CN2606419Y - Multifunctional solar system astroscope - Google Patents
Multifunctional solar system astroscope Download PDFInfo
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- CN2606419Y CN2606419Y CN 02284183 CN02284183U CN2606419Y CN 2606419 Y CN2606419 Y CN 2606419Y CN 02284183 CN02284183 CN 02284183 CN 02284183 U CN02284183 U CN 02284183U CN 2606419 Y CN2606419 Y CN 2606419Y
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- solar system
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Abstract
A multifunctional solar system astroscope comprises solar light source, and further consists of a circumsolar planetary orbit groove (1), planetary elements (2) running in the planetary orbit groove (1). The utility model has the advantages that the complicated movement of the solar system and the consequent astronomy phenomena can be displayed iconically, vividly and intuitively before audience, such as solar eclipse and lunar eclipse, therefore, the audience, especially the students can easily establish an astronomic knowledge space, and can memorize and comprehend easily without feeling bored. The utility model can intrigue the learning interests of students and promote the generalization of astronomical geographic knowledge, meanwhile, the utility model can serve as an intellectual toy, thereby integrating knowledge and fun.
Description
Technical field
The utility model relates to teaching aid performance technology field, the multi-functional astronomical demonstrator of specifically a kind of solar system.
Background technology
Tradition explanation chronometer phenomenon as: earth rotation, revolution, the four seasons, solar term, day alternates with night, polar day, polar night, the phases of the moon, day, lunar eclipse, morning and evening tides etc. mainly lean on the speaker to describe with language and by picture presentation, the teacher often spends all dispute, the student remains and has half knowledge, can not in brain, set up the space of an imagination, so there are many students all can not grasp the knowledge of this respect all sidedly, make teaching not reach the effect of anticipation, the student also learns worried more more, is difficult to set up the learning interest of this respect.
Summary of the invention
The purpose of this utility model is that a kind of usefulness of design is demonstrated the most intuitively, allows the student set up the space of an imagination soon, grasps the multi-functional astronomical demonstrator of the solar system of astronomical geography knowledge with getting twice the result with half the effort.
The multi-functional astronomical demonstrator of the utility model solar system comprises: solar source, circumsolar planetary orbit groove, the planetary assemblies of moving in the planet rail groove.
Planetary assemblies comprises: planet, planet bracing frame, planet revolution motion device, planetary rotation telecontrol equipment, satellite component.
Planet comprises: nine major planets, asteroid and comet.
Planet revolution motion device comprises: band roller underframe, be contained in the gearing of forming by motor and transmission gear on the underframe, or the gearing of clockwork spring and transmission gear means composition, the motion of the motion of the structure of this device and toy for children remote control racing car now or the automobile toy of clockwork spring formula is similar substantially.
The planetary rotation telecontrol equipment comprises: the gearing that motor and transmission gear are formed, or the gearing of clockwork spring and transmission gear means composition, and this device links to each other with the planetary rotation axle, and this device can be contained in outside the planet, also can be contained in the planet.
Satellite component comprises: arm satellite component or rail groove satellite component.
The rail groove satellite component comprises: satellite, and the satellite orbit groove, the suspension rod of satellite orbit groove and pole drive the revolution motion device that satellite rotates, the spinning motion device, satellite public affairs, spinning motion apparatus structure and planet public affairs, spinning motion apparatus structure are basic identical.
The arm satellite component comprises: the telecontrol equipment of arm, satellite, drive arm rotational motion device and drive satellite spin.The telecontrol equipment of arm rotational motion device, satellite spin all is the telecontrol equipment of motor driven gear transmission or the transmission of clockwork spring driven gear.
The satellite spin telecontrol equipment can be contained in outside the satellite, also can be contained in the satellite.
Planet, satellite motion speed and volume size, phase mutual edge distance etc. can design in proportion.
The revolution of planet, satellite, the telecontrol equipment of rotation all can be loaded onto telechiric device, simultaneously also can with the supporting use of computer.
The sun is a liftable illuminating source device.
The planetary orbit groove can be the rail groove of assembly unit, or whole rail groove, and the rail groove cross section can be U type, H type, V-type and other shape, marks corresponding chronometer data at the diverse location of rail groove, as twenty-four solar terms etc.
The multi-functional astronomical demonstrator of the solar system can be pieced together and tear combination open, according to teaching and intelligence development needs, can select wherein part demonstration for use.
The advantage of the multi-functional astronomical demonstrator of the utility model solar system is: can be in face of the audience all sidedly visually, true to nature, show the motion of solar system complexity and the chronometer phenomenon that causes thus intuitively, as: day, lunar eclipse etc. all very are presented in face of the audience intuitively, make student audience be easy to set up the space of an astronomic knowledge, memory is understood easily, study is got up not uninteresting, it can mobilizing students learning interest, to popularizing astronomical geography knowledge very big facilitation is arranged, simultaneously also can be used as puzzle, post knowledge among playing.
Description of drawings
Fig. 1 is that planet is around sun operating structure figure.
Fig. 2 is arm hanging type planet, satellite motion device public affairs, rotating device structural drawing.
Fig. 3 is rail mounted planet, satellite motion device public affairs, rotating device structural drawing.
Fig. 4 is satellite public affairs, spinning motion apparatus structure synoptic diagram.
Embodiment
Embodiment one:
According to Fig. 1, Fig. 2, shown in Figure 4, load onto solar source 3, around the planetary orbit groove 1 of solar source 3, planetary assemblies 2 is contained in the planetary orbit groove 3.Planetary assemblies 2 is by the underframe 8 of band roller and be contained in the planetary driving device of being made up of motor, transmission gear on the underframe 8 of band roller 7 and drive the roller shafts rollings, the axle of planetary rotation device of being made up of motor, transmission gear 6 and planet 4 links to each other, planetary rotation device 6 is contained on the underframe 8 of band roller, and planet bearing support 5 two ends link to each other with the planet axis two ends respectively.Satellite orbit groove 15 links to each other with the suspension rod 13 that is contained in planet bearing support 5 tops, links to each other with the pole 16 that is contained in satellite orbit groove 15 belows simultaneously, and satellite component 14 is contained in the satellite orbit groove 15.Satellite component 14 comprises: satellite revolution motion device 19 and satellite spin telecontrol equipment 18 that satellite 12 links to each other with satellite, satellite public affairs, rotating device 17,18 all are contained on the underframe 17 of band roller.The public spinning motion device of satellite motion revolution, rotating device 19,18 and planet is the same.
Embodiment two:
According to Fig. 1, shown in Figure 3, satellite orbit 15 among the embodiment one, suspension rod 13, pole 16 are removed, satellite revolution motion device 9 on changing cantalever rod 10 1 ends into and being contained in planet bracing frame 5 links to each other, the other end links to each other with satellite spin telecontrol equipment 11, satellite 12 links to each other with rotating device 11, and other is the same with embodiment one.
What embodiment three, four and embodiment one, two were different is that motor all changes clockwork spring in the telecontrol equipment, and other is all the same.
Claims (6)
1, the multi-functional astronomical demonstrator of a kind of solar system, comprising: the light source of the sun (3) is characterized in that: also have circumsolar planetary orbit groove (1), be contained in the planetary assemblies (2) of operation in the planetary orbit groove (1).
2, the multi-functional astronomical demonstrator of a kind of solar system according to claim 1 is characterized in that: planetary orbit groove (1) can be integral body or assembly component.
3, the multi-functional astronomical demonstrator of a kind of solar system according to claim 1, it is characterized in that: planetary assemblies (2) comprising: planet (4) links to each other by axle with planetary rotation telecontrol equipment (6), planetary rotation telecontrol equipment (6) is contained on the band roller underframe (4), planet bearing support 5 is contained on the axle that links to each other with planet 4, planet revolution motion device (7) is contained on the underframe (4) of band roller, and satellite component is contained on the planet bearing support (5).
4, the multi-functional astronomical demonstrator of a kind of solar system according to claim 1, it is characterized in that: satellite component comprises: arm satellite component and rail groove satellite component.
5, the multi-functional astronomical demonstrator of a kind of solar system according to claim 4, it is characterized in that: the arm satellite component comprises: be contained in the satellite spin telecontrol equipment (11) that cantalever rod (10) that the satellite revolution motion device (9) on the planet bearing support (5) links to each other with satellite revolution motion device (9) links to each other with cantalever rod (10), the satellite (12) that links to each other with satellite spin telecontrol equipment (11).
6, the multi-functional astronomical demonstrator of a kind of solar system according to claim 4, it is characterized in that: the rail groove satellite component comprises: rail groove (15), the suspension rod (13) that links to each other with rail groove (15), pole (16), be contained in the satellite component (14) in the rail groove (15), satellite revolution in the satellite component (14), the structure and the planet of spinning motion device (19) (18) revolve round the sun, self-chambering telecontrol equipment (6) (7) structure is the same, and satellite revolution, spinning motion device (19) (18) are contained on the underframe (17) of band roller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02284183 CN2606419Y (en) | 2002-11-14 | 2002-11-14 | Multifunctional solar system astroscope |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02284183 CN2606419Y (en) | 2002-11-14 | 2002-11-14 | Multifunctional solar system astroscope |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2606419Y true CN2606419Y (en) | 2004-03-10 |
Family
ID=34150849
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02284183 Expired - Fee Related CN2606419Y (en) | 2002-11-14 | 2002-11-14 | Multifunctional solar system astroscope |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2606419Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105632324A (en) * | 2016-03-14 | 2016-06-01 | 南京航空航天大学 | Solar system planet motion simulation system |
| CN110161879A (en) * | 2019-05-17 | 2019-08-23 | 南京航空航天大学 | A kind of semi physical experiment simulation platform of satellite in orbit |
-
2002
- 2002-11-14 CN CN 02284183 patent/CN2606419Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105632324A (en) * | 2016-03-14 | 2016-06-01 | 南京航空航天大学 | Solar system planet motion simulation system |
| CN105632324B (en) * | 2016-03-14 | 2018-11-09 | 南京航空航天大学 | Planets of the solar system operates simulation system |
| CN110161879A (en) * | 2019-05-17 | 2019-08-23 | 南京航空航天大学 | A kind of semi physical experiment simulation platform of satellite in orbit |
| CN110161879B (en) * | 2019-05-17 | 2021-04-20 | 南京航空航天大学 | Semi-physical experiment simulation platform for in-orbit operation of satellite |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |