped groove of profile steel roller |
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