Unmanned aerial vehicle regular passing detection device

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle regular passing detection device which comprises an unmanned aerial vehicle body, wings are fixedly connected to the surface of the unmanned aerial vehicle body, top distance detection radars are fixedly connected to the tops of the wings, and bottom distance detection radars are fixedly connected to the bottoms of the wings. According to the utility model, in the flight process of the unmanned aerial vehicle body, the distance of an object is measured through the top distance detection radar and the bottom distance detection radar according to the electromagnetic wave reflection principle, a plurality of independent lenses are adopted by the spliced panoramic camera, and each lens shoots different visual angle images; and then the images are spliced through software to form a complete panoramic image, so that the distance between the specific distance between the unmanned aerial vehicle body and an obstacle is known, and when the travel path of the unmanned aerial vehicle body is planned, the driving route can be monitored through the infrared route detection device, the driving direction can be adjusted in real time, and safety is ensured.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field especially relates to a kind of unmanned plane rule direction passage detection device. BACKGROUND

[0002] The unmanned plane rule direction passage detection device is mainly used to monitor and check whether the unmanned plane flies according to the specified route and rules during flight, so as to ensure the safety and effective management of airspace. This device usually combines multiple technical means, including positioning, sensing, communication and intelligent algorithms, to realize real-time monitoring of the unmanned plane's trajectory, speed, flight height and other information.

[0003] When the unmanned plane is far away from the operator's field of view, most rely on the installed camera to observe the surrounding situation. When encountering complex air environment during flight, due to the limitation of the observation angle of the camera, and the fast flight speed of the unmanned plane, it is not possible to know the situation around the unmanned plane in the first time, and it is easy to cause the unmanned plane to crash into obstacles and cause damage to the unmanned plane. UTILITY MODEL CONTENT

[0004] To solve the above technical problems, the utility model provides an unmanned plane rule direction passage detection device.

[0005] The utility model adopts the following technical scheme to realize: an unmanned plane rule direction passage detection device, comprising an unmanned plane body, the unmanned plane body surface is fixedly connected with airfoil, the airfoil top is fixedly connected with top distance detection radar, the airfoil bottom is fixedly connected with bottom distance detection radar, the airfoil front is fixedly connected with infrared route detection device, the airfoil right side is fixedly connected with spliced panoramic camera, the unmanned plane body inner wall is fixedly connected with GPS positioning device.

[0006] As a further improvement of the above scheme, the airfoil is provided with four, the four airfoils are symmetrically arranged with the unmanned plane body as the center, the top distance detection radar is provided with four, the four top distance detection radars are symmetrically arranged with the center of the unmanned plane body, the bottom distance detection radar is provided with four, the four bottom distance detection radars are symmetrically arranged with the center of the unmanned plane body, the infrared route detection device is provided with four, the four infrared route detection devices are symmetrically arranged with the center of the unmanned plane body, the spliced panoramic camera is provided with four, and the four spliced panoramic cameras are symmetrically arranged with the center of the unmanned plane body.

[0007] Through the above technical scheme, the top distance detection radar and the bottom distance detection radar measure the distance of the object through the electromagnetic wave reflection principle during the flight of the unmanned aerial vehicle body, and then the spliced panoramic camera adopts multiple independent lenses, each lens shoots different angle images, and then the images are spliced through software to form a complete panoramic image, so that the distance between the unmanned aerial vehicle body and the obstacles is known.

[0008] As a further improvement of the above scheme, the unmanned aerial vehicle body is fixedly connected with an adjusting shell, a micro motor is fixedly connected to the inner wall bottom of the adjusting shell, a motor rotating rod is fixedly connected to the output end of the micro motor, and a gear is fixedly connected to the outer wall of the motor rotating rod.

[0009] As a further improvement of the above scheme, the gear is meshingly connected with a gear two, the connecting rod is rotatably connected to the bottom of the gear two, the connecting rod is fixedly connected to the inner wall bottom of the adjusting shell, and a threaded rod is threadedly connected to the inner wall of the gear two.

[0010] As a further improvement of the above scheme, a limiting groove is formed in the outer wall of the threaded rod, a limiting rod is slidably connected to the inner wall of the limiting groove, the outer wall of the limiting rod is fixedly connected to the inner wall of the adjusting shell, and a top plate is fixedly connected to the top of the threaded rod.

[0011] As a further improvement of the above scheme, the top plate is fixedly connected with a connecting block, the connecting block is fixedly connected with a connecting head, the top plate is fixedly connected with a rotating motor, the output end of the rotating motor is fixedly connected with a motor rotating rod two, the outer wall of the motor rotating rod two is fixedly connected with a camera fixing seat, an adjusting groove is formed in the inner wall of the camera fixing seat, and the outer wall of the connecting head is slidably connected in the inner wall of the adjusting groove.

[0012] As a further improvement of the above scheme, the connecting block is provided with four. The four connecting blocks are symmetrically arranged with the center of the adjusting shell, and the connecting head is provided with four, and the four connecting heads are symmetrically arranged with the center of the adjusting shell.

[0013] Through the above technical scheme, the output end of the micro motor rotates the motor rotating rod, the motor rotating rod rotates the gear, the gear meshes with the gear two, the gear two moves the threaded rod threadedly connected to the inner wall upward, and the threaded rod is limited by the limiting rod to ensure that it moves linearly up and down, when the threaded rod moves upward, the threaded rod pushes the top plate upward, the top plate pushes the connecting block, the connecting block pushes the connecting head, and the connecting head pushes the camera fixing seat.

[0014] Compared with the prior art, the beneficial effects of the present application are as follows:

[0015] The utility model discloses a device for measuring the distance of object through the electromagnetic wave reflection principle through the top distance detection radar and bottom distance detection radar in the flight process of unmanned aerial vehicle body, and then adopts a plurality of independent lenses through splicing type panoramic camera, and each lens shoots different visual angle image, then the image is spliced through software, forms a complete panoramic image, thereby knows the distance between unmanned aerial vehicle body and the specific distance of the obstacle, when the travel route of unmanned aerial vehicle body is planned, can monitor the travel route through infrared route detection device, and the travel direction is adjusted in real time, ensures safety, and under the condition of night or low visibility, the infrared device can make up for the deficiency of visible light camera, helps detection obstacle and other information, finally can know the specific position of unmanned aerial vehicle body through GPS positioning device, thereby accurately calibrates the position of the ground data collected, improves the precision of data analysis, thereby reduces the flight difficulty, prevents unmanned aerial vehicle body from being unable to find back after failure, reduces property loss.

[0016] The utility model discloses a rotation motor rotating rod is outputted through the operation micro motor, and motor rotating rod rotates gear, and gear engages gear no. BRIEF DESCRIPTION OF DRAWINGS

[0017] Figure 1 It is the overall structure schematic drawing of the utility model;

[0018] Figure 2 It is the top distance detection radar structure schematic drawing of the utility model;

[0019] Figure 3 It is the bottom distance detection radar structure schematic drawing of the utility model;

[0020] Figure 4 It is the GPS positioning device structure schematic drawing of the utility model;

[0021] Figure 5 It is the adjusting shell section structure schematic drawing of the utility model;

[0022] Figure 6 It is the adjusting groove structure schematic drawing of the utility model.

[0023] MAIN SYMBOL EXPLANATION:

[0024] 1, unmanned aerial vehicle body; 2, wing; 3, top distance detection radar; 4, bottom distance detection radar; 5, infrared route detection device; 6, spliced panoramic camera; 7, GPS positioning device; 8, adjusting shell; 9, micro motor; 10, motor rotating rod; 11, gear; 12, gear two; 13, connecting rod; 14, threaded rod; 15, limiting groove; 16, limiting rod; 17, connecting block; 18, connecting head; 19, camera fixing seat; 20, adjusting groove; 21, high-definition camera; 22, top plate; 23, rotary motor; 24, motor rotating rod two. DETAILED DESCRIPTION

[0025] The utility model will be described further in combination with the drawings and specific embodiments, it is to be noted that, in the case of no conflict, the following described embodiments or between the technical features can be combined to form a new embodiment.

[0026] Embodiment:

[0027] Please combine Figures 1-6 , the embodiment of a unmanned aerial vehicle rule direction detection device, including unmanned aerial vehicle body 1, unmanned aerial vehicle body 1 surface fixedly connected with wing 2, wing 2 top fixedly connected with top distance detection radar 3, wing 2 bottom fixedly connected with bottom distance detection radar 4, wing 2 front fixedly connected with infrared route detection device 5, wing 2 right side fixedly connected with spliced panoramic camera 6, unmanned aerial vehicle body 1 inner wall fixedly connected with GPS positioning device 7.

[0028] Four wing 2s are symmetrically arranged with the unmanned aerial vehicle body 1 as the center, four top distance detection radars 3 are symmetrically arranged with the center of the unmanned aerial vehicle body 1, four bottom distance detection radars 4 are symmetrically arranged with the center of the unmanned aerial vehicle body 1, four infrared route detection devices 5 are symmetrically arranged with the center of the unmanned aerial vehicle body 1, four spliced panoramic cameras 6 are symmetrically arranged with the center of the unmanned aerial vehicle body 1.

[0029] The unmanned aerial vehicle body 1 top is fixedly connected with adjusting shell 8, the adjusting shell 8 inner wall bottom is fixedly connected with micro motor 9, the micro motor 9 output end is fixedly connected with motor rotating rod 10, and the motor rotating rod 10 outer wall is fixedly connected with gear 11.

[0030] The gear 11 outer wall is engagedly connected with gear two 12, the gear two 12 bottom is rotatably connected with connecting rod 13, the connecting rod 13 bottom is fixedly connected to the adjusting shell 8 inner wall bottom, and the gear two 12 inner wall is screwedly connected with threaded rod 14.

[0031] The outer wall of the threaded rod 14 is provided with a limiting groove 15, the inner wall of the limiting groove 15 is slidably connected with a limiting rod 16, the outer wall of the limiting rod 16 is fixedly connected with the inner wall of the adjusting shell 8, and the top of the threaded rod 14 is fixedly connected with a top plate 22.

[0032] The top of the top plate 22 is fixedly connected with a connecting block 17, the top of the connecting block 17 is fixedly connected with a connecting head 18, the top of the top plate 22 is fixedly connected with a rotary motor 23, the output end of the rotary motor 23 is fixedly connected with a motor rotating rod two 24, the outer wall of the motor rotating rod two 24 is fixedly connected with a camera fixing seat 19, the inner wall of the camera fixing seat 19 is provided with an adjusting groove 20, and the outer wall of the connecting head 18 is slidably connected with the inner wall of the adjusting groove 20.

[0033] The four connecting blocks 17 are symmetrically arranged at the center of the adjusting shell 8, the four connecting heads 18 are symmetrically arranged at the center of the adjusting shell 8.

[0034] The implementation principle of the unmanned aerial vehicle normal direction passing detection device in the embodiment of the application is as follows: in the flight process of the unmanned aerial vehicle body 1, the top distance detection radar 3 and the bottom distance detection radar 4 measure the distance of an object by the principle of electromagnetic wave reflection, then the spliced panoramic camera 6 adopts multiple independent lenses, each lens shoots an image of a different angle, and then the images are spliced by software to form a complete panoramic image, so that the distance between the unmanned aerial vehicle body 1 and an obstacle is known, when the route of the unmanned aerial vehicle body 1 is planned, the infrared route detection device 5 can be used to monitor the driving route and adjust the driving direction in real time to ensure safety, meanwhile, the infrared device can make up for the deficiency of the visible light camera at night or in low visibility conditions to help detect obstacles and other information, finally, the GPS positioning device 7 can be used to know the specific position of the unmanned aerial vehicle body 1, so that the position of the collected ground data is accurately calibrated to improve the accuracy of data analysis, thereby reducing the difficulty of flight, preventing the unmanned aerial vehicle body 1 from being unable to be found back after a failure, reducing property loss, the miniature motor 9 is operated to rotate the motor rotating rod 10, the motor rotating rod 10 rotates the gear 11, the gear 11 meshes with the gear two 12, the gear two 12 drives the screw rod 14 connected with the inner wall to move upward, meanwhile, the screw rod 14 is limited by the limiting rod 16 to ensure that it moves up and down in a straight line, when the screw rod 14 moves upward, the screw rod 14 pushes the top plate 22 upward, the top plate 22 pushes the connecting block 17, the connecting block 17 pushes the connecting head 18, the connecting head 18 pushes the camera fixing seat 19, and the camera fixing seat 19 pushes the high-definition camera 21, so that the height of the high-definition camera 21 is increased and the observation range of the high-definition camera 21 is increased, then the rotating motor 23 is operated, the rotating motor 23 rotates the motor rotating rod two 24, the motor rotating rod two 24 rotates the camera fixing seat 19, the connecting head 18 slides in the adjusting groove 20 of the camera fixing seat 19, so that the high-definition camera 21 can rotate horizontally by 360 degrees, and the flexibility and observation range of the high-definition camera 21 are increased.

[0035] The above embodiment is only a preferred embodiment of the utility model, and cannot be used to limit the range of protection of the utility model, and any non-substantial change and replacement made by a person skilled in the art on the basis of the utility model belongs to the range of protection of the utility model.

Claims

1. An unmanned aerial vehicle (UAV) rule direction passage detection device, characterized by, Including unmanned aerial vehicle body (1), the unmanned aerial vehicle body (1) surface fixedly connected with wings (2), the wing (2) top fixedly connected with top distance detection radar (3), the wing (2) bottom fixedly connected with bottom distance detection radar (4), the wing (2) front fixedly connected with infrared route detection device (5), the wing (2) right side fixedly connected with spliced panoramic camera (6), the unmanned aerial vehicle body (1) inner wall fixedly connected with GPS positioning device (7).

2. The unmanned aerial vehicle rule crossing detection device of claim 1, wherein: Four wing (2) are provided, four wing (2) are symmetrically arranged with unmanned aerial vehicle body (1) as center, four top distance detection radar (3) are symmetrically arranged with unmanned aerial vehicle body (1) as center, four bottom distance detection radar (4) are symmetrically arranged with unmanned aerial vehicle body (1) as center, four infrared route detection devices (5) are symmetrically arranged with unmanned aerial vehicle body (1) as center, four spliced panoramic cameras (6) are symmetrically arranged with unmanned aerial vehicle body (1) as center. 3.The device of claim 1, wherein: The unmanned aerial vehicle body (1) top fixedly connected with the adjusting shell (8), the adjusting shell (8) inner wall bottom fixedly connected with the micro motor (9), the micro motor (9) output fixedly connected with the motor rotating rod (10), the motor rotating rod (10) outer wall fixedly connected with the gear (11).

4. The unmanned aerial vehicle rule crossing detection device of claim 3, wherein: The gear (11) outer wall is engaged with gear two (12), the gear two (12) bottom rotatably connected with connecting rod (13), the connecting rod (13) bottom fixedly connected in the adjusting shell (8) inner wall bottom, the gear two (12) inner wall threadedly connected with threaded rod (14).

5. The unmanned aerial vehicle rule crossing detection apparatus of claim 4, wherein: The threaded rod (14) outer wall is provided with a limiting groove (15), the limiting groove (15) inner wall is slidably connected with a limiting rod (16), the limiting rod (16) outer wall is fixedly connected in the adjusting shell (8) inner wall, the threaded rod (14) top fixedly connected with the top plate (22).

6. The unmanned aerial vehicle rule crossing detection apparatus of claim 5, wherein: The top plate (22) top fixedly connected with the connecting block (17), the connecting block (17) top fixedly connected with the connecting head (18), the top plate (22) top fixedly connected with the rotary motor (23), the rotary motor (23) output fixedly connected with the motor rotating rod two (24), the motor rotating rod two (24) outer wall fixedly connected with the camera fixing base (19), the camera fixing base (19) inner wall is provided with an adjusting groove (20), the connecting head (18) outer wall is slidably connected in the adjusting groove (20) inner wall.

7. The unmanned aerial vehicle rule crossing detection apparatus of claim 6, wherein: The connecting block (17) is provided with four; four connecting blocks (17) are symmetrically arranged with the center of the adjusting shell (8), four connecting heads (18) are symmetrically arranged with the center of the adjusting shell (8).

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