CN104949838A - Band-pass filter circuit based engine test and control system - Google Patents

Band-pass filter circuit based engine test and control system Download PDF

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Publication number
CN104949838A
CN104949838A CN201510257667.4A CN201510257667A CN104949838A CN 104949838 A CN104949838 A CN 104949838A CN 201510257667 A CN201510257667 A CN 201510257667A CN 104949838 A CN104949838 A CN 104949838A
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China
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pole
triode
field effect
effect transistor
diode
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CN201510257667.4A
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程社林
曹诚军
余仁伟
文学
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Dynamic Test Instrument Co Ltd Of Sincere Nation In Chengdu
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Dynamic Test Instrument Co Ltd Of Sincere Nation In Chengdu
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Abstract

The invention discloses a band-pass filter circuit based engine test and control system. The system comprises a to-be-tested engine (1), a sensor system (3), a servo motor (2), a servo motor control system (4), a test platform PC (personal computer) (6) and a background server (7). The sensor system (3) and the servo motor (2) are connected with the to-be-tested engine (1), the test platform PC (6) is connected with the servo motor control system (4) which is connected with the servo motor (2), and the background server (7) is connected with the test platform PC (6). The system is characterized in that a band-pass filter circuit (5) is further arranged between the sensor system (3) and the test platform PC (6). The band-pass filter circuit based engine test and control system has the advantages that owing to the band-pass filter circuit, interference signals of the system can be filtered out, and consequently parameter signals of the to-be-tested engine are more accurate.

Description

A kind of engine TT&C system based on bandwidth-limited circuit
Technical field
The present invention relates to a kind of engine TT&C system, specifically refer to a kind of engine TT&C system based on bandwidth-limited circuit.
Background technology
People improve constantly the reliability of automobile, the requirement of the aspect such as security and green, and engine is as the heart component of automobile, its technical merit directly has influence on the performance index such as its dynamic property, economy and discharge, and the frequency of engine breakdown is also the highest.Engine performance measuring is the Main Means judging condition of the engine quality, and be also the important content of automotive check and maintenance job, therefore engine performance measuring is more and more subject to people's attention.As the detection system of test engine performance, engine TT&C system then seems that by for important, it is detection system indispensable on car engine machine production line.But, traditional engine TT&C system its cannot well process the every engine signal collected, thus cause system to engine various performance parameters test inaccurate, affect the outgoing of engine.Therefore, a kind of high-precision engine control system is provided to be then the current task of top priority.
Summary of the invention
It tests inaccurate defect to engine parameter to the object of the invention is to overcome traditional engine TT&C system, provides a kind of engine TT&C system based on bandwidth-limited circuit.
Object of the present invention is achieved through the following technical solutions: a kind of engine TT&C system based on bandwidth-limited circuit it comprise tested engine, the sensing system be connected with tested engine and servomotor, the servo control system be connected with servomotor, the test board PC be connected with servo control system, and the background server to be connected with test board PC, between sensing system and test board PC, be also provided with bandwidth-limited circuit.
Further, described bandwidth-limited circuit comprises amplifier P1, filtering chip U1, triode VT6, one end is connected with the positive pole of amplifier P1, the other end is then as the resistance R10 of the input end of this bandwidth-limited circuit, negative pole is connected with the output terminal of amplifier P1, the polar capacitor C4 that positive pole is then connected with the IN+ pin of filtering chip U1, one end is connected with the IN-pin of filtering chip U1, the resistance R11 of other end ground connection, be serially connected in the resistance R12 between the RG1 pin of filtering chip U1 and RG2 pin, negative pole is connected with the OUT pin of filtering chip U1, the polar capacitor C5 that positive pole is then connected with the emitter of triode VT6, and one end is connected with the emitter of triode VT6, the resistance R13 that the other end is then connected with the REF pin of filtering chip U1 forms.The minus earth of described amplifier P1; The VS+ pin of filtering chip U1 is connected with the base stage of triode VT6 with the equal ground connection of REF pin, its VS-pin, its RG2 pin is then connected with the collector of triode VT6; The emitter of described triode VT6 is then as the output terminal of this bandwidth-limited circuit.
Described servo control system is then by symmetrical expression field effect transistor driving circuit, and the trigger circuit be connected with symmetrical expression field effect transistor driving circuit form.Described symmetrical expression field effect transistor driving circuit is then by the first driving circuit, and the second driving circuit be connected with the first driving circuit forms.
Described first driving circuit is by triode VT1, field effect transistor Q1, field effect transistor Q2, one end is connected with the grid of field effect transistor Q2, the other end is then as the resistance R3 of the input end of this first driving circuit, the diode D1 be in parallel with resistance R3, one end is connected with the base stage of triode VT1, the resistance R1 that the other end is then connected with the P pole of diode D1, N pole is connected with the collector of triode VT1, the diode D2 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q2, P pole is connected with the second driving circuit, the diode D3 that N pole is then connected with the collector of triode VT1 after resistance R2, and positive pole is connected with the N pole of diode D3, the polar capacitor C1 that negative pole is then connected with the P pole of diode D2 forms, the P pole of described diode D1 is extremely all connected with trigger circuit with N, grounded emitter, its collector of described triode VT1 are then connected with the grid of field effect transistor Q1, the drain electrode of described field effect transistor Q1 is connected with the N pole of diode D3, its source electrode is then connected with the drain electrode of field effect transistor Q2, the source electrode of described field effect transistor Q2 is then connected with the second driving circuit and trigger circuit respectively.
The second described driving circuit is by field effect transistor Q3, field effect transistor Q4, triode VT5, one end is connected with the grid of field effect transistor Q4, the other end is then as the resistance R8 of the output terminal of this second driving circuit, the diode D6 be in parallel with resistance R8, one end is connected with the base stage of triode VT5, the resistance R9 that the other end is then connected with the P pole of diode D6, N pole is connected with the collector of triode VT5, the diode D5 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q4, P pole is connected with the P pole of diode D3, the diode D4 that N pole is then connected with the collector of triode VT5 after resistance R7, and positive pole is connected with the N pole of diode D4, the polar capacitor C3 that negative pole is then connected with the P pole of diode D5 forms, the P pole of described diode D6 is also connected with trigger circuit, grounded emitter, its collector of triode VT5 are then connected with the grid of field effect transistor Q3, the drain electrode of described field effect transistor Q3 is connected with the N pole of diode D4, its source electrode is then connected with the drain electrode of field effect transistor Q4, the source electrode of described field effect transistor Q4 is then connected with the source electrode of field effect transistor Q2.
Described trigger circuit are by triode VT2, triode VT3, flip chip U, the resistance R4 be in parallel with diode D1, the resistance R5 that one end is connected with the P pole of diode D1, the other end is then connected with the base stage of triode VT2, the resistance R6 of ground connection while one end is connected with the source electrode of field effect transistor Q2, the other end is then connected with the RESET pin of flip chip U, and the polar capacitor C2 that negative pole is connected with the emitter of triode VT3, positive pole is then connected with the base stage of triode VT4 forms; Grounded emitter, its collector of described triode VT2 are then connected with the N pole of diode D1; The base stage of described triode VT3 is connected with the collector of triode VT2, its collector is then connected with the collector of triode VT4; The grounded emitter of described triode VT4, its collector are then connected with the CLK pin of flip chip U and DATA pin respectively; The SET pin of described flip chip U is connected with its RESET pin, its Q2 pin is then connected with the P pole of diode D6.
In order to reach better implementation result, described flip chip U is preferably CD4013 integrated circuit, and field effect transistor Q1, field effect transistor Q2, field effect transistor Q3 and field effect transistor Q4 are all preferably enhancement mode PNP field effect transistor, filtering chip U1 is then preferably AD620 integrated circuit and realizes.
The present invention comparatively prior art compares, and has the following advantages and beneficial effect:
(1) the present invention uses servomotor to drag tested engine rotation, does not burn, when not doing work, using sensor to gather related data and analyze, assessing engine performance by calculating various engine parameter at engine.
(2) the present invention does not need the resource such as fuel consumption, chilled water, saves the cost in engine testing process.
(3) the present invention is without the need to combustion process, therefore energy-saving and environmental protection more.
(4) the present invention is by the effect of bandwidth-limited circuit, can filter out the undesired signal of system, makes the parameters signal of tested engine more accurate.
Accompanying drawing explanation
Fig. 1 is one-piece construction schematic diagram of the present invention;
Fig. 2 is servo control system electrical block diagram of the present invention;
Fig. 3 is bandwidth-limited circuit structural representation of the present invention.
Reference numeral name in above accompanying drawing is called:
1-tested engine, 2-servomotor, 3-sensing system, 4-servo control system, 5-bandwidth-limited circuit, 6-test board PC, 7-background server.
Embodiment
Below in conjunction with embodiment, the present invention is described in further detail, but embodiments of the present invention are not limited to this.
Embodiment
As shown in Figure 1, the present invention includes tested engine 1, the sensing system 3 be connected with tested engine 1 and servomotor 2, the servo control system 4 be connected with servomotor 2, the test board PC6 be connected with servo control system 4, the background server 7 be connected with test board PC6, in order to reach object of the present invention, the present invention is also provided with bandwidth-limited circuit 5 between sensing system 3 and test board PC6.
Wherein, sensing system 3 is made up of multiple sensor, and the present embodiment preferentially adopts torque sensor, temperature sensor and vibration transducer to realize, and it is for gathering moment of torsion, the signal such as temperature and vibration of tested engine 1.Various signals when bandwidth-limited circuit 5 is for working to tested engine 1 carry out filtering process.Servomotor 2 works for driving tested engine 1, and by adjusting the rotating speed of servomotor 2, the present invention can test the various data of tested engine 1 under different rotating speeds.Test board PC6 is as man-machine conversation window of the present invention, tester can send instruction to servo control system 4 on test board PC6, controlled by the rotating speed of servo control system 4 pairs of servomotors 2, simultaneously, test board PC6 can also receive the various parameters of tested engine 1, and sends to background server 7.Background server 7 stores all standard parameter of tested engine 1, its real-time parameter by the tested engine 1 of contrast and canonical parameter, thus judges that whether the properties of tested engine 1 is up to standard.
Background server 7 adopts existing computing machine, and test board PC6 then adopts existing single-chip microcomputer, and servomotor 2, sensing system 3 all adopt existing technology to realize.Bandwidth-limited circuit 5 is then emphasis of the present invention.
As shown in Figure 2, this servo control system 4 is by symmetrical expression field effect transistor driving circuit, and the trigger circuit be connected with symmetrical expression field effect transistor driving circuit form.Described symmetrical expression field effect transistor driving circuit is then by the first driving circuit, and the second driving circuit be connected with the first driving circuit forms.
Described first driving circuit is by triode VT1, field effect transistor Q1, field effect transistor Q2, one end is connected with the grid of field effect transistor Q2, the other end is then as the resistance R3 of the input end of this first driving circuit, the diode D1 be in parallel with resistance R3, one end is connected with the base stage of triode VT1, the resistance R1 that the other end is then connected with the P pole of diode D1, N pole is connected with the collector of triode VT1, the diode D2 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q2, P pole is connected with the second driving circuit, the diode D3 that N pole is then connected with the collector of triode VT1 after resistance R2, and positive pole is connected with the N pole of diode D3, the polar capacitor C1 that negative pole is then connected with the P pole of diode D2 forms.The P pole of described diode D1 is extremely all connected with trigger circuit with N; Grounded emitter, its collector of described triode VT1 are then connected with the grid of field effect transistor Q1; The drain electrode of described field effect transistor Q1 is connected with the N pole of diode D3, its source electrode is then connected with the drain electrode of field effect transistor Q2; The source electrode of described field effect transistor Q2 is then connected with the second driving circuit and trigger circuit respectively.
The second described driving circuit is by field effect transistor Q3, field effect transistor Q4, triode VT5, one end is connected with the grid of field effect transistor Q4, the other end is then as the resistance R8 of the output terminal of this second driving circuit, the diode D6 be in parallel with resistance R8, one end is connected with the base stage of triode VT5, the resistance R9 that the other end is then connected with the P pole of diode D6, N pole is connected with the collector of triode VT5, the diode D5 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q4, P pole is connected with the P pole of diode D3, the diode D4 that N pole is then connected with the collector of triode VT5 after resistance R7, and positive pole is connected with the N pole of diode D4, the polar capacitor C3 that negative pole is then connected with the P pole of diode D5 forms.The P pole of described diode D6 is also connected with trigger circuit; Grounded emitter, its collector of triode VT5 are then connected with the grid of field effect transistor Q3; The drain electrode of described field effect transistor Q3 is connected with the N pole of diode D4, its source electrode is then connected with the drain electrode of field effect transistor Q4; The source electrode of described field effect transistor Q4 is then connected with the source electrode of field effect transistor Q2.
Signal carries out reverse drive through field effect transistor Q3 and field effect transistor Q4 again after field effect transistor Q1 and field effect transistor Q2 drives, thus improves the control accuracy of the present invention to servomotor 2.Better drive effect to reach, described field effect transistor Q1, field effect transistor Q2, field effect transistor Q3 and field effect transistor Q4 preferentially adopt enhancement mode PNP field effect transistor to realize.
Described trigger circuit are by triode VT2, triode VT3, flip chip U, the resistance R4 be in parallel with diode D1, the resistance R5 that one end is connected with the P pole of diode D1, the other end is then connected with the base stage of triode VT2, the resistance R6 of ground connection while one end is connected with the source electrode of field effect transistor Q2, the other end is then connected with the RESET pin of flip chip U, and the polar capacitor C2 that negative pole is connected with the emitter of triode VT3, positive pole is then connected with the base stage of triode VT4 forms.Grounded emitter, its collector of described triode VT2 are then connected with the N pole of diode D1; The base stage of described triode VT3 is connected with the collector of triode VT2, its collector is then connected with the collector of triode VT4; The grounded emitter of described triode VT4, its collector are then connected with the CLK pin of flip chip U and DATA pin respectively; The SET pin of described flip chip U is connected with its RESET pin, its Q2 pin is then connected with the P pole of diode D6.In order to reach better implementation result, described flip chip U is preferably CD4013 integrated circuit to realize.
As shown in Figure 3, this bandwidth-limited circuit 5 is by amplifier P1, and filtering chip U1, triode VT6, resistance R10, resistance R11, resistance R12, resistance R13, polar capacitor C4 and polar capacitor C5 form.During connection, one end of resistance R10 is connected with the positive pole of amplifier P1, its other end is then as the input end of this bandwidth-limited circuit 5, the negative pole of polar capacitor C4 is connected with the output terminal of amplifier P1, its positive pole is then connected with the IN+ pin of filtering chip U1, one end of resistance R11 is connected with the IN-pin of filtering chip U1, its other end ground connection, resistance R12 is then serially connected between the RG1 pin of filtering chip U1 and RG2 pin, the negative pole of polar capacitor C5 is connected with the OUT pin of filtering chip U1, its positive pole is then connected with the emitter of triode VT6, one end of resistance R13 is connected with the emitter of triode VT6, its other end is then connected with the REF pin of filtering chip U1.The minus earth of described amplifier P1.The VS+ pin of filtering chip U1 is connected with the base stage of triode VT6 with the equal ground connection of REF pin, its VS-pin, its RG2 pin is then connected with the collector of triode VT6.The emitter of described triode VT6 is then as the output terminal of this bandwidth-limited circuit 5.This bandwidth-limited circuit 5 can filter out the undesired signal of system, makes the parameters signal of tested engine 1 more accurate.In order to better implement the present invention, this filtering chip U1 is preferably AD620 integrated circuit to realize.
As mentioned above, just well the present invention can be realized.

Claims (8)

1. the engine TT&C system based on bandwidth-limited circuit, it is by tested engine (1), the sensing system (3) be connected with tested engine (1) and servomotor (2), the servo control system (4) be connected with servomotor (2), the test board PC(6 be connected with servo control system (4)), and with test board PC(6) background server (7) that is connected forms, it is characterized in that: at sensing system (3) and test board PC(6) between be also provided with bandwidth-limited circuit (5), described bandwidth-limited circuit (5) is by amplifier P1, filtering chip U1, triode VT6, one end is connected with the positive pole of amplifier P1, the other end is then as the resistance R10 of the input end of this bandwidth-limited circuit (5), negative pole is connected with the output terminal of amplifier P1, the polar capacitor C4 that positive pole is then connected with the IN+ pin of filtering chip U1, one end is connected with the IN-pin of filtering chip U1, the resistance R11 of other end ground connection, be serially connected in the resistance R12 between the RG1 pin of filtering chip U1 and RG2 pin, negative pole is connected with the OUT pin of filtering chip U1, the polar capacitor C5 that positive pole is then connected with the emitter of triode VT6, and one end is connected with the emitter of triode VT6, the resistance R13 that the other end is then connected with the REF pin of filtering chip U1 forms, the minus earth of described amplifier P1, the VS+ pin of filtering chip U1 is connected with the base stage of triode VT6 with the equal ground connection of REF pin, its VS-pin, its RG2 pin is then connected with the collector of triode VT6, the emitter of described triode VT6 is then as the output terminal of this bandwidth-limited circuit (5).
2. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 1, it is characterized in that: described servo control system (4) is then by symmetrical expression field effect transistor driving circuit, and the trigger circuit be connected with symmetrical expression field effect transistor driving circuit form; Described symmetrical expression field effect transistor driving circuit is then by the first driving circuit, and the second driving circuit be connected with the first driving circuit forms.
3. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 2, it is characterized in that: described first driving circuit is by triode VT1, field effect transistor Q1, field effect transistor Q2, one end is connected with the grid of field effect transistor Q2, the other end is then as the resistance R3 of the input end of this first driving circuit, the diode D1 be in parallel with resistance R3, one end is connected with the base stage of triode VT1, the resistance R1 that the other end is then connected with the P pole of diode D1, N pole is connected with the collector of triode VT1, the diode D2 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q2, P pole is connected with the second driving circuit, the diode D3 that N pole is then connected with the collector of triode VT1 after resistance R2, and positive pole is connected with the N pole of diode D3, the polar capacitor C1 that negative pole is then connected with the P pole of diode D2 forms, the P pole of described diode D1 is extremely all connected with trigger circuit with N, grounded emitter, its collector of described triode VT1 are then connected with the grid of field effect transistor Q1, the drain electrode of described field effect transistor Q1 is connected with the N pole of diode D3, its source electrode is then connected with the drain electrode of field effect transistor Q2, the source electrode of described field effect transistor Q2 is then connected with the second driving circuit and trigger circuit respectively.
4. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 3, it is characterized in that: the second described driving circuit is by field effect transistor Q3, field effect transistor Q4, triode VT5, one end is connected with the grid of field effect transistor Q4, the other end is then as the resistance R8 of the output terminal of this second driving circuit, the diode D6 be in parallel with resistance R8, one end is connected with the base stage of triode VT5, the resistance R9 that the other end is then connected with the P pole of diode D6, N pole is connected with the collector of triode VT5, the diode D5 of ground connection while P pole is then connected with the drain electrode of field effect transistor Q4, P pole is connected with the P pole of diode D3, the diode D4 that N pole is then connected with the collector of triode VT5 after resistance R7, and positive pole is connected with the N pole of diode D4, the polar capacitor C3 that negative pole is then connected with the P pole of diode D5 forms, the P pole of described diode D6 is also connected with trigger circuit, grounded emitter, its collector of triode VT5 are then connected with the grid of field effect transistor Q3, the drain electrode of described field effect transistor Q3 is connected with the N pole of diode D4, its source electrode is then connected with the drain electrode of field effect transistor Q4, the source electrode of described field effect transistor Q4 is then connected with the source electrode of field effect transistor Q2.
5. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 4, it is characterized in that: described trigger circuit are by triode VT2, triode VT3, flip chip U, the resistance R4 be in parallel with diode D1, one end is connected with the P pole of diode D1, the resistance R5 that the other end is then connected with the base stage of triode VT2, one end is connected with the source electrode of field effect transistor Q2, the resistance R6 of ground connection while the other end is then connected with the RESET pin of flip chip U, and negative pole is connected with the emitter of triode VT3, the polar capacitor C2 that positive pole is then connected with the base stage of triode VT4 forms, grounded emitter, its collector of described triode VT2 are then connected with the N pole of diode D1, the base stage of described triode VT3 is connected with the collector of triode VT2, its collector is then connected with the collector of triode VT4, the grounded emitter of described triode VT4, its collector are then connected with the CLK pin of flip chip U and DATA pin respectively, the SET pin of described flip chip U is connected with its RESET pin, its Q2 pin is then connected with the P pole of diode D6.
6. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 5, is characterized in that: described flip chip U is CD4013 integrated circuit.
7. a kind of engine TT&C system based on bandwidth-limited circuit according to claim 6, is characterized in that: described field effect transistor Q1, field effect transistor Q2, field effect transistor Q3 and field effect transistor Q4 are enhancement mode PNP field effect transistor.
8. a kind of engine TT&C system based on bandwidth-limited circuit according to any one of Claims 1 to 5, is characterized in that: described filtering chip U1 is AD620 integrated circuit.
CN201510257667.4A 2015-05-19 2015-05-19 Band-pass filter circuit based engine test and control system Withdrawn CN104949838A (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2294329A1 (en) * 1974-12-11 1976-07-09 United Technologies Corp IMPROVED DETECTOR TO AVOID STALLING GAS TURBINE ENGINES AND METHOD FOR DETERMINING THE IMMINENCE OF THE MOMENT WHEN THE ENGINE STALLS BY MEANS OF THIS DETECTOR
CN1884992A (en) * 2005-06-22 2006-12-27 上海华依科技发展有限公司 Engine testing system and testing method thereof
CN201266130Y (en) * 2008-09-09 2009-07-01 上海师范大学 Dynamic balancing machine test device based on PC machine
CN201352178Y (en) * 2008-12-24 2009-11-25 天津雷沃动力股份有限公司 Starting device of trial-run bench of engine
CN101871834A (en) * 2010-04-23 2010-10-27 北京中科通视科技有限公司 Wireless remote water leakage detection device and system
CN102980771A (en) * 2012-12-04 2013-03-20 南京航空航天大学 Portable failure detection system and method for aero-engine gas path component

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2294329A1 (en) * 1974-12-11 1976-07-09 United Technologies Corp IMPROVED DETECTOR TO AVOID STALLING GAS TURBINE ENGINES AND METHOD FOR DETERMINING THE IMMINENCE OF THE MOMENT WHEN THE ENGINE STALLS BY MEANS OF THIS DETECTOR
CN1884992A (en) * 2005-06-22 2006-12-27 上海华依科技发展有限公司 Engine testing system and testing method thereof
CN201266130Y (en) * 2008-09-09 2009-07-01 上海师范大学 Dynamic balancing machine test device based on PC machine
CN201352178Y (en) * 2008-12-24 2009-11-25 天津雷沃动力股份有限公司 Starting device of trial-run bench of engine
CN101871834A (en) * 2010-04-23 2010-10-27 北京中科通视科技有限公司 Wireless remote water leakage detection device and system
CN102980771A (en) * 2012-12-04 2013-03-20 南京航空航天大学 Portable failure detection system and method for aero-engine gas path component

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