Drones
By designing a drone cutting mechanism and a clamping mechanism, the drone was able to automatically cut cables, solving the problems of high safety risks and low efficiency in manual cable cutting during traditional power line maintenance, and improving the safety and efficiency of power line maintenance.
Patent Information
- Application Number
- CN202411657317.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-19
- Publication Date
- 2026-02-06
- Estimated Expiration
- 2044-11-19
AI Technical Summary
In traditional power line maintenance, manually cutting cables poses a high safety risk and is inefficient.
Design a drone equipped with a cutting mechanism, a clamping mechanism, and a drive mechanism. The drone can automatically cut cables, and the clamping mechanism can stabilize the drone's position, reducing manual operation.
This effectively reduces the safety risks associated with manual cable cutting by staff and improves the efficiency and safety of power line maintenance.
Smart Images

Figure CN119275751B_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the technical field of cable cutting equipment, in particular to a kind of unmanned plane. BACKGROUND
[0002] With the increasing popularity of power facilities and the complexity of power network, power line maintenance and line processing in emergency situation become more and more important. At present, distribution network mainly uses overhead line, among which, part of base station equipment or special transformer equipment still maintains electrical connection with power grid after transformer is shipped out, which leads to safety hazards such as electric shock of social personnel, and due to lack of personnel maintenance, the risk of equipment failure is extremely high, which greatly threatens the safe operation of power grid. In order to eliminate hidden dangers, it is necessary to remove the electrical connection with power grid due to customer's non-removal.
[0003] Traditional power line maintenance often needs workers to climb poles or use aerial work platforms to work, which not only is inefficient, but also has high safety risks. SUMMARY
[0004] The main purpose of the present application is to provide an unmanned plane to solve the problem of high risk when workers manually cut off cables in related technologies.
[0005] In order to achieve the above purpose, according to one aspect of the present application, an unmanned plane is provided, comprising: an unmanned plane body; a cutting mechanism, the cutting mechanism comprising a mounting plate, a first cutting piece and a first driving member, the first driving member being arranged on the mounting plate, the first driving member and the first cutting piece being drivingly connected to make the first cutting piece reciprocate on the mounting plate; a driving mechanism comprising a first connecting member and a second driving member arranged on the first connecting member, the first connecting member being connected with the unmanned plane body, the second driving member being drivingly connected with the mounting plate to make the mounting plate reciprocate on the first connecting member; a clamping mechanism, the clamping mechanism comprising a second connecting member and a clamping arm, a first end of the second connecting member being rotatably connected with the unmanned plane body, the clamping arm being arranged at a second end of the second connecting member.
[0006] Further, the cutting mechanism further comprises a second cutting piece arranged on the mounting plate, the first cutting piece and the second cutting piece being arranged at an acute angle.
[0007] Further, the cutting mechanism further comprises a driving wheel and a transmission wheel meshing with the driving wheel, the number of teeth of the transmission wheel being greater than that of the driving wheel, the driving wheel and the transmission wheel being rotatably arranged on the mounting plate, the driving wheel being arranged on the shaft of the first driving member, the first cutting piece having a transmission tooth part, the transmission wheel transmission tooth part being meshed.
[0008] Further, the clamping arm comprises a first clamping member and a second clamping member which are arranged at intervals on the second connecting member, the first clamping member has a first clamping surface, and a clamping space is formed between the first clamping surface and the second clamping member, and the shape of the first clamping surface is changeable so as to change the shape of the clamping space.
[0009] Further, the second clamping member has a second clamping surface, and a clamping space is formed between the first clamping surface and the second clamping surface, and the shape of the second clamping surface is changeable so as to change the shape of the clamping space.
[0010] Further, the first clamping member comprises a box body, a plurality of clamping rods arranged in an array, and a plurality of elastic return members, the box body has a mounting space, the plurality of clamping rods are arranged in the mounting space in a reciprocating manner along the direction from the first clamping member to the second clamping member, the side of the plurality of clamping rods facing the second clamping member forms the first clamping surface, and the plurality of elastic return members are arranged in one-to-one correspondence with the plurality of clamping rods, and the elastic return member is arranged between the clamping rod and the bottom of the mounting space so as to move the clamping rod towards the outside of the box body.
[0011] Further, the first clamping member further comprises a plurality of connecting rods, the plurality of connecting rods are arranged in one-to-one correspondence with the plurality of clamping rods, an elastic return member is sleeved on the outer periphery of each connecting rod, the first end of the connecting rod is connected with the box body, the second end of the connecting rod is located in the clamping rod, and the clamping rod is movably arranged at the second end of the connecting rod.
[0012] Further, the clamping rod comprises a block body, the block body has a receiving space and a strip-shaped opening in communication with the receiving space, the minimum radial dimension of the receiving space is greater than the length of the strip-shaped opening; the connecting rod comprises a strip-shaped rod body and a shaft body connected with the strip-shaped rod body, and the strip-shaped opening can pass through the strip-shaped rod body; wherein the connecting rod has a mounting state and a limiting state, when the connecting rod is in the mounting state, the strip-shaped rod body is arranged correspondingly with the strip-shaped opening, and when the connecting rod is in the limiting state, the strip-shaped rod body is located in the receiving space and is arranged crosswise with the strip-shaped opening.
[0013] Further, the connecting rod further comprises a shaft body, the first end of the shaft body is connected with the strip-shaped rod body, the bottom of the box body is provided with a plurality of mounting holes, and the second end of the shaft body is detachably connected with the mounting hole.
[0014] Further, the unmanned aerial vehicle body has a controller, the unmanned aerial vehicle further comprises an ultrasonic sensor connected with the unmanned aerial vehicle body, the ultrasonic sensor is in signal connection with the controller, and / or the unmanned aerial vehicle further comprises a camera structure connected with the unmanned aerial vehicle body, and the camera structure is in signal connection with the controller.
[0015] The unmanned aerial vehicle comprises an unmanned aerial vehicle body, a cutting mechanism, a driving mechanism and a clamping mechanism. The cutting mechanism comprises a mounting plate, a first cutting blade movably arranged on the mounting plate and a first driving member, the first driving member is in driving cooperation with the first cutting blade. The driving mechanism comprises a first connecting member and a second driving member, the first connecting member is connected with the unmanned aerial vehicle body, the second driving member is arranged on the first connecting member, and the second driving member is in driving cooperation with the mounting plate to move the mounting plate on the first connecting member. The clamping mechanism comprises a second connecting member and a clamping arm, the first end of the second connecting member is rotatably connected with the unmanned aerial vehicle body, and the clamping arm is arranged on the second end of the second connecting member. Through the above arrangement, the first cutting blade can contact the surface of the cable when moving back and forth, and the cutting of the cable is realized. The second driving member can drive the mounting plate to move, and then the mounting plate can drive the first cutting blade to move, that is, the first cutting blade can move towards the direction close to the cable, and the cutting of the cable is realized, avoiding manual cutting of the cable by the staff. The second connecting member rotates relative to the unmanned aerial vehicle body, and can drive the clamping arm to move to different positions. The clamping arm can clamp the structure near the cable, so that the position of the unmanned aerial vehicle body is more stable. Therefore, the technical scheme of the present application effectively solves the problem of high risk when the staff manually cuts off the cable in the related art. BRIEF DESCRIPTION OF DRAWINGS
[0016] The drawings accompanying the specification of the present application form a part thereof, serve to provide further understanding of the application, and together with the description of the application, explain the application. The embodiments of the present application and its description are used to explain the application, and do not constitute an improper limitation on the application. In the drawings:
[0017] Figure 1 A front view structural schematic diagram of an embodiment of the unmanned aerial vehicle according to the present application is shown;
[0018] Figure 2 A cutting mechanism of the unmanned aerial vehicle is shown Figure 1 A cutting mechanism of the unmanned aerial vehicle is shown
[0019] Figure 3 A clamping mechanism of the unmanned aerial vehicle is shown Figure 1 A clamping mechanism of the unmanned aerial vehicle is shown
[0020] Figure 4 A clamping mechanism of the unmanned aerial vehicle is shown Figure 3 A clamping mechanism of the unmanned aerial vehicle is shown
[0021] Figure 5 A first clamping member of the clamping mechanism is shown Figure 3 A first clamping member of the clamping mechanism is shown
[0022] Figure 6 Another position of the first clamping member of the clamping mechanism is shown Figure 3 Another position of the first clamping member of the clamping mechanism is shown
[0023] wherein the above figures include the following reference signs:
[0024] 10, unmanned aerial vehicle body; 20, cutting mechanism; 21, mounting plate; 22, first cutting blade; 23, second cutting blade; 24, driving wheel; 25, transmission wheel; 30, driving mechanism; 31, first connecting piece; 40, clamping mechanism; 41, second connecting piece; 42, clamping arm; 421, first clamping piece; 4211, box body; 42111, mounting hole; 4212, clamping rod; 42121, block body; 421211, containing space; 421212, strip-shaped opening; 4213, elastic reset piece; 4214, connecting rod; 42141, strip-shaped rod body; 42142, shaft body; 422, second clamping piece; 423, clamping space. DETAILED DESCRIPTION
[0025] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way limiting on the application or its applications or uses. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative labor fall within the scope of the present application.
[0026] It should be noted that the terms used herein are only intended to describe specific embodiments and are not intended to limit exemplary embodiments according to the present application. As used herein, the singular form is intended to include the plural form, unless the context clearly indicates otherwise, and it should also be understood that when the terms "comprise" and / or "include" are used in the specification, there is a reference to the presence of a feature, step, operation, device, component, and / or combinations thereof.
[0027] Unless specifically stated otherwise, the relative arrangements of the components and steps illustrated in these embodiments and the numerical expressions and values set forth herein are not limiting. It should be understood that the various parts of the drawings are not necessarily drawn to scale, and that, for the purpose of convenience and clarity, not all components and steps can be shown in a given figure. Techniques, methods, and devices known to those of ordinary skill in the relevant art can not be discussed in detail, but rather can be assumed to be known by those of ordinary skill in the art. In all examples shown and discussed herein, any specific values are to be interpreted as merely illustrative of the examples, and not as a limitation thereon. Thus, other examples of the exemplary embodiments can have different values. It is noted that like reference numerals and letters in the various figures indicate like parts, and therefore, once a part is defined in one figure, it need not be discussed further in subsequent figures.
[0028] like Figure 1 As shown, the drone in this embodiment includes: a drone body 10, a cutting mechanism 20, a driving mechanism 30, and a clamping mechanism 40. The cutting mechanism 20 includes a mounting plate 21, a first cutting blade 22, and a first driving member. The first driving member is disposed on the mounting plate 21, and the first driving member and the first cutting blade 22 drive each other to reciprocate on the mounting plate 21. The driving mechanism 30 includes a first connecting member 31 and a second driving member disposed on the first connecting member 31. The first connecting member 31 is connected to the drone body 10, and the second driving member drives each other with the mounting plate 21 to reciprocate on the mounting plate 21. The clamping mechanism 40 includes a second connecting member 41 and a clamping arm 42. The first end of the second connecting member 41 is rotatably connected to the drone body 10, and the clamping arm 42 is disposed at the second end of the second connecting member 41.
[0029] According to the technical solution of this invention, the drone includes a drone body 10, a cutting mechanism 20, a driving mechanism 30, and a clamping mechanism 40. The cutting mechanism 20 includes a mounting plate 21, a first cutting blade 22 reciprocally mounted on the mounting plate 21, and a first driving member, which drives the first cutting blade 22. The driving mechanism 30 includes a first connecting member 31 and a second driving member. The first connecting member 31 is connected to the drone body 10, and the second driving member is mounted on the first connecting member 31 and drives the mounting plate 21 to reciprocate on the first connecting member 31. The clamping mechanism 40 includes a second connecting member 41 and a clamping arm 42. The first end of the second connecting member 41 is rotatably connected to the drone body 10, and the clamping arm 42 is located at the second end of the second connecting member 41. With the above configuration, when the first cutting blade 22 reciprocates, it can contact the cable surface, thereby cutting the cable. The second driving component can drive the mounting plate 21 to move, which in turn drives the first cutting blade 22 to move. That is, the first cutting blade 22 can move towards the cable, thus cutting the cable and avoiding manual cable cutting by personnel. The second connecting component 41 rotates relative to the drone body 10, which can move the clamping arm 42 to different positions. The clamping arm 42 can clamp the structure near the cable, making the position of the drone body 10 more stable. Therefore, the technical solution of this application effectively solves the problem of high risk when personnel manually cut cables in related technologies.
[0030] In this embodiment, the cable is an overhead cable.
[0031] It should be noted that both the first driving component and the second driving component are first driving motors.
[0032] The structure near the cable can be other cables, or it can be a crossarm, or other structures.
[0033] The mounting plate 21 is provided with a first sliding groove, and the first cutting blade 22 is movably arranged in the first sliding groove.
[0034] The first connecting piece 31 is a first connecting plate, and the mounting plate 21 is further provided with a second sliding groove, and the first connecting plate is arranged in the second sliding groove.
[0035] As shown in the drawings, Figure 2 In this embodiment, the cutting mechanism 20 further comprises a second cutting blade 23 arranged on the mounting plate 21, and the first cutting blade 22 and the second cutting blade 23 are arranged at an acute angle. When the mounting plate 21 moves, the first cutting blade 22 and the second cutting blade 23 can be moved, and then the first cutting blade 22 and the second cutting blade 23 can cut the cable at the same time, improving the cutting efficiency.
[0036] It should be noted that the second cutting blade can also be movably arranged on the mounting plate.
[0037] The mounting plate 21 is provided with a third sliding groove, and the second cutting blade 23 is movably arranged in the third sliding groove.
[0038] The angle between the first cutting blade 22 and the second cutting blade 23 is between 30° and 60°, which can be 30°, 40°, 45°, 50° or 60°.
[0039] As shown in the drawings, Figure 2 In this embodiment, the cutting mechanism 20 further comprises a driving wheel 24 and a transmission wheel 25 engaged with the driving wheel 24, the number of teeth of the transmission wheel 25 is greater than the number of teeth of the driving wheel 24, and the driving wheel 24 and the transmission wheel 25 are rotatably arranged on the mounting plate 21. The driving wheel 24 is arranged on the rotating shaft of the first driving member, the first cutting blade 22 has a transmission tooth part, and the transmission wheel 25 is engaged with the transmission tooth part. The first driving member can drive the driving wheel 24 to rotate, the driving wheel 24 can drive the transmission wheel 25 to rotate, and the transmission wheel 25 can drive the first cutting blade 22 to move. The number of teeth of the transmission wheel 25 is greater than the number of teeth of the driving wheel 24, so that through the driving wheel 24 and the transmission wheel 25, the speed reduction effect can be achieved, and the torque can be increased to ensure that the first cutting blade 22 can smoothly cut the cable.
[0040] The transmission wheel 25 includes two coaxially arranged transmission wheels 25, one of which is in gear transmission with the first cutting blade 22, and the other is in gear transmission with the second cutting blade 23.
[0041] As shown in the drawings, Figures 3 to 5As shown, in this embodiment, the clamping arm 42 includes a first clamping member 421 and a second clamping member 422 spaced apart on the second connector 41. The first clamping member 421 has a first clamping surface, and a clamping space 423 is formed between the first clamping surface and the second clamping member 422. The shape of the first clamping surface can be changed to alter the shape of the clamping space 423. Structures near the cable can enter the clamping space, allowing the first clamping member 421 and the second clamping member 422 to clamp these structures, thus making the drone's position more stable. The shape of the first clamping surface can be changed, enabling the clamping arm 42 to clamp structures of different shapes.
[0042] The second connector 41 includes a second connecting plate, and the first clamping member 421 and the second clamping member 422 are respectively disposed at opposite ends of the second connecting plate.
[0043] The second connector 41 also includes a third connector plate connected to the middle of the second connector plate, and the drone also includes a connector arm connected to the first connector 31, with the third connector plate hinged to the connector arm.
[0044] The third drive motor is mounted on the connecting arm, and the third drive motor drives the third connecting plate to rotate relative to the connecting arm.
[0045] like Figure 3 and Figure 4 As shown, in this embodiment, the second clamping member 422 has a second clamping surface, and a clamping space 423 is formed between the first clamping surface and the second clamping surface. The shape of the second clamping surface can be changed to change the shape of the clamping space 423. The changeable shape of the second clamping surface allows the clamping arm 42 to clamp structures of different shapes.
[0046] like Figure 4As shown, in the embodiment, the first clamping piece 421 comprises a box body 4211, a plurality of clamping rods 4212 arranged in an array, and a plurality of elastic return pieces 4213. The box body 4211 has a mounting space, the plurality of clamping rods 4212 are movably arranged in the mounting space in the direction from the first clamping piece 421 to the second clamping piece 422, one side of the plurality of clamping rods 4212 towards the second clamping piece 422 forms a first clamping surface, and the plurality of elastic return pieces 4213 are arranged one by one corresponding to the plurality of clamping rods 4212. The elastic return piece 4213 is arranged between the clamping rod 4212 and the bottom of the mounting space to move the clamping rod 4212 towards the outside of the box body 4211. The box body 4211 can limit the outer periphery of the plurality of clamping rods 4212. The plurality of clamping rods 4212 are movably arranged in the mounting space in the direction from the first clamping piece 421 to the second clamping piece 422, so that when the first clamping piece 421 contacts the structure near the cable, the clamping rods 4212 at different positions can move different distances, and the shape of the first clamping surface changes, so that the first clamping piece 421 is more fitted with the structure near the cable, and the structure near the cable is clamped. The elastic return piece 4213 can apply an elastic return force to the clamping rod 4212, so that after the clamping rod 4212 is separated from the structure near the cable, the clamping rod 4212 can move towards the second clamping piece 422, and the clamping arm 42 can clamp the structure near the cable again.
[0047] It should be noted that the second clamping piece 422 has the same structure as the first clamping piece 421.
[0048] The elastic return piece 4213 is a compression spring.
[0049] The box body of the first clamping piece 421 and the box body of the second clamping piece 422 are movably connected with the second connecting piece 41, and the rotation of the box body of the first clamping piece 421 and the box body of the second clamping piece 422 is driven by the second driving motor and the straight tooth gear arranged on the rotating shaft of the second driving motor.
[0050] As Figures 3 to 6As shown, in this embodiment, the first clamping member 421 further includes multiple connecting rods 4214, each corresponding to a clamping rod 4212. Each connecting rod 4214 has an elastic reset member 4213 fitted around its outer periphery. The first end of the connecting rod 4214 is connected to the box body 4211, and the second end of the connecting rod 4214 is located inside the clamping rod 4212, which is movably disposed at the second end of the connecting rod 4214. The connecting rod 4214 facilitates the connection between the clamping rod 4212 and the box body. The connecting rod 4214 also limits the elastic reset member 4213 fitted around its outer periphery. The connecting rod 4214 also limits the clamping rod 4212, preventing it from moving outside the box body 4211 and separating from it.
[0051] like Figures 3 to 5 As shown, in this embodiment, the clamping rod 4212 includes a block 42121, which has a receiving space 421211 and a strip-shaped opening 421212 communicating with the receiving space 421211. The minimum radial dimension of the receiving space 421211 is greater than the length of the strip-shaped opening 421212. The connecting rod 4214 includes a strip-shaped rod 42141 and a shaft 42142 connected to the strip-shaped rod 42141. The strip-shaped opening 421212 allows the strip-shaped rod 42141 to pass through. The first end of the shaft 42142 is connected to the strip-shaped rod 42141, and the second end of the shaft 42142 is connected to the housing 4211. The connecting rod 4214 has an installed state and a limiting state. When the connecting rod 4214 is in the installed state, the strip-shaped rod body 42141 is correspondingly arranged with the strip-shaped opening 421212. When the connecting rod 4214 is in the limiting state, the strip-shaped rod body 42141 is located in the receiving space 421211 and is intersected with the strip-shaped opening 421212. The strip-shaped rod body 42141 can enter the receiving space 421211 through the strip-shaped opening 421212 and rotate within the receiving space 421211, so that the strip-shaped rod body 42141 and the strip-shaped opening 421212 are intersected. This allows the block 42121 to limit the strip-shaped rod body 42141, preventing the clamping rod 4212 from separating from the connecting rod 4214 when the clamping rod 4212 moves, and thus preventing the clamping rod 4212 from separating from the box body. The shaft 42142 can be connected to the housing 4211, thus allowing the connecting rod 4214 to be connected to the housing 4211. The minimum radial dimension of the accommodating space 421211 is greater than the length of the strip opening 421212, thus allowing the strip rod 42141 to rotate within the accommodating space 421211 so that the strip rod 42141 and the strip opening 421212 are arranged intersectingly.
[0052] like Figure 3 and Figure 4As shown, in this embodiment, the bottom of the box body 4211 is provided with a plurality of mounting holes 42111, and the second end of the shaft body 42142 is detachably connected with the mounting holes 42111. The shaft body 42142 can be connected with the mounting holes 42111, and then the connecting rod 4214 can be connected with the box body 4211.
[0053] In this embodiment, the unmanned aerial vehicle body 10 has a controller, and the unmanned aerial vehicle further comprises an ultrasonic sensor connected with the unmanned aerial vehicle body 10, and the ultrasonic sensor is signal connected with the controller. The unmanned aerial vehicle further comprises a camera structure connected with the unmanned aerial vehicle body 10, and the camera structure is signal connected with the controller. Through the ultrasonic sensor, the obstacles near the unmanned aerial vehicle body can be detected, so as to facilitate the controller to control the unmanned aerial vehicle to avoid the obstacles. Through the camera structure, the obstacles near the unmanned aerial vehicle body can be photographed, so as to facilitate the controller to control the unmanned aerial vehicle to avoid the obstacles.
[0054] The ultrasonic sensor and the camera structure are arranged above the unmanned aerial vehicle body 10.
[0055] The cutting mechanism 20 and the clamping mechanism 40 are arranged below the unmanned aerial vehicle body 10.
[0056] The unmanned aerial vehicle of this embodiment can approach the target wire in a manner of remote control or autonomous flight under the operation of the operator, and use the cutting mechanism 20 to shear the wire.
[0057] The unmanned aerial vehicle body is a multi-axle aircraft, which has good stability and load capacity.
[0058] The unmanned aerial vehicle body is equipped with GPS, GLONASS and Beidou positioning system to realize accurate positioning. The unmanned aerial vehicle supports remote control and autonomous flight mode.
[0059] The mounting plate 21 is made of high-strength lightweight materials such as carbon fiber, titanium alloy and the like.
[0060] The blades are made of high-hardness and wear-resistant materials such as high-speed steel, hard alloy and the like to manufacture the first cutting piece 22 and the second cutting piece 23 to ensure the shearing effect.
[0061] The first driving motor is used as the driving source, which is transmitted to the first cutting piece 22 through the gear reduction mechanism (i.e. the driving wheel 24 and the transmission wheel 25) to ensure sufficient shearing torque. The first driving motor has the characteristics of fast response speed and easy control.
[0062] The unmanned aerial vehicle body 10 is provided with overload protection and automatic stop function to improve safety.
[0063] The controller includes remote control software, which supports real-time video transmission, control signal transmission and the like. The controller stores an integrated path planning algorithm to realize autonomous flight to approach the target wire.
[0064] The UAV body 10 is equipped with obstacle avoidance sensors (such as laser radar, ultrasonic sensor), to ensure safety.
[0065] The UAV body 10 is equipped with an LED lighting system to support night operations.
[0066] The UAV body 10 is equipped with a temperature control system to ensure that the UAV body operates within an appropriate temperature range.
[0067] The UAV has a suspension system that can automatically adjust according to the position of the cutting mechanism and the weight of the UAV, ensuring that the cutting mechanism 20 is always in the best state of force.
[0068] The clamping mechanism 40 is added below the UAV body 10, which can extend when the cutting mechanism 20 starts cutting work, providing additional support points for the cutting mechanism 20, ensuring stability during cutting.
[0069] The controller has a dynamic balance adjustment function, which can monitor the attitude change of the UAV in real time, and automatically correct the attitude deviation by adjusting the speed of each motor, ensuring flight stability even when carrying a heavy cutting mechanism 20.
[0070] The controller has an intelligent center of gravity adjustment function, which can automatically adjust the counterweight inside the UAV body according to the position and weight of the breaking shear, thereby optimizing flight performance.
[0071] In the description of the present application, it should be understood that the orientation words such as "front, rear, upper, lower, left, right", "transverse, vertical, perpendicular, horizontal" and "top, bottom" and the like indicate the orientation or position relationship shown in the drawings, which is only for the convenience of describing the present application and simplifying the description, and in the absence of the opposite description, these orientation words do not indicate and imply that the indicated device or element must have a specific orientation or be constructed and operated in a specific orientation, therefore cannot be understood as a limitation on the scope of protection of the present application; the orientation words "inner, outer" refer to the inner and outer of the contour of each component itself.
[0072] For purposes of the description hereinafter, spatial or directional terms, for example, "above", "below", "upper", "lower", and the like, can be used, and relate to the device as illustrated in the figures. However, it is to be understood that no absolute or relative orientation of the device is intended or implied, unless specifically described as such. Terms concerning attachments, coupling and the like, such as "connected" and "coupled" and the like, are to be construed in accordance with their normal meanings, that is, as referring to an indirect or direct connection or coupling. Any reference to "comprising" or "containing" is to be construed as meaning "comprising or containing, but not limited to". Any reference to "comprising" or "containing" is to be construed as meaning "comprising or containing, but not limited to".
[0073] In addition, it should be pointed out that the use of the terms "first", "second" and the like, to describe various elements, is merely intended to differentiate the elements from one another, and does not connote any special order or order of precedence, unless otherwise specifically indicated. Thus, the use of the terms "first", "second" and the like, is not intended to limit the scope of the present application, and is not intended to connote any special order or order of precedence.
[0074] The preferred embodiments herein disclosed are not intended to limit or restrict the scope of the application, but merely convey the best mode contemplated by the inventors of carrying out the claimed application. Any modifications, variations or changes within the spirit and scope of the application as disclosed herein will be considered to fall within the scope of the application.
Claims
1. A drone, characterized in that, include: Unmanned aerial vehicle body (10); The cutting mechanism (20) includes a mounting plate (21), a first cutting blade (22), and a first driving member. The first driving member is disposed on the mounting plate (21), and the first driving member and the first cutting blade (22) drive each other to move back and forth on the mounting plate (21). The drive mechanism (30) includes a first connector (31) and a second drive member disposed on the first connector (31). The first connector (31) is connected to the UAV body (10), and the second drive member drives the mounting plate (21) to reciprocate on the first connector (31). The clamping mechanism (40) includes a second connector (41) and a clamping arm (42). The first end of the second connector (41) is rotatably connected to the UAV body (10), and the clamping arm (42) is disposed at the second end of the second connector (41). The clamping arm (42) includes a first clamping member (421) and a second clamping member (422) spaced apart on the second connector (41). The first clamping member (421) has a first clamping surface, and a clamping space (423) is formed between the first clamping surface and the second clamping member (422). The shape of the first clamping surface can be changed to change the shape of the clamping space (423). The first clamping member (421) includes a housing (4211), a plurality of clamping rods (4212) arranged in an array, and a plurality of elastic reset members (4213). The housing (4211) has an installation space. The plurality of clamping rods (4212) are reciprocally arranged in the installation space along the direction from the first clamping member (421) to the second clamping member (422). The plurality of clamping rods (4212) form the first clamping surface on the side facing the second clamping member (422). The plurality of elastic reset members (4213) are arranged in a one-to-one correspondence with the plurality of clamping rods (4212). The elastic reset members (4213) are arranged between the clamping rods (4212) and the bottom of the installation space so that the clamping rods (4212) can move toward the outside of the housing (4211).
2. The UAV according to claim 1, characterized in that, The cutting mechanism (20) further includes a second cutting blade (23) disposed on the mounting plate (21), wherein the first cutting blade (22) and the second cutting blade (23) are disposed at an acute angle.
3. The UAV according to claim 1, characterized in that, The cutting mechanism (20) further includes a drive wheel (24) and a transmission wheel (25) meshing with the drive wheel (24). The number of teeth of the transmission wheel (25) is greater than the number of teeth of the drive wheel (24). The drive wheel (24) and the transmission wheel (25) are rotatably mounted on the mounting plate (21). The drive wheel (24) is mounted on the shaft of the first drive member. The first cutting blade (22) has a transmission tooth, and the transmission wheel (25) meshes with the transmission tooth.
4. The UAV according to claim 1, characterized in that, The second clamping member (422) has a second clamping surface, and a clamping space (423) is formed between the first clamping surface and the second clamping surface. The shape of the second clamping surface can be changed to change the shape of the clamping space (423).
5. The UAV according to claim 1, characterized in that, The first clamping member (421) further includes a plurality of connecting rods (4214), which are arranged one-to-one with a plurality of clamping rods (4212). Each connecting rod (4214) is fitted with an elastic reset member (4213) on its outer periphery. The first end of the connecting rod (4214) is connected to the box body (4211), and the second end of the connecting rod (4214) is located inside the clamping rod (4212). The clamping rod (4212) is movably arranged at the second end of the connecting rod (4214).
6. The UAV according to claim 5, characterized in that, The clamping rod (4212) includes a block (42121), the block (42121) having a receiving space (421211) and a strip opening (421212) communicating with the receiving space (421211), the minimum radial dimension of the receiving space (421211) being greater than the length of the strip opening (421212); The connecting rod (4214) includes a strip-shaped rod body (42141) and a shaft body (42142) connected to the strip-shaped rod body (42141), and the strip-shaped opening (421212) allows the strip-shaped rod body (42141) to pass through; The connecting rod (4214) has an installation state and a limiting state. When the connecting rod (4214) is in the installation state, the strip rod body (42141) is correspondingly arranged with the strip opening (421212). When the connecting rod (4214) is in the limiting state, the strip rod body (42141) is located in the accommodating space (421211) and is arranged to intersect with the strip opening (421212).
7. The UAV according to claim 6, characterized in that, The connecting rod (4214) also includes a shaft (42142), the first end of which is connected to the strip rod (42141), the bottom of the box (4211) is provided with a plurality of mounting holes (42111), and the second end of the shaft (42142) is detachably connected to the mounting holes (42111).
8. The UAV according to any one of claims 1 to 7, characterized in that, The drone body (10) has a controller, and the drone also includes an ultrasonic sensor connected to the drone body (10), the ultrasonic sensor being signal-connected to the controller, and / or, the drone also includes a camera structure connected to the drone body (10), the camera structure being signal-connected to the controller.
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