Unmanned aerial vehicle airborne crude oil leakage monitoring device and unmanned aerial vehicle monitoring system
By designing a drone-borne crude oil leakage monitoring device and using the combined settings of multi-spectral lens modules, the problems of limited monitoring and acquisition capabilities and low flexibility in the existing technology are solved, and accurate and comprehensive monitoring of crude oil leakage is achieved, ensuring the safety of crude oil extraction and utilization.
Patent Information
- Application Number
- CN202421472084.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-26
- Publication Date
- 2025-02-28
- Estimated Expiration
- 2034-06-26
AI Technical Summary
The existing drone image monitoring methods have limited collection capabilities in crude oil leakage monitoring and low resolution, making it difficult to accurately identify the leakage location in the early stages of crude oil leakage, and have low flexibility in use.
A drone-borne crude oil leakage monitoring device is designed, including a first rotating bracket, a second rotating bracket and a monitoring unit. The monitoring unit is equipped with multiple lens modules, including a visible lens module and a multi-spectral lens module, and image shooting and monitoring in different bands are realized through the multi-spectral lens module.
It realizes the free adjustment of the monitoring unit in three-dimensional space, improves the comprehensiveness and accuracy of crude oil leakage monitoring, and can accurately identify the leakage parts in the early stages of crude oil leakage, ensuring the safety of crude oil exploitation and utilization.
Smart Images

Figure CN222539033U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the field of crude oil monitoring equipment, and specifically relates to a crude oil leakage monitoring device carried by an unmanned aerial vehicle and a unmanned aerial vehicle monitoring system. Background Art
[0002] With the increasing demand for energy utilization, the demand for crude oil exploitation and utilization is also increasing. In the process of crude oil exploitation, transportation, loading and unloading, processing and use, unexpected accidents, abnormal operation or equipment maintenance can easily lead to the spillage and abnormal discharge of crude oil, which have a negative impact on soil, water resources, flora and fauna, and human health. Therefore, the monitoring of crude oil leakage has become an indispensable part of the process of crude oil exploitation and utilization.
[0003] At present, there are three main ways to monitor crude oil spills, namely satellite image monitoring, drone image monitoring (visible light) and manual inspections. Among them, the manual inspection method has great limitations, high labor costs, and is limited by limited patrol routes. It cannot achieve large-scale monitoring, nor can it fully meet the monitoring needs in certain special operation scenarios. It has obvious defects and is gradually being eliminated. Satellite image monitoring is widely used because of its diverse monitoring methods and high collection efficiency; however, the resolution of satellite images is low and is affected by ground buildings and vegetation. It is difficult to achieve for scattered and small amounts of crude oil spills. It cannot effectively meet the monitoring needs of accurately identifying crude oil leaks in the early stages of crude oil leaks, and there are certain application limitations.
[0004] In contrast, drone image monitoring is a more commonly used method for monitoring crude oil spills. It is highly flexible and environmentally compatible, and can meet the needs of crude oil spill monitoring in various application environments. However, for existing drone image monitoring methods, most drone platforms are equipped with visible light cameras, which have limited ability to collect information on crude oil spills, and the collection efficiency and accuracy are usually reduced; moreover, the cameras carried in existing drone platforms are usually fixed cameras, which are generally dedicated to special aircraft, resulting in limited monitoring tasks that can be performed and low flexibility of use. Utility Model Content
[0005] In response to one or more of the above-mentioned defects or improvement needs of the prior art, the utility model provides a UAV-mounted crude oil leakage monitoring device and a UAV monitoring system, which can effectively complete the accurate monitoring of crude oil leakage through UAV image monitoring, thereby ensuring the accuracy and reliability of crude oil monitoring.
[0006] To achieve the above-mentioned purpose, one aspect of the utility model provides an unmanned aerial vehicle airborne crude oil leakage monitoring device, which comprises:
[0007] The first rotating bracket comprises a first rotating connection end and a second rotating connection end which are respectively arranged at two ends of the main body and whose central axes intersect; the first rotating connection end is provided with a quick-connection interface ring for assembly and connection with the mounting connection position of the drone; the quick-connection interface ring is rotatably connected to the first rotating connection end through a first direction motor, so that the first rotating connection end can rotate around the axis relative to the quick-connection interface ring;
[0008] The second rotating bracket is in a C-shaped or U-shaped structure, wherein a rotating connection portion is provided in the middle thereof, and pitch connection ends are provided at both ends thereof opposite to each other; the rotating connection portion is rotatably connected to the second rotating connection end via a second direction motor, so that the second rotating bracket can rotate relative to the first rotating bracket;
[0009] The monitoring unit has two sides that are rotatably connected to the two pitch connection ends respectively, and a third direction motor is provided on at least one side corresponding to the pitch connection end, so that the monitoring unit can rotate around the axis relative to the second rotating bracket; and a plurality of lens modules are provided on the monitoring unit, and the plurality of lens modules include at least one visible light lens module and a plurality of multi-spectral lens modules.
[0010] As a further improvement of the present utility model, a direction motor support is coaxially arranged at the end of the first rotating connection end, and the first direction motor is installed on the direction motor support;
[0011] A quick-connect guide ring is provided between the quick-connect interface ring and the first directional motor, one end of the quick-connect guide ring is fixedly connected to the end of the quick-connect interface ring, and the other end thereof is assembled and connected to the output shaft of the first directional motor through an adapter.
[0012] As a further improvement of the utility model, the adapter comprises a gear and a gear ring meshing with each other;
[0013] The gear ring is fixedly arranged on the inner peripheral wall surface of the quick-connect guide ring, and the gear is axially limited in the gear ring and is coaxially fixedly connected to the output shaft of the first direction motor.
[0014] As a further improvement of the present invention, the central axis of the first rotating connection end and the central axis of the second rotating connection end are arranged orthogonally; and
[0015] Any rotating connection end is spaced a certain distance from another rotating connection end in a direction perpendicular to its central axis.
[0016] As a further improvement of the present invention, the main body of the first rotating bracket extends obliquely between the two rotating connecting ends, and the monitoring unit is located at the intersection of the central axes of the two rotating connecting ends.
[0017] As a further improvement of the present utility model, the monitoring unit includes a box-shaped housing and a monitoring lens arranged on one side of the housing;
[0018] The two sides of the shell are rotatably connected to the two pitch connection ends through the pitch connection parts respectively; and a glass cover is arranged on one side of the shell corresponding to the monitoring lens, and each lens module is encapsulated in the shell by the glass cover.
[0019] As a further improvement of the present invention, a plate-shaped lens holder is provided in the housing, and each of the lens modules is mounted on the lens holder respectively; and
[0020] The lens bracket encapsulates a core control board electrically connected to each of the lens modules in the housing.
[0021] As a further improvement of the present invention, a data transmission module and / or a data storage module is encapsulated in the housing;
[0022] The data transmission module can be communicatively connected with the signal transmission system of the drone for real-time transmission of the collected image data; the data storage module is electrically connected to each of the lens modules respectively for real-time storage of the image data collected by each of the lens modules.
[0023] As a further improvement of the present utility model, the visible light lens module is one, the multi-spectral lens module is multiple, and the multiple lens modules are arranged in an array;
[0024] and / or
[0025] At least two of the multi-spectral lenses have different shooting bands.
[0026] Another aspect of the utility model provides a drone monitoring system for monitoring crude oil leakage, comprising a drone, and the drone is equipped with the drone-borne crude oil leakage monitoring device.
[0027] The above-mentioned improved technical features can be combined with each other as long as they do not conflict with each other.
[0028] In general, compared with the prior art, the above technical solutions conceived by the utility model have the following beneficial effects:
[0029] (1) The crude oil leakage monitoring device mounted on a UAV of the utility model comprises a first rotating bracket, a second rotating bracket and a monitoring unit. By utilizing the separate designs of the two rotating brackets and the combined connection between them, the monitoring unit can be freely adjusted in three-dimensional space to meet the monitoring requirements in all directions. At the same time, combined with the combination setting of the visible light lens module and the multi-spectral lens module in the monitoring unit, image capture and monitoring in different bands can be achieved, further improving the comprehensiveness of crude oil leakage monitoring, avoiding the omission of crude oil leakage sites, and accurately completing the determination of leakage sites in the early stage of crude oil leakage, thereby ensuring the safety of crude oil exploitation and utilization.
[0030] (2) The crude oil leakage monitoring device mounted on a UAV of the utility model, by optimally setting the structures at both ends of the first rotating bracket and utilizing the combination of the direction motor support, the quick-connect interface ring, the quick-connect guide ring and other structures, not only quickly realizes the accurate assembly of the monitoring device and the UAV, but also effectively ensures the stability and accuracy of the rotation adjustment of the device in the plane.
[0031] (3) The crude oil leakage monitoring device mounted on a UAV of the utility model can effectively ensure the stability of the center of gravity of the device and ensure the adjustment stability and flexibility of the device when it is used on the air by optimizing the design of the setting form of the two rotating brackets and the position of the central axis, combined with the optimization of the setting position of the monitoring unit.
[0032] (4) The UAV monitoring system of the utility model utilizes the UAV-mounted crude oil leakage monitoring device to be mounted on the UAV, and can achieve accurate monitoring of crude oil leakage in the monitored area through the drive of the UAV, thereby ensuring the comprehensiveness and accuracy of crude oil leakage monitoring, avoiding the defects and shortcomings of traditional satellite image monitoring, manual patrol monitoring and other methods, and meeting the crude oil leakage monitoring needs in various application environments.
[0033] (5) The crude oil leakage monitoring device mounted on a drone in the utility model has a compact structure and is easy to control. It can accurately monitor crude oil leakage by being mounted on a drone. By using the corresponding settings of the two rotating brackets and the combination of a multi-spectral lens and a visible light lens, the comprehensiveness and accuracy of crude oil leakage monitoring are effectively guaranteed, and the utility model has good practical value. BRIEF DESCRIPTION OF THE DRAWINGS
[0034] In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings required for use in the embodiments will be briefly introduced below. 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 work.
[0035] Figure 1This is a schematic diagram of the overall structure of the crude oil leakage monitoring device onboard a UAV in an embodiment of the utility model;
[0036] Figure 2 This is a schematic diagram of the structure of the first rotating bracket of the crude oil leakage monitoring device in the embodiment of the utility model;
[0037] Figure 3 This is a schematic diagram of the structure of the second rotating bracket of the crude oil leakage monitoring device in the embodiment of the utility model;
[0038] Figure 4 It is a schematic diagram of the structure of the monitoring unit of the crude oil leakage monitoring device in the embodiment of the utility model;
[0039] Figure 5 This is a schematic diagram of the core control board structure of the monitoring unit in the embodiment of the utility model;
[0040] In all the drawings, the same reference numerals represent the same technical features, specifically:
[0041] 1. First rotating bracket; 101. First rotating connection end; 102. Second rotating connection end; 103. Quick-connect interface ring; 104. Quick-connect guide ring; 105. Direction motor support;
[0042] 2. Second rotating bracket; 201. Rotating connection part; 202. First pitch connection end; 203. Second pitch connection end;
[0043] 3. Monitoring unit; 301. Shell; 302. Pitch connection; 303. Monitoring lens; 304. Glass mask; 305. Visible light lens module; 306. Multi-spectral lens module; 307. Lens bracket; 308. Core control board. DETAILED DESCRIPTION
[0044] In order to make the purpose, technical solution and advantages of the utility model more clear, the utility model is further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the utility model and are not used to limit the utility model. In addition, the technical features involved in each embodiment of the utility model described below can be combined with each other as long as they do not conflict with each other.
[0045] In the description of the present invention, it should be understood that, unless otherwise expressly specified and limited, terms such as "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", and "circumferential" indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention.
[0046] In addition, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In the description of the present utility model, the meaning of "plurality" is at least two, such as two, three, etc., unless otherwise clearly and specifically defined.
[0047] In the present invention, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0048] In the present utility model, unless otherwise clearly specified and limited, a first feature being "above" or "below" a second feature may mean that the first and second features are in direct contact, or the first and second features are in indirect contact through an intermediate medium. Moreover, a first feature being "above", "above" or "above" a second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. A first feature being "below", "below" or "below" a second feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is lower in level than the second feature.
[0049] Example:
[0050] See also Figure 1~Figure 5The crude oil leakage monitoring device onboard a drone in the preferred embodiment of the utility model is used to be carried on a drone, and the drone is carried to fly to the monitored area to monitor the crude oil leakage. For the monitoring device in the preferred embodiment, it can be carried on various existing drones.
[0051] Specifically, the crude oil leakage monitoring device onboard a UAV in the preferred embodiment includes a first rotating bracket 1 , a second rotating bracket 2 and a monitoring unit 3 .
[0052] like Figure 2 As shown in the figure, the first rotating bracket 1 in the preferred embodiment has a rod-shaped main body, the two ends of which are respectively a first rotating connecting end 101 and a second rotating connecting end 102, and the central axes of the two rotating connecting ends are arranged to intersect.
[0053] In more detail, the first rotating connection end 101 is used to connect with the airborne connection position on the drone, and includes a quick-connect interface ring 103, a quick-connect guide ring 104 and a direction motor support 105 coaxially arranged on the first rotating connection end 101. The direction motor support 105 is fixedly arranged at the end of the first rotating connection end 101, and is used to correspondingly install the first direction motor; one end of the quick-connect guide ring 104 is fixedly connected to one end of the quick-connect interface ring 103, and the other end thereof is assembled and connected with the output shaft of the first direction motor through an adapter, so that the first direction motor can drive the direction motor support 105 to rotate around the axis relative to the quick-connect guide ring 104.
[0054] In a preferred embodiment, the adapter disposed between the output shaft of the first direction motor and the quick-connect guide ring 104 is a gear-gear ring assembly. At this time, a gear ring is disposed on the inner circumferential wall surface of the quick-connect guide ring 104 in the annular direction, and a gear is coaxially fixed to the output shaft of the first direction motor. The gear is meshed with the gear ring, and the main body of the first rotating bracket 1 can be rotated around the axis relative to the quick-connect guide ring 104 by rotating the output shaft of the first direction motor.
[0055] In actual settings, in order to avoid axial separation between the first direction motor and the quick-connect guide ring 104, it is preferred to configure the quick-connect guide ring 104 to be open at one end and semi-closed at the other end, with the open end fixedly connected to the quick-connect interface ring 103, the gear is coaxially embedded in the quick-connect guide ring 104, and is axially limited after engaging with the gear ring, and the output shaft of the first direction motor extends into the quick-connect guide ring 104 and is coaxially fixedly connected to the gear.
[0056] Of course, in addition to the above-mentioned method, other rotational connection forms can also be provided as required to realize the rotational connection between the quick-connect guide ring 104 and the output shaft of the first direction motor, which will not be elaborated here.
[0057] Furthermore, the end of the quick-connect interface ring 103 that is not connected to the quick-connect guide ring 104 is protruded for quick connection with the airborne connection position of the drone. In a preferred embodiment, the outer periphery of the quick-connect interface ring 103 is provided with a plurality of locking protrusions along the circumferential direction to assist in achieving the connection between the quick-connect interface ring 103 and the airborne connection position.
[0058] In more detail, the second rotating connection end 102 is arranged at the other end of the main body of the first rotating bracket 1 away from the first rotating connection end 101 , and is provided with a corresponding connecting piece corresponding to the rotating connection of the second rotating bracket 2 .
[0059] In actual configuration, any rotating connection end is spaced a certain distance from the other rotating connection end in a direction perpendicular to the central axis thereof, that is, the main body of the first rotating bracket 1 is arranged to extend obliquely between the two rotating connection ends. In this configuration, when the monitoring unit 3 is subsequently installed, the monitoring unit 3 is located at the intersection of the central axes of the two rotating connection ends.
[0060] In more detail, in a specific preferred embodiment, the central axis of the first rotating connection end 101 is orthogonal to the central axis of the second rotating connection end 102. With this arrangement, the rotation control of the monitoring unit 3 in the orthogonal plane can be achieved.
[0061] For example, when the central axis of the first rotating connection end 101 extends vertically, the first rotating bracket 1 can be rotated and adjusted in the horizontal plane relative to the drone; at this time, the central axis of the second rotating connection end 102 extends in the horizontal direction, which is equivalent to that the second rotating bracket 2 can be rotated and adjusted in the vertical plane relative to the second rotating connection end 102.
[0062] Furthermore, if Figure 3 As shown in the figure, the second rotating bracket 2 in the preferred embodiment is of a C-shaped structure or a U-shaped structure, which includes a rotating connection part 201 located in the middle and pitch connection ends respectively arranged at the two free ends of the second rotating bracket 2, namely the first pitch connection end 202 and the second pitch connection end 203 as shown in the figure.
[0063] Specifically, the rotation connection part 201 is disposed on a side of the second rotation bracket 2 away from the two pitch connection ends, and is coaxially rotationally connected to the second rotation connection end 102 , and can rotate around the axis relative to the second rotation connection end 102 .
[0064] More specifically, the rotation connection part 201 is connected to the second rotation connection end 102 via the output shaft of the second direction motor. In actual configuration, the body of the second direction motor is fixedly mounted on the second rotation connection end 102 or the rotation connection part 201; accordingly, the output shaft end of the second direction motor is fixedly connected to the rotation connection part 201 or the second rotation connection end 102.
[0065] With such arrangement, the second directional motor can be controlled to rotate the second rotating bracket 2 relative to the end of the first rotating bracket 1 , thereby realizing the left-right swing of the monitoring unit 3 relative to the first rotating bracket 1 .
[0066] Furthermore, if Figure 4 As shown in the figure, the monitoring unit 3 in the preferred embodiment includes a box-shaped shell 301, and the two sides of the shell 301 are respectively provided with pitch connection parts 302 corresponding to the rotation connection with the pitch connection end, so that the two sides of the monitoring unit 3 can be coaxially rotationally connected with the corresponding pitch connection end through the pitch connection parts 302.
[0067] In actual configuration, a third direction motor is provided between at least one pitch connection part 302 and the corresponding pitch connection end, and its configuration form is the same as the rotation connection form between the rotation connection part 201 and the second rotation connection end 102, and will not be elaborated here.
[0068] In a specific preferred embodiment, one pitch connection part 302 is connected to the corresponding pitch connection end via an output shaft of a third direction motor, and another pitch connection part 302 is rotationally connected to the corresponding pitch connection end via a rotation shaft.
[0069] Of course, it is understandable that third directional motors may be respectively provided corresponding to the two pitch connection parts 302 . In this case, the two third directional motors may be synchronously controlled to achieve the pitch movement of the monitoring unit 3 relative to the second rotating bracket 2 .
[0070] Furthermore, in the preferred embodiment, a monitoring lens 303 and a core control board 308 are combined and arranged in the housing 301 , and the two are electrically connected, so that the monitoring lens 303 can perform image acquisition under the control of the core control board 308 .
[0071] At the same time, corresponding to the setting of the monitoring lens 303, a data transmission module and / or a data storage module (not shown in the figure) is preferably also provided in the housing 301. By using the setting of the data transmission module, the monitoring lens 303 can be interconnected with the signal transmission system of the drone in real time, and then the collected image data can be transmitted back to the control terminal in real time. By using the electrical connection between the data storage module and each lens module, the data collected by the monitoring lens 303 can be stored in real time, which is convenient for data backup and monitoring applications in environments with poor communication signals.
[0072] In more detail, the monitoring lens 303 in the preferred embodiment is as follows: Figure 4 As shown in , it is preferably arranged to protrude from the surface of the housing 301 , and includes a glass mask 304 and a plurality of lens modules encapsulated in the glass mask 304 .
[0073] In actual configuration, a plate-shaped lens bracket 307 is provided to correspond to the installation of multiple lens modules, and each lens module is installed on the lens bracket 307; accordingly, Figure 5 The core control board 308 shown in FIG. 3 is encapsulated in the housing 301 through the lens bracket 307 .
[0074] In more detail, the monitoring lens 303 in the preferred embodiment includes at least one visible light lens module 305 and multiple multi-spectral lens modules 306. The visible light lens module 305 can be used to shoot within the optical band, and the multi-spectral lens module 306 can be used to shoot within multiple optical bands, especially shooting within the non-visible light band.
[0075] In actual configuration, the plurality of lens modules are preferably arranged in an array on the lens support 307 .
[0076] In addition, among the plurality of multi-spectral lens modules 306, at least two multi-spectral lens modules 306 have different working ranges / shooting bands. Figure 4 In the preferred embodiment shown, the shooting bands of each multi-spectral lens module 306 are different, so that shooting within the full band range can be achieved as much as possible, fully ensuring the accuracy of the monitoring results.
[0077] More specifically, in actual configuration, the lens modules in the monitoring lens 303 are arranged in the form of N (multi-spectral lens module) + 1 (visible light lens module), where N is an integer greater than 1. Figure 4 In the preferred embodiment shown, the lens modules are arranged in an 8+1 arrangement, forming a 3×3 module arrangement.
[0078] Of course, according to the actual setting requirements, the arrangement of the lens modules in the monitoring lens 303 can be adjusted or changed accordingly, which will not be elaborated here.
[0079] Preferably, for the multi-spectral lens module 306 in the preferred embodiment, the wavelength range of each lens module when actually working can be determined according to needs, which will not be elaborated here.
[0080] In actual settings, the motors in each direction are preferably connected to the control system of the drone in communication, so that the motors in each direction can respectively receive control instructions issued by the control system of the drone, and then complete the corresponding action process.
[0081] The UAV-mounted crude oil leakage monitoring device in the utility model has a compact structure and is easy to control. It can accurately monitor crude oil leakage by being carried by a UAV. By utilizing the corresponding settings of the two rotating brackets and the combination of a multi-spectral lens and a visible light lens, the comprehensiveness and accuracy of crude oil leakage monitoring are effectively guaranteed, and the utility model has good practical value.
[0082] It is easy for those skilled in the art to understand that the above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions and improvements made within the spirit and principles of the present invention should be included in the protection scope of the present invention.
Claims
1. A crude oil leakage monitoring device mounted on a drone, characterized in that: include: The first rotating bracket comprises a first rotating connection end and a second rotating connection end which are respectively arranged at two ends of the main body and whose central axes intersect; the first rotating connection end is provided with a quick-connection interface ring for assembly and connection with the mounting connection position of the drone; the quick-connection interface ring is rotatably connected to the first rotating connection end through a first direction motor, so that the first rotating connection end can rotate around the axis relative to the quick-connection interface ring; The second rotating bracket is in a C-shaped or U-shaped structure, wherein a rotating connection portion is provided in the middle thereof, and pitch connection ends are provided at both ends thereof opposite to each other; the rotating connection portion is rotatably connected to the second rotating connection end via a second direction motor, so that the second rotating bracket can rotate relative to the first rotating bracket; The monitoring unit has two sides that are rotatably connected to the two pitch connection ends respectively, and a third direction motor is provided on at least one side corresponding to the pitch connection end, so that the monitoring unit can rotate around the axis relative to the second rotating bracket; and a plurality of lens modules are provided on the monitoring unit, and the plurality of lens modules include at least one visible light lens module and a plurality of multi-spectral lens modules.
2. The crude oil leakage monitoring device mounted on a drone according to claim 1 is characterized in that: A direction motor support is coaxially arranged at the end of the first rotating connection end, and the first direction motor is installed on the direction motor support; A quick-connect guide ring is provided between the quick-connect interface ring and the first directional motor, one end of the quick-connect guide ring is fixedly connected to the end of the quick-connect interface ring, and the other end thereof is assembled and connected to the output shaft of the first directional motor through an adapter.
3. The crude oil leakage monitoring device mounted on a drone according to claim 2 is characterized in that: The adapter comprises a gear and a gear ring meshing with each other; The gear ring is fixedly arranged on the inner peripheral wall surface of the quick-connect guide ring, and the gear is axially limited in the gear ring and is coaxially fixedly connected to the output shaft of the first direction motor.
4. The crude oil leakage monitoring device mounted on a drone according to any one of claims 1 to 3, characterized in that: The first rotating connection end and the second rotating connection end are arranged orthogonally to the central axis; and Any rotating connection end is spaced a certain distance from another rotating connection end in a direction perpendicular to its central axis.
5. The crude oil leakage monitoring device mounted on a drone according to claim 4 is characterized in that: The main body of the first rotating bracket extends obliquely between the two rotating connection ends, and the monitoring unit is located at the intersection of the central axes of the two rotating connection ends.
6. The crude oil leakage monitoring device mounted on a drone according to any one of claims 1 to 3 and 5, characterized in that: The monitoring unit includes a box-shaped housing and a monitoring lens arranged on one side of the housing; The two sides of the shell are rotatably connected to the two pitch connection ends through the pitch connection parts respectively; and a glass cover is arranged on one side of the shell corresponding to the monitoring lens, and each lens module is encapsulated in the shell by the glass cover.
7. The crude oil leakage monitoring device mounted on a drone according to claim 6 is characterized in that: A plate-shaped lens holder is disposed in the housing, and each of the lens modules is mounted on the lens holder respectively; and The lens bracket encapsulates a core control board electrically connected to each of the lens modules in the housing.
8. The crude oil leakage monitoring device mounted on a drone according to claim 6 is characterized in that: A data transmission module and / or a data storage module is encapsulated in the housing; The data transmission module can be communicatively connected with the signal transmission system of the drone to transmit the collected image data in real time; The data storage module is electrically connected to each of the lens modules, and is used for storing the image data collected by each of the lens modules in real time.
9. The crude oil leakage monitoring device mounted on a drone according to any one of claims 1 to 3, 5, 7 and 8, characterized in that: There is one visible light lens module, and there are multiple multi-spectral lens modules, and the multiple lens modules are arranged in an array; and / or At least two of the multi-spectral lenses have different shooting bands.
10. An unmanned aerial vehicle monitoring system for monitoring crude oil spills, comprising an unmanned aerial vehicle, characterized in that: The drone is equipped with a drone-mounted crude oil leakage monitoring device as described in any one of claims 1 to 9.