CN202887593U - Operation model for driving rocket to fly to moon by earth in solar system - Google Patents
Operation model for driving rocket to fly to moon by earth in solar system Download PDFInfo
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- CN202887593U CN202887593U CN 201220592022 CN201220592022U CN202887593U CN 202887593 U CN202887593 U CN 202887593U CN 201220592022 CN201220592022 CN 201220592022 CN 201220592022 U CN201220592022 U CN 201220592022U CN 202887593 U CN202887593 U CN 202887593U
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Abstract
The utility model relates to an operation model for driving a rocket to fly to the moon by the earth in a solar system. The operation model comprises a sun shaft which is longitudinally arranged for driving the sun to rotate, wherein a frame is arranged at the bottom part of the sun shaft; a first planetary gear train for driving the earth to rotate is arranged on the sun shaft in a radial manner; a rigid cantilever for driving the earth to rotate is transversely arranged on a planet carrier of the first planetary gear train; an earth shaft is longitudinally arranged at the tail end of the rigid cantilever; an earth shaft is tipsily arranged at the upper end of the earth shaft; a second planetary gear train for driving the moon to rotate, and a third planetary gear train for driving the rocket to rotate are arranged on the earth shaft in the radial manner; a round hood body is arranged at the upper side of the first planetary gear train; a transmission shaft is transversely arranged at the lower side of the round hood body; and the transmission shaft is connected with the rigid cantilever through a bearing. The model operation is visual and comprehensive, and convenient to observe movement of a celestial body by people. Particularly outstandingly, the rocket is arranged at the outer layer of the planet, so that the rocket can simulate a real operation condition in a specific orbit.
Description
Technical field
The utility model relates to solar system earth zone rocket and flies moon moving model.
Background technology
At present, solar system moving model is only summarized planet ruuning situation usually, usually ignores the method for operation of rocket, this is unfavorable for studying the operation conditions of celestial bodies motion, artificial satellite and rocket, can't be familiar with intuitively moving law, therefore, planetarium lacks rocket and artificial satellite has to be solved; In addition, also exist on the market part with the planetarium of rocket, but moving law is single, simulation that can not be practical.
Summary of the invention
In view of the deficiencies in the prior art, the purpose of this utility model is to provide a kind of solar system earth zone rocket simulation to fly moon moving model.
To achieve these goals, the technical solution of the utility model is: a kind of solar system earth zone rocket flies moon moving model, comprise the solar shaft that is vertically arranged with for driving sun rotation, described solar shaft bottom is provided with frame, described solar shaft radially is provided be used to driving geocyclic the first row star wheel series, the planet carrier of described the first row star wheel series is horizontally arranged with the stiff cantilevers that drives revolution of earth, described stiff cantilevers end is vertically arranged with earth axis, described earth axis upper end is tiltedly installed with the earth's axis, the described earth's axis radially is provided with for the second planet circular system that drives moon revolution, and the third planet train that is used for driving the rocket revolution, the upside of described the first row star wheel series is provided with circular cover body, described circular cover body horizontally set is useful on the transmission shaft that drives earth rotation and satellite rotation, and described transmission shaft is connected to stiff cantilevers by bearing and directly makes progress.
Further, be provided with in the described frame for the motor that drives the solar shaft rotation, be provided with luminophor in the described sun, described luminophor and motor are by externally fed.
Further, described transmission shaft one end is provided with the bevel gear corresponding with circular cover body downside end-tooth, the described transmission shaft other end is provided with the bevel gear with earth bottom driving meshed transmission gear, in order to earth rotation, described transmission shaft radially drives earth's axis rotation by worm-and-wheel gear, move along elliptical orbit in order to the earth, then react dividing of the earth four seasons.
Further, the planet carrier side of described the second planet circular system is provided with connecting rod, described connecting rod end is provided with the moon, in order to the moon around revolution of earth, the planet wheel spindle of described the second planet circular system is to being connected with belt pulley, described belt pulley is by the belt Opposite direction connection moon, in order to the reverse rotation of the moon.
Further, described third planet train comprises centre wheel, and described centre wheel connects planet carrier by an end two-stage planetary gear, and the planet carrier side is connected with rocket, does the elliptical orbit operation in order to rocket around the earth.
Further, described circular cover body and stiff cantilevers upside are provided with annular casing, in order to overall appearance, but are not limited to this, also can be arranged on the frame.
The utlity model has following advantage: adopt the running of multistage planet train and driving gear set simulation galaxy, directly perceived and comprehensive, be convenient to people to the observation of celestial bodies motion, particularly outstanding is, be provided with rocket at the planet skin, make the rocket can be with the true ruuning situation of specific orbital simulation, and, moving law can with the phase of planets with.
Description of drawings
Fig. 1 is the organigram of the utility model embodiment.
Among the figure, 1-solar shaft, 2-luminophor, 3-circular cover body, 4-the first row star wheel series, 5-motor, the 6-frame, 7-worm-and-wheel gear, 8-earth axis, 9-the second planet circular system, 10-the second planet circular system, the 11-earth's axis, the 12-moon, 13-rocket, the 14-earth, 15-annular casing, the 16-sun.
Embodiment
Below in conjunction with drawings and Examples the utility model is further elaborated.
With reference to figure 1, a kind of solar system earth zone rocket 13 moving models, comprise the solar shaft 1 that is vertically arranged with for driving the sun 16 rotations, described solar shaft 1 bottom is provided with frame 6, described solar shaft 1 radially is provided with for the first row star wheel series 4 that drives the earth 14 rotations, the planet carrier of described the first row star wheel series 4 is horizontally arranged with the stiff cantilevers that drives the earth 14 revolution, described stiff cantilevers end is vertically arranged with earth axis 8, described earth axis 8 upper ends are tiltedly installed with the earth's axis 11, the described earth's axis 11 radially is provided with for the second planet circular system 9 that drives the moon 12 revolution, and the third planet train 10 that is used for driving rocket 13 revolution, the upside of described the first row star wheel series 4 is provided with circular cover body 3, described circular cover body 3 horizontally sets are useful on the transmission shaft that drives the earth 14 rotations and satellite rotation, and described transmission shaft is connected to stiff cantilevers by bearing and directly makes progress.
In the present embodiment, be provided with in the described frame 6 for the motor 5 that drives solar shaft 1 rotation, be provided with luminophor 2 in the described sun 16, described luminophor 2 and motor 5 are by externally fed.
In the present embodiment, described transmission shaft one end is provided with the bevel gear corresponding with circular cover body 3 downside end-tooths, the described transmission shaft other end is provided with the bevel gear with the earth 14 bottom driving meshed transmission gear, in order to the earth 14 rotations, described transmission shaft radially drives the earth's axis 11 rotations by worm-and-wheel gear 7, along the elliptical orbit operation, then reflect dividing of 14 four seasons of the earth in order to the earth 14.
In the present embodiment, the planet carrier side of described the second planet circular system 9 is provided with connecting rod, described connecting rod end is provided with the moon 12, revolve round the sun around the earth 14 in order to the moon 12, the planet wheel spindle of described the second planet circular system 9 is to being connected with belt pulley, described belt pulley is by the belt Opposite direction connection moon 12, in order to the moon 12 reverse rotations.
In the present embodiment, described third planet train 10 comprises centre wheel, and described centre wheel connects planet carrier by an end two-stage planetary gear, and the planet carrier side is connected with rocket 13, does the elliptical orbit operation in order to rocket 13 around the earth 14.
In the present embodiment, described circular cover body 3 and stiff cantilevers upside are provided with annular casing 15, in order to overall appearance, but are not limited to this, also can be arranged on the frame 6.
The present embodiment principle of work is as follows: solar shaft 1 drives the sun 16 and rotates, simultaneously the first row star wheel series 4 runnings, by cantilever, the earth 14 is around the sun 16 revolution, at this moment, fixing circular cover body 3 downside end-tooths cooperate with the bevel gear of transmission shaft one end, and the transmission shaft rotation is by the bevel gear drive earth's axis 11 rotations of the other end, thereby drive the earth 14 rotations, in addition, transmission shaft is on the bearing that is located in the cantilever one, so transmission shaft is around solar shaft 1 rotation with cantilever.
Cantilever drives earth axis 8 and rotates, the earth's axis 11 is rotated with earth axis 8, simultaneously, transmission shaft drives worm-and-wheel gear 7, the earth 14 rotates around earth axis 8, thereby reach the earth 14 around the elliptical orbit operation of the sun 16, illustrate that the earth 14 has dividing of the four seasons, transmission shaft makes the earth 14 rotations by bevel gear set again; At this moment, the second planet circular system 9 conducts to the moon 12 with power under the drive of the earth's axis 11, and the moon 12 is around the earth's axis 11 revolution, and oppositely under the belt wheel effect, the moon 12 is again reverse rotation; Third planet train 10 is under the drive of the earth's axis 11 simultaneously, power is passed through the two-stage planet gear transmission of an end to planet carrier, planet carrier reaches power on the rocket 13 again, rocket 13 revolves round the sun around the earth 14 along elliptical orbit, when the earth 14, the moon 12 and rocket 13 being aligned money, rocket 13 has produced the effect of goddess in the moon's rocket 13 Benyues gradually near the moon 12.
The above only is preferred embodiment of the present utility model, and all equalizations of doing according to the utility model claim change and modify, and all should belong to covering scope of the present utility model.
Claims (6)
1. a solar system earth zone rocket flies moon moving model, comprise the solar shaft that is vertically arranged with for driving sun rotation, it is characterized in that, described solar shaft bottom is provided with frame, described solar shaft radially is provided be used to driving geocyclic the first row star wheel series, the planet carrier of described the first row star wheel series is horizontally arranged with the stiff cantilevers that drives revolution of earth, described stiff cantilevers end is vertically arranged with earth axis, described earth axis upper end is tiltedly installed with the earth's axis, the described earth's axis radially is provided with for the second planet circular system that drives moon revolution, and the third planet train that is used for driving the rocket revolution, the upside of described the first row star wheel series is provided with circular cover body, described circular cover body horizontally set is useful on the transmission shaft that drives earth rotation and satellite rotation, and described transmission shaft is connected to stiff cantilevers by bearing and directly makes progress.
2. solar system earth zone rocket according to claim 1 flies moon moving model, it is characterized in that, is provided with in the described frame for the motor that drives the solar shaft rotation, is provided with luminophor in the described sun.
3. solar system earth zone rocket according to claim 1 flies moon moving model, it is characterized in that, described transmission shaft one end is provided with the bevel gear corresponding with circular cover body downside end-tooth, the described transmission shaft other end is provided with the bevel gear with earth bottom driving meshed transmission gear, in order to earth rotation, described transmission shaft radially drives earth's axis rotation by worm-and-wheel gear, moves along elliptical orbit in order to the earth.
4. solar system earth zone rocket according to claim 1 flies moon moving model, it is characterized in that, the planet carrier side of described the second planet circular system is provided with connecting rod, described connecting rod end is provided with the moon, in order to the moon around revolution of earth, the planet wheel spindle of described the second planet circular system is to being connected with belt pulley, and described belt pulley is by the belt Opposite direction connection moon, in order to the reverse rotation of the moon.
5. solar system earth zone rocket according to claim 1 flies moon moving model, it is characterized in that, described third planet train comprises centre wheel, and described centre wheel connects planet carrier by an end two-stage planetary gear, the planet carrier side is connected with rocket, does the elliptical orbit operation in order to rocket around the earth.
6. solar system earth zone rocket according to claim 1 flies moon moving model, it is characterized in that, described circular cover body and stiff cantilevers upside are provided with annular casing, in order to overall appearance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220592022 CN202887593U (en) | 2012-11-12 | 2012-11-12 | Operation model for driving rocket to fly to moon by earth in solar system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220592022 CN202887593U (en) | 2012-11-12 | 2012-11-12 | Operation model for driving rocket to fly to moon by earth in solar system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202887593U true CN202887593U (en) | 2013-04-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220592022 Expired - Fee Related CN202887593U (en) | 2012-11-12 | 2012-11-12 | Operation model for driving rocket to fly to moon by earth in solar system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202887593U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104021720A (en) * | 2014-06-10 | 2014-09-03 | 上海理工大学 | Epicyclic gear train experiment training aid |
| CN105374274A (en) * | 2015-11-18 | 2016-03-02 | 苏州育龙科教设备有限公司 | Sun earth moon motion instrument |
-
2012
- 2012-11-12 CN CN 201220592022 patent/CN202887593U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104021720A (en) * | 2014-06-10 | 2014-09-03 | 上海理工大学 | Epicyclic gear train experiment training aid |
| CN105374274A (en) * | 2015-11-18 | 2016-03-02 | 苏州育龙科教设备有限公司 | Sun earth moon motion instrument |
| CN105374274B (en) * | 2015-11-18 | 2018-01-23 | 苏州育龙科教设备有限公司 | Day ground the moon running instrument |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP02 | Change in the address of a patent holder |
Address after: Chinese Hongkong Special Administrative Region Hongkong Zi Hua Yin House Luxury Estate Patentee after: Lin Bindian Address before: 350005 No. 35 Ma Jie street, Cangshan District, Fujian, Fuzhou Patentee before: Lin Bindian |
|
| 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: 20130417 Termination date: 20191112 |