CN204694860U - High-effect big current Electro-magnetic Launcher System - Google Patents
High-effect big current Electro-magnetic Launcher System Download PDFInfo
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- CN204694860U CN204694860U CN201520386270.0U CN201520386270U CN204694860U CN 204694860 U CN204694860 U CN 204694860U CN 201520386270 U CN201520386270 U CN 201520386270U CN 204694860 U CN204694860 U CN 204694860U
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Abstract
The utility model relates to a kind of high-effect big current Electro-magnetic Launcher System, and this system comprises medium-frequency high-voltage power supply, big current electromagnetism transmitter module, main control unit and output waveform generator.Big current electromagnetism transmitter module is made up of medium-frequency high-voltage transformer, electric power conversion unit and the current filter be connected; Medium-frequency high-voltage transformer is adopted as the two secondary coil transformer of large transformer ratio, and its electric power conversion unit is positioned at current transformer out-secondary, comprises two branch roads, can realize double-polarity control, ensures the positive and negative half period symmetry work of transformer work.The utility model comparatively legacy transmission engine efficiency greatly improves, and changes the topological structure of traditional Electro-magnetic Launcher System, and electric power conversion unit adopts modular design, improves controllability and the extensibility of system.
Description
Technical field
The utility model belongs to electromagnetic survey technical field, relates to high-effect big current Electro-magnetic Launcher System.
Background technology
Electromagnetic prospecting Theory and technology is widely used in comprising petroleum prospecting, groundwater exploration, geothermal energy exploration, engineering exploration and addressing, mineral resources exploration, moving fault exploration, seismic safety evaluation, geologic mapping, environment exploration, dykes and dams disease screening, land burial thing and pipeline detection, inwelling and underground pollution scope definition, subsurface resistivity variations at present and monitors and the earth's crust and Upper Mantle Structure research etc., particularly in energy resource survey, have great importance.Its theoretical method and instrument are also at constantly improvement and bring new ideas, and its geologic interpretation precision and effect also improve constantly.Under the exploitation requirement drive of deep-sea oil gas resource, develop the high-efficient electromagnetic transmitter techniques that tens milliohm heavy dutys, kilo-ampere level electric current can be driven to export and seem more and more important, its alap internal resistance design is dynamical gordian technique.
As shown in Figure 7, the tandem compound mode of the single-phase uncontrollable rectifier bridge of main employing and single-phase H inverter bridge realizes transmitter current range-adjusting and pulse code converts, the electric dipole moment Electromagnetic Launching needed for being produced by antenna for the topological structure of classic method.The principal feature of the method is that structure is simple, and control algolithm easily realizes.But traditional scheme entirety adopts the connected mode of series connection, and current return series unit is many, internal resistance is large., power consumption concentrates on power semiconductor device, and cause heat to concentrate, heat radiation difficulty is large.Especially, when under deep-sea detecting condition, space, Electromagnetic Launching cabin and radiating condition are all limited, design difficulty is larger, and cost and installation difficulty significantly increase.Particularly, output current minimum at pull-up resistor and the very large occasion of power, as large power, electrically magnetic transmitter of the present utility model, pull-up resistor tens m Ω is close to short circuit, output current requires to reach 1000A level, the high internal resistance of traditional scheme is much larger than pull-up resistor, and therefore output power major part consumes in internal resistance.There is intrinsic Topology Structure Design defect in the circuit theory of traditional scheme, is thus difficult to realize high power converter and transfer efficiency.
Utility model content
The purpose of this utility model is to provide one to can be applicable to deep-sea controllable source electromagnetic survey, high-effect, big current Electro-magnetic Launcher System.
The technical solution of the utility model is: high-effect big current Electro-magnetic Launcher System, comprises medium-frequency high-voltage power supply, big current electromagnetism transmitter module, main control unit and output waveform generator.Big current electromagnetism transmitter module is made up of medium-frequency high-voltage transformer, electric power conversion unit and the current filter be connected; Medium-frequency high-voltage transformer terminal is the input end of big current electromagnetism transmitter module, is connected with medium-frequency high-voltage power supply, and current filter end is the output terminal of big current electromagnetism transmitter module, is connected with antenna load;
Medium-frequency high-voltage transformer is two secondary coil transformer, comprises primary coil, secondary coil I and secondary coil II; Electric power conversion unit is divided into two-way, every road electric power conversion unit comprises multiple MOS switch, MOS switch on every road can be divided into a MOS switch, the 2nd MOS switch and afterflow MOS switch, a MOS switch on two-way forms the first switches set, 2nd MOS switch forms second switch group, and afterflow MOS switch forms continued flow switch group; Two output terminals of secondary coil I are connected with the drain electrode of the first switches set two MOS switches respectively, and two output terminals of secondary coil II are connected with the drain electrode of second switch group two MOS switches respectively; The source electrode of the first switches set MOS switch, the source electrode of second switch group MOS switch are all connected to the source electrode of continued flow switch group, are connected to antenna load respectively through current filter simultaneously; The drain interconnection of continued flow switch group two MOS switches;
Export output waveform generator to be made up of waveform compilation module and waveform generating module two parts.The expectation waveform instruction that waveform compilation module receives user is assigned, comprises the amplitude of waveform, frequency, dutycycle.The parameter that waveform generating module provides according to waveform compilation module, produces periodic current waveform signal.
Main control unit comprises data acquisition module, driving logic circuit, control algolithm module;
Data acquisition module gathers current value and the magnitude of voltage of the current value of medium-frequency high-voltage power end, magnitude of voltage and antenna load end respectively; The current feedback signal that the output of waveform generating module obtains as setting value and the acquisition module of electric current is carried out deviation calculating by control algolithm module, and controller Gic (s) of control algolithm module carries out computing to deviation, obtains the dutycycle of PWM.
Driving logic circuit comprises PWM generator, drives logic true value table.The dutycycle that PWM generator exports according to control algolithm module, produces pwm pulse, and the pulse by driving logic true value table finally to produce driven MOS switch.
Preferably: big current electromagnetism transmitter module has many groups, the input end of each group is in parallel, is all connected with medium-frequency high-voltage power supply; The output terminal of each group is in parallel, is all connected with antenna load.Each modular unit carries out electric current by total current output waveform and amplitude requirement and automatically distributes and synchro control modulating transformation, exports as each modular unit transmitter current sum.The number of parallel module depends on and exports total current size and power consumption requirements, can flexible combination, and transmitter current number of modules that is larger and (or) the less parallel combination of power consumption requirements is more.
The beneficial effects of the utility model are:
(1) native system adopts medium-frequency high-voltage power supply, realizes the remote high voltage power transmission of low-loss, improves transfer efficiency, meets the requirement of electric energy long range propagation.Two-way MOS switch can realize double-polarity control, this syndeton of MOS switch, and its equivalent resistance is reduced greatly, improves the efficiency of transmitter.The efficiency of traditional transmitter is generally at about 75%-80%, and the efficiency of this transmitter can reach more than 99%.
(2) adopt the two secondary coil high-tension transformer of large transformer ratio, transformer is connected in mode reverse each other with the MOS switches set on electric power conversion unit, ensures that transformer magnetic circuit positive-negative half-cycle Full wave shape symmetrical balance runs, improves the utilization factor of transformer.
(3) electric power conversion unit adopts parallel modular design, is convenient to modularity control, improves the controllability of system, Scalability and expandability, makes this system architecture can meet the requirement of electromagnetism output on a large scale.Meanwhile, this structure decreases the number of electric current outgoing side series power switch, reduces internal resistance, thus reduces power consumption, the efficiency of great elevator system power converter, solves the problem of typical high power Electromagnetic Launching pole heat radiation.
(4) have employed frequency converter mechanism, it is abnormal that each Electromagnetic Launching modular unit is equipped with independently output overcurrent, short circuit, overvoltage, input and output open circuit, and the interlocking linkage safeguard measure such as input undervoltage, overvoltage, overcurrent, short circuit, module be overheated.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation
Fig. 2 is electric power conversion unit structural representation
Fig. 3 is the utility model systematic control algorithm block diagram
Fig. 4 is that the utility model pulse exports control principle structural representation
Fig. 5 is that embodiment 1 system list electric power conversion unit runs output waveform figure
Fig. 6 is that the many electric power conversion unit of embodiment 2 system run output waveform figure
Fig. 7 is prior art electromagnetics transmitter topological structure schematic diagram
Wherein, I
oS: system exports total current setting value, I
l: system exports total current detected value, V
l: system output voltage Ii: system input total current, In: transmitter module unit exports a point electric current, Vi: system input voltage, Tn: module n temperature, (wherein 1≤n≤N, N is required module number), Δ I
0: aims of systems current deviation, Gic (s): system power ring control algolithm, Gif (s): system power feedback processing algorithm, D: control to export PWM dutycycle, Dir: output waveform polarity, EN: each module drive enable signal, Zf: intermediate frequency power supply positive-negative half-cycle identification signal, R: antenna load resistance
Embodiment
Embodiment 1
High-effect big current Electro-magnetic Launcher System, comprise medium-frequency high-voltage power supply, big current electromagnetism transmitter module, main control unit and output waveform generator, big current electromagnetism transmitter module is made up of the high-tension transformer be connected, electric power conversion unit and current filter; High-tension transformer end is the input end of big current electromagnetism transmitter module, is connected with medium-frequency high-voltage power supply, and current filter end is the output terminal of big current electromagnetism transmitter module, is connected with antenna load.
High-tension transformer is the two secondary coil transformer of large transformer ratio, comprises primary coil, secondary coil I and secondary coil II.The power supply of medium-frequency high-voltage power acquisition 2000V/400Hz, exports two low-tension supplies of the low-voltage, high-current twin coil isolation symmetry of 60V/300A through high-tension transformer.
As shown in Figure 2, electric power conversion unit is divided into two-way, upper branch road and lower branch road; Every road electric power conversion unit comprises multiple MOS switch, MOS switch on every road can be divided into a MOS switch, the 2nd MOS switch and afterflow MOS switch, a MOS switch on upper branch road and lower branch road forms the first switches set, 2nd MOS switch forms second switch group, and afterflow MOS switch forms continued flow switch group; The positive pole of secondary coil I is connected with the drain electrode of the MOS switch on upper branch road, the negative pole of secondary coil I is connected with the drain electrode of the MOS switch on lower branch road, the positive pole of secondary coil II is connected with the drain electrode of the 2nd MOS switch on lower branch road, and the negative pole of secondary coil II is connected with the drain electrode of the 2nd MOS switch of upper branch road; The source electrode of a MOS switch on upper branch road, the source electrode of the 2nd MOS switch are all connected to the source electrode of afterflow MOS switch on branch road, are connected to antenna load resistance R respectively through current filter simultaneously
l; The source electrode of a MOS switch on lower branch road, the source electrode of the 2nd MOS switch are all connected to the source electrode of afterflow MOS switch on lower branch road, are connected to antenna load resistance R respectively through current filter simultaneously
l; The drain interconnection of continued flow switch group two MOS switches.
As can be seen from Figure 2, n21, T1D2 and T2D1 form the first switches set, and n22, T3D4 and T4D3 form second switch group, T5D6 and T6D5 forms two-way continued flow switch group, T1D2 and T3D4 is that positive polarity exports modulation switch, T2D1 and T4D3 is that negative polarity exports modulation switch.The same polarity output switch input end of these two groups of modulation switchs connects two secondary coil different name ends of high-tension transformer respectively, exports and connects rear connection power current wave filter.According to output encoder polarity of wave and changes in amplitude, under the control of controller modulation control algorithm, in these two groups of switches, the power switch of corresponding output polarity carries out PWM work along with secondary coil intermediate frequency power supply positive-negative half-cycle alternating polarity, realize the coding waveforms of output current size and polar requirement, also ensure that the symmetry of transformer magnetic circuit positive-negative half-cycle simultaneously.
Alternating, complementary work in two low-tension supply positive and negative half period that this structure makes secondary coil I and secondary coil II be formed, ensures transformer magnetic circuit positive-negative half-cycle balance movement, improves the utilization factor of transformer.During positive-negative half-cycle work, output terminal is all through current filter smothing filtering, ensures the characteristic that current source exports.After the output current parallel connection of each big current electromagnetism transmitter module, the electric current of formation delivers to antenna load resistance R
lon, obtain frequency from continuously adjustable pulse code electromagnetic wave within the scope of 0 ~ 100Hz, amplitude 0 ~ 1200A.
Export output waveform generator to be made up of waveform compilation module and waveform generating module two parts.Data acquisition module gathers current value and the magnitude of voltage of the current value of medium-frequency high-voltage power end, magnitude of voltage and antenna load end respectively; The current feedback signal that control algolithm module comprises the output of waveform generating module obtains as setting value and the acquisition module of electric current carries out deviation calculating, controller Gic (s) of control algolithm module carries out computing to deviation, obtains the dutycycle of PWM.
Driving logic circuit comprises PWM generator, channel selecting module.The dutycycle that PWM generator exports according to control algolithm module, produces pwm pulse, is formed and drives logic true value table, and the pulse by driving logic true value table finally to produce driven MOS switch.
The main control unit of system comprises control algolithm module, driving logic circuit and data acquisition module.
During system initialization work, the current amplitude that waveform compilation module receives user sets, frequency and dutycycle; The parameter that waveform generating module provides according to waveform compilation module, the setting value of generation current; Controller Gic (s) according to setting electric current and the deviation of feedback current, computed duty cycle.PWM produces the pulse meeting dutycycle, and by driving logic true value table to form PWM drive singal, being delivered to the grid of MOS switch, controlling the work of MOS switch in each group of electric power conversion unit, thus at antenna load resistance R
lsupport continuous generation pulse code electromagnetic wave.
When in system operation, main control unit carries out positive and negative half period identification, judges that big current electromagnetism transmitter module is positive conducting or negative conducting.The electric current of antenna load end and Voltage Feedback are in the data acquisition module of main control unit, load end current feedback is compared end to current feedback according to current feedback algorithm by main control unit, compared with the setting value exporting total current with system, draw difference, in conjunction with pid control algorithm, calculate control signal.Control signal resolves to PWM drive singal through PWM generation module; Channel selecting module selects the path between PWM drive singal and MOS switch gate, and PWM modulation signal is sent to the grid of MOS switch respectively through output control module; A MOS switch wherein on every road and the 2nd MOS switch share a PWM modulation signal, and the afterflow MOS switch on every road accepts different PWM modulation signal respectively.
In the present embodiment, system access electric power conversion unit.When carrying out system cloud gray model, given input voltage 150V, given output current 100A, system output waveform as shown in Figure 5.As seen from Figure 5, system can quick adjustment dutycycle, make output current reach setting value, and overshoot is very little, and after stable, current fluctuation is little.As can be seen here, this system is controlled, and Absorbable organic halogens runs.
Data acquisition module also gathers the signal such as temperature value of the current value of medium-frequency high-voltage power end, magnitude of voltage, each electric power conversion unit simultaneously.Main control unit also has status monitoring in an Implement of Function Module electric current, i.e. abnormality processing center.The temperature value of the input voltage of system, input current, output voltage, output current and each group electric power conversion unit all feeds back to data acquisition module, compared by the signal that received and each level threshold value signal, that abnormality processing center is carried out is overheated, overcurrent, short circuit, overvoltage, the abnormality such as under-voltage analysis, and execute exception process action.As shown in Figure 3, abnormality processing center can produce the comprehensive enable signal EN of abnormality processing and abnormality indicator signal, EN is used for carrying out enable control to each MOS switch, thus the duty of regulating circuit, status signal is for identifying Exception Type and safeguarding instruction.
Embodiment 2
As shown in Figure 1, as different from Example 1, big current electromagnetism transmitter module has many groups, and the input end of each group is in parallel, is all connected with medium-frequency high-voltage power supply; The output terminal of each group is in parallel, is all connected with antenna load.
When multiple big current electromagnetism transmitter module is in parallel, output control module controls the big current electromagnetism transmitter module equilibrium of every road and exports.As shown in Figure 6, for input current be 120A time, system output current oscillogram.When multiple wired in parallel, also can reach the current value of setting fast, each blocks current value is basically identical, and output current is modules current value sum, can well increase output current during multiple module paralleling.
Claims (2)
1. high-effect big current Electro-magnetic Launcher System, it is characterized in that: comprise medium-frequency high-voltage power supply, big current electromagnetism transmitter module, main control unit and output waveform generator, described big current electromagnetism transmitter module is made up of medium-frequency high-voltage transformer, electric power conversion unit and the current filter be connected; Medium-frequency high-voltage transformer terminal is the input end of big current electromagnetism transmitter module, is connected with medium-frequency high-voltage power supply, and current filter end is the output terminal of big current electromagnetism transmitter module, is connected with antenna load;
Described medium-frequency high-voltage transformer is two secondary coil transformer, comprises primary coil, secondary coil I and secondary coil II; Described electric power conversion unit is divided into two-way, every road electric power conversion unit comprises multiple MOS switch, MOS switch on every road can be divided into a MOS switch, the 2nd MOS switch and afterflow MOS switch, a MOS switch on two-way forms the first switches set, 2nd MOS switch forms second switch group, and afterflow MOS switch forms continued flow switch group; Two output terminals of secondary coil I are connected with the drain electrode of the first switches set two MOS switches respectively, and two output terminals of secondary coil II are connected with the drain electrode of second switch group two MOS switches respectively; The source electrode of the first switches set MOS switch, the source electrode of second switch group MOS switch are all connected to the source electrode of continued flow switch group, are connected to antenna load respectively through current filter simultaneously; The drain interconnection of continued flow switch group two MOS switches;
Described output waveform generator comprises shape editor module and waveform generating module; Waveform compilation module receives waveform instruction, and waveform generating module produces periodic current waveform signal according to waveform instruction;
Described main control unit comprises waveform compilation module, driving logic circuit, computing unit and data acquisition module;
Described driving logic circuit comprises PWM generator, channel selecting module.
2. high-effect big current Electro-magnetic Launcher System as claimed in claim 1, is characterized in that: described big current electromagnetism transmitter module has many groups, and the input end of each group is in parallel, is all connected with medium-frequency high-voltage power supply; The output terminal of each group is in parallel, is all connected with antenna load.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520386270.0U CN204694860U (en) | 2015-06-05 | 2015-06-05 | High-effect big current Electro-magnetic Launcher System |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520386270.0U CN204694860U (en) | 2015-06-05 | 2015-06-05 | High-effect big current Electro-magnetic Launcher System |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104865606A (en) * | 2015-06-05 | 2015-08-26 | 中国海洋大学 | High-effect large-current electromagnetic transmitting system and method |
| CN107039765A (en) * | 2016-02-04 | 2017-08-11 | 中石化石油工程技术服务有限公司 | Electromagnetic Launching antenna between a kind of well |
-
2015
- 2015-06-05 CN CN201520386270.0U patent/CN204694860U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104865606A (en) * | 2015-06-05 | 2015-08-26 | 中国海洋大学 | High-effect large-current electromagnetic transmitting system and method |
| CN107039765A (en) * | 2016-02-04 | 2017-08-11 | 中石化石油工程技术服务有限公司 | Electromagnetic Launching antenna between a kind of well |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Li Ming Inventor after: Liu Lanjun Inventor after: Wang Jianguo Inventor after: Li Yuguo Inventor after: Pei Jianxin Inventor after: Liu Shuai Inventor after: Zhu Zhongben Inventor after: Du Xiaobin Inventor before: Li Ming Inventor before: Liu Lanjun Inventor before: Wang Jianguo |
|
| COR | Change of bibliographic data | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20151007 Effective date of abandoning: 20170616 |