CN111964524A - Multistage induction type electromagnetic transmitter - Google Patents
Multistage induction type electromagnetic transmitter Download PDFInfo
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- CN111964524A CN111964524A CN202010857746.XA CN202010857746A CN111964524A CN 111964524 A CN111964524 A CN 111964524A CN 202010857746 A CN202010857746 A CN 202010857746A CN 111964524 A CN111964524 A CN 111964524A
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- pulse
- magnetic induction
- electromagnetic transmitter
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- armature
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41B—WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
- F41B6/00—Electromagnetic launchers ; Plasma-actuated launchers
- F41B6/003—Electromagnetic launchers ; Plasma-actuated launchers using at least one driving coil for accelerating the projectile, e.g. an annular coil
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- Electromagnetism (AREA)
- Plasma & Fusion (AREA)
- General Engineering & Computer Science (AREA)
- Switches That Are Operated By Magnetic Or Electric Fields (AREA)
Abstract
The invention discloses a multistage induction type electromagnetic transmitter, which comprises a sleeve, wherein magnetic induction coils are equidistantly arranged on the outer wall of the sleeve, a photoelectric switch and a microswitch are arranged on the surface of the sleeve between the magnetic induction coils, the magnetic induction coils are electrically connected with a high-energy pulse discharge energy collecting device, the multistage induction type electromagnetic transmitter is powered by a power supply, a transformer is used for boosting, so that larger electric energy is stored in a pulse capacitor, a control circuit device is used for controlling the pulse capacitor to release the electric energy, so that current is led into the magnetic induction coils, then the armature induces current, peak current enables the magnetic induction coils to instantly generate larger magnetic traveling waves to push the armature to transmit, pulse magnetic force driving is completed, the armature continuously accelerates under a pulse magnetic field by adopting the multistage magnetic induction coils and continuous pulse magnetic traveling waves in space, and the stress time can be increased, and the time interval of the excitation of the adjacent two stages of power supplies is controlled, so that the purpose of rapidly accelerating the armature to a high speed is achieved, and the reaction force of magnetic force is effectively avoided.
Description
Technical Field
The invention relates to the technical field of electromagnetic emitters, in particular to a multistage induction type electromagnetic emitter.
Background
The electromagnetic launcher is a device for driving and launching the launched object through electromagnetic force, and has the advantages of stable and safe driving and wide application range.
The power supply stability of the existing electromagnetic transmitter is greatly tested, and the thrust time of a transmitting object is short, so that the acceleration time is short, and the transmitting intensity is low.
To this end, we propose a multi-stage inductive electromagnetic transmitter.
Disclosure of Invention
The present invention is directed to a multi-stage induction electromagnetic transmitter to solve the above problems.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a multistage induction type electromagnetic transmitter, includes the sleeve pipe, sleeve pipe outer wall equidistance is installed the magnetic induction coil, sleeve pipe surface is located and installs photoelectric switch and micro-gap switch between the magnetic induction coil, the equal electric connection of magnetic induction coil has the high energy pulse to discharge to gather the device.
Preferably, gather and to put including power supply ware, transformer, pulse capacitance, control circuit ware and discharge device, power supply ware electric connection transformer, transformer electric connection pulse capacitance, and pulse capacitance is connected with magnetic induction coil input, magnetic induction coil output is connected with discharge device, and discharge device electric connection has control circuit ware, control circuit ware and pulse capacitance and transformer electric connection.
Preferably, the control circuit device is composed of a high-speed controllable switch, an IGBT, a microswitch and a high-current diode.
Preferably, the transformer and the pulse capacitor are sleeved with heat dissipation devices.
Preferably, an over-electronic switch is connected between the transformer and the pulse capacitor.
Preferably, the over-electronic switch includes, but is not limited to, a thyristor, an IGBT, an IGCT, a MOS, etc.
Preferably, the energy gathering device has two discharging modes, and the discharging mode comprises physical control and logic control.
Preferably, the number of the magnetic induction coils is N, and N is more than or equal to 1.
Preferably, the armature is made of an electrically conductive material.
Preferably, the armature is positioned at the center of the magnetic induction coil at the end part of the sleeve;
preferably, the micro switch is synchronous with the photoelectric module, and is used for judging the passing condition of the sensed armature in cooperation with the photoelectric switch, so that the next-stage coil is discharged, and meanwhile, the phenomenon that the discharge is triggered by mistake due to the fact that other external objects enter the shielding photoelectric switch is avoided.
Compared with the prior art, the invention has the beneficial effects that:
the invention supplies power through the power supply device, the transformer boosts the voltage, so that the pulse capacitor stores larger electric energy, the control circuit device controls the pulse capacitor to release the electric energy, so that the current is led into the magnetic induction coil, the peak current enables the magnetic induction coil to instantly generate larger magnetic traveling waves to push an object to emit, the return current is released through the discharge device to complete the pulse magnetic driving, the multi-stage magnetic induction coil time and the spatially continuous pulse magnetic traveling waves are adopted, the emitter always follows the movement of the magnetic field traveling waves, the stress time is increased, the time interval of the excitation of two adjacent stages of power supplies is shortened, and the purpose of rapidly accelerating the emitter to high speed is achieved.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic cross-sectional view of the casing of the present invention;
fig. 3 is a schematic view of the structure of the energy gathering device of the present invention.
In the figure: 1. a sleeve; 2. a magnetic induction coil; 3. an energy gathering device; 31. a power supply; 32. a transformer; 33. a pulse capacitor; 34. a control circuit device; 35. a discharge device; 36. an electronic switch; 37. a heat sink; 4. photoelectric switches and micro-switches; 9. an armature.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, a multi-stage induction type electromagnetic transmitter in the figure includes a sleeve 1, magnetic induction coils 2 are installed on the outer wall of the sleeve 1 at equal intervals, a photoelectric switch 4 is installed between the magnetic induction coils 2 on the surface of the sleeve 1, the magnetic induction coils 2 are electrically connected with energy collecting devices 3 for high-energy pulse discharge, a transmitting object is placed in the sleeve 1, pulse energization to the magnetic induction coils 2 is realized by energy collection of the energy collecting devices 3, so that the magnetic induction coils 2 generate magnetic thrust waves of pulses, transmission and pushing to the object are realized, after the object is driven by a first-stage magnetic induction coil 2, the position of the object is detected by the photoelectric switch 4, when the object is close to the position of a second-stage magnetic induction coil 2, the second-stage magnetic induction coil 2 is energized to generate magnetic force, and then the magnetic force is sequentially energized to generate thrust, and continuous transmission to the object is realized.
Referring to fig. 3, the energy collecting device 3 includes a power supply 31, a transformer 32, a pulse capacitor 33, a control circuit 34 and a discharge device 35, the power supply 31 is electrically connected to the transformer 32, the transformer 32 is electrically connected to the pulse capacitor 33, the pulse capacitor 33 is connected to an input end of the magnetic induction coil 2, an output end of the magnetic induction coil 2 is connected to the discharge device 35, the discharge device 35 is electrically connected to the control circuit 34, the control circuit 34 is electrically connected to the pulse capacitor 33 and the transformer 32, the transformer 32 is powered by the power supply 31 to increase the voltage, so that a large electric energy is stored in the pulse capacitor 33, the control circuit 34 controls the pulse capacitor 33 to release the electric energy, so that a current is introduced into the magnetic induction coil 2, and a peak current causes the magnetic induction coil 2 to instantly generate a large magnetic traveling wave to push an object to be emitted, the return current is discharged by the discharging device 35, and the pulse magnetic driving is completed.
The pulse capacitor 33 adopts a superconducting magnetic energy storage technology, has low storage loss and can store energy for a long time, which has unique advantages for pulse power systems which need to accumulate energy for a long time and store energy for a long time, such as space electromagnetic emission power supply systems, and more importantly, the superconducting magnetic energy storage system (SMES) is easy to control and can control pulse discharge waveforms; and the power-on density of the superconducting wire is far greater than that of a normal conducting conductor such as copper, and the volume and the weight of the energy storage device made of the superconducting wire are far smaller than those of the conventional energy storage device, so that the light weight and the miniaturization of a power supply can be realized.
The control circuit device 34 is composed of a high-speed controllable switch, an IGBT, a micro switch and a large-current diode, and obtains current outputs suitable for different loads by controlling the charging/freewheeling/discharging states of each energy storage module.
The micro switch in the circuit controller can trigger the photoelectric switch 4 to discharge at the next stage only when the armature 9 passes through, so that the phenomenon that the object enters the transmitting barrel to shield the photoelectric switch 4 to cause false triggering is avoided.
The transformer 32 and the pulse capacitor 33 are all sleeved with a heat dissipation device 37, the transformer 32 and the pulse capacitor 33 are packaged at low temperature, and the transformer 32 and the pulse capacitor 33 are prevented from being overheated and failing.
In addition, an over-current electronic switch 36 is connected between the transformer 32 and the pulse capacitor 33, and the over-current electronic switch 36 includes, but is not limited to, a thyristor, an IGBT, an IGCT, a MOS, etc., absorbs a voltage spike at a discharging moment, and protects the pulse capacitor 33 and the transformer 32.
The energy collecting device 3 has two discharging modes for discharging control: firstly, the next coil is discharged through physical control, namely the position of the armature 9 is induced by the photoelectric switch 4, and the gradual acceleration is finally realized; and secondly, the discharge of each stage of coil is realized according to a time sequence by adopting logic control, namely, a time sequence algorithm, wherein the time sequence algorithm is an algorithm for performing discharge control by calculating the speed and the position of the armature 9 in the transmitting tube.
The primary side of the transformer 32 is formed by winding a plurality of turns of superconducting tapes in parallel, the negative side of the transformer 32 is formed by connecting a plurality of groups of superconducting tapes in parallel, and the transformation ratio K value is generally 5-50, so that stable and instant boosting is ensured.
The number of the magnetic induction coils 2 is N, N is more than or equal to 1, and different numbers of the magnetic induction coils 2 can be installed in a matched mode according to specific emission length and emission intensity requirements.
The armature 9 is made of a conductive material, and can be made of iron and the like.
The armature (9) is positioned at the central position of the magnetic induction coil (2) at the end part of the sleeve (1), and the efficient primary pushing of alignment is guaranteed.
The micro switch is synchronous with the photoelectric module and senses that the armature is judged cooperatively with the photoelectric switch when passing through, so that the next-stage coil is discharged, and meanwhile, the phenomenon that the discharge is triggered by mistake because other external objects enter the shielding photoelectric switch is avoided.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (11)
1. A multistage inductive electromagnetic transmitter comprising a bushing (1), characterized in that: magnetic induction coil (2) are installed to sleeve pipe (1) outer wall equidistance, armature (9) have been placed to sleeve pipe (1) inside, photoelectric switch and micro-gap switch (4) have been installed to sleeve pipe (1) surface position between magnetic induction coil (2), the equal electric connection of magnetic induction coil (2) has high energy pulse discharge's energy-gathering device (3).
2. The multi-stage inductive electromagnetic transmitter of claim 1 further comprising: gather ability device (3) and include power supply ware (31), transformer (32), pulse capacitance (33), control circuit ware (34) and discharge device (35), power supply ware (31) electric connection transformer (32), transformer (32) electric connection pulse capacitance (33), and pulse capacitance (33) and magnetic induction coil (2) input are connected, magnetic induction coil (2) output is connected with discharge device (35), and discharge device (35) electric connection has control circuit ware (34), control circuit ware (34) and pulse capacitance (33) and transformer (32) electric connection.
3. The multi-stage inductive electromagnetic transmitter of claim 2 wherein: the control circuit device (34) is composed of a high-speed controllable switch, an IGBT, a microswitch and a high-current diode.
4. The multi-stage inductive electromagnetic transmitter of claim 2 wherein: and heat dissipation devices (37) are sleeved outside the transformer (32) and the pulse capacitor (33).
5. The multi-stage inductive electromagnetic transmitter of claim 2 wherein: an over-electronic switch (36) is connected and installed between the transformer (32) and the pulse capacitor (33).
6. The multi-stage inductive electromagnetic transmitter of claim 5, wherein: the over-electronic switch (36) includes, but is not limited to, thyristors, IGCTs, MOS, etc.
7. The multi-stage inductive electromagnetic transmitter of claim 2 wherein: the energy gathering device (3) has two discharging modes, and the discharging modes comprise physical control and logic control.
8. The multi-stage inductive electromagnetic transmitter of claim 1 further comprising: the number of the magnetic induction coils (2) is N, and N is more than or equal to 1.
9. The multi-stage inductive electromagnetic transmitter of claim 1 further comprising: the armature (9) is made of conductive materials and can generate induction current under a pulse magnetic field.
10. The multi-stage inductive electromagnetic transmitter of claim 9, wherein: the armature (9) is positioned at the center of the magnetic induction coil (2) at the end part of the sleeve (1).
11. The multi-stage inductive electromagnetic transmitter of claim 3 wherein: the micro switch is synchronous with the photoelectric module and senses that the armature is judged cooperatively with the photoelectric switch when passing through, so that the next-stage coil is discharged, and meanwhile, the phenomenon that the discharge is triggered by mistake because other external objects enter the shielding photoelectric switch is avoided.
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Cited By (11)
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CN113910008A (en) * | 2021-10-18 | 2022-01-11 | 台州学院 | Multistage accelerating magnetic jet polishing machine |
CN113977358A (en) * | 2021-10-16 | 2022-01-28 | 毕而达 | Automatic control rotating magnetic field magneto-rheological polishing machine |
CN114043319A (en) * | 2021-11-24 | 2022-02-15 | 浙江科惠医疗器械股份有限公司 | Medical multi-stage constant-speed self-circulation magnetorheological polishing machine with wire anchors |
CN114083356A (en) * | 2021-11-24 | 2022-02-25 | 浙江科惠医疗器械股份有限公司 | Screw type medical interface screw through hole polishing machine circulates |
CN114674175A (en) * | 2022-03-25 | 2022-06-28 | 华北电力大学 | Electromagnetic emission simulation experiment platform capable of adjusting initial contact pressure and measuring method thereof |
CN115060113A (en) * | 2022-06-24 | 2022-09-16 | 广州国曜科技有限公司 | Electromagnetic emission device with initial position positioning function |
CN115307486A (en) * | 2022-07-19 | 2022-11-08 | 清华大学 | Electromagnetic transmitter and electromagnetic transmitter |
EP4086920A1 (en) * | 2021-05-06 | 2022-11-09 | Secretary, Department Of Atomic Energy | Inductively driven pellet accelerator and injector |
CN116202367A (en) * | 2022-12-29 | 2023-06-02 | 中国航天空气动力技术研究院 | Ballistic target based on electromagnetic ejection auxiliary driving secondary light air cannon |
CN116952063A (en) * | 2023-09-04 | 2023-10-27 | 广州国曜科技有限公司 | Safety control method and system based on electromagnetic emission |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
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EP4086920A1 (en) * | 2021-05-06 | 2022-11-09 | Secretary, Department Of Atomic Energy | Inductively driven pellet accelerator and injector |
CN113977358A (en) * | 2021-10-16 | 2022-01-28 | 毕而达 | Automatic control rotating magnetic field magneto-rheological polishing machine |
CN113910008A (en) * | 2021-10-18 | 2022-01-11 | 台州学院 | Multistage accelerating magnetic jet polishing machine |
CN114043319A (en) * | 2021-11-24 | 2022-02-15 | 浙江科惠医疗器械股份有限公司 | Medical multi-stage constant-speed self-circulation magnetorheological polishing machine with wire anchors |
CN114083356A (en) * | 2021-11-24 | 2022-02-25 | 浙江科惠医疗器械股份有限公司 | Screw type medical interface screw through hole polishing machine circulates |
CN114674175A (en) * | 2022-03-25 | 2022-06-28 | 华北电力大学 | Electromagnetic emission simulation experiment platform capable of adjusting initial contact pressure and measuring method thereof |
CN114674175B (en) * | 2022-03-25 | 2024-05-24 | 华北电力大学 | Electromagnetic emission simulation experiment platform capable of adjusting initial contact pressure and measurement method thereof |
CN115060113A (en) * | 2022-06-24 | 2022-09-16 | 广州国曜科技有限公司 | Electromagnetic emission device with initial position positioning function |
CN115307486A (en) * | 2022-07-19 | 2022-11-08 | 清华大学 | Electromagnetic transmitter and electromagnetic transmitter |
CN116202367A (en) * | 2022-12-29 | 2023-06-02 | 中国航天空气动力技术研究院 | Ballistic target based on electromagnetic ejection auxiliary driving secondary light air cannon |
CN116952063A (en) * | 2023-09-04 | 2023-10-27 | 广州国曜科技有限公司 | Safety control method and system based on electromagnetic emission |
CN116952063B (en) * | 2023-09-04 | 2024-02-27 | 广州国曜科技有限公司 | Safety control method and system based on electromagnetic emission |
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Application publication date: 20201120 |