Body heat dissipation structure and quadruped robot

Abstract

The utility model provides a kind of fuselage heat dissipation structure and four-legged robot.The fuselage heat dissipation structure includes fuselage main body, motor and first airflow driving member.The fuselage main body is provided with first installation cavity and the first air inlet and air outlet communicated with first installation cavity.The motor is installed in first installation cavity, and is formed with first heat dissipation channel and second heat dissipation channel with the inner wall of first installation cavity.The first airflow driving member is installed on the fuselage main body, and is used to drive the gas in first heat dissipation channel and second heat dissipation channel to flow towards the air outlet.In the present application, the path length of first heat dissipation channel is greater than the path length of second heat dissipation channel, the wind resistance of first heat dissipation channel is designed to be smaller than the wind resistance of second heat dissipation channel, so that the air volume entering first heat dissipation channel is greater than the air volume entering second heat dissipation channel, and then the circumferential four sides of the motor can be uniformly cooled, the heat dissipation performance of fuselage heat dissipation structure is improved, and the four-legged robot can be continuously and stably operated.

Description

Technical Field

[0001] This utility model relates to the field of robot heat dissipation technology, and in particular to a body heat dissipation structure and a quadruped robot. Background Technology

[0002] Quadruped robots possess high flexibility and stability, easily handling complex and varied terrains such as mountains, forests, ruins, and narrow passages. Furthermore, with continuous advancements in motion control technology, quadruped robots can now perform complex actions such as rapid running, jumping, and climbing, demonstrating excellent dynamic motion performance.

[0003] Currently, the main factors affecting the stability of quadruped robots are the walking control algorithm and the mechanical performance of the robot body. Among the mechanical performance of the robot body, the problem of motor heat dissipation is particularly prominent. If the motor overheats, the quadruped robot will enter a self-protection state and stop working. It may even cause problems such as burnt-out circuits, which will greatly affect its performance and stability. Utility Model Content

[0004] Therefore, it is necessary to provide a body heat dissipation structure and a quadruped robot to address the problem of motor heat dissipation in existing quadruped robots.

[0005] The technical solution is as follows:

[0006] On the one hand, a heat dissipation structure for the chassis is provided, including:

[0007] The main body of the unit is provided with a first mounting cavity and a first air inlet and an air outlet communicating with the first mounting cavity;

[0008] The motor is installed in the first mounting cavity, and together with the inner wall of the first mounting cavity, a first heat dissipation channel and a second heat dissipation channel are formed. The first heat dissipation channel and the second heat dissipation channel are arranged along the circumference of the motor and are both connected to the first air inlet and the air outlet. The path length of the first heat dissipation channel is greater than the path length of the second heat dissipation channel, and the wind resistance of the first heat dissipation channel is less than the wind resistance of the second heat dissipation channel.

[0009] A first airflow drive component is installed on the main body of the unit and is used to drive the gas in the first heat dissipation channel and the second heat dissipation channel to flow toward the air outlet.

[0010] The technical solution will be further explained below:

[0011] In one embodiment, there are two first air inlets, which are respectively located on opposite sides of the main body. Two motors are installed in the first mounting cavity. The two motors and the inner wall of the first mounting cavity form a first heat dissipation channel and a second heat dissipation channel. One end of the two first heat dissipation channels and one end of the two second heat dissipation channels are connected to the air outlet. The other end of the two first heat dissipation channels and the other end of the two second heat dissipation channels are respectively connected to the two first air inlets.

[0012] In one embodiment, the air outlet is located at the bottom of the main body of the unit, and the first airflow drive component is installed at the air outlet.

[0013] In one embodiment, the inner wall of the first heat dissipation channel on the side away from the motor is provided with a first guide portion, and the inner wall of the second heat dissipation channel on the side away from the motor is provided with a second guide portion, wherein the distance between the first guide portion and the motor is greater than the distance between the second guide portion and the motor.

[0014] In one embodiment, the main body of the fuselage is further provided with a second air inlet, which is located between the first air inlet and the air outlet and is connected to the first heat dissipation channel.

[0015] In one embodiment, the heat dissipation structure of the fuselage further includes a second airflow drive component, which is installed at the second air inlet and is used to drive gas to flow toward the air outlet.

[0016] In one embodiment, the main body of the fuselage is further provided with a second mounting cavity, a third mounting cavity and a third heat dissipation channel located between the second mounting cavity and the third mounting cavity, and the fuselage heat dissipation structure further includes a battery installed in the second mounting cavity, a control motherboard installed in the third mounting cavity and a third airflow drive component installed in the third heat dissipation channel.

[0017] In one embodiment, the inner wall of the third mounting cavity is provided with a heat dissipation port communicating with the third heat dissipation channel, and the body heat dissipation structure further includes a heat dissipation component, which is installed on the heat dissipation port to seal the heat dissipation port.

[0018] In one embodiment, the heat sink has at least one heat sink fin on the side facing away from the control motherboard, and each heat sink fin extends into the third heat dissipation channel and is spaced apart along the extension direction perpendicular to the third heat dissipation channel.

[0019] On the other hand, a quadruped robot is provided, including the aforementioned body heat dissipation structure. The two ends of the main body are provided with the first mounting cavity, the first air inlet and the air outlet. The number of motors is four, and the four motors are respectively installed in two of the first mounting cavities.

[0020] In the above embodiments, the body heat dissipation structure and quadruped robot, during use, are driven by a first airflow drive component that directs the gas in the first and second heat dissipation channels toward the air outlet. This allows gas from the external environment to enter the first air inlet. The gas at the first air inlet is then split and flows through the first and second heat dissipation channels to the air outlet. During its flow within the first and second heat dissipation channels, the gas carries away the heat generated by the motor. The heated gas converges at the air outlet and is then discharged into the external environment, thus cooling the motor. Furthermore, because the path length of the first heat dissipation channel is greater than that of the second heat dissipation channel, the air resistance of the first heat dissipation channel is designed to be lower than that of the second heat dissipation channel. This results in a greater airflow entering the first heat dissipation channel than the second, allowing for uniform heat dissipation on all four sides of the motor. This improves the heat dissipation performance of the body heat dissipation structure, ensuring the quadruped robot can operate continuously and stably. Attached Figure Description

[0021] The accompanying drawings, which form part of this application, are used to provide a further understanding of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute an undue limitation of this application.

[0022] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0023] Figure 1 This is a schematic diagram of the heat dissipation structure of the fuselage in one embodiment.

[0024] Figure 2 for Figure 1 A cross-sectional view of the fuselage heat dissipation structure.

[0025] Figure 3 This is a cross-sectional view of the fuselage heat dissipation structure according to another embodiment.

[0026] Figure 4 This is a cross-sectional view of the fuselage heat dissipation structure of yet another embodiment.

[0027] Figure 5 for Figure 4 A cross-sectional view of the fuselage heat dissipation structure from another perspective.

[0028] Figure 6 This is a schematic diagram of the structure of a quadruped robot according to one embodiment.

[0029] Figure 7 for Figure 6 A structural diagram of a quadruped robot from another perspective.

[0030] Explanation of reference numerals in the attached figures:

[0031] 1. Quadruped robot; 10. Body heat dissipation structure; 100. Main body; 110. First mounting cavity; 120. First air inlet; 130. Air outlet; 140. Second air inlet; 150. Second mounting cavity; 160. Third mounting cavity; 161. Heat dissipation vent; 170. Third heat dissipation channel; 200. Motor; 300. First airflow drive component; 410. First heat dissipation channel; 420. Second heat dissipation channel; 430. First airflow guide; 440. Second airflow guide; 500. Battery; 600. Control motherboard; 700. Third airflow drive component; 800. Heat dissipation component; 810. Heat dissipation fins. Detailed Implementation

[0032] To make the above-mentioned objectives, features, and advantages of this application more apparent and understandable, the specific embodiments of this application are described in detail below with reference to the accompanying drawings. Many specific details are set forth in the following description to provide a thorough understanding of this application. However, this application can be implemented in many other ways different from those described herein, and those skilled in the art can make similar modifications without departing from the spirit of this application. Therefore, this application is not limited to the specific embodiments disclosed below.

[0033] like Figure 1 and Figure 2 As shown, in one embodiment, a fuselage heat dissipation structure 10 is provided, including a fuselage body 100, a motor 200, and a first airflow drive component 300. The fuselage body 100 has a first mounting cavity 110 and a first air inlet 120 and an air outlet 130 communicating with the first mounting cavity 110. The motor 200 is mounted within the first mounting cavity 110, forming a first heat dissipation channel 410 and a second heat dissipation channel 420 with the inner wall of the first mounting cavity 110. The first heat dissipation channel 410 and the second heat dissipation channel 420 are arranged circumferentially along the motor 200 and are both connected to the first air inlet 120 and the air outlet 130. The path length of the first heat dissipation channel 410 is greater than the path length of the second heat dissipation channel 420, and the air resistance of the first heat dissipation channel 410 is less than the air resistance of the second heat dissipation channel 420. The first airflow drive component 300 is mounted on the fuselage body 100 and is used to drive the gas in the first heat dissipation channel 410 and the second heat dissipation channel 420 to flow towards the air outlet 130.

[0034] In the above embodiment, the body heat dissipation structure 10, when in use, the first airflow driving component 300 drives the gas in the first heat dissipation channel 410 and the second heat dissipation channel 420 to flow toward the air outlet 130, so that the gas in the external environment enters the first air inlet 120. The gas at the first air inlet 120 is split and flows to the air outlet 130 through the first heat dissipation channel 410 and the second heat dissipation channel 420 respectively. During the process of the gas flowing in the first heat dissipation channel 410 and the second heat dissipation channel 420, it will carry away the heat generated by the motor 200. The gas with heat is gathered at the air outlet 130 and discharged to the external environment through the air outlet 130, thereby achieving heat dissipation for the motor 200. In addition, since the path length of the first heat dissipation channel 410 is greater than that of the second heat dissipation channel 420, the wind resistance of the first heat dissipation channel 410 is designed to be smaller than that of the second heat dissipation channel 420. This results in the air volume entering the first heat dissipation channel 410 being greater than that entering the second heat dissipation channel 420, thereby enabling the motor 200 to dissipate heat evenly on all four sides of its circumference and improving the heat dissipation performance of the body heat dissipation structure 10.

[0035] The number and position of the first mounting cavity 110, the number and position of the first air inlet 120, the number and position of the air outlet 130, and the number of motors 200 can all be flexibly adjusted according to actual usage needs.

[0036] like Figure 2 As shown, optionally, there are two first air inlets 120. The two first air inlets 120 are respectively located on opposite sides of the main body 100. Two motors 200 are installed in the first mounting cavity 110. Each of the two motors 200 forms a first heat dissipation channel 410 and a second heat dissipation channel 420 with the inner wall of the first mounting cavity 110. One end of each of the two first heat dissipation channels 410 and one end of each of the two second heat dissipation channels 420 communicates with an air outlet 130. The other ends of each of the two first heat dissipation channels 410 and the two second heat dissipation channels 420 communicate with the two first air inlets 120 respectively. Thus, the two motors 200 are installed in the same first mounting cavity 110, allowing them to share the first airflow drive component 300, saving space and facilitating a compact and integrated design of the body heat dissipation structure 10.

[0037] The first airflow drive component 300 can be configured as a cooling fan, blower, or other structure capable of driving gas flow. The first airflow drive component 300 can be directly installed at the first air inlet 120 or air outlet 130, or it can be installed on the main body 100 and connected to the first air inlet 120 or air outlet 130. The number of first airflow drive components 300 can be flexibly adjusted according to actual usage needs. For example, when there is one first airflow drive component 300, it is installed at the air outlet 130; when there are two first airflow drive components 300, they are installed at the two first air inlets 120 respectively; when there are three first airflow drive components 300, they are installed at the two first air inlets 120 and one air outlet 130 respectively.

[0038] like Figure 2 As shown, optionally, the air outlet 130 is located at the bottom of the main body 100, and the first airflow drive component 300 is installed at the air outlet 130. In this way, by adopting a downward exhaust method, the main body 100 is located above the first airflow drive component 300, which can prevent water from entering the first airflow drive component 300 and improve the reliability of the heat dissipation structure 10.

[0039] It should be noted that the path length of the first heat dissipation channel 410 refers to the length of the first heat dissipation channel 410 along its own extending direction. The path length of the second heat dissipation channel 420 refers to the length of the second heat dissipation channel 420 along its own extending direction.

[0040] The air resistance of the first heat dissipation channel 410 can be controlled by adjusting its cross-sectional dimensions, by incorporating a wind-blocking structure (such as a wind-blocking protrusion) within the first heat dissipation channel 410, or by other methods that can adjust air resistance. Similarly, the air resistance of the second heat dissipation channel 420 can be controlled by adjusting its cross-sectional dimensions, by incorporating a wind-blocking structure within the second heat dissipation channel 420, or by other methods that can adjust air resistance.

[0041] like Figure 2As shown, in one embodiment, the inner wall of the first heat dissipation channel 410 on the side away from the motor 200 is provided with a first airflow guide 430. The inner wall of the second heat dissipation channel 420 on the side away from the motor 200 is provided with a second airflow guide 440. The distance between the first airflow guide 430 and the motor 200 is greater than the distance between the second airflow guide 440 and the motor 200. Thus, by adjusting the distance between the first airflow guide 430 and the motor 200, the air resistance of the first heat dissipation channel 410 can be adjusted, and by adjusting the distance between the second airflow guide 440 and the motor 200, the air resistance of the second heat dissipation channel 420 can be adjusted. The operation is simple and convenient, and the practicality of the body heat dissipation structure 10 can be improved.

[0042] Specifically, in this embodiment, the first guide section 430 is configured as a first arc-shaped guide plate, and the second guide section 440 is configured as a second arc-shaped guide plate. The extension directions of both the first and second arc-shaped guide plates are the same as the circumferential direction of the motor 200. Thus, the arc-shaped design of both the first guide section 430 and the second guide section 440 can guide the gas flow towards the air outlet 130, preventing turbulence and eddies in the gas within the first and second heat dissipation channels 410 and 420. This ensures that the gas can smoothly pass through the first and second heat dissipation channels 410 and carry away the heat generated by the motor 200, improving the reliability of the body heat dissipation structure 10.

[0043] It should be noted that the distances between the first airflow guide 430 and the motor 200, and between the second airflow guide 440 and the motor 200, can be flexibly adjusted according to actual usage needs. For example, the distances between the first airflow guide 430 and the motor 200, and between the second airflow guide 440 and the motor 200, can be flexibly adjusted according to the overall dimensions of the heat dissipation structure 10 and the dimensions and power consumption of the motor 200.

[0044] Specifically, in this embodiment, the distance between the first guide section 430 and the motor 200 can be set to 4mm to 6.5mm; the distance between the second guide section 440 and the motor 200 can be set to 0mm to 2mm.

[0045] It should be noted that when the distance between the second air guide 440 and the motor 200 is 0mm, the second heat dissipation channel 420 cannot allow gas to pass through, and all the gas at the first air inlet 120 flows to the air outlet 130 through the first heat dissipation channel 410. In this way, while taking into account the heat dissipation of the motor 200, the stability of the motor 200 support can be ensured.

[0046] like Figure 3As shown, in one embodiment, the fuselage body 100 is further provided with a second air inlet 140. The second air inlet 140 is located on the airflow path and is connected to the first heat dissipation channel 410. Thus, the arrangement of the second air inlet 140 increases the airflow speed between the second air inlet 140 and the air outlet 130. According to Bernoulli's principle, the pressure between the second air inlet 140 and the air outlet 130 is correspondingly reduced, forming a negative pressure zone. This causes more gas in the external environment to pass through the first air inlet 120 and be diverted into the first heat dissipation channel 410 and the second heat dissipation channel 420, accelerating the transfer and dissipation of heat, effectively enhancing the convective heat transfer effect of the air, and improving the heat dissipation rate of the fuselage heat dissipation structure 10. In addition, based on the fuselage heat dissipation structure 10 utilizing Bernoulli's principle, greater airflow can be generated within the first heat dissipation channel 410 and the second heat dissipation channel 420, enabling the first airflow drive component 300 to achieve efficient heat dissipation with lower energy consumption. That is, while achieving the same heat dissipation effect, the power of the first airflow drive component 300 can be reduced, thereby reducing the noise generated by the first airflow drive component 300 during operation and improving the practicality of the fuselage heat dissipation structure 10.

[0047] Specifically, in this embodiment, the second air inlet 140 being located on the airflow path means that the second air inlet 140 is located on the airflow path between the first air inlet 120 and the air outlet 140.

[0048] Specifically in this embodiment, the second air inlet 140 is located at the top of the main body 100, between the two motors 200, and directly above the air outlet 130.

[0049] Optionally, the fuselage heat dissipation structure 10 also includes a second airflow drive component. The second airflow drive component is installed at the second air inlet 140 and is used to drive the gas to flow toward the air outlet 130. In this way, the second airflow drive component can further accelerate the airflow speed between the second air inlet 140 and the air outlet 130, further enhance the convective heat transfer effect of the air, and improve the heat dissipation performance of the fuselage heat dissipation structure 10.

[0050] The second airflow drive component can be configured as a cooling fan, a blower, or other structure capable of driving gas flow.

[0051] like Figure 4 and Figure 5As shown, in one embodiment, the main body 100 further includes a second mounting cavity 150, a third mounting cavity 160 spaced apart, and a third heat dissipation channel 170 located between the second mounting cavity 150 and the third mounting cavity 160. The body heat dissipation structure 10 also includes a battery 500 installed in the second mounting cavity 150, a control motherboard 600 installed in the third mounting cavity 160, and a third airflow drive component 700 installed in the third heat dissipation channel 170. Thus, the battery 500 and the control motherboard 600 share the third heat dissipation channel 170, achieving effective heat dissipation for both the battery 500 and the control motherboard 600, while also facilitating the integrated design of the body heat dissipation structure 10.

[0052] The third airflow drive component 700 can be configured as a cooling fan, blower, or other structure capable of driving gas flow; the battery 500 can be connected to the third heat dissipation channel 170 through heat transfer components such as a heat transfer plate.

[0053] Specifically, in this embodiment, there are two third airflow drive components 700, which are respectively installed at the air inlet and air outlet of the third heat dissipation channel 170. This further improves the heat dissipation performance of the chassis heat dissipation structure 10.

[0054] like Figure 4 and Figure 5 As shown, the inner wall of the third mounting cavity 160 is further provided with a heat dissipation vent 161 communicating with the third heat dissipation channel 170. The chassis heat dissipation structure 10 also includes a heat sink 800, which is installed at the heat dissipation vent 161 to seal the heat dissipation vent 161. Thus, since the heat generated by the control motherboard 600 is greater than that generated by the battery 500, the heat sink 800 is installed at the heat dissipation vent 161, and the control motherboard 600 can be in close contact with the heat sink 800, thereby accelerating the heat dissipation efficiency of the control motherboard 600 and improving the reliability of the chassis heat dissipation structure 10.

[0055] The heat sink 800 can be configured as a heat sink plate, heat sink cover, heat sink fin, or other heat dissipation structure.

[0056] In this specific embodiment, the heat sink 800 is a separately detachable component. Thus, waterproofing only needs to be applied to the contact surface between the heat sink 800 and the third heat dissipation channel 170, which simplifies manufacturing, enhances the waterproofing method, and improves the practicality of the chassis heat dissipation structure 10.

[0057] like Figure 4 and Figure 5As shown, optionally, the heat sink 800 has at least one heat dissipation fin 810 on the side facing away from the control motherboard 600. Each heat dissipation fin 810 extends into the third heat dissipation channel 170 and is spaced apart along the extension direction perpendicular to the third heat dissipation channel 170. In this way, the heat dissipation fins 810 can further increase the heat dissipation area of ​​the third heat dissipation channel 170, thereby improving the heat dissipation performance of the chassis heat dissipation structure 10.

[0058] like Figure 2 , Figure 6 and Figure 7 As shown, in one embodiment, a quadruped robot 1 is also provided, including the body heat dissipation structure 10 of any of the above embodiments. The main body 100 has a first mounting cavity 110, a first air inlet 120, and an air outlet 130 at both ends. There are four motors 200, each mounted in one of the two first mounting cavities 110. In this way, all four motors 200 can receive uniform and reliable heat dissipation, ensuring that the quadruped robot 1 can operate continuously and stably.

[0059] It should be noted that the heat dissipation structure 10 can also be applied to cleaning robots, delivery robots or other equipment.

[0060] Specifically, in this embodiment, the motor 200 can be configured as a side-swing motor. The side-swing motor is located inside the main body 100 and can cooperate with the main body 100 and the first airflow drive component 300 to dissipate heat, ensuring that the side-swing motor will not overheat during long-term operation and improving the reliability of the quadruped robot 1.

[0061] In the description of this application, it should be understood that if terms such as "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential" appear, these terms indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this application 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, and therefore should not be construed as a limitation of this application.

[0062] Furthermore, where the terms "first" and "second" appear, these terms are for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined with "first" or "second" may explicitly or implicitly include at least one of that feature. In the description of this application, where the term "multiple" appears, "multiple" means at least two, such as two, three, etc., unless otherwise explicitly specified.

[0063] In this application, unless otherwise expressly specified and limited, the terms "installation," "connection," "joining," and "fixing," etc., should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral part; they can refer to a mechanical connection or an electrical connection; 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, unless otherwise expressly limited. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0064] In this application, unless otherwise expressly specified and limited, the use of descriptions such as "above" or "below" the second feature indicates that the first and second features are in direct contact or indirect contact via an intermediate medium. Furthermore, "above," "on top of," and "over" the second feature can mean that the first feature is directly above or diagonally above the second feature, or simply that the first feature is at a higher horizontal level than the second feature. Similarly, "below," "below," and "under" the second feature can mean that the first feature is directly below or diagonally below the second feature, or simply that the first feature is at a lower horizontal level than the second feature.

[0065] It should be noted that if an element is referred to as being "fixed to" or "set on" another element, it can be directly on the other element or there may be an intervening element. If an element is considered to be "connected to" another element, it can be directly connected to the other element or there may be an intervening element. If so, the terms "vertical," "horizontal," "upper," "lower," "left," "right," and similar expressions used in this application are for illustrative purposes only and do not represent the only possible implementation.

[0066] It should also be understood that, in interpreting the connection or positional relationships of components, although not explicitly described, connection and positional relationships are interpreted to include a range of error, which should be within the acceptable deviation range of a specific value as determined by a person skilled in the art. For example, "approximately," "about," or "substantially" can mean within one or more standard deviations, without limitation herein.

[0067] The technical features of the above embodiments can be combined in any way. For the sake of brevity, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0068] The above embodiments merely illustrate several implementation methods of this application, and while the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the patent application. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of this application, and these all fall within the protection scope of this application. Therefore, the protection scope of this patent application should be determined by the appended claims.

Claims

1. A fuselage heat dissipation structure, characterized in that, include: The main body of the unit is provided with a first mounting cavity and a first air inlet and an air outlet communicating with the first mounting cavity; The motor is installed in the first mounting cavity, and together with the inner wall of the first mounting cavity, a first heat dissipation channel and a second heat dissipation channel are formed. The first heat dissipation channel and the second heat dissipation channel are arranged along the circumference of the motor and are both connected to the first air inlet and the air outlet. The path length of the first heat dissipation channel is greater than the path length of the second heat dissipation channel, and the wind resistance of the first heat dissipation channel is less than the wind resistance of the second heat dissipation channel. A first airflow drive component is installed on the main body of the unit and is used to drive the gas in the first heat dissipation channel and the second heat dissipation channel to flow toward the air outlet.

2. The fuselage heat dissipation structure according to claim 1, characterized in that, There are two first air inlets, which are respectively located on opposite sides of the main body. Two motors are installed in the first mounting cavity. The two motors and the inner wall of the first mounting cavity form a first heat dissipation channel and a second heat dissipation channel. One end of the two first heat dissipation channels and one end of the two second heat dissipation channels are connected to the air outlet. The other end of the two first heat dissipation channels and the other end of the two second heat dissipation channels are respectively connected to the two first air inlets.

3. The fuselage heat dissipation structure according to claim 1, characterized in that, The air outlet is located at the bottom of the main body of the unit, and the first airflow drive component is installed at the air outlet.

4. The fuselage heat dissipation structure according to claim 1, characterized in that, The inner wall of the first heat dissipation channel on the side away from the motor is provided with a first flow guide, and the inner wall of the second heat dissipation channel on the side away from the motor is provided with a second flow guide. The distance between the first flow guide and the motor is greater than the distance between the second flow guide and the motor.

5. The fuselage heat dissipation structure according to claim 1, characterized in that, The main body of the unit is also provided with a second air inlet, which is located between the first air inlet and the air outlet and is connected to the first heat dissipation channel.

6. The fuselage heat dissipation structure according to claim 5, characterized in that, The heat dissipation structure of the fuselage also includes a second airflow driving component, which is installed at the second air inlet and is used to drive the gas to flow toward the air outlet.

7. The fuselage heat dissipation structure according to any one of claims 1 to 6, characterized in that, The main body of the fuselage is also provided with a second mounting cavity, a third mounting cavity and a third heat dissipation channel located between the second mounting cavity and the third mounting cavity. The fuselage heat dissipation structure also includes a battery installed in the second mounting cavity, a control motherboard installed in the third mounting cavity and a third airflow drive component installed in the third heat dissipation channel.

8. The fuselage heat dissipation structure according to claim 7, characterized in that, The inner wall of the third mounting cavity is provided with a heat dissipation port that communicates with the third heat dissipation channel. The body heat dissipation structure also includes a heat dissipation component, which is installed on the heat dissipation port to seal the heat dissipation port.

9. The fuselage heat dissipation structure according to claim 8, characterized in that, The heat sink has at least one heat sink fin on the side facing away from the control motherboard. Each heat sink fin extends into the third heat dissipation channel and is spaced apart along the extension direction perpendicular to the third heat dissipation channel.

10. A quadruped robot, characterized in that, The device includes the heat dissipation structure of the fuselage as described in any one of claims 1 to 9, wherein the fuselage body has a first mounting cavity, a first air inlet and an air outlet at both ends, and the number of motors is four, with the four motors respectively installed in two of the first mounting cavities.

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