CN205541574U - Electromagnetic propulsion ware - Google Patents
Electromagnetic propulsion ware Download PDFInfo
- Publication number
- CN205541574U CN205541574U CN201521123591.8U CN201521123591U CN205541574U CN 205541574 U CN205541574 U CN 205541574U CN 201521123591 U CN201521123591 U CN 201521123591U CN 205541574 U CN205541574 U CN 205541574U
- Authority
- CN
- China
- Prior art keywords
- electric capacity
- input
- trigger
- cells
- metal column
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000002184 metal Substances 0.000 claims abstract description 29
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 16
- 239000010703 silicon Substances 0.000 claims abstract description 16
- 230000001939 inductive effect Effects 0.000 claims description 28
- 230000008676 import Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 abstract 2
- 238000012856 packing Methods 0.000 abstract 1
- 238000004804 winding Methods 0.000 abstract 1
- 230000005674 electromagnetic induction Effects 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
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- Magnetic Treatment Devices (AREA)
Abstract
The utility model discloses an electromagnetic propulsion ware, including shell, metal column, trigger, packing mouth, transmission mouth and advancing device, advancing device includes the group battery, the device that steps up, electric capacity, silicon controlled rectifier, high -voltage pulse circuit board and launching tube, and the winding has a plurality of inductance circles on the launching tube, the input of the device that steps up is connected to the group battery, the input of the parallelly connected a plurality of electric capacity of output of the device that steps up, and the input of inductance circle is connected to the output of electric capacity, and the silicon controlled rectifier input is connected to the output of inductance circle, and the output connection group battery of the input and the input of electric capacity of trigger, trigger is connected to the output of silicon controlled rectifier. The utility model discloses a charge -discharge of electric capacity provides the electric current of change for the inductance circle, makes the magnetic field in the inductance circle change, when provide an initial kinetic energy for the metal column time, under the effect in multistage magnetic field, makes the metal column accelerate gradually, reaches the accelerated mesh of a lot of to finally accomplish the transmission of metal column.
Description
Technical field
This utility model relates to the model of mathematics, is specifically related to a kind of electromagnetic propeller.
Background technology
This knowledge of electromagnetic induction is belonging to a kind of knowledge that comparison is uninteresting, depending teacher's explanation alone cannot allow students can be good at understanding and study, at this moment it is accomplished by a kind of having the experimental provision of certain entertaining to improve the interest of students, and the electromagnetic propeller developed according to electromagnetic induction principle just can reach this effect.
Electromagnetic propeller is that one is converted into metal column kinetic energy electromagnetic energy, makes metal column reach the device of high speed ejection.Electromagnetic propeller operation principle and various data are required for utilizing electromagnetic propeller experimental provision to be verified in Physical Experiment.Existing electromagnetic propeller model, can reach this purpose, but this device has the most not foot point, i.e. this circuit and only has one-level discharge circuit, and therefore the magnetic field strength of coil is inadequate, and speed and the distance of bullet are the most fairly limited, not ideal enough.
Utility model content
This utility model is intended to provide a kind of electromagnetic propeller, to solve the problem that the electromagnetic propeller of prior art only has one-level to accelerate.
A kind of electromagnetic propeller in this programme, including shell, metal column, trigger, charging port, emission port and propulsion plant, described propulsion plant includes set of cells, increasing apparatus, electric capacity, controllable silicon, high-voltage pulse circuit plate and transmitting tube;Being wound with multiple inductive loop on transmitting tube, set of cells, electric capacity, controllable silicon, inductive loop connect described high-voltage pulse circuit plate;Described set of cells connects the input of increasing apparatus, the outfan of described increasing apparatus is connected to the input of multiple electric capacity, the outfan of multiple described electric capacity is connected to the input of inductive loop, the outfan of described inductive loop connects controllable silicon input, described silicon controlled outfan is connected with the input of trigger and the input of electric capacity respectively, and the outfan of described trigger is connected with set of cells;Described charging port is positioned at the import of transmitting tube, and described trigger is the bottom of the high-voltage pulse circuit plate near charging port side, and described emission port is positioned at the outlet of transmitting tube;Described electric capacity is fixed on upper surface of outer cover, and described increasing apparatus is positioned on shell and near the side of emission port.
Operation principle of the present utility model: a kind of electromagnetic propeller, including shell, trigger, charging port, emission port and propulsion plant, set of cells, trigger, electric capacity, controllable silicon, inductive loop are both connected to high-voltage pulse circuit plate, too much cause confusion because line reducing electric connection line;Set of cells connects the input of increasing apparatus, after the boosting of power supply boosted device, charges to electric capacity, after electric capacity is fully charged, not in charging;Now, metal column is loaded in charging port, cocking, one initial kinetic energy of metal column is given while connection discharge circuit, electric capacity is made to discharge, the electric current of one change is provided to inductive loop, inductive loop is made to produce the magnetic field of change, when metal column moves to be wound with in the transmitting tube of inductive loop, metal column is accelerated by Lorentz force, move on when running in the transmitting tube of secondary inductance circle, metal column continues to be again speeded up by Lorentz force, after after, Lorentz force through multiple inductive loops accelerates step by step, metal column accelerates to maximum in transmitting tube, finally go out transmitting tube.
The beneficial effect of this utility model: emission port, inductive loop and high-voltage pulse circuit plate etc. on propulsion plant are placed in shell, avoid operation time because of touching initiation potential, supply electricity to inductive loop by the charge and discharge of electric capacity and the electric current of change is provided, the magnetic field in inductive loop is made to change, when providing an initial kinetic energy to metal column, under the effect of multi-stage magnetic field, metal column is made to ramp up, reach the purpose repeatedly accelerated, and be finally completed the transmitting of metal column.
Further, on described emission port, connection has prolongation to launch boring.Metal column guide-localization is more accurate.
Further, the described boring mouth extending transmitting boring connects muzzle brake.In order to reduce the recoil of electromagnetic propeller emission port, prevent kick excessive and hurt user.
Further, the infrared calibration instrument electrically connected with set of cells is also included.Transmitting direction with correcting electromagnetic propeller metal column.
Further, the LED numeric display electrically connected with set of cells is also included.In order to observe the situation etc. of metal column in curent change, capacitance variations and transmitting tube.
Further, also include that handle, described handle are provided close to the bottom of the high-voltage pulse circuit plate of emission port side.It is convenient to the operation to electromagnetic propeller.
Further, the transmitting tube between adjacent inductive circle is provided with corresponding perforate, is provided with infrared photoelectric sensor in described corresponding perforate.Can ensure that when advancing to corresponding perforate, when the electric capacity of next stage starts to discharge, next stage magnetic field just produces change, it is to avoid the loss of magnetic force after metal column is accelerated by first order inductive loop.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of electromagnetic propeller of this utility model.
Detailed description of the invention
Below by detailed description of the invention, this utility model is described in further detail:
Reference in Figure of description includes: boring 10, muzzle brake 11 are launched in charging port 1, electric capacity 2, electric capacity bracket 3, shell 4, set of cells 5, propulsion plant 6, inductive loop 601, infrared photoelectric sensor 602, high-voltage pulse circuit plate 603, infrared calibration instrument 7, handle 8, emission port 9, prolongation.
As shown in Figure 1: a kind of electromagnetic propeller, including shell 4, metal column, trigger, charging port 1, emission port 9 and propulsion plant 6, propulsion plant 6 includes set of cells 5, increasing apparatus, electric capacity 2, controllable silicon, high-voltage pulse circuit plate 603, transmitting tube and 7 inductive loops 601 being wrapped on transmitting tube, be equivalent to 7 grades of acceleration, transmitting tube between adjacent inductive circle 601 is provided with corresponding perforate, is provided with infrared photoelectric sensor 602 in corresponding perforate;Set of cells 5, electric capacity 2, controllable silicon, inductive loop 601 are both connected on high-voltage pulse circuit plate 603, and electric capacity 2 is placed in electric capacity bracket 3, and electric capacity bracket 3 is arranged on the top of shell 4 and is positioned at the side of charging port 1;Set of cells 5 connects the input of increasing apparatus, the input of the outfan of increasing apparatus multiple electric capacity 2 in parallel, electric capacity 2 outfan connects the input of inductive loop 601, the outfan of inductive loop 601 connects controllable silicon input, silicon controlled outfan connects input and the input of electric capacity 2 of trigger, and the outfan of trigger connects set of cells 5;Charging port 1 is positioned at the import of transmitting tube, and trigger is the bottom near charging port 1 side high-voltage pulse circuit plate 603, and emission port 9 is positioned at the outlet of transmitting tube;Electric capacity 2 is positioned on shell 4 and near the top of charging port 1 side, and increasing apparatus is positioned on shell 4 and near the side of emission port 9;Connecting on described emission port 9 and have prolongation to launch boring 10, the boring mouth extending transmitting boring 10 connects muzzle brake 11, and the side of shell 4 is provided with infrared calibration instrument 7, is provided with handle 8 near the bottom of the high-voltage pulse circuit plate 603 of emission port 9 side.
Set of cells 5 is pressurizeed by increasing apparatus, after boost in voltage, charges to electric capacity 2, after electric capacity 2 is fully charged, not in charging;Now, metal column is put into charging port 1, press trigger, while one initial kinetic energy of metal column, electric capacity 2 discharges, an electric current changed is provided to inductive loop 601, inductive loop 601 is made to produce the magnetic field of change, when moving metal column and moving to be wound around in the transmitting tube of inductive loop 601, metal column is accelerated by Lorentz force, when metal column advances to corresponding perforate afterwards, the electric capacity 2 of next stage starts electric discharge, next stage magnetic field produces change, metal column accelerates at this, go down step by step, after 7 grades are accelerated, the speed making metal column rises to maximum, finally go out transmitting tube.
Above-described is only embodiment of the present utility model, and in scheme, the known general knowledge such as concrete structure and characteristic too much describes at this.Should be understood that; for a person skilled in the art, on the premise of without departing from this utility model structure, it is also possible to make some deformation and improvement; these also should be considered as protection domain of the present utility model, and these are all without affecting effect and the practical applicability that this utility model is implemented.The protection domain that this application claims should be as the criterion with the content of its claim, and the detailed description of the invention in description etc. records the content that may be used for explaining claim.
Claims (7)
1. an electromagnetic propeller, including shell, metal column, trigger, charging port, emission port and propulsion plant, described propulsion plant includes set of cells, increasing apparatus, electric capacity, controllable silicon, high-voltage pulse circuit plate and transmitting tube;It is characterized in that, transmitting tube is wound with multiple inductive loop, and set of cells, electric capacity, controllable silicon, inductive loop connect described high-voltage pulse circuit plate;Described set of cells connects the input of increasing apparatus, the outfan of described increasing apparatus is connected to the input of multiple electric capacity, the outfan of multiple described electric capacity is connected to the input of inductive loop, the outfan of described inductive loop connects controllable silicon input, described silicon controlled outfan is connected with the input of trigger and the input of electric capacity respectively, and the outfan of described trigger is connected with set of cells;Described charging port is positioned at the import of transmitting tube, and described trigger is the bottom of the high-voltage pulse circuit plate near charging port side, and described emission port is positioned at the outlet of transmitting tube;Described electric capacity is fixed on upper surface of outer cover, and described increasing apparatus is positioned on shell and near the side of emission port.
Electromagnetic propeller the most according to claim 1, it is characterised in that: connect on described emission port and have prolongation to launch boring.
Electromagnetic propeller the most according to claim 2, it is characterised in that: the described boring mouth extending transmitting boring connects muzzle brake.
Electromagnetic propeller the most according to claim 3, it is characterised in that: also include the infrared calibration instrument electrically connected with set of cells.
Electromagnetic propeller the most according to claim 4, it is characterised in that: also include the LED numeric display electrically connected with set of cells.
Electromagnetic propeller the most according to claim 5, it is characterised in that: also include that handle, described handle are provided close to the bottom of the high-voltage pulse circuit plate of emission port side.
Electromagnetic propeller the most according to claim 6, it is characterised in that: the transmitting tube between adjacent inductive circle is provided with corresponding perforate, is provided with infrared photoelectric sensor in described corresponding perforate.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201521123591.8U CN205541574U (en) | 2015-12-31 | 2015-12-31 | Electromagnetic propulsion ware |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201521123591.8U CN205541574U (en) | 2015-12-31 | 2015-12-31 | Electromagnetic propulsion ware |
Publications (1)
Publication Number | Publication Date |
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CN205541574U true CN205541574U (en) | 2016-08-31 |
Family
ID=56762002
Family Applications (1)
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CN201521123591.8U Expired - Fee Related CN205541574U (en) | 2015-12-31 | 2015-12-31 | Electromagnetic propulsion ware |
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CN (1) | CN205541574U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105469676A (en) * | 2015-12-31 | 2016-04-06 | 贵州励天科技发展有限公司 | Electromagnetic propeller |
-
2015
- 2015-12-31 CN CN201521123591.8U patent/CN205541574U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105469676A (en) * | 2015-12-31 | 2016-04-06 | 贵州励天科技发展有限公司 | Electromagnetic propeller |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right | ||
TR01 | Transfer of patent right |
Effective date of registration: 20220610 Address after: 563299 science and technology enterprise incubation building, Guizhou Loushanguan high tech Zone, Chumi Town, Tongzi County, Zunyi City, Guizhou Province Patentee after: Guizhou Duoduo Industrial Co.,Ltd. Address before: 563299 4th floor, incubation building, Loushanguan high tech Zone, Tongzi County, Zunyi City, Guizhou Province Patentee before: GUIZHOU LITIAN TECHNOLOGY DEVELOPMENT Co.,Ltd. |
|
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160831 |