Air traffic police aircraft

Abstract

The invention discloses an air traffic police aircraft, and relates to the technical field of unmanned aerial vehicles, the air traffic police aircraft comprises a main body structure, the main body structure comprises a cabin, one side of the bottom of the cabin is fixedly connected with a phased array radar, the bottom of the cabin is provided with a storage bin, the bottom of the storage bin is provided with a panoramic camera, and the top of the panoramic camera is provided with a protection part; one side of the panoramic camera is provided with a frequency spectrum monitoring device and is fixedly connected with the cabin, one side of the frequency spectrum monitoring device is provided with an ADS-B receiver and is fixedly connected with the cabin, and the top of the cabin is fixedly connected with a multi-band relay radio station; and a folding assembly; an active phased array radar, a panoramic camera, frequency spectrum monitoring equipment and an ADS-B / 1090ES receiver are integrated through a main body structure, target legality is cooperatively captured and discriminated, electromagnetic interference is avoided through intelligent skin, an emergency air base station is built through a multi-band relay radio station, and therefore monitoring precision and scene adaptability are improved.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to aerial traffic police aircraft. Background Technology

[0002] With the rapid development of drone technology, drones have been widely used in various fields such as aerial photography, logistics, and surveying. However, a large number of unregistered and unlicensed "black flight" drones have also emerged. These black flight drones fly arbitrarily and in uncontrolled areas, which not only easily leads to collisions with civil aircraft and buildings, causing safety accidents, but may also be used for illegal surveying, surreptitious photography, and the transportation of contraband, posing a serious threat to public safety, national security, and social order.

[0003] Existing civilian or general police drones often have limited functionality, typically only possessing basic high-definition shooting or video recording capabilities. These drones are unable to conduct comprehensive information collection and analysis of suspicious targets, making them ill-suited for complex air traffic control tasks. Secondly, the landing gear of existing drones generally employs a traditional fixed structure design. While this structure is simple to manufacture and highly reliable, during monitoring missions, the fixed landing gear protruding from under the fuselage easily obstructs the field of view of the onboard camera equipment, creating significant blind spots. This deficiency severely impacts the integrity and continuity of image acquisition, leading to the loss of crucial images during low-altitude patrols, target locking, and close-range identification, making it impossible to obtain clear target details and thus reducing the accuracy of monitoring and evidence collection. Summary of the Invention

[0004] The purpose of this section is to outline some aspects of embodiments of the present invention and to briefly describe some preferred embodiments. Simplifications or omissions may be made in this section, as well as in the abstract and title of this application, to avoid obscuring the purpose of these documents; however, such simplifications or omissions should not be construed as limiting the scope of the invention.

[0005] In view of the problems existing in the above and / or existing air traffic control aircraft, the present invention is proposed.

[0006] Therefore, the problem to be solved by this invention is how to address the inability to collect and analyze information about suspicious targets from all angles, and how the fixed landing gear can easily obstruct the field of view of the mounted shooting equipment, creating obvious blind spots.

[0007] To solve the above-mentioned technical problems, the present invention provides the following technical solution: an air traffic police aircraft, comprising: a main structure including a cabin, a phased array radar fixedly connected to one side of the bottom of the cabin, a storage compartment opened at the bottom of the cabin, a panoramic camera installed at the bottom of the storage compartment, a protective component installed at the top of the panoramic camera, a spectrum monitoring device installed on one side of the panoramic camera and fixedly connected to the cabin, an ADS-B receiver installed on one side of the spectrum monitoring device and fixedly connected to the cabin, and a multi-band relay radio fixedly connected to the top of the cabin; and a folding assembly including wings fixedly connected to both sides of the cabin, a folding groove opened at the bottom of the wing, a landing gear installed in the inner cavity of the folding groove, a hinge seat hinged to a corresponding side of the landing gear and fixedly connected to the inner cavity of the folding groove, and folding parts installed on the surface of the landing gear.

[0008] In a preferred embodiment of the aerial traffic police aircraft of the present invention, the protective component includes a movable plate fixedly connected to the top of the panoramic camera, a threaded sleeve fixedly connected to the top of the movable plate, and a drive unit provided on the top of the threaded sleeve.

[0009] In a preferred embodiment of the aerial traffic police aircraft of the present invention, the drive unit includes a motor fixedly connected to the top of the inner cavity of the storage compartment, the output shaft of the motor is fixedly connected to a lead screw, the bottom of the lead screw passes through a threaded sleeve and is threadedly connected to the threaded sleeve.

[0010] In a preferred embodiment of the aerial traffic police aircraft of the present invention, support rods are provided on both sides of the motor and are fixedly connected to the top of the inner cavity of the storage compartment. The bottom of the support rod passes through a threaded sleeve and is slidably connected to the threaded sleeve.

[0011] As a preferred embodiment of the air traffic police aircraft of the present invention, the side wall of the cabin is provided with a cavity, the inner cavity of the cavity is provided with a swing rod, a corresponding side of the swing rod penetrates the cavity and is fixedly connected to a sealing plate, a gear is fixedly connected to the surface of the swing rod, a corresponding side of the gear penetrates the cavity and extends into the storage compartment, the surface of the gear is rotatably connected to the inner cavity of the storage compartment, a toothed plate is meshed with a corresponding side of the gear and is fixedly connected to a movable plate.

[0012] In a preferred embodiment of the aerial traffic police aircraft of the present invention, a slider is fixedly connected to a corresponding side of the toothed plate, and a groove is provided in the inner cavity of the storage compartment, which cooperates with the slider.

[0013] In a preferred embodiment of the air traffic police aircraft of the present invention, the folding component includes guide rails fixedly connected to both sides of the top of the movable plate, guide wheels are slidably connected to the inner cavity of the guide rails, and bending rods are rotatably connected to the surface of the guide wheels and fixedly connected to the landing gear.

[0014] In a preferred embodiment of the aerial traffic police aircraft of the present invention, the surface of the sealing plate is provided with a limiting groove and cooperates with the bending rod.

[0015] As a preferred embodiment of the air traffic police aircraft of the present invention, the storage compartment has a first through slot on both sides of its inner cavity, and the wing has a second through slot on the corresponding side, which cooperates with the first through slot.

[0016] As a preferred embodiment of the air traffic police aircraft of the present invention, a docking block is fixedly connected to a corresponding side of the sealing plate surface, docking grooves are provided on both sides of the cabin, and ball bearings are rotatably connected to both sides of the docking block and in contact with the inner cavity of the docking groove.

[0017] The beneficial effects of this invention are as follows: By integrating an active phased array radar, a panoramic camera, a spectrum monitoring device, and an ADS-B / 1090ES receiver into the main structure, the invention collaboratively captures and identifies the legitimacy of targets; intelligent skin avoids electromagnetic interference; and a multi-band relay radio establishes an emergency airborne base station, thereby improving monitoring accuracy and scene adaptability. By using folding components to drive the landing gear retraction, blind spots in shooting are completely eliminated. Combined with protective components and equipment, this enables efficient management and control of unauthorized drones, thus balancing monitoring stability and equipment safety, and strengthening the comprehensive capabilities of air traffic control. Attached Figure Description

[0018] To more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the following description of the embodiments will be briefly introduced. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a structural diagram of an aerial traffic police aircraft.

[0020] Figure 2 This is a structural diagram of an aerial traffic police aircraft from another perspective.

[0021] Figure 3 This is a cross-sectional view of the cabin and wings of an air traffic police aircraft.

[0022] Figure 4 For air traffic police aircraft Figure 3 Enlarged view of region A in the middle.

[0023] Figure 5 This is a partial structural diagram of the protective and folding components of an air traffic police aircraft.

[0024] Figure 6 For air traffic police aircraft Figure 5 Enlarged view of region B in the middle.

[0025] Figure 7 This is a diagram showing the structural changes of an aerial traffic police aircraft from another perspective.

[0026] In the diagram: 1. Main structure; 2. Folding assembly; 11. Cabin; 12. Phased array radar; 13. Storage compartment; 14. Panoramic camera; 15. Protective components; 16. Spectrum monitoring equipment; 17. ADS-B receiver; 18. Multi-band relay radio; 21. Wing; 22. Folding slot; 23. Landing gear; 24. Hinge; 25. Folding component; 151. Movable plate; 152. Threaded sleeve; 153. Motor; 154. Lead screw; 155. Support rod; 156. Cavity; 157. Swing rod; 158. Sealing plate; 159. Gear; 1510. Toothed plate; 1511. Slider; 1512. Slide groove; 251. Guide rail; 252. Guide wheel; 253. Bending rod; 254. Limiting groove; 255. First through groove; 256. Second through groove; 1581. Docking block. Detailed Implementation

[0027] To make the above-mentioned objects, features and advantages of the present invention more apparent and understandable, the specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

[0028] Many specific details are set forth in the following description in order to provide a full understanding of the invention. However, the invention may also be practiced in other ways different from those described herein, and those skilled in the art can make similar extensions without departing from the spirit of the invention. Therefore, the invention is not limited to the specific embodiments disclosed below.

[0029] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that is mutually exclusive with other embodiments.

[0030] Example 1, referring to Figures 1-7This is the first embodiment of the present invention, which provides an air traffic police aircraft, including: a main structure 1, including a cabin 11, a phased array radar 12 fixedly connected to one side of the bottom of the cabin 11, a storage compartment 13 opened at the bottom of the cabin 11, a panoramic camera 14 installed at the bottom of the storage compartment 13, a protective component 15 installed at the top of the panoramic camera 14, a spectrum monitoring device 16 installed on one side of the panoramic camera 14 and fixedly connected to the cabin 11, an ADS-B receiver 17 installed on one side of the spectrum monitoring device 16 and fixedly connected to the cabin 11, and a multi-band relay radio 18 fixedly connected to the top of the cabin 11; and a folding assembly 2, including wings 21 fixedly connected to both sides of the cabin 11, a folding groove 22 opened at the bottom of the wings 21, a landing gear 23 installed in the inner cavity of the folding groove 22, a hinge seat 24 hinged to the corresponding side of the landing gear 23 and fixedly connected to the inner cavity of the folding groove 22, and a folding component 25 installed on the surface of the landing gear 23.

[0031] The drone features a built-in lift angle design, which shortens the takeoff distance. The bottom of the cabin 11 of the main structure 1 is the core monitoring area. The active phased array radar 12 is equipped with a phased array radar opening and closing door on the outside, which is driven by a sliding rail and a dedicated motor to achieve smooth sliding opening and closing. This ensures the detection field of view when the radar is in operation and can also be sealed and protected when not in use. The bottom of the cabin 11 has a corresponding storage compartment 13, which houses a panoramic camera 14. It is equipped with a spectrum monitoring device 16, an ADS-B / 1090ES receiver 17, and a multi-band relay radio 18 on one side. All devices are connected to the control module inside the cabin 11 through hidden electrical control circuits to form a collaborative monitoring network. The outer surface of the cabin 11 is covered with a smart skin with an internal electromagnetic shielding layer and interference suppression circuit to avoid electromagnetic interference between devices. The protective component 15 solves the protection problem of the panoramic camera 14 during flight and takeoff and landing, and also provides a structural basis for subsequent linkage with the folding component 2.

[0032] The folding component 2 achieves the folding and storage of the landing gear 23 through structures such as the wing 21 and folding slot 22, eliminating the obstruction of the camera component's shooting and improving the monitoring accuracy in conjunction with the main monitoring equipment.

[0033] The cabin 11, phased array radar 12, panoramic camera 14, spectrum monitoring equipment 16, ADS-B receiver 17, multi-band relay radio 18, wing 21 and landing gear 23 are all existing technologies, which are clearly known to those skilled in the art, and will not be described in detail here.

[0034] Example 2, refer to Figures 1-7 This is the second embodiment of the present invention, which is based on the previous embodiment.

[0035] Specifically, the protective component 15 includes a movable plate 151 fixedly connected to the top of the panoramic camera 14, a threaded sleeve 152 fixedly connected to the top of the movable plate 151, and a drive unit provided on the top of the threaded sleeve 152.

[0036] The protective component 15 includes a movable plate 151 and a threaded sleeve 152 fixed to the top of the panoramic camera 14. The movable plate 151 can drive the panoramic camera 14 to rise and fall along the storage compartment 13. When it extends out of the storage compartment 13, it can be used for 360-degree shooting without blind spots. When it retracts, the sealing plate 158 prevents debris from damaging the lens. The threaded sleeve 152 serves as the core of power transmission and cooperates precisely with the top drive unit to achieve smooth raising and lowering of the panoramic camera 14.

[0037] Specifically, the drive unit includes a motor 153 fixedly connected to the top of the inner cavity of the storage compartment 13. The output shaft of the motor 153 is fixedly connected to a lead screw 154. The bottom of the lead screw 154 passes through a threaded sleeve 152 and is threadedly connected to the threaded sleeve 152.

[0038] The drive unit includes a motor 153 fixed to the top of the inner cavity of the storage compartment 13. The output shaft of the motor 153 is fixed to a lead screw 154, which is threadedly connected to a threaded sleeve 152, converting the rotational motion into linear motion, thereby driving the movable plate 151 and the panoramic camera 14 to rise and fall smoothly.

[0039] Specifically, the motor 153 has support rods 155 on both sides and is fixedly connected to the top of the inner cavity of the storage compartment 13. The bottom of the support rod 155 passes through the threaded sleeve 152 and is slidably connected to the threaded sleeve 152.

[0040] The support rod 155 is symmetrically fixed on both sides of the main motor 153, and the bottom passes through the threaded sleeve 152 and is slidably connected to it, forming a two-way guide structure to restrict the rotation tendency of the threaded sleeve 152 and ensure that the movement path of the threaded sleeve 152 is correct.

[0041] Specifically, the side wall of the cabin 11 has a cavity 156. A swing rod 157 is provided in the inner cavity of the cavity 156. A corresponding side of the swing rod 157 passes through the cavity 156 and is fixedly connected to a sealing plate 158. A gear 159 is fixedly connected to the surface of the swing rod 157. A corresponding side of the gear 159 passes through the cavity 156 and extends into the storage compartment 13. The surface of the gear 159 is rotatably connected to the inner cavity of the storage compartment 13. A toothed plate 1510 meshes with a corresponding side of the gear 159 and is fixedly connected to the movable plate 151.

[0042] The cavity 156 has a built-in swing rod 157 and gear 159. One end of the swing rod 157 is connected to the sealing plate 158, and the other end is engaged with the gear plate 1510 through the gear 159. The gear plate 1510 is fixed to the movable plate 151, forming a linkage mechanism of "panoramic camera 14 lifting and closing - sealing plate 158 opening and closing". When the sealing plate 158 is closed, it seals the entire storage compartment 13 to prevent debris from entering during lifting and lowering.

[0043] Specifically, a slider 1511 is fixedly connected to the corresponding side of the toothed plate 1510, and a groove 1512 is provided in the inner cavity of the storage compartment 13, which cooperates with the slider 1511.

[0044] The slider 1511 is fixed to one side of the toothed plate 1510 and slides along the groove 1512 in the inner cavity of the storage compartment 13 to provide guidance and limit for the toothed plate 1510, ensuring that it meshes precisely with the gear 159, thereby ensuring the synchronization of the actions of the sealing plate 158 and the panoramic camera 14.

[0045] Specifically, the folding component 25 includes guide rails 251 fixedly connected to both sides of the top of the movable plate 151. Guide wheels 252 are slidably connected to the inner cavity of the guide rails 251. A bending rod 253 is rotatably connected to the surface of the guide wheel 252 and is fixedly connected to the landing gear 23.

[0046] The guide rail 251 of the folding component 25 is fixed to the top of the movable plate 151. The guide wheel 252 slides along the guide rail 251, driving the bending rod 253 to drive the landing gear 23 to rotate around the hinge seat 24 and fold into the folding slot 22 of the wing 21. This structure is linked with the panoramic camera 14 to ensure that the landing gear 23 folds synchronously when the panoramic camera 14 extends, eliminating blind spots and ensuring that the panoramic camera 14 can capture 360 ​​degrees without blind spots, providing an unobstructed field of view for image combination recognition of black-flying drones.

[0047] Specifically, a limiting groove 254 is provided on the surface of the sealing plate 158, and it cooperates with the bending rod 253.

[0048] The limiting groove 254 is opened on the surface of the sealing plate 158 and precisely matches the bending rod 253. After the landing gear 23 is folded, the bending rod 253 is engaged in the limiting groove 254, which can form a limit to prevent the landing gear 23 from being accidentally deployed due to the disturbance of the airflow during flight. This not only prevents the camera's field of vision from being obstructed, but also ensures the aerodynamic stability of the fuselage.

[0049] Specifically, the storage compartment 13 has a first through slot 255 on both sides of its inner cavity, and the wing 21 has a second through slot 256 on the corresponding side, which cooperates with the first through slot 255.

[0050] The two through slots connect the storage compartment 13 and the folding slot 22, providing ample space for the bending rod 253 to move, avoiding structural interference, ensuring smooth linkage of various components, and improving the overall reliability of the mechanism.

[0051] Working principle: During the takeoff preparation phase, the UAV with its own lift angle achieves short-distance takeoff. The intelligent skin on the outer surface of the cabin 11 activates the electromagnetic shielding function. The control module links the self-test of each device through the hidden electronic control circuit. The phased array radar 12, spectrum monitoring equipment 16, ADS-B / 1090ES receiver 17, and multi-band relay radio 18 start up simultaneously. The radar drive motor drives the phased array radar 12 to open and close the door through the slide rail to prepare for detection. The multi-band relay radio 18 sets up a temporary airborne base station to cover the disaster-stricken area without signal.

[0052] During the collaborative detection phase, the main motor 153 is activated. The output shaft of motor 153 drives the lead screw 154 to rotate, which in turn drives the threaded sleeve 152 to move smoothly down along the support rod 155, causing the movable plate 151 and the panoramic camera 14 to move out of the storage compartment 13. At the same time, the movable plate 151 drives the toothed plate 1510 to move synchronously, causing the gear 159 to rotate. This drives the swing rod 157 to open the sealing plate 158, at which point the docking block 1581 slides along the docking groove to ensure smooth operation. Simultaneously, the movable plate 151 drives the guide rail 251 to move down, and the guide wheel 252 drives the bending mechanism. The lever 253 drives the landing gear 23 to fold into the folding slot 22 with the hinge 24 as the center. Then, the bending lever 253 is locked into the limiting slot 254 of the sealing plate 158. At this time, the active phased array radar 12 scans and detects the position of the black flying UAV, the spectrum monitoring equipment 16 captures its radio signals, and the panoramic camera 14 captures the image. The control module combines them to form a complete image of the monitoring area. The data fusion of the three improves the monitoring accuracy. The ADS-B / 1090ES receiver 17 captures the signals of the surrounding legal aircraft, providing a basis for subsequent identification.

[0053] During the data identification and transmission phase, the control module compares the data acquired by the phased array radar 12, camera components, and spectrum monitoring equipment 16 with the legitimate signals captured by the ADS-B / 1090ES receiver 17 to determine whether the detected target is an unauthorized drone. After accurate identification, the data is transmitted to the ground control terminal via the multi-band relay radio 18. If the area is in a disaster-stricken area with no signal, the multi-band relay radio 18 continuously provides temporary signal coverage to ensure the transmission of control commands. During this process, the intelligent skin and all shielding structures work throughout to avoid electromagnetic interference and ensure data accuracy.

[0054] When the drone is preparing to land, motor 153 rotates in the reverse direction, driving panoramic camera 14 to retract into storage compartment 13. Tooth plate 1510 drives gear 159 and swing rod 157 in the reverse direction, causing sealing plate 158 to close and radar door to close synchronously. At the same time, guide rail 251 moves upward, bending rod 253 disengages from limit groove 254, landing gear 23 unfolds to support fuselage, and resets. Intelligent skin and all equipment go into sleep mode synchronously to ensure equipment safety.

[0055] Example 3, referring to Figure 5 This is the third embodiment of the present invention, which is based on the first two embodiments.

[0056] Specifically, a docking block 1581 is fixedly connected to one side of the surface of the sealing plate 158, and docking grooves are provided on both sides of the engine compartment 11. Ball bearings are rotatably connected to both sides of the docking block 1581 and are in contact with the inner cavity of the docking groove.

[0057] The docking block 1581 is fixed to one side of the sealing plate 158 and precisely matches the docking groove of the engine compartment 11. It can support the sealing plate 158, while the ball bearings on both sides convert sliding friction into rolling friction, ensuring that the sealing plate 158 opens and closes quickly.

[0058] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit it. Although the present invention has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, and all such modifications or substitutions should be covered within the scope of the claims of the present invention.

Claims

1. An aerial traffic police aircraft, characterized in that: include, The main structure (1) includes a cabin (11), a phased array radar (12) is fixedly connected to one side of the bottom of the cabin (11), a storage compartment (13) is opened at the bottom of the cabin (11), a panoramic camera (14) is installed at the bottom of the storage compartment (13), a protective part (15) is installed on the top of the panoramic camera (14), a spectrum monitoring device (16) is installed on one side of the panoramic camera (14) and is fixedly connected to the cabin (11), an ADS-B receiver (17) is installed on one side of the spectrum monitoring device (16) and is fixedly connected to the cabin (11), and a multi-band relay radio (18) is fixedly connected to the top of the cabin (11); and, The folding assembly (2) includes wings (21) fixedly connected to both sides of the cabin (11). The bottom of the wings (21) is provided with a folding groove (22). The inner cavity of the folding groove (22) is provided with a landing gear (23). A hinge seat (24) is hinged to the corresponding side of the landing gear (23) and fixedly connected to the inner cavity of the folding groove (22). The surface of the landing gear (23) is provided with a folding piece (25).

2. The aerial traffic police aircraft as described in claim 1, characterized in that: The protective component (15) includes a movable plate (151) fixedly connected to the top of the panoramic camera (14), a threaded sleeve (152) fixedly connected to the top of the movable plate (151), and a drive unit provided on the top of the threaded sleeve (152).

3. The aerial traffic police aircraft as described in claim 2, characterized in that: The drive unit includes a motor (153) fixedly connected to the top of the inner cavity of the storage compartment (13). The output shaft of the motor (153) is fixedly connected to a lead screw (154). The bottom of the lead screw (154) passes through a threaded sleeve (152) and is threadedly connected to the threaded sleeve (152).

4. The aerial traffic police aircraft as described in claim 3, characterized in that: The motor (153) is provided with support rods (155) on both sides and is fixedly connected to the top of the inner cavity of the storage compartment (13). The bottom of the support rod (155) passes through the threaded sleeve (152) and is slidably connected to the threaded sleeve (152).

5. The aerial traffic police aircraft as described in claim 4, characterized in that: The side wall of the cabin (11) is provided with a cavity (156). A swing rod (157) is provided in the inner cavity of the cavity (156). A corresponding side of the swing rod (157) passes through the cavity (156) and is fixedly connected to a sealing plate (158). A gear (159) is fixedly connected to the surface of the swing rod (157). A corresponding side of the gear (159) passes through the cavity (156) and extends into the storage compartment (13). The surface of the gear (159) is rotatably connected to the inner cavity of the storage compartment (13). A toothed plate (1510) meshes with a corresponding side of the gear (159) and is fixedly connected to a movable plate (151).

6. The aerial traffic police aircraft as described in claim 5, characterized in that: A slider (1511) is fixedly connected to the corresponding side of the toothed plate (1510), and a groove (1512) is provided in the inner cavity of the storage compartment (13), which cooperates with the slider (1511).

7. The aerial traffic police aircraft as described in claim 1, characterized in that: The folding component (25) includes guide rails (251) fixedly connected to the top two sides of the movable plate (151). The inner cavity of the guide rails (251) is slidably connected to guide wheels (252). The surface of the guide wheels (252) is rotatably connected to bending rods (253) and fixedly connected to the landing gear (23).

8. The aerial traffic police aircraft as described in claim 5, characterized in that: The sealing plate (158) has a limiting groove (254) on its surface, which cooperates with the bending rod (253).

9. The aerial traffic police aircraft as described in claim 1, characterized in that: The storage compartment (13) has a first through slot (255) on both sides of its inner cavity, and the wing (21) has a second through slot (256) on the corresponding side, which cooperates with the first through slot (255).

10. The aerial traffic police aircraft as described in claim 8, characterized in that: A docking block (1581) is fixedly connected to one side of the surface of the sealing plate (158). A docking groove is provided on both sides of the cabin (11). Ball bearings are rotatably connected to both sides of the docking block (1581) and are in contact with the inner cavity of the docking groove.

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