A UAV status detection platform based on multi-sensor

Abstract

The invention discloses a multi-sensor based unmanned aerial vehicle state detection platform, which relates to the technical field of unmanned aerial vehicle detection, and comprises: a detection platform, on the upper surface of which an input conveyor belt, a clamping moving component, a main detection component, two transfer conveyor components, a secondary detection component and an output conveyor belt are horizontally fixedly arranged, one side of the input conveyor belt is provided with a transfer conveyor component, the other side is provided with a main detection component, and the other side of the main detection component is provided with another transfer conveyor component; the clamping moving component is arranged above the transfer conveyor component on one side of the input conveyor belt and the main detection component, and is fixedly assembled on one side of the detection platform; the secondary detection component is arranged in parallel with the input conveyor belt and placed between the two transfer conveyor components; a unmanned aerial vehicle fixing ring is horizontally placed on the upper surface of the input conveyor belt; autonomous detection can be performed through automated operation, so as to make an effective evaluation of the unmanned aerial vehicle to prevent it from being potentially dangerous.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle detection, and in particular to a multi-sensor based unmanned aerial vehicle state detection platform. Background Art

[0002] For some warehouse management equipment with drones as the core, it usually involves the management of drones’ outbound and inbound storage. When drones are put into storage, they need to be comprehensively inspected and evaluated to analyze the potential dangers generated during the outbound process, and formulate appropriate maintenance plans based on these dangers to ensure the integrity of the drone functions in the warehouse.

[0003] However, the existing testing platforms can only test the appearance of the drone and whether it can take off, but cannot test potential problems such as the stability, flight attitude, and operating efficiency of the drone. At the same time, the testing agencies on the market for this type usually require a larger site and have high requirements for wireless signals. They are not suitable for most warehouse management and may cause secondary damage to the drone during the testing process. At the same time, the existing equipment cannot simulate the performance of drones under wind conditions.

[0004] Therefore, it is necessary to provide a multi-sensor based UAV status detection platform to solve the above problems. Summary of the invention

[0005] To achieve the above object, the present invention provides the following technical solution, a multi-sensor based drone status detection platform, comprising:

[0006] The detection platform has an input conveyor belt, a clamping moving assembly, a main detection assembly, two transfer conveyor assemblies, a secondary detection assembly and an output conveyor belt fixedly arranged horizontally on its upper surface, wherein the transfer conveyor assembly is arranged on one side of the input conveyor belt, the main detection assembly is arranged on the other side, and another transfer conveyor assembly is arranged on the other side of the main detection assembly;

[0007] A clamping moving assembly is arranged above the transfer conveying assembly on one side of the input conveyor belt and the main detection assembly, and is fixedly assembled on one side surface of the detection platform;

[0008] The auxiliary detection assembly is arranged parallel to the input conveyor belt and is placed between the two transfer conveyor assemblies;

[0009] An output conveyor belt is coaxially arranged with the auxiliary detection assembly and is placed on the other side of the transfer conveyor assembly adjacent to the input conveyor belt;

[0010] The drone fixing ring is placed horizontally on the upper surface of the input conveyor belt.

[0011] Preferably, an elastic rubber ring is fixedly provided on the inner side of the drone fixing ring.

[0012] Preferably, the clamping moving assembly includes a fixed frame, which is fixedly mounted on one side surface of the detection platform, and the upper surface of the fixed frame is fixedly mounted with two parallel first rails, and two first sliders are slidably mounted on the two first rails, and a clamping claw is fixedly mounted on the upper surface of each first slider, and the two clamping claws are mirror-imaged.

[0013] Preferably, the main detection component comprises:

[0014] A cylindrical detection chamber is fixedly mounted on the upper surface of the detection platform. The cylindrical detection chamber is in the shape of a regular triangular prism, and a closing plate is provided on the top, bottom and side parallel to the clamping moving component, and a rolling shutter opening and closing door is fixedly embedded on the other two side surfaces;

[0015] A temperature and humidity regulator, fixedly embedded on a closing plate provided on the side of the cylindrical detection chamber;

[0016] An ultrasonic sensor is fixedly mounted on a sealing plate provided at the top of the cylindrical detection chamber;

[0017] Two optical sensors and one infrared sensor are fixedly mounted on a closing plate arranged at the bottom of the columnar detection chamber, and the two optical sensors are arranged on both sides of the infrared sensor.

[0018] Preferably, the columnar detection bin comprises a detection bin support frame, the inner sides of the three vertical support columns of the detection bin support frame are vertically fixed with second tracks, two second sliders are slidably arranged on each second track, the two second sliders are vertically arranged, and universal connectors are arranged on both sides of each second slider, a telescopic rod is hinged on each universal connector, and another universal connector is hinged on the other end of each telescopic rod, and the universal connectors hinged on the other ends of the two telescopic rods connected to the second sliders at the upper end are fixed on the outer ring surface of the fixed ring frame;

[0019] The universal joints hinged at the other ends of the two telescopic rods connected to the second sliding block at the lower end are all fixed on the outer side surface of the wind control component.

[0020] Preferably, an automatic locker is provided on the inner ring surface of the fixing ring frame, which can be locked with the fixing ring of the drone.

[0021] Preferably, a tension sensor is provided at the extension point of each telescopic rod.

[0022] Preferably, the wind force regulating component comprises a fixed bearing block, the fixed bearing block is fixedly arranged between the six universal joints of the six telescopic rods at the lower end away from the corresponding second sliding block, a through hole is arranged in the middle of the fixed bearing block, a fixed ring is fixedly assembled in the through hole, two driving motors are fixedly embedded on the fixed ring, the two driving motors are arranged in a mirror image, and their output shafts are fixedly assembled on the rotating ring, the rotating ring is fixedly embedded with another two driving motors, the other two driving motors are arranged in a mirror image, and their output shafts are fixedly assembled on the hair dryer;

[0023] The included angle between the central axes of the four driving motors is a right angle.

[0024] Preferably, the transfer conveying assembly comprises a fixed plate, the fixed plate is fixedly mounted on the upper surface of the detection platform, a third track is fixedly mounted on the upper surface of the fixed plate, a third slider is slidably mounted on the third track, and a movable conveyor belt is fixedly mounted on the upper surface of the third slider;

[0025] Two limiters are mirror-imaged and respectively fixedly assembled on the fixing plates at both ends of the third track.

[0026] Preferably, the secondary detection component comprises:

[0027] There are multiple fixed columns, all of which are fixedly assembled on the upper surface of the detection platform. A conveyor belt is horizontally arranged on the upper ends of the multiple fixed columns. A software function detection mechanism, a battery performance detection mechanism, a communication system detection mechanism and a drone clamping and separation mechanism are arranged above the conveyor belt. The software function detection mechanism, the battery performance detection mechanism, the communication system detection mechanism and the drone clamping and separation mechanism are all fixedly assembled on the detection platform on the side of the conveyor belt away from the input conveyor belt.

[0028] The drone fixing ring clamp is fixedly assembled on the conveyor belt and placed between the drone clamping and separating mechanism and the conveyor belt.

[0029] Compared with the prior art, the present invention provides a multi-sensor based drone status detection platform, which has the following beneficial effects:

[0030] The present invention places the drone to be inspected horizontally in a drone fixing ring, and can perform autonomous inspection through automated operation. The platform divides the inspection of the drone into a main inspection component for inspection in a flying state and a secondary inspection component for inspection in a stationary state. In addition, multiple inspection mechanisms or sensors are provided in both the main inspection component and the secondary inspection component to detect the actual condition of the drone, thereby making an effective assessment of the drone and preventing it from being potentially dangerous.

[0031] In the present invention, the main detection component can be controlled to move through the six second sliders and the corresponding six telescopic rods arranged at the upper end, so that the fixed ring frame can move synchronously with the motion trajectory of the drone. The synchronous follow-up of the fixed ring frame can ignore its influence on the drone, and in the case that the drone is out of control due to damage, the drone will have a tendency to deviate from the trajectory. At this time, the fixed ring frame will firmly control the drone in this position to prevent the drone from losing control and causing further damage. The six second sliders and the corresponding six telescopic rods arranged below it will adjust the position of the wind control component, thereby adjusting the wind direction, thereby simulating the external flight environment and ensuring the accuracy of the detection. The temperature and humidity adjustment arranged therein The device can adjust the temperature and humidity inside the main detection component, simulate different temperature and humidity conditions, and evaluate the environmental adaptability of the drone. The ultrasonic sensor can measure the actual position of the drone during flight, so as to determine its flight stability and maneuverability. The optical sensor captures images and videos of the drone, and through image recognition technology, it can identify the model, color and other features of the drone, so as to detect whether there is any damage to the appearance of the drone. The infrared sensor can detect the heat distribution of the drone, so as to identify the position and status of the drone, and further ensure the detection of the flight stability and maneuverability of the drone. In actual work, the number and type of sensors can be changed according to actual detection needs.

[0032] In the present invention, the auxiliary detection component can evaluate the stability and reliability of the drone operating system and application software through the software function detection mechanism, the battery performance detection mechanism can detect the battery capacity, discharge rate, charging time, etc., and the communication system detection mechanism can evaluate the communication capability between the drone and the ground control station. After the detection is completed, the drone fixing ring clamp 77 will clamp the drone fixing ring, and the drone clamping and separation mechanism will clamp the drone to separate the drone and the drone fixing ring, and then the conveyor belt will start, the drone fixing ring clamp and the drone clamping and separation mechanism will respectively place the drone fixing ring and the drone on the conveyor belt, so that the drone fixing ring and the drone are arranged front and back in the running direction of the conveyor belt. In actual work, the number and type of detection mechanisms can be changed according to actual detection needs. BRIEF DESCRIPTION OF THE DRAWINGS

[0033] Figure 1 It is a schematic diagram of the overall structure of a multi-sensor based UAV status detection platform;

[0034] Figure 2 It is a structural schematic diagram of the clamping and moving assembly in the present invention;

[0035] Figure 3 It is a structural schematic diagram of the main detection component in the present invention;

[0036] Figure 4It is a structural schematic diagram of the cylindrical detection chamber in the present invention;

[0037] Figure 5 It is a structural schematic diagram of the wind force control component in the present invention;

[0038] Figure 6 It is a structural schematic diagram of the transfer and conveying assembly in the present invention;

[0039] Figure 7 It is a structural schematic diagram of the auxiliary detection component in the present invention;

[0040] In the figure: 1. Detection platform; 2. Input conveyor belt; 3. Drone fixing ring; 4. Clamping and moving assembly; 5. Main detection assembly; 6. Transfer conveyor assembly; 7. Auxiliary detection assembly; 8. Output conveyor belt; 41. Fixed frame; 42. First track; 43. First slider; 44. Clamping claw; 51. Columnar detection chamber; 52. Rolling shutter door; 53. Temperature and humidity regulator; 54. Ultrasonic sensor; 55. Optical sensor; 56. Infrared sensor; 511. Detection chamber support frame; 512. Second track; 513. Second slider; 514. Universal joint Head; 515, telescopic rod; 516, fixed ring frame; 517, wind control component; 5171, fixed bearing block; 5172, fixed ring; 5173, driving motor; 5174, rotating ring; 5175, hair dryer; 61, fixed plate; 62, third track; 63, third slider; 64, moving conveyor belt; 65, limiter; 71, fixed column; 72, conveyor belt; 73, software function detection mechanism; 74, battery performance detection mechanism; 75, communication system detection mechanism; 76, drone clamping and separation mechanism; 77, drone fixed ring clamp. DETAILED DESCRIPTION

[0041] See also Figure 1 to Figure 7 The present invention provides a multi-sensor based UAV status detection platform, comprising:

[0042] The detection platform 1 has an input conveyor belt 2, a clamping moving component 4, a main detection component 5, two transfer conveyor components 6, a secondary detection component 7 and an output conveyor belt 8 fixedly arranged horizontally on its upper surface, wherein the transfer conveyor component 6 is arranged on one side of the input conveyor belt 2, and the main detection component 5 is arranged on the other side, and another transfer conveyor component 6 is arranged on the other side of the main detection component 5;

[0043] The clamping moving assembly 4 is arranged above the transfer conveying assembly 6 on one side of the input conveyor belt 2 and the main detection assembly 5, and is fixedly assembled on one side surface of the detection platform 1;

[0044] The auxiliary detection assembly 7 is arranged parallel to the input conveyor belt 2 and is placed between the two transfer conveyor assemblies 6;

[0045] The output conveyor belt 8 is coaxially arranged with the auxiliary detection assembly 7 and is placed on the other side of the transfer conveyor assembly 6 adjacent to the input conveyor belt 2;

[0046] The drone fixing ring 3 is horizontally placed on the upper surface of the input conveyor belt 2;

[0047] As a preferred embodiment, the drone to be detected is placed horizontally in the drone fixing ring 3, and the drone fixing ring 3 will be mounted on the outside of the drone without affecting the flight of the drone. Then the input conveyor belt 2 is started, and the drone fixing ring 3 with the drone mounted on it is moved toward the main detection component 5 until it moves to the limit position of the input conveyor belt 2. The clamping moving component 4 will start to clamp the drone fixing ring 3 and place it in the main detection component 5. The main detection component 5 will detect the drone by changing the internal temperature and humidity, wind force, wind direction and other conditions when the drone is flying, and effectively record it through various sensors in the main detection component 5. Then the clamping moving component 4 will move the drone fixing ring 3 (and the drone on it) that has completed the preliminary detection. Machine), clamped by the main detection component 5 to its adjacent transfer and conveying component 6, the transfer and conveying component 6 will convey the drone fixing ring 3 (and the drone thereon) to the auxiliary detection component 7, the auxiliary detection component 7 will perform targeted detection on the drone in a stationary state, the detection result will be comprehensively analyzed with the detection result of the main detection component 5, and the various performances of the drone will be evaluated in combination with the detection data, thereby avoiding potential dangers of the drone, and after the detection is completed, the drone and the drone fixing ring 3 will be separated, and another transfer and conveying component 6 will convey the separated drone to the output conveyor belt 8, which will be sent out of the device, and the transfer and conveying component 6 will convey the separated drone fixing ring 3 to the input conveyor belt 2 to continue working.

[0048] Furthermore, an elastic rubber ring is fixedly arranged inside the drone fixing ring 3;

[0049] As a preferred embodiment, the setting of the elastic rubber ring can make the inner ring of the drone fixing ring 3 have a certain degree of variability, so that it can fix drones of different models, and at the same time avoid damage to the drone caused by relative friction between the drone fixing ring 3 and the drone during the detection process.

[0050] Furthermore, the clamping and moving assembly 4 includes a fixed frame 41, which is fixedly mounted on one side of the detection platform 1, and the upper surface of the fixed frame 41 is fixedly mounted with two parallel first rails 42, and two first sliders 43 are slidably mounted on the two first rails 42, and a clamping claw 44 is fixedly mounted on the upper surface of each first slider 43, and the two clamping claws 44 are mirror-imaged.

[0051] Further, the main detection component 5 includes:

[0052] A cylindrical detection chamber 51 is fixedly mounted on the upper surface of the detection platform 1. The cylindrical detection chamber 51 is in the shape of a regular triangular prism, and a closing plate is provided at the top, bottom and side parallel to the clamping moving assembly 4, and a rolling shutter opening and closing door 52 is fixedly embedded on the other two side surfaces;

[0053] A temperature and humidity regulator 53 is fixedly mounted on a sealing plate provided on the side of the cylindrical detection chamber 51;

[0054] The ultrasonic sensor 54 is fixedly mounted on a sealing plate disposed at the top of the cylindrical detection chamber 51;

[0055] Two optical sensors 55 and an infrared sensor 56 are fixedly mounted on a closed plate at the bottom of the cylindrical detection chamber 51, and the two optical sensors 55 are arranged on both sides of the infrared sensor 56;

[0056] As a preferred embodiment, the two rolling shutter doors 52 may not affect the UAV fixing ring 3 (and the UAV thereon) from entering and exiting the main detection component 5 when in the open state, and may form a closed space with the cylindrical detection chamber 51 when in the closed state, thereby facilitating the temperature and humidity regulator 53 to adjust the temperature and humidity inside the main detection component 5, simulate different temperature and humidity conditions, and evaluate the environmental adaptability of the UAV. The ultrasonic sensor 54 may measure the actual position of the UAV during flight, thereby determining its flight stability and maneuverability. The optical sensor 55 may capture images and videos of the UAV, and may identify the model, color and other features of the UAV through image recognition technology, thereby detecting whether the appearance of the UAV is damaged. The infrared sensor 56 may detect the heat distribution of the UAV, thereby identifying the position and state of the UAV, further ensuring the detection of the flight stability and maneuverability of the UAV. In actual work, the number and type of sensors may be changed according to actual detection requirements.

[0057] Further, the columnar detection chamber 51 includes a detection chamber support frame 511, and the inner sides of the three vertical support columns of the detection chamber support frame 511 are vertically fixed with second rails 512, and two second sliders 513 are slidably arranged on each second rail 512, and the two second sliders 513 are vertically arranged, and universal connectors 514 are arranged on both sides of each second slider 513, and each universal connector 514 is hinged with a telescopic rod 515, and the other end of each telescopic rod 515 is hinged with another universal connector 514, and the universal connectors 514 hinged at the other ends of the two telescopic rods 515 connected to the second sliders 513 at the upper end are fixed on the outer ring surface of the fixed ring frame 516;

[0058] The universal joints 514 hinged at the other ends of the two telescopic rods 515 connected to the second slider 513 at the lower end are fixed on the outer surface of the wind control component 517;

[0059] As a preferred embodiment, the clamping and moving component 4 will clamp the drone fixing ring 3 (and the drone thereon) and place it horizontally in the fixing ring frame 516. When the drone is controlled to take off, the fixing ring frame 516 will be controlled to move through the six second sliders 513 and the corresponding six telescopic rods 515 arranged at the upper end, so that the fixing ring frame 516 follows the motion trajectory of the drone for synchronous movement, and the synchronous follow-up of the fixing ring frame 516 can ignore its influence on the drone, and in the case that the drone is out of control due to damage, the drone will have a tendency to deviate from the trajectory. At this time, the fixing ring frame 516 will firmly control the drone in this position to prevent the drone from losing control and causing further damage. The six second sliders 513 and the corresponding six telescopic rods 515 arranged below it will adjust the position of the wind control component 517, thereby adjusting the wind direction, thereby simulating the external flight environment and ensuring the accuracy of the detection.

[0060] Furthermore, an automatic locker is provided on the inner ring surface of the fixing ring frame 516, which can be locked with the drone fixing ring 3;

[0061] As a preferred embodiment, the automatic locker on the inner ring surface of the fixed ring frame 516 can maintain a relatively static state with the drone fixing ring 3 thereon in a locked state, and the controller of the automatic locker is on the two clamping claws 44. When the clamping claw 44 adjacent to the input conveyor belt 2 clamps the drone fixing ring 3 (and the drone thereon) and places it on the fixed ring frame 516, the controller on the clamping claw 44 will control the automatic locker to lock. When the clamping claw 44 adjacent to the transfer conveying component 6 clamps the drone fixing ring 3 (and the drone thereon) and detaches from the fixed ring frame 516, the controller on the clamping claw 44 will control the automatic locker to open, so as to facilitate the detachment of the fixed ring frame 516 from the drone fixing ring 3.

[0062] Furthermore, a tension sensor is provided at the extension position of each telescopic rod 515;

[0063] As a preferred embodiment, when the flight state of the UAV deviates from the predetermined trajectory, it will conflict with the operation of the fixed ring frame 516. Under the premise of ensuring that the fixed ring frame 516 runs according to the original trajectory, the telescopic rod 515 that deviates from the direction will be subjected to additional pressure. Therefore, the subtle state of the UAV can be detected by the tension sensor, thereby ensuring the accuracy of the UAV stability detection.

[0064] Further, the wind force regulating component 517 includes a fixed bearing block 5171, which is fixedly arranged between six universal joints 514 at one end of the six telescopic rods 515 at the lower end away from the corresponding second slider 513. A through hole is arranged in the middle of the fixed bearing block 5171, in which a fixed ring 5172 is fixedly assembled. Two driving motors 5173 are fixedly embedded on the fixed ring 5172. The two driving motors 5173 are arranged in a mirror image, and their output shafts are fixedly assembled on the rotating ring 5174. Another two driving motors 5173 are fixedly embedded on the rotating ring 5174. The other two driving motors 5173 are arranged in a mirror image, and their output shafts are fixedly assembled on the hair dryer 5175.

[0065] The included angle between the central axes of the four drive motors 5173 is a right angle;

[0066] As a preferred embodiment, the hair dryer 5175 can be adjusted to any angle through the rotation of four driving motors 5173, so as to simulate outdoor wind conditions more accurately and efficiently. At the same time, the hair dryer 5175 can control the wind speed conditions by adjusting its output efficiency.

[0067] Further, the transfer conveying assembly 6 includes a fixed plate 61, the fixed plate 61 is fixedly mounted on the upper surface of the detection platform 1, a third track 62 is fixedly mounted on the upper surface of the fixed plate 61, a third slider 63 is slidably arranged on the third track 62, and a moving conveyor belt 64 is fixedly arranged on the upper surface of the third slider 63;

[0068] The limiters 65 are provided in two mirror images and are respectively fixedly assembled on the fixing plates 61 at both ends of the third track 62;

[0069] As a preferred embodiment, the setting of the limiter 65 can limit the moving range of the movable conveyor belt 64, so that its central axis can coincide with the central axis positions of the input conveyor belt 2 and the conveyor belt 72 respectively at the positions of the two limiters 65.

[0070] Further, the auxiliary detection component 7 includes:

[0071] There are multiple fixed columns 71, all of which are fixedly assembled on the upper surface of the detection platform 1. A conveyor belt 72 is horizontally arranged on the upper ends of the multiple fixed columns 71. A software function detection mechanism 73, a battery performance detection mechanism 74, a communication system detection mechanism 75 and a drone clamping and separation mechanism 76 are arranged above the conveyor belt 72. The software function detection mechanism 73, the battery performance detection mechanism 74, the communication system detection mechanism 75 and the drone clamping and separation mechanism 76 are all fixedly assembled on the detection platform 1 on the side of the conveyor belt 72 away from the input conveyor belt 2;

[0072] The drone fixing ring clamp 77 is fixedly mounted on the conveyor belt 72 and placed between the drone clamping and separating mechanism 76 and the conveyor belt 72;

[0073] As a preferred embodiment, the software function detection mechanism 73 can evaluate the stability and reliability of the drone operating system and application software, the battery performance detection mechanism 74 can detect the battery capacity, discharge rate, and charging time, and the communication system detection mechanism 75 can evaluate the communication capability between the drone and the ground control station. After the detection is completed, the drone fixing ring clamp 77 will clamp the drone fixing ring 3, and the drone clamping and separation mechanism 76 will clamp the drone to separate the drone and the drone fixing ring 3, and then the conveyor belt 72 will start, and the drone fixing ring clamp 77 and the drone clamping and separation mechanism 76 will respectively place the drone fixing ring 3 and the drone on the conveyor belt 72 (so that the drone fixing ring 3 and the drone are arranged front and back in the running direction of the conveyor belt 72). In actual work, the number and type of detection mechanisms can be changed according to actual detection needs.

[0074] During the specific implementation, the following steps are included: the drone to be detected is horizontally placed in the drone fixing ring 3, and the drone fixing ring 3 is sleeved on the outside of the drone without affecting the flight of the drone, and then the input conveyor belt 2 is started, and the drone fixing ring 3 with the drone sleeved is moved toward the main detection component 5 until it moves to the limit position of the input conveyor belt 2, and the clamping moving component 4 is started to clamp the group of drone fixing rings 3 and place them in the main detection component 5, and the main detection component 5 will detect the drone by changing the internal temperature and humidity, wind force, wind direction and other conditions when the drone is flying, and effectively record it through a variety of sensors in the main detection component 5, and then the clamping moving component 4 will move the drone fixing ring 3 (and its upper The UAV) is clamped by the main detection component 5 to the adjacent transfer and conveying component 6, and the transfer and conveying component 6 will convey the UAV fixing ring 3 (and the UAV thereon) to the auxiliary detection component 7, and the auxiliary detection component 7 will perform targeted detection on the UAV in a stationary state, and the detection result will be comprehensively analyzed with the detection result of the main detection component 5, and the various performances of the UAV will be evaluated in combination with the detection data, so as to avoid potential dangers of the UAV. After the detection is completed, the UAV and the UAV fixing ring 3 are separated, and another transfer and conveying component 6 conveys the separated UAV to the output conveyor belt 8, which is sent out of the device by the output conveyor belt 8, and the transfer and conveying component 6 conveys the separated UAV fixing ring 3 to the input conveyor belt 2 to continue working.

[0075] What is described above is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes according to the technical scheme and inventive concept of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A multi-sensor based drone status detection platform, characterized in that: include: An inspection platform (1) has an input conveyor belt (2), a clamping moving assembly (4), a main inspection assembly (5), two transfer conveyor assemblies (6), a secondary inspection assembly (7) and an output conveyor belt (8) fixedly arranged horizontally on its upper surface, wherein the transfer conveyor assembly (6) is arranged on one side of the input conveyor belt (2), the main inspection assembly (5) is arranged on the other side, and another transfer conveyor assembly (6) is arranged on the other side of the main inspection assembly (5); A clamping and moving assembly (4) is arranged above the transfer conveying assembly (6) on one side of the input conveyor belt (2) and the main detection assembly (5), and is fixedly mounted on a side surface of the detection platform (1); A secondary detection component (7) is arranged parallel to the input conveyor belt (2) and is placed between the two transfer conveyor components (6); An output conveyor belt (8) is coaxially arranged with the auxiliary detection assembly (7) and is placed on the other side of the transfer conveyor assembly (6) adjacent to the input conveyor belt (2); A drone fixing ring (3) is horizontally placed on the upper surface of the input conveyor belt (2); The main detection component (5) comprises a columnar detection chamber (51), the columnar detection chamber (51) being fixedly mounted on the upper surface of the detection platform (1), the columnar detection chamber (51) being in the shape of a regular triangular prism, and having a sealing plate disposed at its top, bottom and side surfaces parallel to the clamping and moving component (4), and having rolling shutter opening and closing doors (52) fixedly embedded on its other two side surfaces; A temperature and humidity regulator (53) fixedly mounted on a sealing plate provided on a side of the cylindrical detection chamber (51); An ultrasonic sensor (54) is fixedly mounted on a sealing plate provided at the top end of the cylindrical detection chamber (51); Two optical sensors (55) and an infrared sensor (56) are fixedly mounted on a closed plate arranged at the bottom of the columnar detection chamber (51), and the two optical sensors (55) are arranged on both sides of the infrared sensor (56).

2. The multi-sensor based drone status detection platform according to claim 1, characterized in that: An elastic rubber ring is fixedly arranged on the inner side of the drone fixing ring (3).

3. The multi-sensor based drone status detection platform according to claim 1, characterized in that: The clamping moving assembly (4) comprises a fixed frame (41), the fixed frame (41) is fixedly mounted on a side surface of the detection platform (1), the upper surface of the fixed frame (41) is fixedly mounted with two first rails (42) arranged in parallel, two first sliders (43) are slidably mounted on the two first rails (42), a clamping claw (44) is fixedly mounted on the upper surface of each first slider (43), and the two clamping claws (44) are arranged in a mirror image.

4. The multi-sensor based drone status detection platform according to claim 1, characterized in that: The columnar detection chamber (51) comprises a detection chamber support frame (511), the inner sides of the three vertical support columns of the detection chamber support frame (511) are all vertically fixed with second rails (512), each second rail (512) is slidably provided with two second sliders (513), the two second sliders (513) are vertically provided, and both sides of each second slider (513) are provided with universal connectors (514), each universal connector (514) is hinged with a telescopic rod (515), the other end of each telescopic rod (515) is hinged with another universal connector (514), and the universal connectors (514) hinged at the other ends of the two telescopic rods (515) connected to the second sliders (513) at the upper end are both fixed to the outer ring surface of the fixed ring frame (516); The universal connectors (514) hinged at the other ends of the two telescopic rods (515) connected to the second sliding block (513) at the lower end are both fixed on the outer side surface of the wind force control component (517).

5. The multi-sensor based drone status detection platform according to claim 4, characterized in that: An automatic locker is provided on the inner ring surface of the fixed ring frame (516) and can be locked with the drone fixed ring (3).

6. The multi-sensor based drone status detection platform according to claim 4, characterized in that: A tension sensor is provided at the extension position of each telescopic rod (515).

7. The multi-sensor based drone status detection platform according to claim 4, characterized in that: The wind force control component (517) comprises a fixed bearing block (5171), wherein the fixed bearing block (5171) is fixedly arranged between six universal joints (514) at one end of the six telescopic rods (515) at the lower end away from the corresponding second slider (513); a through hole is arranged in the middle of the fixed bearing block (5171), and a fixed ring (5172) is fixedly assembled therein; two driving motors (5173) are fixedly embedded on the fixed ring (5172), the two driving motors (5173) are arranged in a mirror image, and their output shafts are fixedly assembled on the rotating ring (5174); another two driving motors (5173) are fixedly embedded on the rotating ring (5174), the other two driving motors (5173) are arranged in a mirror image, and their output shafts are fixedly assembled on the hair dryer (5175); The included angle between the central axes of the four drive motors (5173) is a right angle.

8. The multi-sensor based drone status detection platform according to claim 1, characterized in that: The transfer conveying assembly (6) comprises a fixed plate (61), the fixed plate (61) is fixedly mounted on the upper surface of the detection platform (1), a third track (62) is fixedly mounted on the upper surface of the fixed plate (61), a third slider (63) is slidably mounted on the third track (62), and a movable conveyor belt (64) is fixedly mounted on the upper surface of the third slider (63); Two limiters (65) are provided in mirror image and are respectively fixedly mounted on the fixing plates (61) at both ends of the third track (62).

9. The multi-sensor based drone status detection platform according to claim 1, characterized in that: The auxiliary detection component (7) comprises: A plurality of fixed columns (71) are provided, all of which are fixedly mounted on the upper surface of the detection platform (1); a conveyor belt (72) is horizontally arranged on the upper ends of the plurality of fixed columns (71); a software function detection mechanism (73), a battery performance detection mechanism (74), a communication system detection mechanism (75), and a drone clamping and separation mechanism (76) are arranged above the conveyor belt (72); the software function detection mechanism (73), the battery performance detection mechanism (74), the communication system detection mechanism (75), and the drone clamping and separation mechanism (76) are all fixedly mounted on the detection platform (1) on the side of the conveyor belt (72) away from the input conveyor belt (2); The drone fixing ring clamp (77) is fixedly mounted on the conveyor belt (72) and is placed between the drone clamping and separating mechanism (76) and the conveyor belt (72).

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