CN220984055U - Moon exploration satellite orbit demonstration model - Google Patents
Moon exploration satellite orbit demonstration model Download PDFInfo
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- CN220984055U CN220984055U CN202321877074.4U CN202321877074U CN220984055U CN 220984055 U CN220984055 U CN 220984055U CN 202321877074 U CN202321877074 U CN 202321877074U CN 220984055 U CN220984055 U CN 220984055U
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- 238000004088 simulation Methods 0.000 claims abstract description 78
- 239000002184 metal Substances 0.000 claims abstract description 27
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of demonstration equipment, and discloses a lunar exploration satellite orbit demonstration model, wherein a plurality of orbits are arranged on the surface of a sphere model, the orbits can rotate freely, and a satellite model capable of moving along the orbits is arranged on each orbit, so that the effect of simultaneously simulating different orbit orbits of a plurality of satellites is realized, and the lunar exploration satellite orbit demonstration model can meet the requirements of simulation demonstration of various lunar exploration satellite orbits; can carry out flexible removal at the metal pole through extension branch to when the inside of shrink metal pole, can dismantle or install additional to the simulation orbit, can run through all simulation orbits when extending branch and stretch out simultaneously, thereby the simulation orbit can reach the function of being convenient for according to the different satellite orbits of teaching demand quantity through extension branch at the surface free rotation's of spheroid model setting during, improve demonstration model's practicality.
Description
Technical Field
The utility model relates to the technical field of demonstration equipment, in particular to a lunar exploration satellite orbit demonstration model.
Background
The satellite orbit demonstration model is mainly used for simulating the earth outside detection satellite orbit so as to facilitate better understanding of students, and the existing satellite orbit demonstration model is mainly used for demonstrating through connecting the surface of a sphere model with an arc and placing a satellite model on the arc;
The current publication number is: CN210467013U discloses a device for demonstrating satellite motion, the lower surface of the box is fixedly provided with a protection base, the outer surface of the protection base is fixedly provided with a first controller, the upper surface of the protection base is fixedly provided with a supporting seat, the upper surface of the box is fixedly connected with a fixed bracket, the interior of the fixed bracket is penetrated with a first driving motor, the upper surface of the supporting seat is fixedly provided with a second driving motor, and the upper end of the second driving motor is connected with a first rotating assembly.
The existing sphere model surface generally has only a single orbit and cannot move, so that when a satellite orbit is simulated, the same orbit can only be simulated, and the orbit of a plurality of satellites can not be simulated when the satellites cooperatively work, so that the demonstration model is poor in interestingness, can not attract students to learn, can not meet the use of education, is inconvenient to assemble the satellite orbit at the sphere model, cannot install the actual number of the satellite orbits according to actual teaching requirements, and reduces the practicability of the demonstration model.
Disclosure of utility model
The utility model aims at providing a lunar exploration satellite orbit demonstration model for the existing device, and has the advantages of being capable of simulating different orbit orbits of a plurality of satellites simultaneously and facilitating the functions of different satellite orbits according to the number of teaching requirements.
The technical aim of the utility model is realized by the following technical scheme: the moon exploration satellite orbit demonstration model comprises a sphere model, wherein a metal rod is connected in a penetrating and rotating manner in the sphere model, an inner ring simulation orbit, a middle ring simulation orbit and an outer ring simulation orbit are sequentially arranged on the surface of the metal rod from inside to outside, satellite models are arranged on one sides of the tops of the inner ring simulation orbit, the middle ring simulation orbit and the outer ring simulation orbit, guide grooves are formed in the inner ring simulation orbit, the middle ring simulation orbit and the outer ring simulation orbit, gears which are in sliding connection with the guide grooves are connected with the bottoms of the satellite models in a rotating manner, and tooth grooves meshed with the gears are formed in the guide grooves; the two ends of the metal rod are connected with extension supporting rods which are connected with the inner ring simulation track, the middle ring simulation track and the outer ring simulation track in a rotating mode, a hexagonal groove is formed in one end, far away from the metal rod, of each extension supporting rod, and magnet rings which are magnetically connected with the extension supporting rods are arranged inside the inner ring simulation track, the middle ring simulation track and the outer ring simulation track.
The technical scheme is adopted: the surface of the sphere model is provided with a plurality of orbits, the orbits can rotate freely, and each orbit is provided with a satellite model capable of moving along the orbit, so that the effect of simulating different orbit orbits of a plurality of satellites is realized, and the simulation demonstration requirement of the orbits of a plurality of lunar exploration satellites can be met; can carry out flexible removal at the metal pole through extension branch to when the inside of shrink metal pole, can dismantle or install additional to the simulation orbit, can run through all simulation orbits when extending branch and stretch out simultaneously, thereby the simulation orbit can reach the function of being convenient for according to the different satellite orbits of teaching demand quantity through extension branch at the surface free rotation's of spheroid model setting during, improve demonstration model's practicality.
The utility model is further characterized in that the bottom of the sphere model is provided with a supporting rod, the inside of the supporting rod is connected with an extension rod connected with the sphere model in a sliding way, and the front surface of the supporting rod is connected with a limit bolt connected with the extension rod in a clamping way in a threaded way.
The technical scheme is adopted: the sliding extension rod drives the sphere model to be adjusted up and down, and then the setting that the sphere model can be fixed by rotating the limit bolt achieves the function of being convenient for adjust the satellite orbit demonstration model height according to user's height to make the satellite orbit demonstration model applicable to the people of different heights, improve the practicality of satellite orbit demonstration model.
The utility model further provides that one end of the extension supporting rod far away from the metal rod is clamped with a clamping cover through a hexagonal groove.
The technical scheme is adopted: one end of the extension supporting rod can be blocked and covered, so that the extension supporting rod can be conveniently fixed.
The utility model further provides that the surface of the sphere model is adhered with the simulation sticker.
The technical scheme is adopted: the reality of the lunar exploration satellite orbit demonstration model can be improved by arranging the simulation sticker, so that a user can simulate the lunar exploration satellite orbit demonstration model better.
The utility model further provides that the surface of the limit bolt is provided with anti-skid stripes.
The technical scheme is adopted: the friction force during rotation of the limit bolt can be improved by arranging the anti-skid stripes, so that the limit bolt can be conveniently rotated.
The utility model is further arranged that the bottom of the supporting rod is welded with a bottom plate, and the bottom of the anti-skid pad is adhered with an anti-skid pad.
The technical scheme is adopted: the stability of the lunar exploration satellite orbit demonstration model can be improved by arranging the bottom plate and the anti-skid pad.
Compared with the prior art, the utility model has the following beneficial effects:
According to the utility model, the plurality of orbits are arranged on the surface of the sphere model, the orbits can rotate freely, and each orbit is provided with the satellite model capable of moving along the orbit, so that the effect of simulating different orbit of a plurality of satellites simultaneously is realized, and the simulation demonstration requirement of the orbits of a plurality of lunar exploration satellites can be met;
According to the utility model, the extension support rod can stretch and retract on the metal rod, so that the simulation orbit can be disassembled or added when the extension support rod is retracted into the metal rod, and meanwhile, the extension support rod can penetrate through all the simulation orbits when extended, so that the simulation orbits can freely rotate on the surface of the sphere model through the arrangement of the extension support rod, the function of conveniently changing satellite orbits according to the number of teaching requirements is achieved, and the practicability of the demonstration model is improved.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a side cross-sectional view of the present utility model;
Fig. 3 is a partial structural cross-sectional view of the present utility model.
In the figure: 1. a sphere model; 2. a metal rod; 3. an inner ring simulates a track; 4. middle ring simulation track; 5. an outer ring simulation track; 6. a satellite model; 7. a magnet ring; 8. a support rod; 9. an extension rod; 10. a limit bolt; 11. a guide groove; 12. a gear; 13. tooth slots; 14. an anti-slip pad; 15. a bottom plate; 16. an extension strut; 17. hexagonal grooves; 18. and (5) clamping the cover.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Example 1:
Referring to fig. 1, 2 and 3, a lunar exploration satellite orbit demonstration model comprises a sphere model 1, wherein a metal rod 2 is connected in a penetrating and rotating manner in the sphere model 1, an inner ring simulation orbit 3, an intermediate ring simulation orbit 4 and an outer ring simulation orbit 5 are sequentially arranged on the surface of the metal rod 2 from inside to outside, satellite models 6 are arranged on one side of the tops of the inner ring simulation orbit 3, the intermediate ring simulation orbit 4 and the outer ring simulation orbit 5, guide grooves 11 are formed in the inner ring simulation orbit 3, the intermediate ring simulation orbit 4 and the outer ring simulation orbit 5, a gear 12 which is in sliding connection with the guide grooves 11 is rotationally connected to the bottom of the satellite models 6, and tooth grooves 13 meshed with the gear 12 are formed in the guide grooves 11; the multiple orbits are arranged on the surface of the sphere model, the orbits can rotate freely, and each orbit is provided with the satellite model capable of moving along the orbit, so that the effect of simulating different orbit orbits of multiple satellites is achieved, and the simulation demonstration requirement of multiple moon exploration satellite orbits can be met.
Referring to fig. 1 and 2, the bottom of the sphere model 1 is provided with a supporting rod 8, an extension rod 9 rotationally connected with the sphere model 1 is slidingly connected in the supporting rod 8, a limit bolt 10 clamped with the extension rod 9 is connected with the front thread of the supporting rod 8, the sliding extension rod drives the sphere model to be adjusted up and down, and then the setting that the sphere model can be fixed by rotating the limit bolt is achieved, so that the function of conveniently adjusting the height of the satellite orbit demonstration model according to the height of a user is achieved, the satellite orbit demonstration model can be suitable for people with different heights, and the practicability of the satellite orbit demonstration model is improved.
Referring to fig. 1, a simulation sticker is adhered to the surface of a sphere model, and the reality of a lunar exploration satellite orbit demonstration model can be improved by arranging the simulation sticker, so that a user can perform simulation better.
Referring to fig. 2, anti-slip stripes are provided on the surface of the limit bolt, and friction force during rotation of the limit bolt can be improved by providing the anti-slip stripes, so that the limit bolt can be conveniently rotated.
The use process is briefly described: when different track orbits of a plurality of satellites are required to be simulated simultaneously, the inner ring simulation orbit 3, the middle ring simulation orbit 4 and the outer ring simulation orbit 5 are respectively stirred according to teaching requirements, so that the inner ring simulation orbit 3, the middle ring simulation orbit 4 and the outer ring simulation orbit 5 rotate on the surface of the sphere model 1, then the satellite model 6 is stirred to drive the gear 12 to be meshed with the tooth grooves 13, and then the gear is made to slide in the guide grooves 11, so that the satellite model 6 can freely move in the inner ring simulation orbit 3, the middle ring simulation orbit 4 and the outer ring simulation orbit 5 respectively, and a demonstration model can demonstrate the movement modes of the plurality of satellites under different tracks.
Example 2:
Referring to fig. 1 and 2, a lunar exploration satellite orbit demonstration model is provided, two ends of a metal rod 2 are connected with an extension support rod 16 in a threaded manner, the extension support rod 16 is in rotary connection with an inner ring simulation orbit 3, an intermediate ring simulation orbit 4 and an outer ring simulation orbit 5, one end of the extension support rod 16, which is far away from the metal rod 2, is provided with a hexagonal groove 17, and magnet rings 7 which are magnetically connected with the extension support rod 16 are arranged in the inner ring simulation orbit 3, the intermediate ring simulation orbit 4 and the outer ring simulation orbit 5; can carry out flexible removal at the metal pole through extension branch 16 to when the inside of shrink metal pole, can dismantle or install additional to the simulation orbit, can run through all simulation orbits when extension branch 16 stretches out simultaneously, thereby the simulation orbit can reach the function of being convenient for according to the different satellite orbits of teaching demand quantity through extension branch 16 at the surface free rotation's of spheroid model setting, improves demonstration model's practicality.
Referring to fig. 2, the end of the extension strut 16 far away from the metal rod 2 is clamped with a clamping cover 18 through a hexagonal groove 17, so that the end of the extension strut 16 can be clamped and covered, and the extension strut 16 is convenient to fix.
Referring to fig. 1 and 2, the bottom of the support rod is welded with a bottom plate, the bottom of the anti-slip pad is adhered with an anti-slip pad, and the stability of the lunar exploration satellite orbit demonstration model can be improved by arranging the bottom plate and the anti-slip pad.
The use process is briefly described: when the satellite orbits are different in quantity according to teaching requirements, the hexagonal wrench is used for inserting the inside of the hexagonal groove 17 to enable the hexagonal groove to rotate, the extension supporting rod 16 is meshed with the internal threads of the metal rod 2, the extension supporting rod 16 slides into the metal rod 2, then the extension supporting rod 16 is taken out or added according to the quantity of the analog orbits required by teaching, and then the extension supporting rod 16 is reversely rotated to extend out of the metal rod 2, so that the extension supporting rod 16 can penetrate through all the analog orbits, the analog orbits are fixed, meanwhile, the analog orbits can rotate on the surface of the extension supporting rod 16 through the magnet ring 7, and when the analog orbits are not stirred by an unmanned person, the magnetic force of the magnet ring 7 can be adsorbed on the extension supporting rod 16, so that the position of the analog orbits is limited and fixed.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The moon exploration satellite orbit demonstration model comprises a sphere model (1), and is characterized in that: the inner part of the sphere model (1) is connected with a metal rod (2) in a penetrating and rotating manner, the surface of the metal rod (2) is sequentially provided with an inner ring simulation track (3), an intermediate ring simulation track (4) and an outer ring simulation track (5) from inside to outside, one side of the tops of the inner ring simulation track (3), the intermediate ring simulation track (4) and the outer ring simulation track (5) is provided with a satellite model (6), the interiors of the inner ring simulation track (3), the intermediate ring simulation track (4) and the outer ring simulation track (5) are provided with guide grooves (11), the bottom of the satellite model (6) is rotationally connected with a gear (12) which is in sliding connection with the guide grooves (11), and the interiors of the guide grooves (11) are provided with tooth grooves (13) meshed with the gear (12); the two ends of the metal rod (2) are connected with an extension supporting rod (16) which is connected with the inner ring simulation track (3), the middle ring simulation track (4) and the outer ring simulation track (5) in a rotating mode, a hexagonal groove (17) is formed in one end, far away from the metal rod (2), of the extension supporting rod (16), and the inner ring simulation track (3), the middle ring simulation track (4) and the inner ring simulation track (5) are respectively provided with a magnet ring (7) which is connected with the extension supporting rod (16) in a magnetic mode.
2. The lunar exploration satellite orbit demonstration model according to claim 1, wherein: the bottom of spheroid model (1) is provided with bracing piece (8), the inside sliding connection of bracing piece (8) has extension rod (9) with spheroid model (1) rotation connection, the positive threaded connection of bracing piece (8) has limit bolt (10) with extension rod (9) joint.
3. The lunar exploration satellite orbit demonstration model according to claim 1, wherein: one end of the extension supporting rod (16) far away from the metal rod (2) is clamped with a clamping cover (18) through a hexagonal groove (17).
4. The lunar exploration satellite orbit demonstration model according to claim 1, wherein: the surface of the sphere model (1) is adhered with a simulation sticker.
5. The lunar exploration satellite orbit demonstration model according to claim 2, wherein: anti-slip stripes are formed on the surface of the limit bolt (10).
6. The lunar exploration satellite orbit demonstration model according to claim 2, wherein: the bottom of the supporting rod (8) is welded with a bottom plate (15), and an anti-slip pad (14) is adhered to the bottom of the bottom plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321877074.4U CN220984055U (en) | 2023-07-17 | 2023-07-17 | Moon exploration satellite orbit demonstration model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321877074.4U CN220984055U (en) | 2023-07-17 | 2023-07-17 | Moon exploration satellite orbit demonstration model |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220984055U true CN220984055U (en) | 2024-05-17 |
Family
ID=91040649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321877074.4U Active CN220984055U (en) | 2023-07-17 | 2023-07-17 | Moon exploration satellite orbit demonstration model |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220984055U (en) |
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2023
- 2023-07-17 CN CN202321877074.4U patent/CN220984055U/en active Active
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