Unmanned aerial vehicle equipment for electric power engineering investigation

Abstract

The utility model discloses unmanned aerial vehicle equipment for electric power engineering investigation, which comprises an unmanned aerial vehicle lower body, a buffer mounting assembly is arranged at one end of the lower part of the unmanned aerial vehicle lower body, and a support frame assembly is arranged at one end of the buffer mounting assembly; according to the utility model, the mounting clamping ring groove at one end of the support frame body is aligned with the open arc-shaped clamping ring and is jacked in, and the fixing bolt penetrates through the locking through hole to lock the open arc-shaped clamping ring, so that the support frame assembly can be flexibly and conveniently disassembled and assembled, and the support frame assembly can be conveniently adjusted and adaptively used according to different use scene environments; a damping telescopic rod and a buffering elastic piece are arranged during landing, the good buffering effect can be achieved, and the length of the portion, screwed into a threaded connection adjusting base, of an adjusting threaded rod body can be conveniently adjusted by arranging an inserting rod assembly screwed into an adjusting threaded hole and rotating a hexagonal rotating head; in this way, the unmanned aerial vehicle can take off and land in some environments with poor ground, so that the unmanned aerial vehicle can stably stand on the ground.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to unmanned aerial vehicle equipment for electric power engineering survey. Background Art

[0002] Power survey drones play an increasingly important role in the power industry. They can efficiently measure, take photos, record videos and collect data on power lines. These drones are usually equipped with high-definition cameras, infrared thermal imagers, ultrasonic detectors and other equipment, which can perform non-destructive testing on power equipment and quickly and reliably find equipment problems.

[0003] However, the existing UAV equipment used for power engineering surveys cannot flexibly and conveniently disassemble and adjust the supporting structure according to different usage environments and scenarios, which makes it inconvenient to use. Utility Model Content

[0004] The purpose of the utility model is to provide a UAV equipment for electric power engineering survey in order to solve the problem that the existing UAV equipment for electric power engineering survey cannot flexibly and conveniently disassemble and adjust the supporting structure according to different usage environments and scenarios, which is inconvenient to use.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV equipment for power engineering survey, comprising: a UAV lower body, a buffer mounting assembly is arranged at one end below the UAV lower body, a support frame assembly is arranged at one end of the buffer mounting assembly, an insert rod assembly is screwed at one end of the support frame assembly, the buffer mounting assembly includes an installation fixing plate, the support frame assembly includes a support frame body, and the insert rod assembly includes an adjustment threaded rod body.

[0006] As a further solution of the utility model: a shooting assembly is arranged in the middle of one end below the lower body of the drone, an L-shaped connecting pipe is fixedly connected to one end of the side of the lower body of the drone, a rotor motor is fixedly arranged at one end of the L-shaped connecting pipe, and four groups of the L-shaped connecting pipe and the rotor motor are arranged.

[0007] As a further solution of the utility model: a damping telescopic rod is arranged at one end of the mounting and fixing plate, a buffering elastic member is sleeved on the outer side of the damping telescopic rod, a mounting and connecting seat is fixedly arranged at one end of the damping telescopic rod, open arc-shaped clamping rings are fixedly arranged on both sides of one end of the mounting and connecting seat, a locking through hole is opened inside one end of the open arc-shaped clamping ring, and mounting through holes are opened at four ends inside the mounting and fixing plate.

[0008] As a further solution of the utility model: mounting clamping ring grooves are provided at both ends of the upper side of the support frame body, a threaded adjustment seat is fixedly provided inside one end of the lower side of the support frame body, and an adjusting threaded hole is provided inside the threaded adjustment seat.

[0009] As a further solution of the utility model: a hexagonal rotating head is fixedly arranged above the adjusting threaded rod body, and a ground-inserting pointed head is fixedly arranged below the adjusting threaded rod body.

[0010] As a further solution of the utility model: the number of the buffer installation components is set to four groups, the number of the support frame components is set to two groups, the number of the insertion rod components is set to six groups, and every two groups of the buffer installation components are adapted to one group of the support frame components and three groups of the insertion rod components.

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

[0012] In the utility model, the installation snap ring groove at one end of the support frame body is aligned with the open arc-shaped snap ring and pushed in, and the fixing bolt is passed through the locking through hole to lock it, so that the support frame assembly can be flexibly and conveniently disassembled and assembled, so that it can be conveniently adjusted and adapted for use in different usage scenarios and environments, and a good buffering effect can be achieved through the provided damping telescopic rod and buffer elastic member during landing, and an inserted rod assembly screwed inside the adjusting threaded hole can be provided, and the length of the adjusting threaded rod body screwed into the screwed adjusting seat can be conveniently adjusted by rotating the hexagonal rotating head, so that the drone can take off and land in some environments with poor ground conditions, so that it can stand firmly on the ground. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 It is a schematic diagram of the overall structure of a UAV device for electric power engineering survey described in the utility model;

[0014] Figure 2 It is a structural schematic diagram of a buffer installation component in a UAV device for electric power engineering survey described in the utility model;

[0015] Figure 3 It is a structural schematic diagram of a support frame assembly in a UAV device for electric power engineering survey described in the utility model;

[0016] Figure 4 It is a structural schematic diagram of a rod insertion assembly in an unmanned aerial vehicle device for electric power engineering survey described in the utility model.

[0017] In the figure: 1. UAV lower body; 2. Buffer installation assembly; 3. Support frame assembly; 4. Rod assembly; 5. Shooting assembly; 6. L-shaped connecting pipe; 7. Rotor motor; 20. Installation fixing plate; 21. Damping telescopic rod; 22. Buffer elastic member; 23. Installation connecting seat; 24. Open arc-shaped clamping ring; 25. Locking through hole; 26. Installation through hole; 30. Support frame body; 31. Installation clamping ring groove; 32. Screw-on adjustment seat; 33. Adjustment threaded hole; 40. Adjustment threaded rod body; 41. Hexagonal rotating head; 42. Ground plugging tip. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0019] In the description of the present utility model, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, which are only for the convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as a limitation of the present utility model. In addition, the terms "first", "second", and "third" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance. In the description of the present utility model, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "set" 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 directly connected, or indirectly connected through an intermediate medium, or it can be the internal connection of two elements. For ordinary technicians in this field, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances. The following is an explanation of the embodiments of the present utility model based on the overall structure of the present utility model.

[0020] Reference Figures 1 to 4In an embodiment of the utility model, a UAV equipment for power engineering survey includes: a UAV lower body 1, a buffer installation component 2 is arranged at one end below the UAV lower body 1, a support frame component 3 is arranged at one end of the buffer installation component 2, a plug rod component 4 is screwed at one end of the support frame component 3, the buffer installation component 2 includes a mounting fixing plate 20, the support frame component 3 includes a support frame body 30, the plug rod component 4 includes an adjusting threaded rod body 40, the buffer installation component 2 is arranged in four groups, the support frame component 3 is arranged in two groups, the plug rod component 4 is arranged in six groups, and every two groups of buffer installation components 2 are adapted to one group of support frame components 3 and three groups of plug rod components 4.

[0021] Reference Figure 1 A shooting assembly 5 is arranged in the middle of one end below the lower body 1 of the drone, an L-shaped connecting pipe 6 is fixedly connected to one end of the side of the lower body 1 of the drone, a rotor motor 7 is fixedly arranged at one end of the L-shaped connecting pipe 6, and four groups of L-shaped connecting pipes 6 and rotor motors 7 are arranged.

[0022] Reference Figure 2 A damping telescopic rod 21 is provided at one end of the mounting fixing plate 20, and a buffer elastic member 22 is sleeved on the outer side of the damping telescopic rod 21. A mounting connecting seat 23 is fixedly provided at one end of the damping telescopic rod 21, and open arc-shaped clamping rings 24 are fixedly provided on both sides of one end of the mounting connecting seat 23. A locking through hole 25 is opened inside one end of the open arc-shaped clamping ring 24, and mounting through holes 26 are opened at the four ends inside the mounting fixing plate 20.

[0023] Reference Figure 3 The upper two ends of the support frame body 30 are provided with mounting clamping ring grooves 31 , and the lower end of the support frame body 30 is fixedly provided with a screw-connected adjustment seat 32 , and the screw-connected adjustment seat 32 is provided with an adjustment threaded hole 33 .

[0024] Reference Figure 4 A hexagonal rotating head 41 is fixedly provided above the adjusting threaded rod body 40 , and a ground-inserting pointed head 42 is fixedly provided below the adjusting threaded rod body 40 .

[0025] The working principle of the utility model is: when in use, first install the buffer mounting assembly 2 under the lower body 1 of the drone by inserting the fixing bolt in the mounting through hole 26, then select the support frame assembly 3 of qualified model and specification according to different usage scenarios, align the mounting snap ring groove 31 opened at one end thereof with the open arc-shaped snap ring 24 and push it in, then insert the fixing bolt in the locking through hole 25 to lock it, so that the support frame assembly 3 can be flexibly and conveniently disassembled and assembled, so that it can be conveniently adjusted and adapted for use according to different usage scenarios, and during landing, the damping telescopic rod 21 and the buffer elastic member 22 provided can have a good buffering effect, and by providing the plug rod assembly 4 screwed in the adjusting threaded hole 33, the length of the adjusting threaded rod body 40 screwed into the screwed adjusting seat 32 can be conveniently adjusted by rotating the hexagonal rotating head 41, so that the drone can take off and land in some environments with poor ground so that it can stand firmly on the ground.

[0026] What is described above is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A UAV device for power engineering survey, characterized in that: include: A lower body (1) of an unmanned aerial vehicle, wherein a buffer installation assembly (2) is arranged at one end below the lower body (1), a support frame assembly (3) is arranged at one end of the buffer installation assembly (2), an insertion rod assembly (4) is screwed to one end of the support frame assembly (3), the buffer installation assembly (2) includes a mounting fixing plate (20), the support frame assembly (3) includes a support frame body (30), and the insertion rod assembly (4) includes an adjusting threaded rod body (40).

2. The UAV equipment for electric power engineering survey according to claim 1 is characterized in that: A shooting assembly (5) is arranged in the middle of one lower end of the lower body (1) of the drone, an L-shaped connecting pipe (6) is fixedly connected to one side end of the lower body (1) of the drone, a rotor motor (7) is fixedly arranged at one end of the L-shaped connecting pipe (6), and four sets of the L-shaped connecting pipe (6) and the rotor motor (7) are arranged.

3. The UAV equipment for electric power engineering survey according to claim 1 is characterized in that: A damping telescopic rod (21) is arranged at one end of the mounting fixing plate (20), a buffer elastic member (22) is sleeved on the outer side of the damping telescopic rod (21), a mounting connection seat (23) is fixedly arranged at one end of the damping telescopic rod (21), open arc-shaped clamping rings (24) are fixedly arranged on both sides of one end of the mounting connection seat (23), a locking through hole (25) is provided inside one end of the open arc-shaped clamping ring (24), and mounting through holes (26) are provided at four ends inside the mounting fixing plate (20).

4. The UAV equipment for electric power engineering survey according to claim 1 is characterized in that: The upper two ends of the support frame body (30) are provided with mounting clamping ring grooves (31), and the lower end of the support frame body (30) is internally fixedly provided with a threaded adjustment seat (32), and the threaded adjustment seat (32) is internally provided with an adjustment threaded hole (33).

5. The UAV equipment for electric power engineering survey according to claim 1 is characterized in that: A hexagonal rotating head (41) is fixedly arranged above the adjusting threaded rod body (40), and a ground-inserting pointed head (42) is fixedly arranged below the adjusting threaded rod body (40).

6. The UAV equipment for electric power engineering survey according to claim 1 is characterized in that: The number of the buffer installation components (2) is four, the number of the support frame components (3) is two, and the number of the insertion rod components (4) is six. Every two groups of the buffer installation components (2) are adapted to one group of the support frame components (3) and three groups of the insertion rod components (4).

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