A drone-mounted structure for a gas leak detection device

Abstract

This application provides a drone-mounted structure for a gas leak detection device, relating to the field of drones. It includes a frame, with several connecting plates equidistantly fixed on both sides of the frame's bottom. The bottom of each connecting plate is fixed to the same support plate. Each connecting plate has a primary adjustment component, with the primary adjustment components on both sides symmetrically arranged. A support member is located on the opposite side of each primary adjustment component, and a primary adaptation component is located outside the support member. This application, through the primary adjustment component and primary adaptation component, enables the primary adaptation component to be moved closer to the detection device in the center by controlling the primary adjustment component, thereby clamping the detection device in the middle. It can also accommodate detection devices of various sizes and shapes, improving the adaptability and efficiency of the mounting.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicles (UAVs), and more specifically, to a UAV-mounted structure for a gas leak detection device. Background Technology

[0002] With the acceleration of urbanization and the widespread use of natural gas, gas leak detection has become an important issue in the field of public safety. Traditional gas leak detection methods mainly rely on manual on-site investigation using portable detection equipment. This method is not only inefficient, but also exposes detection personnel to high health and safety risks, especially in environments where there may be high concentrations of gas leaks.

[0003] To address the aforementioned issues, in recent years, drone technology has gradually demonstrated enormous application potential in the field of gas leak detection due to its high efficiency, flexibility, and safety. However, there are many types of gas leak detection equipment with varying shapes and sizes. Most existing drone mounting structures adopt a fixed mounting method, but this method is often only applicable to detection equipment of specific sizes and shapes. Once the equipment is replaced, the mounting structure needs to be redesigned and manufactured, resulting in poor adaptability, high costs, and low efficiency.

[0004] Therefore, we have made improvements and proposed a drone-mounted structure for gas leak detection equipment. Utility Model Content

[0005] The purpose of this invention is to solve the problem of poor adaptability of current UAV mounting structures.

[0006] To achieve the above-mentioned objectives and improve the above-mentioned problems, this utility model provides a drone-mounted structure for a gas leak detection device, including a frame. Several connecting plates are fixedly arranged at equal intervals on both sides of the bottom end of the frame. The bottom end of the several connecting plates is fixedly provided with the same support plate. An adjustment component is provided on the connecting plate. The adjustment components on both sides are symmetrically arranged. A support member is provided on the opposite side of the adjustment components on both sides. An adaptation component is provided on the outside of the support member.

[0007] As a preferred technical solution of this application, the first adjustment component includes a connecting cylinder fixedly connected to the side of the connecting plate away from the support member. One end of the connecting cylinder extends through the connecting plate to the other side of the connecting plate. The connecting cylinder has a connecting rod threaded inside. The end of the connecting rod away from the connecting plate is fixedly provided with a first handle.

[0008] As a preferred technical solution of this application, the support member includes a mounting plate disposed at the end of the connecting rod.

[0009] As a preferred technical solution of this application, the first adaptation component includes two hinge plates hinged to the top and bottom of the mounting plate. A first elastic pad is fixedly provided at the front end of the mounting plate. The first elastic pad at the front end of the mounting plate is fixedly connected to the upper and lower hinge plates. A second elastic pad is fixedly provided at the upper and lower ends of the rear end of the mounting plate. The two second elastic pads located at the upper and lower ends of the rear end of the mounting plate are respectively fixedly connected to the hinge plates at the upper and lower ends of the mounting plate.

[0010] As a preferred technical solution of this application, the connecting rod is rotatably connected to the mounting plate at the end.

[0011] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0012] In the scheme of this application:

[0013] By setting up a No. 1 adjustment component and a No. 1 adaptation component, the No. 1 adaptation component can be controlled to move closer to the detection device in the middle, thereby clamping the detection device in the middle. At the same time, it can adapt to detection devices of more sizes and shapes, improving the adaptability and efficiency of the mounting. Furthermore, it eliminates the need to purchase separate mounting structures for different models of detection devices, reducing costs and solving the problem of poor adaptability of UAV mounting structures in the existing technology. Attached Figure Description

[0014] Figure 1 A schematic diagram of the UAV-mounted structure of the gas leak detection equipment provided in this application;

[0015] Figure 2 A schematic diagram of the No. 2 adaptation component in the UAV-mounted structure of the gas leak detection equipment provided in this application;

[0016] Figure 3 A schematic diagram of the No. 1 adjustment component in the UAV-mounted structure of the gas leak detection equipment provided in this application;

[0017] Figure 4 A schematic diagram of the No. 1 adaptation component in the UAV-mounted structure of the gas leak detection equipment provided in this application;

[0018] Figure 5 A schematic diagram of the second regulating component in the UAV-mounted structure of the gas leak detection equipment provided in this application.

[0019] The image shows:

[0020] 1. Frame; 21. Support plate; 22. Connecting plate; 23. Through hole; 3. Adjustment component No. 1; 31. Connecting cylinder; 32. Connecting rod; 33. Handle No. 1; 41. Mounting plate; 4. Adaptation component No. 1; 42. Hinge plate; 51. Elastic pad No. 1; 52. Elastic pad No. 2; 6. Adjustment component No. 2; 61. Mounting cylinder; 62. Mounting rod; 63. Handle No. 2; 71. Fixing plate No. 1; 7. Adaptation component No. 2; 72. Fixing plate No. 2; 81. Elastic pad No. 3; 82. Elastic pad No. 4. Detailed Implementation

[0021] To enable those skilled in the art to better understand the present invention, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort should fall within the protection scope of the present invention.

[0022] To enable those skilled in the art to better understand the present invention, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings.

[0023] It should be noted that, unless otherwise specified, the embodiments and features and technical solutions in the present invention can be combined with each other.

[0024] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0025] Example 1

[0026] Please refer to Figure 1 , Figure 2 and Figure 4 A UAV-mounted structure for a gas leak detection device includes a frame 1, which is specifically a UAV. Several connecting plates 22 are fixedly fixed at equal intervals on both sides of the bottom end of the frame 1. The connecting plates 22 on both sides are used to accommodate the gas leak detection device, which includes, but is not limited to, a gas sensor and a laser methane telemeter.

[0027] The gas sensor converts gas concentration information into an electrical signal. When the electrical signal exceeds a set threshold, the device will activate the alarm system.

[0028] The laser methane telemetry instrument uses tuned diode laser absorption spectroscopy (TDLAS) technology to detect the CH4 component of methane in the air;

[0029] Several connecting plates 22 are fixedly provided with the same support plate 21 at their bottom ends. The connecting plates 22 are provided with a first adjustment component 3. The first adjustment components 3 on both sides are symmetrically arranged. A support member is provided on the opposite side of the first adjustment components 3 on both sides. The first adjustment component 3 is used to drive the support member to move closer to the middle position, thereby accommodating more sizes of testing equipment. Multiple support members can contact and fix different areas on the side of the testing equipment, thereby accommodating different shapes of the testing equipment. A first adaptation component 4 is provided on the outside of the support member, which is used to further enhance the adaptability of the support member.

[0030] Furthermore, such as Figure 2 and Figure 3 As shown, the first adjustment component 3 includes a connecting cylinder 31 fixedly connected to the side of the connecting plate 22 away from the support member. One end of the connecting cylinder 31 extends through the connecting plate 22 to the other side of the connecting plate 22. The connecting cylinder 31 has a connecting rod 32 threaded inside. The connecting cylinder 31 is used to increase the length of the connection with the connecting rod 32, making its structure more stable. The connecting rod 32 moves through the thread when it rotates. The end of the connecting rod 32 away from the connecting plate 22 is fixedly provided with a first handle 33. The first handle 33 is used to facilitate the user to rotate the connecting rod 32.

[0031] Furthermore, such as Figure 2 and Figure 4 As shown, the support includes a mounting plate 41 located at the end of the connecting rod 32. When the connecting rod 32 rotates and moves left and right, the mounting plate 41 also moves left and right accordingly.

[0032] Furthermore, such as Figure 2 , Figure 3 and Figure 4 As shown, the first adaptation component 4 includes two hinge plates 42 hinged to the top and bottom of the mounting plate 41. The hinge plates 42 are used to increase the contact area with the testing equipment and fix the testing equipment more stably. A first elastic pad 51 is fixedly provided at the front end of the mounting plate 41. The first elastic pad 51 at the front end of the mounting plate 41 is fixedly connected to the upper and lower hinge plates 42. A second elastic pad 52 is fixedly provided at the upper and lower ends of the rear end of the mounting plate 41. The first elastic pad 51 and the second elastic pad 52 include, but are not limited to, rubber materials. The rubber materials have a certain elasticity and anti-slip ability, which can better fix the testing equipment. The two second elastic pads 52 located at the upper and lower ends of the rear end of the mounting plate 41 are fixedly connected to the hinge plates 42 at the upper and lower ends of the mounting plate 41, respectively. The first elastic pad 51 contacts the side of the testing equipment. When the second elastic pad 52 is bent due to its shell, the elastic force of the first elastic pad 51 and the second elastic pad 52 makes the first elastic pad 51 contact the shell of the testing equipment more tightly.

[0033] Furthermore, such as Figure 2As shown, the connecting rod 32 is rotatably connected to the mounting plate 41 at the end. The rotatable connection can further enhance the flexibility of the first adaptation component 4 and the mounting plate 41. Users can rotate the mounting plate 41 according to the size or shape of the testing equipment to make the first adaptation component 4 fit the shell of the testing equipment more closely.

[0034] Furthermore, such as Figure 2 and Figure 5 As shown, the support plate 21 has two through holes 23, which are used to reduce material consumption.

[0035] Example 2

[0036] The UAV-mounted structure of the gas leak detection equipment provided in Example 1 has been further optimized, specifically, as follows: Figure 2 and Figure 5 As shown, several second adjustment components 6 are equidistantly arranged at the bottom end of the support plate 21. Each second adjustment component 6 includes a mounting cylinder 61 fixedly connected to the support plate 21. The two through holes 23 are offset from the positions of the second adjustment components 6. The top end of the mounting cylinder 61 extends through the support plate 21 to the top of the support plate 21. The mounting cylinder 61 has an internal threaded mounting rod 62. When the mounting rod 62 is rotated, it moves up and down through the threaded connection with the mounting cylinder 61, thereby adjusting the height of the testing equipment on the support plate 21 and increasing the contact area to further improve the effect of fixing the testing equipment. The bottom end of the mounting rod 62 is fixedly provided with a second handle 63, which is used to facilitate the user to rotate the mounting rod 62. The top end of the mounting rod 62 is rotatably provided with a first fixing plate 71.

[0037] Furthermore, such as Figure 2 and Figure 5 As shown, a second adaptation component 7 is provided on the outside of the first fixing plate 71. The second adaptation component 7 includes two second fixing plates 72 hinged to both sides of the first fixing plate 71. The second fixing plates 72 increase the contact area with the testing equipment. A third elastic pad 81 is fixedly provided at the top of the first fixing plate 71 and fixedly connected to the second fixing plates 72 on both sides. A fourth elastic pad 82 is fixedly provided on both sides of the bottom end of the first fixing plate 71. The third elastic pad 81 and the fourth elastic pad 82 include, but are not limited to, rubber materials. The two fourth elastic pads 82 are fixedly connected to the second fixing plate 72 on the same side. When the second fixing plate 72 is flipped by hinge, it is reset by the elastic force of the fourth elastic pad 82 and the third elastic pad 81. This allows the fourth elastic pad 82 to contact the outer shell of the testing equipment. Due to the shape of the outer shell, the second fixing plate 72 bends downward. At this time, the elastic force of the third elastic pad 81 and the fourth elastic pad 82 can give it a certain contact force, thereby making it more tightly contacted with the outer shell of the testing equipment.

[0038] The usage process of the UAV-mounted structure of the gas leak detection equipment provided by this utility model is as follows:

[0039] When it is necessary to install the gas leak detection equipment under the drone, place the detection equipment on several No. 3 elastic pads 81, turn the No. 2 handle 63 to make the mounting rod 62 pass through the thread, drive the No. 3 elastic pad 81 at its top to move upward, push the detection equipment upward until it contacts the bottom of the frame 1, and clamp the detection equipment.

[0040] Then, rotating the first handle 33 on both sides drives the connecting rod 32 to rotate. Through the threaded connection with the connecting cylinder 31, its end and the component installed at the end move closer to the detection device in the middle, so that the first elastic pads 51 on both sides contact the outer shell on the side of the detection device. Multiple first elastic pads 51 are fixed to different areas on the side of the detection device, thereby adapting to different shaped shells and completing the fixing.

[0041] In this utility model, unless otherwise explicitly specified and limited, the terms "installation," "connection," "joining," and "fixing," etc., should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral part; they can refer to a mechanical connection, an electrical connection, or a connection that allows communication between them; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication of two components or the interaction between two components, unless otherwise explicitly limited. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0042] Obviously, the embodiments described above are only some embodiments of this utility model, not all embodiments. The accompanying drawings show preferred embodiments of this utility model, but do not limit the patent scope of this utility model. This utility model can be implemented in many different forms; rather, the purpose of providing these embodiments is to provide a more thorough and comprehensive understanding of the disclosure of this utility model. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing specific embodiments, or make equivalent substitutions for some of the technical features. Any equivalent structures made using the content of this utility model specification and drawings, directly or indirectly applied to other related technical fields, are similarly within the patent protection scope of this utility model.

Claims

1. A gas leak detection apparatus drone mounting structure characterized by comprising: The frame (1) includes a frame (1), on both sides of the bottom end of the frame (1) a plurality of connecting plates (22) are fixedly provided at equal intervals, and the bottom ends of the plurality of connecting plates (22) are fixedly provided with the same support plate (21). The connecting plate (22) is provided with a first adjustment component (3), the first adjustment components (3) on both sides are symmetrically arranged, and a support member is provided on the opposite side of the first adjustment components (3) on both sides. A first adaptation component (4) is provided on the outside of the support member.

2. The unmanned aerial vehicle mounting structure for a gas leakage detection device according to claim 1, characterized by The first adjustment component (3) includes a connecting cylinder (31) fixedly connected to the side of the connecting plate (22) away from the support member. One end of the connecting cylinder (31) extends through the connecting plate (22) to the other side of the connecting plate (22). The connecting cylinder (31) has a connecting rod (32) threaded inside. The end of the connecting rod (32) away from the connecting plate (22) is fixedly provided with a first handle (33).

3. The drone mounting structure for a gas leak detection device according to claim 2, characterized by The support includes a mounting plate (41) located at the end of the connecting rod (32).

4. The drone mounting structure for a gas leak detection device according to claim 3, characterized by The first adaptation component (4) includes two hinge plates (42) hinged to the top and bottom of the mounting plate (41). A first elastic pad (51) is fixedly provided at the front end of the mounting plate (41). The first elastic pad (51) at the front end of the mounting plate (41) is fixedly connected to the upper and lower hinge plates (42). A second elastic pad (52) is fixedly provided at the upper and lower ends of the rear end of the mounting plate (41). The two second elastic pads (52) located at the upper and lower ends of the rear end of the mounting plate (41) are fixedly connected to the hinge plates (42) at the upper and lower ends of the mounting plate (41) respectively.

5. The drone-mounting structure for a gas leak detection device according to claim 4, characterized by The connecting rod (32) is rotatably connected to the mounting plate (41) at the end.

6. The drone-mounting structure of a gas leakage detection device according to claim 5, characterized by Two through holes (23) are provided on the support plate (21).

7. The UAV-mounted structure for a gas leak detection device according to claim 5 or 6, characterized in that, The bottom end of the support plate (21) is provided with a plurality of second adjustment components (6) at equal intervals. The second adjustment component (6) includes an installation cylinder (61) fixedly connected to the support plate (21). The top end of the installation cylinder (61) extends through the support plate (21) to the top of the support plate (21). The installation cylinder (61) is provided with an installation rod (62) with internal threads. The bottom end of the installation rod (62) is fixedly provided with a second handle (63). The top end of the installation rod (62) is rotatably provided with a first fixing plate (71).

8. The drone mounting structure for a gas leak detection device according to claim 7, characterized by The first fixing plate (71) is provided with a second adaptation component (7) on its exterior. The second adaptation component (7) includes two second fixing plates (72) hinged to both sides of the first fixing plate (71). The top of the first fixing plate (71) is fixedly provided with a third elastic pad (81) which is fixedly connected to the second fixing plates (72) on both sides. The bottom of the first fixing plate (71) is fixedly provided with a fourth elastic pad (82) on both sides. The two fourth elastic pads (82) are respectively fixedly connected to the second fixing plate (72) on the same side.

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