CN203825912U - Ion dynamic propulsion demonstration instrument - Google Patents
Ion dynamic propulsion demonstration instrument Download PDFInfo
- Publication number
- CN203825912U CN203825912U CN201420183186.4U CN201420183186U CN203825912U CN 203825912 U CN203825912 U CN 203825912U CN 201420183186 U CN201420183186 U CN 201420183186U CN 203825912 U CN203825912 U CN 203825912U
- Authority
- CN
- China
- Prior art keywords
- suspension
- insulated column
- air track
- air
- dot matrix
- 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
Landscapes
- Electron Sources, Ion Sources (AREA)
Abstract
The utility model discloses an ion dynamic propulsion demonstration instrument. The structure is that a small-scale gas source is connected with a gas pipe, and the gas pipe is connected with an air track through an air track air inlet. The air track is provided with a left insulating column and a right insulating column. A suspension fiber is horizontally led to the right insulating column from the left insulating column. The right end of the suspension fiber is provided with a suspension fiber interface, and is connected with a static high-voltage power supply through a wire. The suspension fiber is provided with a threading guide wheel. The lower end of the threading guide wheel is connected with a suspended sliding body through a support. Two pinpoint matrixes are in the same size and are connected with two sides of the suspended sliding body by the support in a symmetric manner. Effects of the demonstration instrument are that the intensive pinpoint matrixes are made, so air is ionized under the action of high voltage, so as to obtain larger momentum; under the action of high voltage, the pinpoint matrixes achieve to move forward in a suspended manner with the help of the air track and a sliding device, so the instrument has more intuitive ion dynamic propulsion demonstration effect.
Description
Technical field
The utility model relates to the point discharge of a kind of dependence electrostatic high-pressure, and ionized air, to obtain the demonstrating experiment device of power, can be used as the demonstration test instrument of each colleges and universities, is specifically related to a kind of ion power and advances demonstrator.
Background technology
At present, what in colleges and universities' lecture experiment, relate to high-pressure electrostatic has electrostatic precipitation, a Franklin wheel etc., the principle of Franklin is to discharge in flywheel tip under High Pressure, under the effect of highfield, near most advanced and sophisticated, airborne remaining charged ion is accelerated and vigorous exercise, and the acting in conjunction of a large amount of microcosmic ions has realized the macroscopic view of flywheel and rotated.But only rely on angular momentum effect, its rotating effect cannot be given beholder's impression that ion sprays intuitively.The utility model is set up intensive metal needle cusp battle array, and moment produces a large amount of ions, to obtain larger momentum.
Summary of the invention
For more intuitively showing that ion power advances effect, make beholder to ion power, advance that there is a profound understanding, the purpose of this utility model is to provide a kind of ion power to advance demonstrator.
The utility model is achieved like this, it comprises small-sized source of the gas, tracheae, air track air intake opening, left closure plate, left insulated column, suspension sliding body, crosses wire carrier, support, right insulated column, wire, electrostatic high-pressure source, air track, needle point dot matrix, right closure plate, suspension and suspension interface; It is characterized in that: small-sized source of the gas connects tracheae, tracheae connects air track by air track air intake opening, air track left and right two ends are respectively arranged with left insulated column, left closure plate, right insulated column and right closure plate, suspension level is guided right insulated column into from left insulated column, suspension right-hand member is provided with suspension interface, and connect electrostatic high-pressure source by wire, suspension was provided with wire carrier, cross wire carrier lower end and connect suspension sliding body by support, two needle point dot matrix sizes are identical by the symmetrical both sides that are placed in suspension sliding body that connect of support.
Small-sized source of the gas described in the utility model, tracheae and air track air intake opening form a device that suspension power is provided.
Suspension sliding body described in the utility model, mistake wire carrier, support and needle point dot matrix form a suspension propulsion plant.
The power source of suspension propulsion plant described in the utility model consists of needle point dot matrix, and needle point dot matrix consists of a large amount of elongated needle points, and vertical panel face is arranged intensive, is level and points to.
Suspension propulsion plant described in the utility model is realized and being suspended by the airflow function of air track.
The high pressure that electrostatic high-pressure described in the utility model source discharges passes to needle point dot matrix by suspension, mistake wire carrier and support, realizes the ionization of air is obtained to power.
Its principle of work is: suspension propulsion plant is placed on air track, opens small-sized source of the gas, and the propulsion plant that now suspends floats through airflow function, crossing make progress ejection and suspension of wire carrier suits, the chimeric corresponding suspension of its groove, suspension is arranged in guide rail top, by both sides insulated column, is fixed.Start electrostatic high-pressure source, electrostatic high-pressure to suspension, arrives needle point dot matrix through wire carrier and support through wire transmission, realizes the ionization to air, and needle point dot matrix obtains the boosting power of high-speed ion, and whole suspension propulsion plant can suspension level move ahead.
Effect of the present utility model is: make intensive needle point dot matrix, under High Pressure, ionized air obtains larger momentum; Under High Pressure, needle point dot matrix moves ahead by air track and glider realization suspension, possesses ion power more intuitively and advances demonstration effect.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
In the drawings, 1, the left insulated column 6. suspension sliding bodies 7. of the left closure plate 5. of small-sized source of the gas 2. tracheae 3. air track air intake opening 4. are crossed the right closure plate 15. suspension 16. suspension interfaces of the wire carrier right insulated column 10. wire 11. electrostatic high-pressure source 12. air track 13. needle point dot matrix 14. of 8. support 9..
Embodiment
Below in conjunction with accompanying drawing explanation, embodiment of the present utility model is described in further detail, but the present embodiment is not limited to the utility model, every employing analog structure of the present utility model and similar variation thereof, all should list protection domain of the present utility model in.
As shown in Figure 1, the utility model is to come like this work and enforcement, and it comprises small-sized source of the gas 1, tracheae 2, air track air intake opening 3, left closure plate 4, left insulated column 5, suspension sliding body 6, crosses wire carrier 7, support 8, right insulated column 9, wire 10, electrostatic high-pressure source 11, air track 12, needle point dot matrix 13, right closure plate 14, suspension 15 and suspension interface 16, it is characterized in that: small-sized source of the gas 1 connects tracheae 2, tracheae connects air track 12 by air track air intake opening 3, air track 12 left and right two ends are respectively arranged with left insulated column 5, left closure plate 4, right insulated column 9 and right closure plate 14, suspension 15 levels are guided right insulated column 9 into from left insulated column 8, suspension 15 right-hand members are provided with suspension interface 16, and connect electrostatic high-pressure source 11 by wire 10, suspension 15 was provided with wire carrier 7, cross wire carrier 7 lower ends and connect suspension sliding body 6 by support 8, two needle point dot matrix 13 sizes are identical by the symmetrical both sides that are placed in suspension sliding body 6 that connect of support 8.
During use, it is upper that suspended propulsion system is placed in air track (12), opens small-sized source of the gas (1), and now suspended propulsion system floats through airflow function, cross wire carrier (7) upwards ejection and suspension 15 suit, the chimeric corresponding suspension of its groove (15).Suspension 15 is arranged in guide rail top, by both sides, by insulated column, is fixed.Start electrostatic high-pressure source (11), electrostatic high-pressure is transferred to suspension (15) through wire (10), now crossing wire carrier (7) contacts with suspension (15), electrostatic high-pressure passed to wire carrier (7), passed to needle point dot matrix (13) again through support (8), realized the ionization to air, needle point dot matrix (13) obtains the boosting power of high-speed ion, the motion of drive suspended propulsion system, through wire carrier (7) and suspension (15) guiding, whole suspended propulsion system can suspension level move ahead.
Claims (3)
1. ion power advances a demonstrator, and it comprises small-sized source of the gas, tracheae, air track air intake opening, left closure plate, left insulated column, suspension sliding body, crosses wire carrier, support, right insulated column, wire, electrostatic high-pressure source, air track, needle point dot matrix, right closure plate, suspension and suspension interface; It is characterized in that: small-sized source of the gas connects tracheae, tracheae connects air track by air track air intake opening, air track left and right two ends are respectively arranged with left insulated column, left closure plate, right insulated column and right closure plate, suspension level is guided right insulated column into from left insulated column, suspension right-hand member is provided with suspension interface, and connect electrostatic high-pressure source by wire, suspension was provided with wire carrier, cross wire carrier lower end and connect suspension sliding body by support, two needle point dot matrix sizes are identical by the symmetrical both sides that are placed in suspension sliding body that connect of support.
2. a kind of ion power according to claim 1 advances demonstrator, it is characterized in that: described suspension sliding body, mistake wire carrier, support and needle point dot matrix form a suspension propulsion plant.
3. a kind of ion power according to claim 2 advances demonstrator, it is characterized in that: the power source of described suspension propulsion plant consists of needle point dot matrix, and needle point dot matrix consists of a large amount of elongated needle points, and vertical panel face is arranged intensive, is level and points to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420183186.4U CN203825912U (en) | 2014-04-16 | 2014-04-16 | Ion dynamic propulsion demonstration instrument |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420183186.4U CN203825912U (en) | 2014-04-16 | 2014-04-16 | Ion dynamic propulsion demonstration instrument |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203825912U true CN203825912U (en) | 2014-09-10 |
Family
ID=51481386
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201420183186.4U Expired - Fee Related CN203825912U (en) | 2014-04-16 | 2014-04-16 | Ion dynamic propulsion demonstration instrument |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203825912U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109285431A (en) * | 2018-11-02 | 2019-01-29 | 安徽新华学院 | A kind of demonstration Biot-Sa farr's law experimental system and experimental method |
CN112802384A (en) * | 2021-01-14 | 2021-05-14 | 山东师范大学 | Mechanical experiment equipment, system and method based on air cushion guide rail |
-
2014
- 2014-04-16 CN CN201420183186.4U patent/CN203825912U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109285431A (en) * | 2018-11-02 | 2019-01-29 | 安徽新华学院 | A kind of demonstration Biot-Sa farr's law experimental system and experimental method |
CN109285431B (en) * | 2018-11-02 | 2023-11-21 | 安徽新华学院 | Experimental system and experimental method for demonstrating Biaoo-Safire law |
CN112802384A (en) * | 2021-01-14 | 2021-05-14 | 山东师范大学 | Mechanical experiment equipment, system and method based on air cushion guide rail |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN203825912U (en) | Ion dynamic propulsion demonstration instrument | |
CN204034281U (en) | 4d dynamic chair | |
CN203733382U (en) | Physics teaching experiment tool | |
CN204143694U (en) | Miao Le-Lai Yier optical illusion demonstrator | |
MY168400A (en) | Moisturizing apparatus and electrical equipment including the same, and moisturizing method | |
CN203588486U (en) | English teaching tool | |
CN202563766U (en) | Level-throwing movement demonstration instrument | |
Sahoo et al. | Control of non-solid diffusers by electrostatic charging | |
CN201629081U (en) | Electrostatic comprehensive demonstration device | |
CN205541578U (en) | Appearance is demonstrated with higher speed to static | |
CN204155525U (en) | A kind of refraction demonstrator of light | |
CN203648062U (en) | Spraying device for flying simulation | |
CN203887354U (en) | Solar battery piece series welding machine | |
CN202736362U (en) | High-frequency electric field demonstration device | |
CN203773821U (en) | Current magnetic effect and current heat effect demonstration instrument for teaching | |
CN202997302U (en) | Lightning arrester | |
CN203134216U (en) | A demonstrator of reactive movement of force | |
CN203786981U (en) | Electromagnetic acceleration demonstration device | |
CN202996141U (en) | Soap bubble non-polar molecule polarization demonstration instrument | |
CN204558889U (en) | The artificial negative ion emitter of a kind of high concentration | |
CN206162947U (en) | Physical experiment device | |
CN204383006U (en) | A kind of blackboard eraser | |
CN204505804U (en) | A kind of robot device | |
CN208298404U (en) | A kind of portable multi-media classroom learning machine | |
CN204414881U (en) | A kind of pressing Dustproof chalk |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140910 Termination date: 20150416 |
|
EXPY | Termination of patent right or utility model |