Electronic building block for simulating satellite environment exploration
By designing the electronic building block system that simulates the satellite environment, it is difficult to comprehensively simulate the existing satellite display methods that simulate the effective load data and attitude of satellite, realize a more vivid satellite education experience, and improve students' learning interest and ability.
Patent Information
- Application Number
- CN202420855405.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-24
- Publication Date
- 2025-01-28
- Estimated Expiration
- 2034-04-24
AI Technical Summary
The existing satellite display methods mainly rely on physical or composite material models. Although they can simulate displays, it is difficult for students to understand the various data of satellite payloads and satellite attitudes, which limits the effectiveness of educational promotion.
Design an electronic building block system that simulates the satellite environment, including substrates, solid bars, data display load boards, thermal control sub -system boards, experimental load boards, music infrared remote control boards, battery boards, and solar panels. The use of sensors, simulation satellites monitor and move in space.
Through the electronic building block system, students can more intuitively understand the monitoring of satellites and changes in movement, improve their learning interests and master satellite knowledge, and at the same time exercise hands -on ability, space imagination and thinking ability.
Smart Images
Figure CN222421162U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of electronic building blocks, and in particular to an electronic building block for simulating satellite environment exploration. Background Art
[0002] Electronic building blocks are modular components that can be connected and assembled to form different model products, and adjacent electronic building blocks can be electrically connected. In this way, electronic building blocks can be connected and assembled according to the set circuit route to complete various model products with different series and parallel circuits. Satellites are a major aerospace project in my country, involving complex scientific and technological knowledge. In order to popularize satellite-related knowledge to young people, satellite models are usually displayed to young people. The existing satellite display method is to display the model in real objects or composite materials in proportion. The existing display model has also been well received and loved by everyone, allowing the audience to get close to the satellite that is so far away from them and feel magical. Its external shape can be clearly seen and touched.
[0003] Existing satellites are all displayed through real objects or scaled models made of composite materials. Although they can be simulated, students have limited knowledge about satellites and are unable to simulate various data of satellite payloads, satellite attitudes, etc., which is not conducive to their promotion and use. Utility Model Content
[0004] The present application provides an electronic building block for simulating satellite environment exploration to solve the technical problem that the inventors realized that existing satellites are all displayed through real objects or scaled models of composite materials. Although they can be simulated, students have limited knowledge of satellites and cannot simulate various data of satellite payloads, satellite attitudes, etc., which is not conducive to popularization and use.
[0005] The present application provides an electronic building block for simulating satellite environment exploration, comprising a substrate, a reinforcement strip and a data display load board, wherein the front side of the substrate is detachably connected to the back side of the reinforcement strip, the back side of the data display load board is detachably connected to the front side of the reinforcement strip, the number of the reinforcement strips is six, and the electronic building block further comprises a thermal control subsystem board, an experimental load board, a music infrared remote control load board, a battery panel and a solar panel, the number of the solar panels is two, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the battery panel and the two solar panels are all detachably connected to the surface of the reinforcement strip, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the battery panel, the two solar panels, the substrate, the reinforcement strip and the data display load board limit a cavity, the front side of the substrate and located inside the cavity is detachably connected to a management subsystem board, the front side of the management subsystem board is detachably connected to a functional integrated board, the two solar panels on the front side of the substrate are symmetrically arranged about the horizontal line of the substrate, and a sailboard unit is arranged on the solar panel.
[0006] In any of the above technical solutions, further, the sailboard unit includes a servo, which is detachably connected to the surface of the solar panel and is located in the cavity, and the output shaft of the servo passes through the solar panel and extends to the outside of the cavity and is connected to a first gear, the surface of the solar panel is detachably connected to a fixing disk, the surface of the fixing disk is provided with a fixing column, the surface of the fixing column is sleeved with a second gear, the surface of the first gear and the surface of the second gear are meshed, the surface of the second gear is provided with a ring plate, the surface of the ring plate is detachably connected to a mounting plate, the surface of the mounting plate is detachably connected to a sailboard, and the surface of the fixing column is detachably connected to a clamping plate.
[0007] In any of the above technical solutions, further, a smart touch screen is provided on the front side of the data display load plate.
[0008] In any of the above technical solutions, further, a light sensor and a temperature sensor are provided on the surface of the thermal control subsystem board.
[0009] In any of the above technical solutions, further, a temperature and humidity sensor and an air pressure sensor are provided on the surface of the experimental load plate.
[0010] In any of the above technical solutions, further, a music player and an infrared remote control sensor are provided on the surface of the music infrared remote control loading board.
[0011] In any of the above technical solutions, further, a battery slot is provided on the surface of the battery panel and inside the cavity.
[0012] In any of the above technical solutions, further, it also includes connecting wires, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the data display load board, the battery panel and the servo are all connected to the front side of the functional integrated board through the connecting wires.
[0013] In any of the above technical solutions, further, the front side of the management subsystem board is provided with pins, and the back side of the function integration board is provided with an interface, and the pins can be inserted into the interface.
[0014] In any of the above technical solutions, further, the base plate, the data display load board, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the battery panel and the two solar panels are all detachably connected to the reinforcement strips by bolts, and the servo, the solar panel, the sailboard, the mounting plate and the ring plate are detachably connected by bolts.
[0015] The beneficial effects of this application are mainly:
[0016] When the electronic building blocks are installed, the monitoring situation of the satellite in space can be simulated through the temperature and humidity sensors, air pressure sensors, music players and infrared remote control sensors. The servo can also be started, and the continuous engagement of the first gear and the second gear allows the angle of the sailboard to change. In this process, the movement changes of the satellite in space can be simulated, which effectively improves students' interest in learning and thus improves students' learning about satellites. In the process of assembling electronic building blocks, students' hands-on ability, spatial imagination and thinking ability can be effectively trained.
[0017] It should be understood that both the foregoing general description and the following specific embodiments are for the purpose of example and illustration and do not necessarily limit the present application. The accompanying drawings, which are incorporated into and constitute a part of the specification, illustrate the subject matter of the present application. At the same time, the specification and the drawings are used to explain the principles of the present application. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] In order to more clearly illustrate the specific implementation methods of the present application or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.
[0019] Figure 1 This is a schematic diagram of the electronic building block structure of an embodiment of the present application;
[0020] Figure 2 This is a schematic diagram of the electronic building block structure of an embodiment of the present application (front view);
[0021] Figure 3 This is a schematic diagram of the solar panel and sailboard unit structure in an embodiment of the present application (side view);
[0022] Figure 4 This is a schematic diagram (side view) of the structure of the management subsystem board, the function integration board and the base board in the embodiment of the present application;
[0023] Figure 5 This is a schematic structural diagram (front view) of the substrate, functional integrated board, reinforcement strip, thermal control subsystem board, experimental load board, music infrared remote control load board, battery panel, solar panel and functional integrated board in the embodiment of the present application.
[0024] icon:
[0025] 100-base plate; 101-reinforcement strip; 102-data display load board; 103-thermal control subsystem board; 104-experimental load board; 105-music infrared remote control load board; 106-solar panel; 107-solar panel; 108-management subsystem board; 109-function integration board; 110-servo; 111-first gear; 112-fixed plate; 113-second gear; 114-ring plate; 115-mounting plate; 116-sailboard; 117-card board; 118-smart touch screen; 119-pin; 120-interface; 121-socket; 122-battery slot. DETAILED DESCRIPTION
[0026] The technical solution of the present application will be clearly and completely described below in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all of the embodiments.
[0027] Based on the embodiments in this application, all other embodiments obtained by ordinary technicians in this field without making any creative work shall fall within the scope of protection of this application.
[0028] In the description of the present application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present application. In addition, the terms "first", "second", and "third" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.
[0029] In the description of this application, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in this application can be understood according to specific circumstances.
[0030] See also Figure 1 , Figure 2 , Figure 3 and Figure 5In one or more embodiments, an electronic building block for simulating satellite environment exploration is provided, including a base plate 100, a reinforcement strip 101, and a data display load plate 102. The front side of the base plate 100 is detachably connected to the back side of the reinforcement strip 101. The back side of the data display load plate 102 is detachably connected to the front side of the reinforcement strip 101. The number of the reinforcement strips 101 is six. The electronic building block also includes a thermal control subsystem board 103, an experimental load plate 104, a music infrared remote control load plate 105, a battery panel 106, and a solar panel 107. The number of the solar panels 107 is two. The control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the battery panel 106 and the two solar panels 107 are all detachably connected to the surface of the reinforcement strip 101, and the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the battery panel 106, the two solar panels 107, the substrate 100, the reinforcement strip 101 and the data display load board 102 limit a cavity, and the front side of the substrate 100 and the inside of the cavity are detachably connected with the management subsystem board 108 The front of the management subsystem board 108 is detachably connected with a function integrated board 109. The two solar panels 107 on the front of the substrate 100 are symmetrically arranged with respect to the horizontal line of the substrate 100. The solar panels 107 are provided with sailboards 116. The front of the data display load board 102 is provided with a smart touch screen 118. The surface of the thermal control subsystem board 103 is provided with a light sensor and a temperature sensor. The surface of the experimental load board 104 is provided with a temperature and humidity sensor and an air pressure sensor. The surface of the music infrared remote control load board 105 is provided with a music player and an infrared remote control. A control sensor is provided on the surface of the battery panel 106 and inside the cavity. A battery slot 122 is provided, and also includes connecting wires. The thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the data display load board 102, the battery panel 106 and the servo 110 are all connected to the front of the function integration board 109 through the connecting wires. The front of the management subsystem board 108 is provided with a pin 119, and the back of the function integration board 109 is provided with an interface 120, and the pin 119 can be inserted into the interface 120.
[0031] In this embodiment, the management subsystem board 108 is taken out in advance and connected to the base plate 100, and then the pin 119 of the management subsystem board 108 is inserted into the interface 120 of the function integration board 109, and the connection is achieved by means of bolts and other structures, and the reinforcement strip 101 is connected to the base plate 100, and then the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the battery board 106 and the data display load board 102 are connected to the reinforcement strip 101 in sequence, and then the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105 are connected to the reinforcement strip 101 in sequence, and then the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105 are connected to the reinforcement strip 101 by means of connecting wires. , the data shows the connection between the load board 102, the battery panel 106 and the function integrated board 109, and after the sailboard 116 unit is installed on the solar panel 107, the servo 110 and the function integrated board 109 are connected in advance through the connecting line, and then the solar panel 107 and the reinforcement strip 101 are connected to complete the installation of the electronic building blocks. The monitoring situation of the satellite in space can be simulated through the temperature and humidity sensor, the air pressure sensor, the music player and the infrared remote control sensor to help students learn and master satellite knowledge, and to improve students' interest in learning. In the process of assembling, it can also effectively exercise students' hands-on ability, spatial imagination ability and thinking ability.
[0032] In this embodiment, the management subsystem board 108 is model HI3861RNLV100, and the onboard functions include onboard power supply voltage detection function, 6-ring colored light module, nine-axis attitude sensor, 16-channel PWM output, and the function integration board 109 includes an analog-to-digital conversion module, model SGM58031_0X49, and also includes an I2C16-bit ADC acquisition module; the thermal control subsystem board 103 has an analog-to-digital conversion module and an I2C16-bit ADC acquisition module for 4-channel light sensor (PT550) acquisition, the analog-to-digital conversion module model of the thermal control subsystem board 103 is SGM58031_0X48, and the thermal control subsystem board 103 also has a temperature sensor for satellite internal temperature acquisition, model LM75_0X4F The experimental payload board 104 is provided with a temperature and humidity sensor for collecting the external temperature and humidity of the satellite and a pressure sensor for collecting the external air pressure sensor of the satellite. The model of the temperature and humidity sensor is AHT21_0X38, and the model of the air pressure sensor is HP203N_0X76. The music infrared remote control payload board 105 is provided with a music player and an infrared remote control sensor. The music player is based on YX6100 and integrates MP3, WAV The hardware decoding of the device is built-in with 16M Flash memory. Files can be updated in the form of a virtual U disk through the USB interface 120. The specified voice can be played through simple serial port commands, and functions such as how to play voice can be completed. There is no need for cumbersome underlying operations and it is easy to use. The infrared remote control sensor adopts IRM-3638T, a 38khz standard infrared receiver, which is used to modulate and decode all infrared transmission signals and is processed by the microcontroller; the battery slot 122 of the battery board 106 supports the placement of +3.7 / 4.2V, 14500 lithium batteries, and the onboard function of the battery board 106 is used to power the core motherboard. The onboard power management chip can support charging, discharging, overcharge and over discharge, and short circuit protection. The data display load board 102 includes There is a T1-2.4-inch smart touch screen 118 with a resolution of 320*240, a resistive touch type, a built-in Flash storage of 4M, a running memory of 3584 bytes, and a serial port instruction buffer area of 1K bytes; wherein the data display load board 102 is connected to the P5 socket 121 of the function integration board 109 through a connecting line, the music infrared remote control load board 105 is connected to the P6 socket 121 of the function integration board 109 through a connecting line, the experimental load board 104 is connected to the IIC socket 121 of the function integration board 109 through a connecting line, the thermal control subsystem board 103 is connected to the IIC socket 121 of the function integration board 109 through a connecting line, and the two servos 110 are respectively connected to the S0 and S1 sockets 121 of the function integration board 109 through connecting lines.
[0033] See also Figure 1 , Figure 2 and Figure 3In some embodiments, the sailboard 116 unit includes a servo 110, which is detachably connected to the surface of the solar panel 107 and is located in the cavity. The output shaft of the servo 110 passes through the solar panel 107 and extends to the outside of the cavity and is connected to a first gear 111. A fixing disk 112 is detachably connected to the surface of the solar panel 107. A fixing column is provided on the surface of the fixing disk 112. A second gear 113 is sleeved on the surface of the fixing column. The surface of the first gear 111 is meshed with the surface of the second gear 113. A ring plate 114 is provided on the surface of the second gear 113. A mounting plate 115 is detachably connected to the surface of the ring plate 114. A sailboard 116 is detachably connected to the surface of the mounting plate 115. A clamping plate 117 is detachably connected to the surface of the fixing column.
[0034] In this embodiment, the servo 110 is connected to the solar panel 107 by means of bolts and other structures, and then the fixing plate 112 is installed on the surface of the solar panel 107, wherein the fixing plate 112 and the fixing column preferably adopt an integrally formed structure, and the second gear 113 and the ring plate 114 preferably adopt an integrally formed structure, the second gear 113 and the ring plate 114 are sleeved on the surface of the fixing column, and then the mounting plate 115 is taken out and connected to the ring plate 114, and finally the sailboard 116 is connected to the mounting plate 115, so as to complete the assembly of the sailboard 116 unit. In the actual teaching process, the servo 110 can be started, and the mounting plate 115 is ordered to rotate under the continuous engagement of the first gear 111 and the second gear 113, thereby driving the rotation of the sailboard 116 to simulate the movement changes of the satellite in space, which is helpful for students to understand and master satellite-related knowledge.
[0035] See also Figure 1 , Figure 2 , Figure 3 , Figure 4 and Figure 5 In some embodiments, the base plate 100, the data display load plate 102, the thermal control subsystem plate 103, the experimental load plate 104, the music infrared remote control load plate 105, the battery panel 106 and the two solar panels 107 are all detachably connected to the reinforcement strip 101 by bolts, and the servo 110, the solar panel 107, the sailboard 116, the mounting plate 115 and the ring plate 114 are detachably connected by bolts.
[0036] In this embodiment, the detachable connection in this application can be achieved by a bolt structure, but the detachable structure mentioned in this application includes but is not limited to a bolt structure, and can be replaced by other detachable structures that belong to the protected objects in this application.
[0037] Specifically, the working principle of an electronic building block for simulating satellite environment exploration provided by the present application is:
[0038] The management subsystem board 108 is taken out in advance and connected to the base plate 100, and then the pin 119 of the management subsystem board 108 is inserted into the interface 120 of the function integrated board 109, and the connection is achieved by means of bolts and other structures, and the reinforcement strip 101 is connected to the base plate 100, and then the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the battery board 106 and the data display load board 102 are connected to the reinforcement strip 101 in sequence, and then the thermal control subsystem board 103, the experimental load board 104, the music infrared remote control load board 105, the data display load board 102, the battery board 106 and the function integrated board 109 are connected by connecting wires;
[0039] The servo 110 is connected to the solar panel 107 by means of bolts and other structures, and then the fixing plate 112 is installed on the surface of the solar panel 107, wherein the fixing plate 112 and the fixing column preferably adopt an integrated structure, and the second gear 113 and the ring plate 114 preferably adopt an integrated structure, and the second gear 113 and the ring plate 114 are sleeved on the surface of the fixing column, and then the mounting plate 115 is taken out and connected to the ring plate 114, and finally the sailboard 116 is connected to the mounting plate 115, so as to complete the assembly of the sailboard 116 unit;
[0040] The servo 110 and the function integrated board 109 are connected in advance through connecting lines, and then the solar panel 107 and the reinforcement strip 101 are connected to complete the installation of the electronic building blocks. The monitoring situation of the satellite in space can be simulated through the temperature and humidity sensor, the air pressure sensor, the music player and the infrared remote control sensor to help students learn and master satellite knowledge, and to improve students' interest in learning. In the process of assembling, students' hands-on ability, spatial imagination ability and thinking ability can also be effectively exercised.
[0041] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, rather than to limit it. Although the present application has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the scope of the technical solutions of the embodiments of the present application.
Claims
1. An electronic building block for simulating satellite environment exploration, characterized in that: It includes a substrate, a reinforcement strip and a data display load plate, the front side of the substrate is detachably connected to the back side of the reinforcement strip, the back side of the data display load plate is detachably connected to the front side of the reinforcement strip, the number of the reinforcement strips is six, and it also includes a thermal control subsystem board, an experimental load plate, a music infrared remote control load plate, a battery panel and a solar panel, the number of the solar panels is two, the thermal control subsystem board, the experimental load plate, the music infrared remote control load plate, the battery panel and the two solar panels are all detachably connected to the surface of the reinforcement strip, the thermal control subsystem board, the experimental load plate, the music infrared remote control load plate, the battery panel, the two solar panels, the substrate, the reinforcement strip and the data display load plate limit a cavity, the front side of the substrate and the interior of the cavity is detachably connected to a management subsystem board, the front side of the management subsystem board is detachably connected to a functional integrated board, the two solar panels on the front side of the substrate are symmetrically arranged about the horizontal line of the substrate, and a sailboard unit is arranged on the solar panel.
2. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: The sailboard unit includes a servo, which is detachably connected to the surface of the solar panel and is located in the cavity. The output shaft of the servo passes through the solar panel and extends to the outside of the cavity and is connected to a first gear. The surface of the solar panel is detachably connected to a fixing disk, a fixing column is provided on the surface of the fixing disk, a second gear is sleeved on the surface of the fixing column, the surface of the first gear is meshed with the surface of the second gear, a ring plate is provided on the surface of the second gear, a mounting plate is detachably connected to the surface of the ring plate, a sailboard is detachably connected to the surface of the mounting plate, and a clamping plate is detachably connected to the surface of the fixing column.
3. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: The front side of the data display load plate is provided with an intelligent touch screen.
4. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: A light sensor and a temperature sensor are arranged on the surface of the thermal control subsystem board.
5. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: The surface of the experimental load plate is provided with a temperature and humidity sensor and an air pressure sensor.
6. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: A music player and an infrared remote control sensor are arranged on the surface of the music infrared remote control loading board.
7. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: A battery slot is arranged on the surface of the battery plate and inside the cavity.
8. The electronic building block for simulating satellite environment exploration according to claim 2, characterized in that: It also includes connecting wires, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the data display load board, the battery board and the servo are all connected to the front side of the functional integration board through the connecting wires.
9. The electronic building block for simulating satellite environment exploration according to claim 1, characterized in that: The front side of the management subsystem board is provided with pins, and the back side of the function integration board is provided with interfaces, into which the pins can be inserted.
10. The electronic building block for simulating satellite environment exploration according to claim 2, characterized in that: The base plate, the data display load board, the thermal control subsystem board, the experimental load board, the music infrared remote control load board, the battery panel and the two solar panels are all detachably connected to the reinforcement strips by bolts, and the servo, the solar panel, the sailboard, the mounting plate and the ring plate are detachably connected by bolts.