Foldable radar wave flow velocity measuring device based on unmanned aerial vehicle
By installing a foldable radar wave flow rate measurement device on the top of the unmanned aerial vehicle, the problem of large monitoring errors in rivers far-shore ends and the device is not suitable for small unmanned aerial vehicles in the prior art is solved, and accurate monitoring and convenient operation are achieved.
Patent Information
- Application Number
- CN202422180709.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-04
- Publication Date
- 2025-08-08
- Estimated Expiration
- 2034-09-04
AI Technical Summary
Existing unmanned aerial vehicles are difficult to accurately monitor the flow and water level of the river far from the bank, and existing devices cannot be adapted to small unmanned aerial vehicles and are inconvenient to operate.
A foldable radar wave flow rate measurement device is designed, installed on the top of the unmanned aircraft. The radar body is foldable and switched at different positions through electric push rods. Combined with the cover protection antenna, it is adapted to a small unmanned aircraft for easy storage.
It realizes accurate monitoring of the overall water flow of the river, reduces measurement errors, and is adapted to small unmanned aircraft for easy operation and storage.
Smart Images

Figure CN223200303U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, and in particular to a foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle. Background Art
[0002] With population growth and economic development, the contradiction between increasing water demand and water resource shortages is becoming increasingly severe, making water scarcity a global issue. Improving water use efficiency has become a pressing need for promoting sustainable social development. Monitoring river flow and water levels is fundamental to the scheduling and full utilization of water resources. Furthermore, river flow and water level measurement and monitoring are also necessary for flood prevention and control. Flow and water level data monitored upstream are often crucial for downstream decisions regarding flood releases, scheduling, and diversion. Furthermore, research in hydrology, ecology, and environmental protection, sometimes involving studying the circulation and conversion between precipitation, surface water, and groundwater, as well as the natural recovery functions of natural rivers, requires flow rate and flow monitoring.
[0003] According to the Chinese patent application number 202020216652.X, a device for online monitoring of water flow and flow rate is disclosed, which allows maintenance personnel to repair the radar monitor while standing on the ground, making maintenance convenient and quick, saving a lot of maintenance time, speeding up maintenance efficiency, and ensuring that the radar monitor can quickly resume real-time monitoring of water flow and flow rate. However, when the device is in use, it is difficult to detect areas of the river far away from the shore, and it can only be judged based on the monitoring situation within a short distance on both sides of the river. The results obtained in this way often have large errors, and in the process of flood prevention and control, it is difficult to play its specific role because it is impossible to obtain more accurate water flow and water level data. At present, there are several flow rate measuring devices based on unmanned aerial vehicles, but they are basically based on larger unmanned aerial vehicles and adopt a bottom-mounted method. On the one hand, they cannot be adapted to small unmanned aerial vehicles. On the other hand, the installation and storage of the equipment are also very inconvenient in actual operation. Utility Model Content
[0004] Based on the above description, the utility model provides a foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle. By being installed on the top of the unmanned aerial vehicle, it can measure the water flow conditions, and then, driven by the unmanned aerial vehicle, it can fly to a designated location in the river or along a designated route. It can not only monitor the conditions on both sides of the river, but also detect the overall water flow conditions of the river, thereby reducing the error of the measurement results. In addition, the radar body and the mounting base are foldable, can be adapted to small unmanned aerial vehicles, and are easy to store.
[0005] The utility model provides a technical solution to the above-mentioned technical problems as follows: a foldable radar wave velocity measuring device based on an unmanned aerial vehicle, comprising a mounting base and a radar body; the mounting base is used to be mounted on the top of the unmanned aerial vehicle, a hinged base is provided on the top front side of the mounting base, and the radar body is hinged to the hinged base; the radar body includes a radar panel provided on one side thereof, and the radar body has a first position in which it is closed with the mounting base for storage, and a second position in which it is flipped open with the mounting base at an obtuse angle; when the radar body is in the first position, the radar panel faces upward; when the radar body is in the second position, the radar panel faces front and downward.
[0006] On the basis of the above technical solution, the present invention can also be improved as follows.
[0007] Furthermore, the measuring device also includes a driving mechanism for driving the radar body to move back and forth between the first position and the second position; the driving mechanism includes an electric push rod, the rear end of the electric push rod is hinged to the top of the mounting seat, and the front end of the electric push rod is hinged to the radar body.
[0008] Furthermore, a hinge seat groove and a push rod groove are provided on the side of the radar body away from the radar panel, the hinge seat groove is used to accommodate the hinge seat when the radar body is in the first position, and the push rod groove is used to accommodate the push rod when the radar body is in the first position.
[0009] Furthermore, the radar body includes a back cover and the radar panel, the back cover and the radar panel are sealed together to form a sealed cavity, a chip and an antenna body are arranged in the sealed cavity, and the antenna body faces the radar panel.
[0010] Furthermore, a plurality of transmitting slots are provided on the radar panel, and the transmitting slots are arranged to form an antenna array.
[0011] Furthermore, the measuring device further includes a cover; when the radar body is located at the first position, the cover covers the emission slit; when the radar body is located at the second position, the emission slit is exposed.
[0012] Furthermore, connecting blocks are provided on both sides of the edge of the radar panel away from the hinge seat, and slide grooves extending forward and backward are provided on both sides of the cover body, and sliders are provided on the inner sides of the connecting blocks for sliding cooperation with the slide grooves on the same side; a downwardly bent connecting portion is provided on the rear side of the cover body, and the bottom of the connecting portion is hinged to one end of a connecting rod, and the other end of the connecting rod is hinged to the mounting seat.
[0013] Furthermore, a connecting rod groove is provided on the rear cover, and the connecting rod groove is used to accommodate the connecting rod when the radar body is located at the first position.
[0014] Furthermore, the mounting base is provided with a plurality of mounting holes for being mounted on the top of the unmanned aerial vehicle via bolts.
[0015] Compared with the prior art, the technical solution of this application has the following beneficial technical effects:
[0016] 1. The utility model can measure the water flow by being installed on the top of an unmanned aerial vehicle. Then, driven by the unmanned aerial vehicle, it can fly to a designated location in the river or along a designated route. It can not only monitor the conditions on both sides of the river, but also detect the water flow conditions of the entire river, thereby reducing the error of the measurement results.
[0017] 2. The radar body and mounting base of the utility model are foldable, which can be adapted to small unmanned aerial vehicles and is easy to store;
[0018] 3. By setting a transmitting gap that matches the antenna body, the obstruction and interference caused by the metal shell can be effectively avoided, thereby avoiding the defects of antenna gain reduction and radiation pattern distortion; in addition, by setting a cover to cover the transmitting gap when stored, the antenna body can be effectively protected when stored. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 A schematic structural diagram of a foldable radar wave velocity measurement device based on an unmanned aerial vehicle provided by an embodiment of the present utility model when the radar body is in a first position;
[0020] Figure 2 A schematic structural diagram of a foldable radar wave velocity measurement device based on an unmanned aerial vehicle provided by an embodiment of the present utility model when the radar body is located in the second position;
[0021] Figure 3 This is a structural diagram of the mounting base in an embodiment of the present utility model;
[0022] Figure 4 This is a schematic structural diagram of the radar body in an embodiment of the present utility model;
[0023] Figure 5 This is a schematic structural diagram of the radar body from another perspective in an embodiment of the present invention;
[0024] Figure 6 This is a schematic diagram of the internal structure of the radar body in an embodiment of the present utility model;
[0025] In the accompanying drawings, the components represented by the reference numerals are as follows:
[0026] 1. Mounting seat; 11. Mounting hole; 12. Articulated seat; 2. Radar body; 21. Back cover; 211. Articulated seat slot; 212. Push rod slot; 213. Connecting rod slot; 22. Radar panel; 221. Transmitting gap; 222. Connecting block; 223. Slider; 23. Chip; 24. Antenna body; 3. Cover; 31. Slide groove; 32. Connecting part; 4. Electric push rod; 5. Connecting rod. DETAILED DESCRIPTION
[0027] To facilitate understanding of the present application, the present application will be described more fully below with reference to the accompanying drawings. The accompanying drawings provide embodiments of the present application. However, the present application may be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to make the disclosure of the present application more thorough and comprehensive.
[0028] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those commonly understood by those skilled in the art to which this application pertains. The terms used herein in the specification of this application are for the purpose of describing specific embodiments only and are not intended to limit this application.
[0029] When used herein, the singular forms "a", "an", and "the" may also include the plural forms, unless the context clearly indicates otherwise. It should also be understood that the terms "include / comprise" or "have" and the like specify the presence of stated features, integers, steps, operations, components, parts, or combinations thereof, but do not preclude the possibility of the presence or addition of one or more other features, integers, steps, operations, components, parts, or combinations thereof.
[0030] A foldable radar wave velocity measuring device based on an unmanned aerial vehicle comprises a mounting seat 1, a radar body 2 and a driving mechanism.
[0031] In this embodiment, the mounting base 1 is symmetrically provided with four mounting holes 11, which can be bolted to the top of an unmanned aerial vehicle, such as an M30 drone. A hinged base 12 is provided on the top front side of the mounting base 1, and the radar body 2 is hingedly connected to the hinged base 12.
[0032] The radar body 2 includes a rear cover 21 and a radar panel 22. The rear cover 21 and radar panel 22 seal together to form a sealed cavity. A chip 23 and an antenna body 24 are located within the sealed cavity, with the antenna body 24 facing the radar panel 22. The radar body 2 has a first position, closed against the mounting base 1 for storage, and a second position, open to the mounting base 1 at an obtuse angle. When the radar body 2 is in the first position, the radar panel 22 faces upward. When the radar body 2 is in the second position, the radar panel 22 faces forward and downward. In this embodiment, when the radar body 2 is in the second position, the angle between the radar body 2 and the mounting base 1 is 150°.
[0033] This embodiment is installed on the top of an unmanned aerial vehicle to measure the water flow conditions. Then, driven by the unmanned aerial vehicle, it can fly to a designated location in the river or along a designated route. It can not only monitor the conditions on both sides of the river, but also detect the overall water flow conditions of the river, thereby reducing the error of the measurement results. In addition, the radar body 2 and the mounting base 1 are foldable, can be adapted to small unmanned aerial vehicles, and are easy to store.
[0034] In addition, the radar panel 22 is provided with a plurality of transmitting slots 221, which are arranged to form an antenna array. By providing transmitting slots 221 that match the antenna body 24, the obstruction and interference caused by the metal shell can be effectively avoided, thereby preventing the defects of reduced antenna gain and distorted radiation pattern.
[0035] The measurement device of this embodiment further includes a cover 3. When the radar body 2 is in the first position, the cover 3 covers the transmission slot 221. When the radar body 2 is in the second position, the transmission slot 221 is exposed. By providing the cover 3 to cover the transmission slot 221 when stowed, the antenna body 24 can be effectively protected when stowed.
[0036] Specifically, connecting blocks 222 are provided on both sides of the edge of the radar panel 22 away from the hinged base 12. Both sides of the cover 3 are provided with forward and backward extending slide slots 31. Inside the connecting blocks 222 are respectively provided sliders 223 that slidably engage with the slide slots 31 on the same side. A downwardly bent connecting portion 32 is provided on the rear side of the cover 3. The bottom of the connecting portion 32 is hinged to one end of the connecting rod 5, the other end of which is hinged to the mounting base 1.
[0037] This embodiment includes two drive mechanisms, which are respectively arranged on both sides of the top of the mounting base 1. The drive mechanism includes an electric push rod 4, the rear end of which is hinged to the top of the mounting base 1, and the front end of which is hinged to the radar body 2, and is used to drive the radar body 2 to move back and forth between the first position and the second position.
[0038] The rear cover 21 is provided with a hinge seat groove 211, a push rod groove 212 and a connecting rod groove 213. The hinge seat groove 211 is used to accommodate the hinge seat 12 when the radar body 2 is in the first position, the push rod groove 212 is used to accommodate the push rod when the radar body 2 is in the first position, and the connecting rod groove 213 is used to accommodate the connecting rod 5 when the radar body 2 is in the first position.
[0039] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.
Claims
1. A foldable radar wave velocity measuring device based on an unmanned aerial vehicle, characterized in that: The radar body comprises a mounting base and a radar body; the mounting base is used to be installed on the top of an unmanned aerial vehicle, and a hinged base is provided on the top front side of the mounting base, and the radar body is hinged to the hinged base; the radar body includes a radar panel provided on one side thereof, and the radar body has a first position in which it is closed with the mounting base for storage, and a second position in which it is opened with the mounting base at an obtuse angle; when the radar body is in the first position, the radar panel faces upward; when the radar body is in the second position, the radar panel faces forward and downward.
2. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 1, characterized in that: It also includes a driving mechanism for driving the radar body to move back and forth between the first position and the second position; the driving mechanism includes an electric push rod, the rear end of the electric push rod is hinged to the top of the mounting seat, and the front end of the electric push rod is hinged to the radar body.
3. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 2, characterized in that: A hinge seat groove and a push rod groove are provided on the side of the radar body away from the radar panel, the hinge seat groove is used to accommodate the hinge seat when the radar body is in the first position, and the push rod groove is used to accommodate the electric push rod when the radar body is in the first position.
4. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 1, characterized in that: The radar body includes a back cover and the radar panel. The back cover and the radar panel are sealed together to form a sealed cavity. A chip and an antenna body are arranged in the sealed cavity. The antenna body faces the radar panel.
5. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 4, characterized in that: The radar panel is provided with a plurality of transmitting slots, which are arranged to form an antenna array.
6. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 5, characterized in that: It also includes a cover; when the radar body is located in the first position, the cover covers the emission gap; when the radar body is located in the second position, the emission gap is exposed.
7. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 6, characterized in that: The radar panel is provided with connecting blocks on both sides of the edge away from the hinge seat, and the two sides of the cover body are provided with slide grooves extending forward and backward, and the inner sides of the connecting blocks are respectively provided with sliders that slide with the slide grooves on the same side; the rear side of the cover body is provided with a downwardly bent connecting portion, the bottom of the connecting portion is hinged to one end of the connecting rod, and the other end of the connecting rod is hinged to the mounting seat.
8. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 7, characterized in that: The rear cover is provided with a connecting rod groove, and the connecting rod groove is used to accommodate the connecting rod when the radar body is located at the first position.
9. The foldable radar wave flow velocity measuring device based on an unmanned aerial vehicle according to claim 1, characterized in that: The mounting base is provided with a plurality of mounting holes for being mounted on the top of the unmanned aerial vehicle via bolts.
Citation Information
Patent Citations
Equipment for monitoring water flow and flow velocity on line
CN211346936U