Unmanned aerial vehicle arm machining clamp

Abstract

The utility model provides a kind of unmanned aerial vehicle arm processing fixture, belong to arm processing technical field.It include mounting plate, the top of mounting plate is drilled with the hole of passing, the top of mounting plate is equipped with the fixed component of auxiliary arm fixed location corresponding the hole of passing, the fixed component includes protruding seat, the top of protruding seat is protrudingly provided with hinged seat, the hinged seat is symmetrically hinged and is equipped with support and extension rod, the support and the extension rod are fixedly connected by handle, the end of extension rod away from support is equipped with the installation block of sleeve installation, the bottom of installation block is equipped with the pressing seat of auxiliary arm top pressure, the protruding seat is symmetrically equipped with positioning assembly, and the positioning assembly is fixed between the hole of passing cooperation.The utility model is formed dynamic adaptation mechanism by the hole of passing of rectangular array setting and detachable fixed component, effectively solve the size compatible problem of multiple-specification unmanned aerial vehicle arm processing.

Description

Technical Field

[0001] This utility model relates to the field of robotic arm processing technology, and in particular to a jig for processing unmanned aerial vehicle (UAV) robotic arms. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices. Types include unmanned vertical takeoff and landing aircraft, unmanned airships, unmanned helicopters, unmanned multi-rotor aircraft, and unmanned paragliders. Compared to manned aircraft, UAVs are smaller, less expensive, and easier to use. Before leaving the factory, UAVs require drilling and installation work on their entire arms.

[0003] Existing UAV arm machining fixtures mostly adopt fixed mounting holes and non-adjustable clamping structures. Conventional fixtures typically only have a single row or fixed spacing of mounting holes on the mounting plate, which makes it impossible to adjust the position of the fixing components according to the different diameters of the arms. Therefore, this application provides a UAV arm machining fixture to meet the requirements. Utility Model Content

[0004] The technical problem to be solved by this utility model is to provide a UAV arm processing fixture to solve the problem that existing UAV arm processing fixtures mostly adopt fixed mounting holes and non-adjustable clamping structures. Conventional fixtures usually only have a single row or fixed spacing of mounting holes on the mounting plate, which makes it impossible to adjust the position of the fixing components according to the different diameters of the arms.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: A jig for machining a drone arm includes a mounting plate with a through hole drilled at the top. A fixing component for fixing the drone arm is installed on the top of the mounting plate corresponding to the through hole. The fixing component includes a protruding seat with a hinge seat protruding from the top of the protruding seat. A support rod and an extension rod are symmetrically hinged at the hinge seat. The support rod and the extension rod are fixedly connected by a handle. A mounting block is sleeved on the end of the extension rod away from the support rod. A pressing seat for pressing the drone arm is installed at the bottom of the mounting block. Positioning components are symmetrically installed on the protruding seat and are fixedly engaged with the through hole.

[0006] Optionally, a screw is vertically fixed at the top of the pressing seat, the screw is installed through the mounting block, and a nut is threaded onto the screw, the nut pressing against the top of the mounting block.

[0007] Optionally, the mounting block has a U-shaped plate structure, and two mounting blocks are symmetrically arranged.

[0008] Optionally, a plurality of through holes are provided, and the plurality of through holes are arranged in a rectangular array on the top of the mounting plate, and the through holes penetrate the mounting plate vertically.

[0009] Optionally, the positioning assembly includes a positioning cylinder fixed on a protruding seat, a pressure chamber inside the positioning cylinder, a pressure seat slidably disposed in the pressure chamber, a trumpet-shaped extrusion chamber on the side of the positioning cylinder, a positioning ball rollingly disposed in the extrusion chamber, a slide rod vertically fixed at the top of the pressure seat, a sealing seat fixed at the top of the slide rod, and a pressure spring for assisting the pressure seat in pressing down is installed in the pressure chamber.

[0010] Optionally, the bottom of the pressure seat is conical, the positioning ball presses against the outer edge of the pressure seat, and a pull ring is fixed at the top of the sealing seat.

[0011] Optionally, a base is installed below the mounting plate, and support columns are vertically fixed at each of the four corners between the base and the mounting plate.

[0012] Compared with the prior art, this utility model has at least the following beneficial effects: In the above solution, the through holes set by the rectangular array and the detachable fixing components form a dynamic adaptation mechanism, which effectively solves the size compatibility problem in the processing of multi-specification UAV arms; The fixed component, which uses a linkage structure of support rod and extension rod, allows for synchronous pressing action of the pressing seat through a single point operation of the handle. This simplifies the operation process and improves positioning efficiency. The screw and nut mechanism of the pressing seat enables precise adjustment of the pressing position, making it suitable for processing different sizes of machine arm shapes and avoiding the limited applicability of traditional clamps due to their fixed dimensions. Attached Figure Description

[0013] The accompanying drawings, which are incorporated herein and form part of the specification, illustrate embodiments of the present invention and, together with the specification, further serve to explain the principles of the present invention and enable those skilled in the art to implement and use the present invention.

[0014] Figure 1 A schematic diagram of the three-dimensional structure of a machining fixture for a drone arm; Figure 2 A three-dimensional structural diagram of the fixing component in the machining fixture for the UAV arm; Figure 3 Fixtures for UAV Arms Figure 1 Enlarged structural diagram at point A; Figure 4 A longitudinal sectional view of the positioning assembly for the machining fixture of a drone arm.

[0015] [Figure Labels]

[0016] 1. Base; 2. Mounting plate; 3. Support column; 4. Through hole; 5. Fixing component; 6. Protruding seat; 7. Handle; 8. Support rod; 9. Extension rod; 10. Mounting block; 11. Pressing seat; 111. Screw; 112. Nut; 12. Positioning component; 13. Positioning cylinder; 131. Extrusion chamber; 14. Positioning ball; 15. Top pressure seat; 16. Slide rod; 161. Sealing seat; 17. Top pressure spring.

[0017] As shown in the figure, specific structures and devices are marked in the figure to clearly illustrate the structure of the embodiment of this utility model. However, this is only for illustrative purposes and is not intended to limit this utility model to this specific structure, device and environment. Those skilled in the art can adjust or modify these devices and environments according to specific needs. Detailed Implementation

[0018] The following is a detailed description of a UAV arm processing fixture provided by this utility model, with reference to the accompanying drawings and specific embodiments. It should be noted that, to make the embodiments more detailed, the following embodiments are the best and preferred embodiments; those skilled in the art can also use other alternative methods to implement some known technologies; and the accompanying drawings are only for more specific description of the embodiments and are not intended to specifically limit this utility model.

[0019] It should be noted that the use of terms such as "an embodiment," "an embodiment," "an exemplary embodiment," and "some embodiments" in the specification indicates that the described embodiment may include a specific feature, structure, or characteristic, but not every embodiment necessarily includes that specific feature, structure, or characteristic. Furthermore, when a specific feature, structure, or characteristic is described in connection with an embodiment, implementing such a feature, structure, or characteristic in conjunction with other embodiments (whether explicitly described or not) should be within the knowledge of those skilled in the art.

[0020] Generally, terms can be understood at least partly from their use in context. For example, depending at least partly on the context, the term "one or more" as used herein can be used to describe any feature, structure, or characteristic in a singular sense, or a combination of features, structures, or characteristics in a plural sense. Additionally, the term "based on" can be understood not necessarily to convey an exclusive set of factors, but rather, alternatively, depending at least partly on the context, to allow for the presence of other factors that are not necessarily explicitly described.

[0021] It is understood that the meanings of “on”, “above”, and “above” in this utility model should be interpreted in the broadest manner, such that “on” not only means “directly on” something, but also includes the meaning of being “on” something with an intervening feature or layer, and that “above” or “above” not only means “on” something, but also includes the meaning of being “on” something without an intervening feature or layer.

[0022] Furthermore, spatially related terms such as “below,” “under,” “lower,” “above,” and “upper” are used herein for convenience to describe the relationship of one element or feature to one or more other elements or features, as illustrated in the accompanying drawings. Spatially related terms are intended to cover different orientations in the use or operation of the device other than those depicted in the accompanying drawings. The device may be oriented in other ways, and the spatially related descriptive terms used herein can be interpreted similarly.

[0023] like Figure 1-4 As shown, an embodiment of this utility model provides a UAV arm processing fixture, including a mounting plate 2, a base 1 mounted below the mounting plate 2, and support columns 3 vertically fixed at the four corners between the base 1 and the mounting plate 2. A through hole 4 is drilled at the top of the mounting plate 2, and a fixing component 5 for auxiliary arm fixing is installed at the top of the mounting plate 2 corresponding to the through hole 4. A plurality of through holes 4 are provided, and the plurality of through holes 4 are arranged in a rectangular array at the top of the mounting plate 2. The through holes 4 vertically penetrate the mounting plate 2. The through holes 4 arranged in a rectangular array and the detachable fixing component 5 form a dynamic adaptation mechanism, which effectively solves the size compatibility problem of processing UAV arms of various specifications.

[0024] The aforementioned fixing component 5 includes a protruding seat 6, with a hinge seat protruding from the top of the protruding seat 6. A support rod 8 and an extension rod 9 are symmetrically hinged at the hinge seat. The support rod 8 and the extension rod 9 are fixedly connected by a handle 7. An installation block 10 is sleeved on the end of the extension rod 9 away from the support rod 8. The installation block 10 has a U-shaped plate structure, and there are two installation blocks 10 symmetrically arranged. A pressing seat 11 for auxiliary arm pressing is installed at the bottom of the installation block 10. A screw 111 is vertically fixed at the top of the pressing seat 11. The screw 111 is installed through the installation block 10, and a nut 112 is threaded onto the screw 111. The nut 112 presses against the top of the installation block 10.

[0025] By using the fixed component 5, which employs a linkage structure of support rod 8 and extension rod 9, the synchronous pressing action of the pressing seat 11 can be achieved through a single-point operation of handle 7, simplifying the operation process and improving positioning efficiency. Through the screw 111 and nut 112 cooperation structure of the pressing seat 11, the pressing position can be finely adjusted, which can adapt to the processing requirements of different specifications of machine arm shapes, avoiding the problem of limited applicability caused by the fixed size of traditional fixtures.

[0026] The protruding seat 6 is symmetrically equipped with positioning components 12, which are fixed to the through hole 4. The positioning components 12 include a positioning cylinder 13 fixed on the protruding seat 6. The positioning cylinder 13 has a pressure chamber inside, and a pressure seat 15 is slidably arranged in the pressure chamber. The bottom of the pressure seat 15 is conical. Positioning balls 14 press against the outer edge of the pressure seat 15. A pull ring is fixed at the top of the sealing seat 161. A trumpet-shaped extrusion chamber 131 is opened on the side of the positioning cylinder 13. Positioning balls 14 are slidably arranged in the extrusion chamber 131. A slide rod 16 is vertically fixed at the top of the pressure seat 15. The sealing seat 161 is fixed at the top of the slide rod 16. A pressure spring 17 is installed in the pressure chamber to assist the pressure seat 15 in pressing.

[0027] By using the positioning component 12, the horn-shaped extrusion cavity 131 of the positioning component 12 and the rolling engagement design of the positioning ball 14 transform the traditional sliding friction into rolling friction, significantly reducing the frictional resistance during the positioning process. At the same time, the continuous top pressure provided by the top pressure spring 17 ensures that the positioning ball 14 and the inner wall of the through hole 4 always maintain close contact, effectively preventing displacement or vibration during the machining process of the machine arm. The sealing structure of the top pressure cavity inside the positioning cylinder 13, combined with the pull ring design on the top of the sealing seat 161, not only ensures the working stability of the top pressure spring 17, but also facilitates quick disassembly and maintenance.

[0028] The working principle of the technical solution provided by this utility model is as follows: The mounting plate 2 serves as the main support structure, and the rectangular array of through holes 4 drilled on its top penetrates the thickness direction of the mounting plate 2, which can reduce the overall weight and facilitate real-time observation of the fixed status of the machine arm during processing. The hinged support rod 8 and extension rod 9 form a linkage mechanism. The operating handle 7 can synchronously control the swing angle of the two rods, so that the mounting block 10 at the end of the extension rod 9 drives the pressing seat 11 to achieve a vertical pressing action. The pressing seat 11 is inserted into the bottom of the mounting block 10 through the screw 111. With the threaded locking structure of the nut 112, the extension length of the pressing seat 11 can be finely adjusted to adapt to machine arms of different diameters.

[0029] The positioning components 12 are symmetrically arranged on both sides of the protruding seat 6. The positioning cylinder 13 has a top pressure cavity. The top pressure spring 17 pushes the top pressure seat 15 to move downward. The conical structure at the bottom of the top pressure seat 15 squeezes the positioning ball 14 to expand outward along the trumpet-shaped squeezing cavity 131, and finally forms a three-point positioning fit with the bottom inner wall of the through hole 4, and fixes the fixing component 5 in the corresponding position, thereby adapting to the fixing requirements of different sized arms.

[0030] This utility model encompasses any substitutions, modifications, equivalent methods, and solutions made within the spirit and scope of this utility model. To provide the public with a thorough understanding of this utility model, specific details are described in detail in the following preferred embodiments; however, those skilled in the art will fully understand this utility model even without these detailed descriptions. Furthermore, to avoid unnecessary confusion regarding the essence of this utility model, well-known methods, processes, procedures, components, and circuits are not described in detail.

[0031] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the principle of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.

Claims

1. A machining fixture for a drone arm, characterized in that, The system includes a mounting plate (2), with a through hole (4) drilled at the top of the mounting plate (2). A fixing component (5) for fixing the auxiliary arm is installed at the top of the mounting plate (2) corresponding to the through hole (4). The fixing component (5) includes a protruding seat (6). A hinge seat is protruding at the top of the protruding seat (6). A support rod (8) and an extension rod (9) are symmetrically hinged at the hinge seat. The support rod (8) and the extension rod (9) are fixedly connected by a handle (7). An installation block (10) is installed at the end of the extension rod (9) away from the support rod (8). A pressing seat (11) for pressing the auxiliary arm is installed at the bottom of the installation block (10). A positioning component (12) is symmetrically installed on the protruding seat (6). The positioning component (12) is fixedly engaged with the through hole (4).

2. The UAV arm machining fixture according to claim 1, characterized in that, A screw (111) is vertically fixed at the top of the pressing seat (11). The screw (111) is installed through the mounting block (10). A nut (112) is threaded onto the screw (111). The nut (112) presses against the top of the mounting block (10).

3. The UAV arm machining fixture according to claim 2, characterized in that, The mounting block (10) has a U-shaped plate structure, and two mounting blocks (10) are symmetrically arranged.

4. The UAV arm machining fixture according to claim 1, characterized in that, The through holes (4) are provided in a plurality of them. The plurality of through holes (4) are arranged in a rectangular array on the top of the mounting plate (2). The through holes (4) penetrate the mounting plate (2) vertically.

5. The UAV arm machining fixture according to claim 1, characterized in that, The positioning assembly (12) includes a positioning cylinder (13) fixed on the protruding seat (6). The positioning cylinder (13) has a top pressure cavity inside. A top pressure seat (15) is slidably arranged in the top pressure cavity. A trumpet-shaped extrusion cavity (131) is opened on the side of the positioning cylinder (13). A positioning ball (14) is slidably arranged in the extrusion cavity (131). A slide rod (16) is vertically fixed at the top of the top pressure seat (15). A sealing seat (161) is fixed at the top of the slide rod (16). A top pressure spring (17) is installed in the top pressure cavity to assist the top pressure seat (15) in pressing.

6. The UAV arm machining fixture according to claim 5, characterized in that, The bottom of the top pressure seat (15) is conical, the positioning ball (14) presses against the outer edge of the top pressure seat (15), and a pull ring is fixed at the top of the sealing seat (161).

7. The UAV arm machining fixture according to claim 1, characterized in that, A base (1) is installed below the mounting plate (2), and support columns (3) are vertically fixed at the four corners between the base (1) and the mounting plate (2).

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