A cutting metal spark sputter protection system

Abstract

The application discloses a cutting metal spark sputtering protection system, and relates to the technical field of construction safety protection, which comprises a sputtering protection device, a capturing device for capturing sparks flying in the cutting metal process, at least seven airflow traction mechanisms and an image collector, and the sputtering protection device, the airflow traction mechanisms and the image collector are respectively connected with a controller in communication; the controller controls the operation of the airflow traction mechanisms and the sputtering protection device according to the data collected by the image collector after analysis, so as to capture the flying sparks; the upper and lower capturing devices are adopted to make the metal sparks be captured into the capturing device under the action of airflow, so that the problems that the metal sparks cannot be effectively collected in the existing metal cutting process and the health of construction personnel is easily damaged are solved.

Description

Technical Field

[0001] This invention relates to the field of construction safety protection technology, specifically to a spark protection system for cutting metal. Background Technology

[0002] During the construction process, metal cutting is involved in many procedures, including but not limited to the cutting of steel bars, the prefabrication of metal components, and the processing and assembly of steel structure projects. A large number of sparks are generated during the cutting operation.

[0003] When high-temperature sparks fly and cool rapidly, the metal particles within them solidify into tiny solid particles, known as metal dust. These dust particles are typically very small, can remain suspended in the air, and can impact human health and the environment. Furthermore, high-temperature metal sparks can pose a fire hazard if they fly onto flammable materials.

[0004] In existing construction processes, to prevent metal sparks from flying everywhere, baffles are generally installed in the direction of the splash to block the sparks. However, because metal sparks are affected by airflow during the splashing process, they will be carried by the airflow and splash randomly. This makes the baffles less effective. On the other hand, the metal dust formed after the metal sparks cool can be easily inhaled by construction workers, which can cause damage to their health if no effective protective measures are taken. Summary of the Invention

[0005] This invention provides a spark protection system for cutting metal. It uses upper and lower capturing devices to capture metal sparks by entraining and converging them under the action of airflow. This solves the problem that existing metal cutting processes cannot effectively collect metal sparks and cause harm to the health of construction workers.

[0006] A metal cutting spark sputtering protection system includes:

[0007] A sputter protection device having a capturing device for capturing sparks splashed during metal cutting, wherein the capturing device includes an upper capturing device and a lower capturing device, the upper capturing device capturing sparks splashed toward the upper part of the sputter protection device by means of negative pressure attraction, and the lower capturing device capturing sparks splashed toward the lower part of the sputter protection device by means of negative pressure attraction.

[0008] The splash protection device is also equipped with at least seven airflow traction mechanisms and image acquisition devices. The splash protection device, airflow traction mechanisms and image acquisition devices are all connected to the controller.

[0009] The controller analyzes the data collected by the image acquisition device and then controls the operation of the airflow traction mechanism and the splash protection device to capture the splashing sparks.

[0010] Furthermore, the sputtering protection device includes a concentrator, wherein the concentrator has an independent upper cavity and a lower cavity inside, and an exhaust pipe communicating with the interior of the concentrator is provided on the back of the concentrator.

[0011] Furthermore, the upper capture device includes a flame-retardant filter bag a and a negative pressure generator a. The flame-retardant filter bag a is detachably installed inside the upper cavity. The inlet of the flame-retardant filter bag a is connected to the outside of the front of the upper collection container. The negative pressure generator a is installed outside the upper cavity. Its suction end is connected to the inside of the upper cavity, and its output end is connected to the outside of the splash protection device through an exhaust pipe. The signal output end of the controller is communicatively connected to the signal input end of the negative pressure generator a.

[0012] Furthermore, the upper capture device also includes an upper capture shroud, which is located on the upper front of the collection container, and an image acquisition device is mounted on the upper capture shroud, suitable for acquiring image data of Martian ejecta.

[0013] Furthermore, the lower capture device includes a flame-retardant filter bag b and a negative pressure generator b. The flame-retardant filter bag b is detachably installed inside the lower cavity, and the negative pressure generator b is installed outside the lower cavity. Its suction end is connected to the inside of the lower cavity, and its output end is connected to the outside of the splash protection device through an exhaust pipe. It also includes a lower capture hood hinged to the centralized container. The lower capture hood has a suction port, and the inlet of the flame-retardant filter bag b is connected to the suction port through at least one suction tube. The signal output terminal of the controller is communicatively connected to the signal input terminal of the negative pressure generator b.

[0014] Furthermore, the airflow traction mechanism is installed on the upper capture hood and communicates with its interior. The airflow traction mechanism includes a suction head, and a suction pump is installed inside the suction head. The signal output terminal of the controller is communicatively connected to the signal input terminal of the suction pump.

[0015] Furthermore, the controller includes a Mars analysis module, a power control module, and an airflow traction control module;

[0016] The Mars analysis module is suitable for analyzing acquired image data to identify the splash range and trajectory of Mars.

[0017] The power control module is adapted to calculate the operating power of the upper and lower capture devices based on the splash range and trajectory of Mars, so that Mars can be captured by the airflow and enter the upper and / or lower capture devices.

[0018] The airflow traction control module is suitable for analyzing the splash range and trajectory of Mars. When it is detected that the upper capture device and / or lower capture device cannot capture Mars, it controls the corresponding airflow traction mechanism to pull the Mars according to the trajectory and movement trend of Mars, so that the Mars is captured by the airflow and enters the upper capture device.

[0019] Furthermore, the Mars analysis module includes a Mars feature extraction unit and a Mars trajectory recognition unit. The Mars feature extraction unit is suitable for extracting Mars features using image data and identifying Mars and its splash range. The Mars trajectory recognition unit is suitable for tracking the trajectory of Mars based on the recognition results.

[0020] Furthermore, the power control module includes a Mars trajectory trend analysis unit a and a dynamic power calculation unit. The Mars trajectory trend analysis unit a is adapted to predict the motion trend of Mars based on its motion trajectory; the dynamic power calculation unit is adapted to calculate the operating power of the upper capture device and / or the lower capture device based on the motion trajectory and motion trend of Mars.

[0021] Furthermore, the airflow traction control module includes a Mars trajectory trend analysis unit b and an airflow traction calculation unit. The Mars trajectory trend analysis unit b is adapted to predict the motion trend of Mars based on its motion trajectory. The airflow traction calculation unit is adapted to activate the airflow traction mechanism at the corresponding position based on the predicted motion trend when the motion trend of Mars is to leave the capture range of the upper capture device.

[0022] The beneficial effects of the above-described technical solutions provided in the embodiments of the present invention include at least the following:

[0023] 1. By using an upper and lower capture device arranged vertically, and employing airflow traction, the metal sparks generated during the metal cutting process are entrained and captured by the airflow into the capture device. Compared with existing technologies, this method can more effectively collect metal sparks, prevent them from splashing to other locations and causing fires, and prevent the metal dust formed from being inhaled by construction workers.

[0024] 2. The airflow traction mechanism can enhance the capture range of the capture device, prevent metal sparks from escaping, improve the capture rate of the capture device, and effectively enhance the capture effect of the capture device on metal dust.

[0025] Other features and advantages of the invention will be set forth in the description which follows, and will be apparent in part from the description, or may be learned by practicing the invention. The objects and other advantages of the invention may be realized and obtained by means of the structures particularly pointed out in the written description, claims, and drawings.

[0026] The technical solution of the present invention will be further described in detail below with reference to the accompanying drawings and embodiments. Attached Figure Description

[0027] The accompanying drawings are provided to further illustrate the invention and form part of the specification. They are used in conjunction with embodiments of the invention to explain the invention and do not constitute a limitation thereof. In the drawings:

[0028] Figure 1 This is a communication block diagram of the protection system disclosed in an embodiment of the present invention;

[0029] Figure 2 This is a schematic diagram of the structure of the protection system disclosed in an embodiment of the present invention;

[0030] Figure 3 for Figure 2 Enlarged structural diagram at point A;

[0031] Figure 4 for Figure 2 A schematic diagram of the folded structure of the lower and middle capture device;

[0032] Figure 5 This is a side cross-sectional view of the protection system disclosed in an embodiment of the present invention.

[0033] Figure label:

[0034] 1. Splash protection device; 11. Vehicle body; 12. Concentrated container; 121. Upper cavity; 122. Lower cavity; 13. Upper capture device; 131. Upper capture hood; 132. Negative pressure generator a; 133. Flame-retardant filter bag a; 14. Lower capture device; 141. Lower capture hood; 142. Suction pipe; 143. Negative pressure generator b; 144. Flame-retardant filter bag b; 15. Exhaust pipe; 2. Airflow traction mechanism; 21. Suction head; 22. Suction pump; 3. Image acquisition device; 4. Controller; 41. Smoke separator Analysis module; 411, Smoke feature extraction unit; 412, Smoke range identification unit; 42, Mars analysis module; 421, Mars feature extraction unit; 422, Mars trajectory identification unit; 43, Power control module; 431, Smoke movement trend analysis unit a; 432, Mars trajectory trend analysis unit a; 433, Dynamic power calculation unit; 44, Airflow traction control module; 441, Smoke movement trend analysis unit b; 442, Mars trajectory trend analysis unit b; 443, Airflow traction calculation unit. Detailed Implementation

[0035] Exemplary embodiments of the present disclosure will now be described in more detail with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be implemented in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.

[0036] like Figures 1-5 As shown, the present invention proposes a metal cutting spark sputtering protection system comprising:

[0037] Sputter protection device 1 has a capturing device for capturing sparks splashed during metal cutting, wherein the capturing device includes an upper capturing device 13 and a lower capturing device 14. The upper capturing device 13 captures sparks splashed toward the upper part of the sputter protection device 1 by means of negative pressure attraction, and the lower capturing device 14 captures sparks splashed toward the lower part of the sputter protection device 1 by means of negative pressure attraction.

[0038] The splash protection device 1 is also equipped with at least seven airflow traction mechanisms 2 and image acquisition devices 3. The splash protection device 1, airflow traction mechanisms 2 and image acquisition devices 3 are respectively connected to the controller 4.

[0039] The controller 4 analyzes the data collected by the image acquisition device 3 and controls the operation of the airflow traction mechanism 2 and the splash protection device 1 respectively to capture the splashing sparks.

[0040] like Figure 2 , 4 As shown, the splash protection device 1 can be installed on the vehicle body 11 to achieve the effect of mobile use, or it can be fixedly installed to achieve the effect of fixed-point use.

[0041] When the container 12 is installed on the vehicle body 11, it is fixedly installed on the plate of the vehicle body 11, so as to achieve the effect of running together with the vehicle body 11.

[0042] like Figure 1 As shown, the controller 4 has a Mars analysis module 42, a power control module 43, and an airflow traction control module 44;

[0043] The Mars analysis module 42 is suitable for analyzing the acquired image data and identifying the splash range and trajectory of Mars.

[0044] The Mars analysis module 42 includes a Mars feature extraction unit 421 and a Mars trajectory recognition unit 422. The Mars feature extraction unit 421 is adapted to extract Mars features using image data and identify Mars and its splash range. The Mars trajectory recognition unit 422 is adapted to track the trajectory of Mars based on the recognition results.

[0045] In another embodiment, the controller 4 also has a smoke analysis module 41, which is adapted to identify smoke generated during the cutting process.

[0046] Specifically, the smoke analysis module 41 includes a smoke feature extraction unit 411 and a smoke range recognition unit 412;

[0047] The smoke feature extraction unit 411 is adapted to extract smoke features using image data and identify smoke and its range;

[0048] The smoke range recognition unit 412 is adapted to track the trajectory of the smoke based on the recognition result.

[0049] Using the above embodiment, it is necessary to add materials for adsorbing smoke to the upper capture device 13 and the lower capture device 14. The materials for adsorbing smoke include activated carbon, nanomaterials, metal-organic frameworks (MOFs), etc., which are integrated with the flame-retardant filter bag of the upper capture device 13 so that it can adsorb smoke while collecting sparks.

[0050] The power control module 43 is adapted to calculate the operating power of the upper capture device 13 and the lower capture device 14 based on the splash range and trajectory of the Mars, so that the Mars is captured by the airflow and enters the upper capture device 13 and / or the lower capture device 14.

[0051] The power control module 43 includes a Mars trajectory trend analysis unit a432 and a dynamic power calculation unit 433. The Mars trajectory trend analysis unit a432 is adapted to predict the motion trend of Mars based on its motion trajectory. The dynamic power calculation unit 433 is adapted to calculate the operating power of the upper capture device 13 and / or the lower capture device 14 based on the motion trajectory and motion trend of Mars.

[0052] In another embodiment, the power control module 43 further includes a smoke movement trend analysis unit a431, which is adapted to predict the movement trend of the smoke based on the smoke's trajectory. The dynamic power calculation unit 433 calculates the operating power of the upper capture device 13 and / or the lower capture device 14 based on the smoke range and movement trend, so as to achieve the absorption of the smoke.

[0053] like Figures 2-5As shown, specifically, the sputter protection device 1 includes a collection container 12, wherein the collection container 12 has an independent upper cavity 121 and a lower cavity 122 inside, and an exhaust pipe 15 communicating with the interior of the collection container 12 is also provided on the back of the collection container 12. The upper capture device 13 includes a flame-retardant filter bag a133 and a negative pressure generator a132. The flame-retardant filter bag a133 is detachably installed inside the upper cavity 121, and the inlet of the flame-retardant filter bag a133 is connected to the outside of the front of the upper collection container 12. The negative pressure generator a132 is located outside the upper cavity 121, its suction end is connected to the interior of the upper cavity 121, and its output end is connected to the outside of the sputter protection device 1 through the exhaust pipe 15. The signal output end of the controller 4 is communicatively connected to the signal input end of the negative pressure generator a132. The upper capture device 13 also includes an upper capture device. The upper capture hood 131 is located on the upper front of the collection container 12. The image acquisition device 3 is located on the upper capture hood 131 and is suitable for acquiring image data of spark ejection. The lower capture device 14 includes a flame-retardant filter bag b144 and a negative pressure generator b143. The flame-retardant filter bag b144 is detachably located inside the lower cavity 122. The negative pressure generator b143 is located outside the lower cavity 122. Its suction end is connected to the inside of the lower cavity 122, and its output end is connected to the outside of the ejection protection device 1 through the exhaust pipe 15. The lower capture hood 141 is hinged to the collection container 12. The lower capture hood 141 has a suction port. The inlet of the flame-retardant filter bag b144 is connected to the suction port through at least one suction pipe 142. The signal output end of the controller 4 is communicatively connected to the signal input end of the negative pressure generator b143.

[0054] When capturing metal sparks and / or smoke:

[0055] 1. When the negative pressure generator a132 is activated, a negative pressure environment is created in the upper cavity 121. The front of the collection container 12 faces the metal sparks and / or smoke source. Under the action of suction, the airflow carries and gathers the metal sparks and / or smoke, and draws them into the flame-retardant filter bag a133. The flame-retardant filter bag a133 is detachably connected to the upper cavity 121 by means of snap-fit ​​connection or flange connection. When the flame-retardant filter bag a133 needs to be replaced, it is removed and replaced with a new flame-retardant filter bag a133.

[0056] 2. When the negative pressure generator b143 is activated, a negative pressure environment is created in the lower cavity 122. The front of the collection container 12 faces the source of metal sparks and / or smoke. Under the action of suction, the airflow carries and gathers the metal sparks and / or smoke, and draws them into the flame-retardant filter bag b144. The flame-retardant filter bag b144 is detachably connected to the interior of the upper cavity 121 by means of snap-fit ​​connection or flange connection. When the flame-retardant filter bag b144 needs to be replaced, it is removed and replaced with a new flame-retardant filter bag b144.

[0057] The airflow traction control module 44 is suitable for analyzing the splash range and trajectory of Mars. When it is detected that the upper capture device 13 and / or the lower capture device 14 cannot capture Mars, it controls the corresponding airflow traction mechanism 2 to operate to traction Mars according to the trajectory and movement trend of Mars, so that Mars is captured by the airflow and enters the upper capture device 13.

[0058] The airflow traction control module 44 includes a Mars trajectory trend analysis unit b442 and an airflow traction calculation unit 443. The Mars trajectory trend analysis unit b442 is adapted to predict the motion trend of Mars based on its motion trajectory. The airflow traction calculation unit 443 is adapted to activate the corresponding airflow traction mechanism 2 based on the predicted motion trend when the motion trend of Mars is to leave the capture range of the upper capture device 13.

[0059] In another embodiment, the airflow traction control module 44 further includes a smoke movement trend analysis unit b441, which is adapted to predict the movement trend of the smoke based on the smoke's trajectory. When the airflow traction calculation unit 443 detects that the smoke's movement trend is to leave the capture range of the upper capture device 13, it activates the airflow traction mechanism 2 at the corresponding position based on the predicted movement trend.

[0060] like Figures 2-5 As shown, specifically, the airflow traction mechanism 2 is installed on the upper capture hood 131 and communicates with its interior. The airflow traction mechanism 2 includes a suction head 21, and a suction pump 22 is provided inside the suction head 21. The signal output terminal of the controller 4 is communicatively connected to the signal input terminal of the suction pump 22. After the corresponding airflow traction mechanism 2 is started, the suction pump 22 starts to work. The metal sparks and / or smoke are captured by the airflow under the action of suction force through the suction head 21 and enter the interior of the upper capture device 13.

[0061] This invention utilizes an upper capturing device 13 and a lower capturing device 14 arranged vertically, employing airflow traction technology to entrain metal sparks generated during metal cutting. The sparks are captured and drawn into the capturing device by the airflow. Compared to existing technologies, this method more effectively collects metal sparks, preventing them from scattering and causing fires, and preventing the inhalation of metal dust by workers. Simultaneously, the airflow traction mechanism 2 enhances the capturing range of the device, preventing metal sparks from escaping and improving the capture rate, thus effectively enhancing the device's ability to capture metal dust.

[0062] It should be noted that the specific models and specifications of controller 4, negative pressure generator a132, negative pressure generator b143, suction pump 22, and image acquisition device 3 need to be selected and determined according to the actual specifications of the device. The specific selection calculation method adopts the existing technology in this field, so it will not be described in detail.

[0063] The power supply and operating principles of controller 4, negative pressure generator a132, negative pressure generator b143, suction pump 22, and image acquisition device 3 are clear to those skilled in the art and will not be described in detail here.

[0064] It should be understood that the specific order or hierarchy of steps in the disclosed process is an example of an exemplary method. Based on design preferences, it should be understood that the specific order or hierarchy of steps in the process may be rearranged without departing from the scope of this disclosure. The appended method claims provide elements of various steps in an exemplary order and are not intended to limit the scope to the specific order or hierarchy described.

[0065] In the detailed description above, various features are combined together in a single embodiment to simplify this disclosure. This approach to disclosure should not be construed as reflecting an intention that embodiments of the claimed subject matter require more features than are explicitly stated in each claim. Rather, as reflected in the appended claims, the invention is presented with fewer features than all of the features in a single disclosed embodiment. Therefore, the appended claims are hereby explicitly incorporated into the detailed description, with each claim representing a separate preferred embodiment of the invention.

[0066] Those skilled in the art will also understand that the various illustrative logic blocks, modules, circuits, and algorithm steps described in conjunction with the embodiments herein can be implemented as electronic hardware, computer software, or a combination thereof. To clearly illustrate the interchangeability between hardware and software, the various illustrative components, blocks, modules, circuits, and steps described above are generally described in terms of their functionality. Whether such functionality is implemented as hardware or software depends on the specific application and the design constraints imposed on the overall system. Those skilled in the art can implement the described functionality in alternative ways for each specific application; however, such implementation decisions should not be construed as departing from the scope of this disclosure.

[0067] The steps of the methods or algorithms described in conjunction with the embodiments herein can be directly embodied in hardware, software modules executed by a processor, or a combination thereof. The software modules can reside in RAM memory, flash memory, ROM memory, EPROM memory, EEPROM memory, registers, hard disks, removable disks, CD-ROMs, or any other form of storage medium well known in the art. An exemplary storage medium is connected to the processor, enabling the processor to read information from and write information to the storage medium. Of course, the storage medium can also be a component of the processor. The processor and storage medium can reside in an ASIC. The ASIC can reside in a user terminal. Alternatively, the processor and storage medium can exist as discrete components in the user terminal.

[0068] For software implementation, the techniques described in this application can be implemented using modules (e.g., procedures, functions, etc.) that perform the functions described in this application. This software code can be stored in memory units and executed by a processor. The memory units can be implemented within the processor or outside the processor; in the latter case, they are communicatively coupled to the processor via various means, as is well known in the art.

[0069] The foregoing description includes examples of one or more embodiments. It is certainly impossible to describe all possible combinations of components or methods in order to describe the above embodiments, but those skilled in the art will recognize that the various embodiments can be further combined and arranged. Therefore, the embodiments described herein are intended to cover all such changes, modifications, and variations that fall within the scope of the appended claims. Furthermore, the term "comprising" as used in the specification or claims is interpreted in a manner similar to the term "including," as interpreted when used as a conjunction in the claims. Additionally, the use of any term "or" in the specification of the claims is intended to mean "non-exclusive or."

Claims

1. A spark sputtering protection system for cutting metal, characterized in that, include: A sputter protection device (1) has a capturing device for capturing sparks splashed during metal cutting. The capturing device includes an upper capturing device (13) and a lower capturing device (14). The upper capturing device (13) captures sparks splashed towards the upper part of the sputter protection device (1) by means of negative pressure suction, and the lower capturing device (14) captures sparks splashed towards the lower part of the sputter protection device (1) by means of negative pressure suction. The sputter protection device (1) includes a concentrator (12), wherein the concentrator (12) has an independent upper cavity (121) and a lower cavity (122) inside. 2) The back is also provided with an exhaust pipe (15) that communicates with its interior; the upper capture device (13) includes a flame-retardant filter bag a (133) and a negative pressure generator a (132), the flame-retardant filter bag a (133) is detachably installed inside the upper cavity (121); the negative pressure generator a (132) is installed outside the upper cavity (121); the lower capture device (14) includes a flame-retardant filter bag b (144) and a negative pressure generator b (143), the flame-retardant filter bag b (144) is detachably installed inside the lower cavity (122), and the negative pressure generator b (143) is installed outside the lower cavity (122); The splash protection device (1) is also equipped with at least seven airflow traction mechanisms (2) and image acquisition devices (3). The splash protection device (1), airflow traction mechanisms (2) and image acquisition devices (3) are respectively connected to the controller (4). The controller (4) analyzes the data collected by the image acquisition device (3) and controls the operation of the airflow traction mechanism (2) and the splash protection device (1) respectively to capture the splashing sparks. The controller (4) has a Mars analysis module (42), a power control module (43), and an airflow traction control module (44). The Mars analysis module (42) is suitable for analyzing the acquired image data and identifying the splash range and trajectory of the Mars. The power control module (43) is suitable for calculating the operating power of the upper capture device (13) and the lower capture device (14) based on the splash range and trajectory of the Mars, so that the Mars is captured by the airflow and enters the upper capture device (13) and / or the lower capture device (14). The airflow traction control module (44) is suitable for analyzing the splash range and trajectory of the Mars. When it is identified that the upper capture device (13) and / or the lower capture device (14) cannot capture the Mars, it controls the corresponding airflow traction mechanism (2) to traction the Mars based on the trajectory and movement trend of the Mars, so that the Mars is captured by the airflow and enters the upper capture device (13).

2. The system as described in claim 1, characterized in that, The inlet of the flame-retardant filter bag a (133) is connected to the outside of the front of the centralized container (12), the suction end of the negative pressure generator a (132) is connected to the inside of the upper cavity (121), and its output end is connected to the outside of the splash protection device (1) through the exhaust pipe (15). The signal output end of the controller (4) is connected to the signal input end of the negative pressure generator a (132).

3. The system as described in claim 2, characterized in that, The upper capture device (13) also includes an upper capture shroud (131), which is located on the upper front of the collection container (12), and an image acquisition device (3) is located on the upper capture shroud (131) and is suitable for acquiring image data of Martian ejection.

4. The system as described in claim 1, characterized in that, The suction end of the negative pressure generator b (143) is connected to the interior of the lower cavity (122), and its output end is connected to the exterior of the splash protection device (1) through the exhaust pipe (15). It also includes a lower capture hood (141) hinged to the centralized container (12). The lower capture hood (141) has a suction port. The inlet of the flame-retardant filter bag b (144) is connected to the suction port through at least one suction pipe (142). The signal output end of the controller (4) is communicatively connected to the signal input end of the negative pressure generator b (143).

5. The system as described in claim 3, characterized in that, The airflow traction mechanism (2) is set on the upper capture cover (131) and communicates with its interior. The airflow traction mechanism (2) includes a suction head (21) and a suction pump (22) is provided inside the suction head (21). The signal output terminal of the controller (4) is connected to the signal input terminal of the suction pump (22).

6. The system as described in claim 1, characterized in that, The Mars analysis module (42) includes a Mars feature extraction unit (421) and a Mars trajectory recognition unit (422). The Mars feature extraction unit (421) is adapted to extract Mars features using image data and identify Mars and its splash range. The Mars trajectory recognition unit (422) is adapted to track the trajectory of Mars based on the recognition results.

7. The system as described in claim 1, characterized in that, The power control module (43) includes a Mars trajectory trend analysis unit a (432) and a dynamic power calculation unit (433). The Mars trajectory trend analysis unit a (432) is adapted to predict the motion trend of Mars based on its motion trajectory. The dynamic power calculation unit (433) is adapted to calculate the operating power of the upper capture device (13) and / or the lower capture device (14) based on the motion trajectory and motion trend of Mars.

8. The system as described in claim 1, characterized in that, The airflow traction control module (44) includes a Mars trajectory trend analysis unit b (442) and an airflow traction calculation unit (443). The Mars trajectory trend analysis unit b (442) is adapted to predict the motion trend of Mars based on its motion trajectory. The airflow traction calculation unit (443) is adapted to activate the corresponding airflow traction mechanism (2) based on the predicted motion trend when the motion trend of Mars is to leave the capture range of the upper capture device (13).

Images