Space station model

Abstract

The utility model discloses a space station model, relates to model toy field, including model main part, fixed structure and astronaut model, model main part is placed in the top of fixed structure, astronaut model magnetic attraction fixed in the model main part top side, fixed structure includes fixed base, support rod, T-shaped bracket and fixed bolt, the top end of the fixed base is provided with an inserting groove, the bottom end of the supporting rod is inserted into the inserting groove to achieve fixation with the fixed base, the T-shaped bracket is placed at the top end of the supporting rod, and the supporting rod and the T-shaped bracket are fixedly connected through the fixing bolt. The space station model is simple in structure and high in overall reduction degree and model precision, the blank that no space station model exists in the market is filled up, the model body can be well supported and protected through the fixing structure in a three-point lifting and fixing mode during display, and the possibility that the model gets loose and falls off is reduced.

Description

Technical Field

[0001] This utility model relates to the field of model toys, specifically a space station model. Background Technology

[0002] The Chinese Space Station, also known as Tiangong Space Station, is a manned space station designed, built, and operated independently by China. It marks China's entry into the space station era and aims to support long-term personnel stays and conduct scientific and technological experiments. The Chinese Space Station consists of a core module and two experimental modules, operating in a low Earth orbit approximately 400 kilometers above the Earth. It is designed for an on-orbit lifespan of more than 10 years and serves as a crucial platform for scientific research and international cooperation in the space domain for China.

[0003] Currently, although the Chinese space station, as a major national scientific research project, has attracted widespread attention in the scientific community and among the public, detailed models of the Chinese space station are relatively scarce on the market. However, as the public's enthusiasm for China's space program continues to grow, the demand for models that can intuitively showcase the majestic appearance of the Chinese space station is becoming increasingly urgent. There is an urgent need for a high-quality model of the Chinese space station that can not only satisfy the public's curiosity and desire for exploration, but also serve as an important symbol of the achievements of China's space program, inspiring more young people to develop an interest and love for space science. Utility Model Content

[0004] The purpose of this invention is to provide a space station model to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a space station model, comprising a model body, a fixing structure, and an astronaut model. The model body is placed on top of the fixing structure, and the astronaut model is magnetically fixed to one side of the top of the model body. The fixing structure includes a fixing base, a support rod, a T-shaped bracket, and fixing bolts. The top of the fixing base has a slot, and the bottom end of the support rod is inserted into the slot to fix it to the fixing base. The T-shaped bracket is placed on top of the support rod, and the fixing bolts achieve a fixed connection between the support rod and the T-shaped bracket.

[0006] Preferably, the main body of the model includes a Tianzhou cargo spacecraft model, a Tianzhou spacecraft solar panel model, a Tianhe core module model, a Tianhe core module solar panel model, a Mengtian experimental module solar panel model, a Mengtian experimental module model, a Shenzhou spacecraft solar panel model, a Shenzhou manned spacecraft model, a robotic arm model, a Wentian experimental module model, and a Wentian experimental module solar panel model. The Wentian experimental module model and the Mengtian experimental module model are fixed together as a whole. The Shenzhou manned spacecraft model has two sets, which are magnetically fixed to the front end and bottom of the Wentian experimental module model and the Mengtian experimental module model, respectively. The Tianhe core module model is magnetically fixed to the Wentian experimental module model and the Mengtian experimental module model. At the rear end, the Tianzhou cargo spacecraft model is magnetically fixed to the rear end of the Tianhe core module model. The Tianzhou spacecraft solar panel model has two sets and is rotatably mounted on both sides of the Tianzhou cargo spacecraft model. The Tianhe core module solar panel model has two sets and is rotatably mounted on both sides of the Tianhe core module model. The Mengtian experimental module solar panel model has two sets and is rotatably mounted on the outside of the Mengtian experimental module model. The Wentian experimental module solar panel model has two sets and is rotatably mounted on the outside of the Wentian experimental module model. The Shenzhou spacecraft solar panel model has two sets and is rotatably mounted on the front end of the Shenzhou manned spacecraft model. The robotic arm model is rotatably connected to the top of the Tianhe core module model.

[0007] Preferably, the top of the T-shaped bracket is provided with three sets of annular brackets, which respectively support the bottom of the Tianhe core module model, the Mengtian experimental module model and the Wentian experimental module model, so as to place the main body of the model on the fixed structure surface.

[0008] Preferably, the bottom of the fixed base is a magnetic suction plate to achieve magnetic fixation between the astronaut model and the fixed structure.

[0009] Compared with the prior art, the beneficial effects of this utility model are:

[0010] This utility model proposes a space station model that is easy to assemble, has a high degree of overall accuracy and precision, fills the gap in the market for space station models, and utilizes a three-point support and fixing method to effectively support and protect the main body of the model during display, reducing the possibility of the model falling off. Attached Figure Description

[0011] The present invention will be further described below with reference to the accompanying drawings:

[0012] Figure 1 This is a schematic diagram of the space station model of this utility model. Figure 1 ;

[0013] Figure 2This is a schematic diagram of the space station model of this utility model. Figure 2 ;

[0014] Figure 3 This is a schematic diagram of the fixed structure of the space station model of this utility model.

[0015] As shown in the figure: 1. Main model; 11. Tianzhou cargo spacecraft model; 12. Tianzhou spacecraft solar panel model; 13. Tianhe core module model; 14. Tianhe core module solar panel model; 15. Mengtian experimental module solar panel model; 16. Mengtian experimental module model; 17. Shenzhou spacecraft solar panel model; 18. Shenzhou manned spacecraft model; 19. Mechanical arm model; 110. Wentian experimental module model; 111. Wentian experimental module solar panel model; 2. Fixed structure; 21. Fixed base; 22. Support rod; 23. T-shaped bracket; 24. Fixing bolts; 3. Astronaut model. Detailed Implementation

[0016] To more clearly illustrate the overall concept of this utility model, a detailed description will be provided below with reference to the accompanying drawings.

[0017] It should be noted that many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Therefore, the scope of protection of the present invention is not limited to the specific embodiments disclosed below.

[0018] Furthermore, it should be understood in the description of this utility model that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "axial," "radial," and "circumferential" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0019] In this utility model, unless otherwise explicitly specified and limited, the terms "installation," "connection," "joining," and "fixing" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral unit; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components. However, specifying a direct connection indicates that the two entities connected are not linked by an intermediate structure but are connected as a whole through a transmission structure. For those skilled in the art, the specific meaning of the above terms in this utility model can be understood according to the specific circumstances.

[0020] In this utility model, unless otherwise expressly specified and limited, the first feature "on" or "below" the second feature may be in direct contact with the first and second features, or indirect contact through an intermediate medium. In the description of this specification, references to terms such as "one embodiment," "some embodiments," "example," "specific example," or "some examples," etc., indicate that a specific feature, structure, material, or characteristic described in connection with that embodiment or example is included in at least one embodiment or example of this utility model. In this specification, the illustrative expressions of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in one or more embodiments or examples.

[0021] Please see Figures 1 to 3 This utility model provides a technical solution: a space station model, including a model body 1, a fixing structure 2, and an astronaut model 3. The model body 1 is placed on the top of the fixing structure 2, and the astronaut model 3 is magnetically fixed to one side of the top of the model body 1. The fixing structure 2 includes a fixing base 21, a support rod 22, a T-shaped bracket 23, and fixing bolts 24. The top of the fixing base 21 has a slot, and the bottom end of the support rod 22 is inserted into the slot to fix it to the fixing base 21. The T-shaped bracket 23 is placed on the top of the support rod 22, and the support rod 22 and the T-shaped bracket 23 are fixedly connected by fixing bolts 24.

[0022] This space station model is easy to assemble, has a high degree of overall accuracy and high precision, filling the gap in the market for space station models. When displayed, the fixed structure 2 uses a three-point support and fixation method to effectively support and protect the main body of the model 1, reducing the possibility of the model falling off.

[0023] When assembling the fixing structure 2, the threads pre-assembled on the bottom of the support rod 22 can be unscrewed, and then the support rod 22 can be inserted into the groove at the top of the fixing base 21. Then, the bolts can be passed through the bottom of the fixing base 21 and tightened to the support rod 22 to complete the assembly of the fixing base 21 and the support rod 22. Align the threaded hole of the T-shaped bracket 23 with the threaded hole at the top of the support rod 22, and screw in the fixing bolts 24 to complete the assembly of the fixing structure 2.

[0024] The main body of the model 1 includes the Tianzhou cargo spacecraft model 11, the Tianzhou spacecraft solar panel model 12, the Tianhe core module model 13, the Tianhe core module solar panel model 14, the Mengtian experimental module solar panel model 15, the Mengtian experimental module model 16, the Shenzhou spacecraft solar panel model 17, the Shenzhou manned spacecraft model 18, the robotic arm model 19, the Wentian experimental module model 110, and the Wentian experimental module solar panel model 111. The Wentian experimental module model 110 and the Mengtian experimental module model 16 are fixed together as a whole. The Shenzhou manned spacecraft model 18 has two sets, which are magnetically fixed to the front and bottom of the Wentian experimental module model 110 and the Mengtian experimental module model 16, respectively. The Tianhe core module model 13 is magnetically fixed to the Wentian experimental module model 110. The rear end of the Tianhe core module model 13 is magnetically fixed to the rear end of the Tianhe core module model 13. The Tianzhou spacecraft solar panel model 12 has two sets and is rotatably set on both sides of the Tianzhou cargo spacecraft model 11. The Tianhe core module solar panel model 14 has two sets and is rotatably set on both sides of the Tianhe core module model 13. The Mengtian experimental module solar panel model 15 has two sets and is rotatably set on the outside of the Mengtian experimental module model 16. The Wentian experimental module solar panel model 111 has two sets and is rotatably set on the outside of the Wentian experimental module model 110. The Shenzhou spacecraft solar panel model 17 has two sets and is rotatably set on the front end of the Shenzhou manned spacecraft model 18. The mechanical arm model 19 is rotatably connected to the top of the Tianhe core module model 13.

[0025] The magnetic fixing connection method makes installation simpler and does not require additional tools. At the same time, the rotatable solar panel model can be flexibly rotated and adjusted according to the user's preferences. The model can also be freely disassembled and installed to simulate the docking of the Shenzhou manned spacecraft and the Tianzhou cargo spacecraft. The two Shenzhou manned spacecraft models 18 are respectively attached to the docking mechanism of the Tianhe core module model 13 from the bottom longitudinal docking interface and the front transverse docking interface. Then, the Tianzhou cargo spacecraft model 11 is attached to the tail docking interface of the Tianhe core module model 13 to realize the rendezvous and docking function and achieve the demonstration effect of docking of the six-module combination.

[0026] The robotic arm model 19 has magnets installed at both ends, which can be attached to the magnetic attraction area on the top of the Tianhe core module model 13 and the other two experimental modules. The robotic arm has multiple joints with rotation function, which can be attached to the Tianhe core module model 13 and the other two experimental modules at the same time, simulating the crawling function of a real robotic arm.

[0027] The top of the T-shaped bracket 23 is provided with three sets of ring brackets. The three sets of ring brackets support the bottom of the Tianhe core module model 13, the Mengtian experimental module model 16 and the Wentian experimental module model 110 respectively, so as to place the main body of the model 1 on the surface of the fixed structure 2.

[0028] The bottom of the fixed base 21 is a magnetic suction plate, which enables the astronaut model 3 to be magnetically fixed to the fixed structure 2;

[0029] The astronaut model 3 is quite exquisite, and together with the main model 1, it enhances the overall aesthetics.

[0030] Those skilled in the art should understand that the discussion of any of the above embodiments is merely exemplary and is not intended to imply that the scope of the present invention includes the claims being limited to these examples; within the framework of the present invention, the technical features of the above embodiments or different embodiments can also be combined, the steps can be implemented in any order, and there are many other variations of the different aspects of the present invention as described above, which are not provided in the details for the sake of brevity.

[0031] This utility model is intended to cover all such substitutions, modifications, and variations that fall within the broad scope of the appended claims. Therefore, any omissions, modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. A space station model, comprising a main model body (1), a fixed structure (2), and an astronaut model (3), characterized in that: The model body (1) is placed on the top of the fixed structure (2), and the astronaut model (3) is magnetically fixed to one side of the top of the model body (1). The fixed structure (2) includes a fixed base (21), a support rod (22), a T-shaped bracket (23) and a fixing bolt (24). The top of the fixed base (21) has a slot, and the bottom end of the support rod (22) is inserted into the slot to fix it to the fixed base (21). The T-shaped bracket (23) is placed on the top of the support rod (22), and the support rod (22) and the T-shaped bracket (23) are fixedly connected by the fixing bolt (24).

2. A space station model according to claim 1, characterized in that: The main body of the model (1) includes a Tianzhou cargo spacecraft model (11), a Tianzhou spacecraft solar panel model (12), a Tianhe core module model (13), a Tianhe core module solar panel model (14), a Mengtian experimental module solar panel model (15), a Mengtian experimental module model (16), a Shenzhou spacecraft solar panel model (17), a Shenzhou manned spacecraft model (18), a robotic arm model (19), a Wentian experimental module model (110), and a Wentian experimental module solar panel model (111). The Wentian experimental module model (110) and the Mengtian experimental module model (16) are fixed together as a whole. The Shenzhou manned spacecraft model (18) has two sets, which are magnetically fixed to the front and bottom of the Wentian experimental module model (110) and the Mengtian experimental module model (16), respectively. The Tianhe core module model (13) is magnetically fixed to the Wentian experimental module model (110) and the Mengtian experimental module model (16). At the rear end of the Mengtian experimental module model (16), the Tianzhou cargo spacecraft model (11) is magnetically fixed to the rear end of the Tianhe core module model (13). The Tianzhou spacecraft solar panel model (12) has two sets and is rotatably set on both sides of the Tianzhou cargo spacecraft model (11). The Tianhe core module solar panel model (14) has two sets and is rotatably set on both sides of the Tianhe core module model (13). The Mengtian experimental module solar panel model (15) has two sets and is rotatably set on the outside of the Mengtian experimental module model (16). The Wentian experimental module solar panel model (111) has two sets and is rotatably set on the outside of the Wentian experimental module model (110). The Shenzhou spacecraft solar panel model (17) has two sets and is rotatably set on the front end of the Shenzhou manned spacecraft model (18). The robotic arm model (19) is rotatably connected to the top of the Tianhe core module model (13).

3. A space station model according to claim 2, characterized in that: The top of the T-shaped bracket (23) is provided with three sets of ring brackets. The three sets of ring brackets support the bottom of the Tianhe core module model (13), the Mengtian experimental module model (16) and the Wentian experimental module model (110) respectively, so as to realize the placement of the model body (1) on the surface of the fixed structure (2).

4. A space station model according to claim 3, characterized in that: The bottom of the fixed base (21) is a magnetic suction plate, which enables the astronaut model (3) to be magnetically fixed to the fixed structure (2).

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