CN210804966U - Aerospace moon exploration science popularization demonstration device - Google Patents
Aerospace moon exploration science popularization demonstration device Download PDFInfo
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- CN210804966U CN210804966U CN201922156002.0U CN201922156002U CN210804966U CN 210804966 U CN210804966 U CN 210804966U CN 201922156002 U CN201922156002 U CN 201922156002U CN 210804966 U CN210804966 U CN 210804966U
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Abstract
The utility model discloses a space flight moon exploration science popularization presentation device belongs to show technical field. An aerospace moon exploration science popularization demonstration device, comprising: the horizontal plate still includes: set up in vertical board, the remote controller of horizontal plate one end and vertical arrangement, the horizontal plate top surface be provided with moon ground pattern, vertical board openly is provided with the space pattern, the horizontal plate top surface still be provided with lunar rover model, astronaut model, the module of lunar chamber of stepping on, energy station model, earth model be one-eighth hemisphere and earth model and be located between horizontal plate and the vertical board, vertical board on be provided with red model mechanism in the east, model mechanism in the sky palace, national flag elevating system, vertical board on seted up the track groove, this practicality makes presentation device more vivid through dynamic display, is full of taste.
Description
Technical Field
The utility model belongs to the technical field of the show, especially, relate to a space flight moon exploration science popularization presentation device.
Background
With the rapid development of science and technology and the rapidness of network transmission information, aerospace science and technology walks into the visual field of people, although the science and technology of human beings changes day by day, the resource consumption is more and more, so that at present, the marching of marching into the military space is accelerated in various countries, so that in the age of the exhaustion of earth resources, the resource shortage is prevented by collecting space resources, more space workers are needed, the interest of people in space industry can be increased by a space science popularization demonstration device, so that people put into space industry, but the existing space display device is only static display, is not vivid enough, and the existing dynamic display is expensive in price and complex in structure.
SUMMERY OF THE UTILITY MODEL
1. Technical problem to be solved
Static show problem directly perceived inadequately to the space flight show that exists among the prior art, the utility model aims to provide a space flight visit scientific popularization presentation device solves the space flight show and is static show problem directly perceived inadequately.
2. Technical scheme
In order to solve the above problems, the utility model adopts the following technical proposal.
An aerospace moon exploration science popularization demonstration device, comprising: the horizontal plate still includes: the device comprises a horizontal plate, a vertical plate and a remote controller, wherein the vertical plate and the remote controller are arranged at one end of the horizontal plate and are vertically arranged, a moon ground pattern is arranged on the top surface of the horizontal plate, a space pattern is arranged on the front surface of the vertical plate, a lunar vehicle model, an astronaut model, a lunar chamber model, an energy station model and an earth model are further arranged on the top surface of the horizontal plate, the earth model is an eighth hemisphere and is positioned between the horizontal plate and the vertical plate, an oriental red model mechanism, a celestial palace model mechanism and a national flag lifting mechanism are arranged on the vertical plate, a track groove is formed in the vertical plate, one end of the track groove extends to the earth model, a space plane model mechanism is arranged on the track groove, and the remote controller is used for controlling the motion of the space plane model mechanism, the oriental red model mechanism, the celestial palace model mechanism and;
the national flag lifting mechanism comprises a supporting rod vertically arranged at the center of the top surface of a vertical plate, one side of the supporting rod, which is far away from a horizontal plate, is provided with a fixed shaft which is axially vertical to the vertical plate, a first driven wheel is coaxially sleeved outside the fixed shaft, the back surface of the vertical plate is provided with a first driving wheel matched with the first driven wheel, the first driving wheel is positioned under the first driven wheel, the first driving wheel is coaxially provided with an output shaft which extends towards the direction far away from the vertical plate, the suspension end of the output shaft is provided with a lifting motor, the lifting motor is connected with the vertical plate through a first fixed frame, the first driven wheel and the first driving wheel are belt wheels, a belt is arranged between the first driven wheel and the first driving wheel, the first driven wheel and the first driving wheel realize connection transmission through the belt, the outer side of the;
the Tiangong model I mechanism comprises a connecting rod penetrating through a vertical plate, a Tiangong model I is arranged at one end of the connecting rod, which is positioned in front of the vertical plate, a stressed gear is coaxially sleeved at one end of the connecting rod, which is positioned behind the vertical plate, an oval lantern ring is sleeved outside the stressed gear, a rack meshed with the stressed gear is arranged on the inner side of the lantern ring, an output rod, the extending direction of which is parallel to the length direction of the lantern ring, is arranged at one end of the lantern ring, and an air cylinder is arranged at the suspension end of the output rod and connected with the vertical;
the space shuttle model mechanism comprises a connecting belt which is arranged in a track groove in a matching way, a second driven wheel is arranged at the top end of the track groove, a second driving wheel is arranged at the bottom end of the connecting belt, the second driven wheel and the second driving wheel are belt pulleys, the connecting belt is sleeved on the second driven wheel and the second driving wheel, the length of the second driven wheel and the length of the second driving wheel are equal to half of the width of the connecting belt, the second driven wheel and the second driving wheel are close to the back surface of the vertical plate, a plurality of limiting component vertical plate back surfaces used for keeping the shape of the connecting belt are arranged on the connecting belt, a limiting component is arranged on the second driven wheel, the limiting component is close to the second driven wheel, the second driven wheel is movably connected with the vertical plate through the limiting component, the limiting component comprises a limiting plate and a limiting rod, the limiting rods are perpendicular to the limiting plates, the length of the limiting rods is equal to half of the width of the connecting belt, one of the two limiting rods supports or presses the connecting belt surface, the other limiting rod is connected with the vertical plate, a driving rod is coaxially arranged on one side, close to the back surface of the vertical plate, of the second driving wheel, a driving motor is arranged at the suspension end of the driving rod, the driving motor is connected with the vertical plate through a third fixing frame, a fixing rod axially perpendicular to the vertical plate is arranged on the inner side of the connecting belt, the fixing rod is close to the front surface of the vertical plate and is fixedly connected with the connecting belt, the length of the fixing rod is equal to half of the width of the connecting;
the red model mechanism of oriental is including wearing to locate the dwang on the vertical board, the one end that the dwang is located vertical board the place ahead is provided with the red model of oriental, the one end that the dwang is located the vertical board back is provided with the rotation motor, the rotation motor passes through the fourth mount and is connected with vertical board.
Preferably, the second driving wheel is five centimeters away from the bottom of the track groove.
Preferably, a music player is arranged in the oriental red model I, and plays the oriental red music.
Preferably, the remote controller is used for controlling the operation of the lifting motor, the air cylinder, the driving motor and the rotating motor, and the lifting motor, the driving motor and the rotating motor are all speed reducing motors.
3. Has the advantages that:
1. the utility model discloses elevator motor drives the output shaft and rotates, and the output shaft drives first action wheel, and first action wheel drives the belt motion, and the belt drives the show board motion, can realize the show board up-and-down motion through elevator motor's positive reverse rotation, can simulate national flag and go up and down, and the cylinder promotes the output pole along output pole axial back and forth movement, and the output pole drives the lantern ring back and forth movement, and the lantern ring passes through the rack and drives the positive and negative rotation of atress gear, and the atress gear drives the model of Tiangong through the connecting rod and rocks, realizes the dynamic.
2. The utility model discloses driving motor drives the actuating lever and rotates, and the actuating lever drives the second action wheel and rotates, and the second action wheel drives the connecting band motion, drives the space plane model motion through the dead lever when the connecting band motion, and can realize the back and forth movement of space plane model on the track groove, rotates the motor and drives the red model rotation in east through the dwang, realizes dynamic show, increases taste for presentation device is vivid.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic structural view of a national flag lifting mechanism of the present invention;
FIG. 3 is a schematic structural view of the Tiangong model I of the present invention;
FIG. 4 is a schematic structural view of the model mechanism of the utility model, Oriental Red I;
fig. 5 is a schematic structural diagram of the aerospace plane model mechanism of the present invention;
fig. 6 is a schematic structural diagram of the mechanism of the aerospace plane model of the present invention;
fig. 7 is a schematic structural diagram of the aerospace plane model mechanism of the present invention;
fig. 8 is a schematic structural diagram of the mechanism of the aerospace plane model of the present invention;
fig. 9 is a schematic structural view of the stop member of the present invention.
The reference numbers in the figures illustrate:
10. a horizontal plate; 110. a lunar vehicle model; 120. an astronaut model; 130. a lunar chamber model; 140. an energy station model; 150. an earth model; 20. a vertical plate; 210. a track groove; 30. a space plane model mechanism; 310. a connecting belt; 320. a second drive wheel; 330. a second driven wheel; 340. a stop member; 341. a limiting plate; 342. a limiting rod; 350. a space shuttle model; 360. a drive motor; 370. fixing the rod; 380. a drive rod; 40. eastern red model mechanism No. one; 410. model oriental red No. one; 420. rotating the rod; 430. rotating the motor; 50. a Tiangong model I mechanism; 510. a Tiangong model I; 520. a connecting rod; 530. a stressed gear; 540. a collar; 550. a rack; 560. an output rod; 570. a cylinder; 60. national flag lifting mechanism; 610. a support bar; 620. a fixed shaft; 630. a first driven wheel; 640. a belt; 650. a first drive wheel; 660. an output shaft; 670. a lifting motor; 680. a display board.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the mechanism or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.
As shown in fig. 1-9, an aerospace moon exploration science popularization demonstration device comprises: the horizontal plate 10 further includes: the lunar rover model comprises a horizontal plate 10, a vertical plate 20 and a remote controller, wherein the vertical plate 20 and the remote controller are vertically arranged at one end of the horizontal plate 10, a lunar ground pattern is arranged on the top surface of the horizontal plate 10, a space pattern is arranged on the front surface of the vertical plate 20, a lunar rover model 110, an astronaut model 120, a lunar chamber model 130, an energy station model 140 and an earth model 150 are further arranged on the top surface of the horizontal plate 10, the earth model 150 is an eighth hemisphere, the earth model 150 is located between the horizontal plate 10 and the vertical plate 20, an east red model mechanism 40, a Tiangong model mechanism 50 and a national flag lifting mechanism 60 are arranged on the vertical plate 20, a track groove 210 is formed in the vertical plate 20, one end of the track groove 210 extends to the earth model 150, a space rover model mechanism 30 is arranged on the track groove 210, and the remote controller is used for controlling the space rover model mechanism 30, the Tiangong model I mechanism 50 and the national flag lifting mechanism 60 move; orbital slot 210 is used to simulate the flight trajectory of a space shuttle, and extension of orbital slot 210 to earth model 150 is intended to launch the space shuttle from earth into space.
The national flag lifting mechanism 60 comprises a support rod 610 vertically arranged at the center of the top surface of the vertical plate 20, a fixing shaft 620 axially vertical to the vertical plate 20 is arranged on one side of the support rod 610 departing from the horizontal plate 10, a first driven wheel 630 is coaxially sleeved outside the fixing shaft 620, a first driving wheel 650 matched with the first driven wheel 630 is arranged on the back surface of the vertical plate 20, the first driving wheel 650 is positioned under the first driven wheel 630, an output shaft 660 extending towards the direction departing from the vertical plate 20 is coaxially arranged on the first driving wheel 650, a lifting motor 670 is arranged at the suspension end of the output shaft 660, the lifting motor 670 is connected with the vertical plate 20 through a first fixing frame, the first driven wheel 630 and the first driving wheel 650 are belt wheels, a belt 640 is arranged between the first driven wheel 630 and the first driving wheel 650, and the first driven wheel 630 and the first driving wheel 650 realize connection transmission through the belt, a display board 680 is arranged at the outer side of the belt 640, and national flag patterns are arranged on the front surface of the display board 680; the lifting motor 670 drives the output shaft 660 to rotate, the output shaft 660 drives the first driving wheel 650, the first driving wheel 650 drives the belt 640 to move, the belt 640 drives the display board 680 to move, the display board 680 can move up and down through the forward and reverse rotation of the lifting motor 670, and the national flag can be simulated to lift.
The Tiangong model mechanism 50 comprises a connecting rod 520 penetrating through the vertical plate 20, a Tiangong model 510 is arranged at one end of the connecting rod 520 in front of the vertical plate 20, a stressed gear 530 is coaxially sleeved at one end of the connecting rod 520 in back of the vertical plate 20, an oval lantern ring 540 is sleeved outside the stressed gear 530, a rack 550 meshed with the stressed gear 530 is arranged on the inner side of the lantern ring 540, an output rod 560 with the extending direction parallel to the length direction of the lantern ring 540 is arranged at one end of the lantern ring 540, an air cylinder 570 is arranged at the suspension end of the output rod 560, and the air cylinder 570 is connected with the vertical plate 20 through a second fixing frame; the cylinder 570 pushes the output rod 560 to move back and forth along the axial direction of the output rod 560, the output rod 560 drives the lantern ring 540 to move back and forth, the lantern ring 540 drives the stressed gear 530 to rotate forward and backward through the rack 550, and the stressed gear 530 drives the Tiangong model I510 to shake through the connecting rod 520, so that dynamic display is realized.
The aerospace plane model mechanism 30 comprises a connecting belt 310 arranged in the track groove 210 in a matching manner, a second driven wheel 330 is arranged at the top end of the track groove 210, a second driving wheel 320 is arranged at the bottom end of the connecting belt 310, the second driven wheel 330 and the second driving wheel 320 are both belt pulleys, the connecting belt 310 is sleeved on the second driven wheel 330 and the second driving wheel 320, the lengths of the second driven wheel 330 and the second driving wheel 320 are equal to half of the width of the connecting belt 310, the second driven wheel 330 and the second driving wheel 320 are close to the back of the vertical plate 20, a plurality of limiting members 340 for keeping the shape of the connecting belt 310 are arranged on the connecting belt 310, a limiting member 340 is arranged on the second driven wheel 330, the limiting member 340 is close to the second driven wheel 330, the second driven wheel 330 is movably connected with the vertical plate 20 through the limiting members 340, and the limiting members 340, The two limiting rods 342 are arranged on the limiting rod 342, the two limiting rods 342 are positioned on the same side of the limiting plate 341, the limiting rods 342 are vertical to the limiting plate 341, the length of the limiting rods 342 is equal to half of the width of the connecting band 310, one of the two limiting rods 342 is used for supporting or pressing the band surface of the connecting band 310, the other limiting rod 342 is connected with the vertical plate 20, a driving rod 380 is coaxially arranged at one side of the second driving wheel 320 close to the back surface of the vertical plate 20, a driving motor 360 is arranged at the suspension end of the driving rod 380, the driving motor 360 is connected with the vertical plate 20 through a third fixing frame, a fixing rod 370 axially perpendicular to the vertical plate 20 is arranged on the inner side of the connecting band 310, the fixing rod 370 is close to the front surface of the vertical plate 20, the fixing rod 370 is fixedly connected with the connecting band 310, the length of the fixing rod 370 is equal to half of the width of the connecting band 310, and a space shuttle model 350 is arranged at one end of the fixing rod 370 close to the front surface of the vertical plate 20; the driving motor 360 drives the driving rod 380 to rotate, the driving rod 380 drives the second driving wheel 320 to rotate, the second driving wheel 320 drives the connecting belt 310 to move, the connecting belt 310 drives the space shuttle model 350 to move through the fixing rod 370 while moving, and the space shuttle model 350 can move back and forth on the track groove 210.
The oriental red model mechanism 40 comprises a rotating rod 420 penetrating through the vertical plate 20, the oriental red model 410 is arranged at one end of the rotating rod 420 in front of the vertical plate 20, a rotating motor 430 is arranged at one end of the rotating rod 420 in back of the vertical plate 20, and the rotating motor 430 is connected with the vertical plate 20 through a fourth fixing frame; the rotation motor 430 rotates the oriental red model No. one 410 by rotating the rotation lever 420.
To avoid the influence of the earth model 150 on the change of the space shuttle model 350, the second driving wheel 320 is spaced five centimeters from the bottom of the track groove 210.
More perfectly, a music player is arranged in the oriental red first model 410, and plays the oriental red music; the music played by the music player is the music sent back by the east red satellite I, and brings the first step of recalling the development of the Chinese space cause into the time sense.
More perfect, the remote controller is used for controlling the operation of the lifting motor 670, the cylinder 570, the driving motor 360 and the rotating motor 430, and the lifting motor 670, the driving motor 360 and the rotating motor 430 are all speed reducing motors.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (4)
1. An aerospace moon exploration science popularization demonstration device, comprising: horizontal plate (10), characterized by, still include: the moon-shaped ground model building block is characterized by comprising a vertical plate (20) and a remote controller, wherein the vertical plate (20) and the remote controller are arranged at one end of a horizontal plate (10) and are vertically arranged, a moon ground pattern is arranged on the top surface of the horizontal plate (10), a space pattern is arranged on the front surface of the vertical plate (20), a moon rover model (110), an astronaut model (120), a moon-boarding cabin model (130), an energy station model (140) and an earth model (150) are further arranged on the top surface of the horizontal plate (10), the earth model (150) is an eighth hemisphere, the earth model (150) is positioned between the horizontal plate (10) and the vertical plate (20), an oriental red model mechanism (40), a Tiangong model mechanism (50) and a national flag lifting mechanism (60) are arranged on the vertical plate (20), a track groove (210) is formed in the vertical plate (20), one end of the track groove (210) extends to the, the rail groove (210) is provided with an aerospace plane model mechanism (30), and the remote controller is used for controlling the aerospace plane model mechanism (30), the east red model mechanism (40), the Tiangong model mechanism (50) and the national flag lifting mechanism (60) to move;
the national flag lifting mechanism (60) comprises a supporting rod (610) vertically arranged at the center of the top surface of a vertical plate (20), a fixing shaft (620) axially vertical to the vertical plate (20) is arranged on one side of the supporting rod (610) departing from a horizontal plate (10), a first driven wheel (630) is coaxially sleeved outside the fixing shaft (620), a first driving wheel (650) matched with the first driven wheel (630) is arranged on the back surface of the vertical plate (20), the first driving wheel (650) is positioned under the first driven wheel (630), an output shaft (660) extending towards the direction departing from the vertical plate (20) is coaxially arranged on the first driving wheel (650), a lifting motor (670) is arranged at the suspension end of the output shaft (660), the lifting motor (670) is connected with the vertical plate (20) through a first fixing frame, the first driven wheel (630) and the first driving wheel (650) are belt wheels, and a belt (640) is arranged between the first driven wheel (630) and the first driving wheel (650), the first driven wheel (630) and the first driving wheel (650) are connected and driven through a belt (640), a display board (680) is arranged on the outer side of the belt (640), and national flag patterns are arranged on the front face of the display board (680);
the Tiangong model mechanism (50) comprises a connecting rod (520) penetrating through a vertical plate (20), a Tiangong model (510) is arranged at one end, located in front of the vertical plate (20), of the connecting rod (520), a stressed gear (530) is coaxially sleeved at one end, located behind the vertical plate (20), of the connecting rod (520), an oval lantern ring (540) is sleeved outside the stressed gear (530), a rack (550) meshed with the stressed gear (530) is arranged on the inner side of the lantern ring (540), an output rod (560) with the extending direction parallel to the length direction of the lantern ring (540) is arranged at one end of the lantern ring (540), an air cylinder (570) is arranged at the suspension end of the output rod (560), and the air cylinder (570) is connected with the vertical plate (20) through a second fixing frame;
the aerospace plane model mechanism (30) comprises a connecting belt (310) which is arranged in a track groove (210) in a matching manner, a second driven wheel (330) is arranged at the top end of the track groove (210), a second driving wheel (320) is arranged at the bottom end of the connecting belt (310), the second driven wheel (330) and the second driving wheel (320) are both belt pulleys, the connecting belt (310) is sleeved on the second driven wheel (330) and the second driving wheel (320), the lengths of the second driven wheel (330) and the second driving wheel (320) are equal to half of the width of the connecting belt (310), the second driven wheel (330) and the second driving wheel (320) are close to the back face of a vertical plate (20), the connecting belt (310) is provided with a plurality of limiting members (340) for keeping the shape of the connecting belt (310), the back face of the vertical plate (20) is provided with the limiting members (340), the limiting component (340) is close to, the second driven wheel (330) is movably connected with the vertical plate (20) through the limiting component (340), the limiting component (340) comprises a limiting plate (341) and a limiting rod (342), the limiting rod (342) is provided with two limiting rods (342) which are positioned at the same side of the limiting plate (341), the limiting rod (342) is perpendicular to the limiting plate (341) and the length of the limiting rod (342) is equal to half of the width of the connecting belt (310), one of the two limiting rods (342) supports or presses the belt surface of the connecting belt (310), the other limiting rod (342) is connected with the vertical plate (20), one side of the second driving wheel (320) close to the back of the vertical plate (20) is coaxially provided with a driving rod (380), the suspension end of the driving rod (380) is provided with a driving motor (360), the driving motor (360) is connected with the vertical plate (20) through a third fixing frame, a fixing rod (370) which is axially vertical to the vertical plate (20) is arranged on the inner side of the connecting band (310), the fixing rod (370) is close to the front face of the vertical plate (20), the fixing rod (370) is fixedly connected with the connecting band (310), the length of the fixing rod (370) is equal to half of the width of the connecting band (310), and a space shuttle model (350) is arranged at one end, close to the front face of the vertical plate (20), of the fixing rod (370);
the red model mechanism of east (40) including wear to locate dwang (420) on vertical board (20), the one end that dwang (420) is located vertical board (20) the place ahead is provided with red model of east (410), the one end that dwang (420) is located vertical board (20) the back is provided with rotation motor (430), rotation motor (430) are connected with vertical board (20) through the fourth mount.
2. An aerospace moon-exploring science popularization demonstration apparatus according to claim 1, wherein: the distance between the second driving wheel (320) and the bottom of the track groove (210) is five centimeters.
3. An aerospace moon-exploring science popularization demonstration apparatus according to claim 1, wherein: the oriental red first model (410) is internally provided with a music player, and the music player plays oriental red music.
4. An aerospace moon-exploring science popularization demonstration apparatus according to claim 1, wherein: the remote controller is used for controlling the operation of the lifting motor (670), the air cylinder (570), the driving motor (360) and the rotating motor (430), and the lifting motor (670), the driving motor (360) and the rotating motor (430) are all speed reducing motors.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922156002.0U CN210804966U (en) | 2019-12-05 | 2019-12-05 | Aerospace moon exploration science popularization demonstration device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201922156002.0U CN210804966U (en) | 2019-12-05 | 2019-12-05 | Aerospace moon exploration science popularization demonstration device |
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| CN210804966U true CN210804966U (en) | 2020-06-19 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114247158A (en) * | 2021-12-22 | 2022-03-29 | 山西中天世纪科技股份有限公司 | Airplane model |
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2019
- 2019-12-05 CN CN201922156002.0U patent/CN210804966U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114247158A (en) * | 2021-12-22 | 2022-03-29 | 山西中天世纪科技股份有限公司 | Airplane model |
| CN114247158B (en) * | 2021-12-22 | 2024-05-28 | 山西中天世纪科技股份有限公司 | Aircraft model |
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