A cutting device and system for UAV processing

The machining system addresses the challenge of securely holding irregular drone components by using a modular and adjustable fixture system, enabling continuous processing without disassembly, thus enhancing machining efficiency.

CN118832220BActive Publication Date: 2025-07-15SHENZHEN DEXIDO MANUFACTURING CO LTD
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Patent Information

Application Number
CN202411134525.4
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-08-19
Publication Date
2025-07-15
Estimated Expiration
2044-08-19

AI Technical Summary

Technical Problem

When existing milling machines process drone workpieces, since most of the drone workpieces are irregular in shape, it is difficult to use traditional fixtures to apply to all parts, and the fixture needs to be completely released after processing one workpiece to hold the next workpiece.

Method used

A cutting device for machining of UAVs is designed, including a milling machine body, a Y-axis screw platform, an X-axis screw platform and a workpiece operation platform. It adopts a detachable clamping structure. The clamping structure consists of a base assembly, an adjustment assembly and a workpiece limiting assembly. The limit clamping of irregular workpieces is achieved through clamping holes and clamping units, and the workpiece is replaced easily after processing is completed.

Benefits of technology

The stable clamping of irregular drone workpieces is achieved, avoiding offset during processing, and no need to completely release the fixture when the workpiece is replaced, improving processing efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention provides a cutting device and system for unmanned aerial vehicle (UAV) processing, belonging to the technical field of UAV processing. It includes a milling machine body, on which a Y-axis lead screw platform is fixedly connected. A lead screw nut of the Y-axis lead screw platform is fixedly connected with an X-axis lead screw platform, and a lead screw nut of the X-axis lead screw platform is fixedly connected with a workpiece operation platform. A number of uniformly arranged clamping holes are formed on the workpiece operation platform; a clamping structure, located inside the clamping holes and detachably connected thereto, is used for limiting and clamping UAV processing parts; the clamping structure includes a base assembly detachably connected to the inside of the clamping holes. The clamping structure of the present invention can clamp irregular UAV workpieces, and after the workpiece processing is completed, it is convenient to fixedly clamp the next workpiece to be processed.
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Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV) processing, and particularly to a cutting device and system for UAV processing. Background Art

[0002] A milling machine refers to a machine tool that uses a milling cutter to process various surfaces of a workpiece. Usually, the rotational movement of the milling cutter is the main movement, and the movement of the workpiece and the milling cutter is the feed movement. On a milling machine, planes, grooves, toothed parts, spiral surfaces, and various curved surfaces can be processed. It can also be used for machining the surface of a rotating body, internal holes, and cutting work, etc. When the milling machine is working, the workpiece is installed on the workbench or attachments such as a dividing head. The rotation of the milling cutter is the main movement, supplemented by the feed movement of the workbench or the milling head, and the required machined surface of the workpiece can be obtained.

[0003] When the current milling machine processes UAV workpieces, since most UAV workpieces are irregular in shape, it is difficult to apply traditional fixtures to all UAV components. Moreover, after machining one workpiece, the fixture needs to be completely released and then clamped to the next workpiece. Therefore, the present application provides a cutting device and system for UAV processing to meet the requirements. Summary of the Invention

[0004] The technical problem to be solved by the present invention is to provide a cutting device and system for UAV processing to solve the problem that when the current milling machine processes UAV workpieces, since most UAV workpieces are irregular in shape, it is difficult to apply traditional fixtures to all UAV components, and after machining one workpiece, the fixture needs to be completely released and then clamped to the next workpiece.

[0005] To solve the above technical problem, the present invention provides the following technical solutions:

[0006] A cutting device for UAV processing, comprising a milling machine body, on which a Y-axis lead screw platform is fixedly connected. A lead screw nut of the Y-axis lead screw platform is fixedly connected with an X-axis lead screw platform. A lead screw nut of the X-axis lead screw platform is fixedly connected with a workpiece operation platform, and a plurality of rows of uniformly arranged clamping holes are formed on the workpiece operation platform; a clamping structure, located inside the clamping holes and detachably connected thereto, and the clamping structure is used for limiting and clamping UAV processing parts; the clamping structure includes a base assembly detachably connected inside the clamping holes, an adjusting assembly is slidably connected to the base assembly, an internal gear ring is fixedly connected to the adjusting assembly, and a workpiece limiting assembly is clamped inside the internal gear ring.

[0007] Optionally, the base assembly includes a first rotating column and a second rotating column connected by rotation. The outer surface walls at both ends of the first rotating column are respectively sleeved with a first sliding sleeve and an embedding column. The length of the first sliding sleeve is 1 / 4 of the length of the embedding column, and the diameter of the first sliding sleeve is smaller than the diameter of the embedding column. The outer surface wall of the second rotating column is sleeved with a second sliding sleeve, and the diameter of the second sliding sleeve is the same as the diameter of the first sliding sleeve. Four corresponding sliding grooves are provided on the outer surface walls of the first sliding sleeve and the second sliding sleeve, and the four sliding grooves are distributed at 90° to each other; a first clamping unit is further included for detachably connecting the embedding column and the clamping hole.

[0008] Optionally, the first clamping unit includes a first clamping piece fixedly connected to the outer surface wall of the embedding column. The first clamping piece is connected by a first limiting section and two supporting sections. The first limiting section is an annular elastic sheet structure with a convex middle and concave sides. The two ends of the first limiting section are fixedly connected to the outer surface wall of the embedding column. The two ends of the supporting section are respectively fixedly connected to the inner surface wall of the concave section of the first limiting section and the outer surface wall of the embedding column corresponding to the center of the convex section of the first limiting section. The two supporting sections are symmetrically installed in the gap between the first limiting section and the embedding column. A first clamping groove adapted to the shape of the first clamping piece is provided on the inner surface wall of the clamping hole. The embedding column and the clamping hole are adaptively clamped through the first clamping piece and the first clamping groove.

[0009] Optionally, the adjusting assembly includes an adjusting sleeve slidably connected to the second sliding sleeve. Four sliding rods adapted to the sliding grooves are provided on the inner surface wall of the adjusting sleeve. The length of the sliding rod is 1 / 2 of the distance between the farthest two ends of the sliding groove on the first sliding sleeve and the sliding groove on the second sliding sleeve. An installation groove is provided on the outer surface wall of the adjusting sleeve; a second clamping unit is further included for clamping the adjusting sleeve and the first sliding sleeve to each other.

[0010] Optionally, the second clamping unit includes a second clamping piece fixedly connected to the inner surface wall of the open end of the adjusting sleeve. A second clamping groove is provided on the outer surface wall of the first sliding sleeve near the embedding column. The adjusting sleeve and the first sliding sleeve are clamped through the cooperation of the second clamping piece and the second clamping groove; the second clamping piece is connected by two deformation sections and a second limiting section. The two ends of the second limiting section are fixedly connected with deformation sections, and the other ends of the two deformation sections are fixedly connected to the inner surface wall of the adjusting sleeve. The two deformation sections are concave, the second limiting section is convex, and the thickness of the deformation section and the second limiting section gradually changes from thin to thick from the middle to both sides.

[0011] Optionally, the inner gear ring is fixedly connected to the bottom end of the mounting groove, and an adjustment gap is provided between the inner ring of the inner gear ring and the inner surface wall of the mounting groove, and the angle marking groove is opened on one side of the inner gear ring.

[0012] Optionally, the workpiece limiting assembly includes an external rack symmetrically placed in the adjustment gap, the external rack is clamped with the inner ring of the inner gear ring, one side of the external rack is fixedly connected with an adjustment limit plate, one end of the adjustment limit plate is fixedly connected with a connecting strip, one end of the connecting strip is fixedly connected with a workpiece baffle, and a convex strip is fixedly connected to the top of one side of the workpiece baffle.

[0013] Optionally, an annular adjustment groove matching the shape of the adjustment limit piece is opened on the top of the installation groove, and the height of the adjustment groove is the sum of the height of the adjustment limit piece and the height of the connecting strip.

[0014] Optionally, the height of the outer rack and the height of the connecting strip are consistent with the height of the outer rack, the height of the mounting groove is three times the height of the inner gear ring, the bottom end of the workpiece baffle is an outward-turned structure, and an eight-shaped structure is formed between the two workpiece baffles.

[0015] Another aspect of the present invention provides a cutting system for unmanned aerial vehicle processing, including the cutting device for unmanned aerial vehicle processing described above, and also including a control unit, connected to the Y-axis screw platform, the X-axis screw platform and the milling head motor, used to control the Y-axis screw platform and the X-axis screw platform to drive the workpiece operating platform to move in the X-axis and Y-axis directions, and control the milling head motor to drive the vertical milling head to perform cutting processing on the workpiece.

[0016] Compared with the prior art, the present invention has at least the following beneficial effects:

[0017] In the above scheme, by setting up a clamping structure, irregular drone workpieces can be clamped by the clamping structure, and after the workpiece processing is completed, it is convenient to fix and clamp the next workpiece to be processed.

[0018] A base assembly is provided to fix the entire clamping structure in the clamping hole. When the workpiece needs to be replaced, it can be cooperated with the adjusting assembly to release the limit on the workpiece without removing the base assembly. The adjusting assembly adjusts the workpiece limiting assembly. The workpiece limiting assembly is used to limit and fix the drone workpiece to be processed. Through several workpiece limiting assemblies, non-standard workpieces can be cooperated and limited so that they will not deviate during the processing process.

[0019] By setting an adjusting sleeve and turning the adjusting sleeve, the second rotating column can be driven to rotate on the first rotating column, so that the workpiece limiting assembly on the adjusting sleeve is offset, thereby releasing the limiting of the workpiece.

[0020] By providing the first clamping unit and the second clamping unit, the first clamping unit is used to limit and fix the embedding post in the clamping hole, facilitating the placement and removal of the embedding post. The second clamping unit is used to increase the fixing strength between the adjusting sleeve and the first sliding sleeve when fixing the workpiece, preventing the adjusting sleeve from sliding upwards due to vibration during the cutting operation of the workpiece. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] The drawings incorporated herein and constituting a 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 relevant art to implement and use the present invention.

[0022] Figure 1 is a schematic three-dimensional structure diagram of a cutting device for UAV processing;

[0023] Figure 2 is a schematic three-dimensional structure diagram of the assembly of a workpiece operation platform and a clamping structure;

[0024] Figure 3 is a schematic three-dimensional structure diagram of the clamping structure;

[0025] Figure 4 is a schematic exploded three-dimensional structure diagram of the clamping structure;

[0026] Figure 5 is a schematic partially cut-away three-dimensional structure diagram of the clamping structure;

[0027] Figure 6 is a schematic cut-away three-dimensional structure diagram of the base assembly;

[0028] Figure 7 is Figure 6 a schematic three-dimensional structure diagram of part A in

[0029] Figure 8 is a schematic partially cut-away assembled three-dimensional structure diagram of an adjusting assembly, an internal gear ring, and a workpiece limiting assembly;

[0030] Figure 9 is Figure 8 a schematic three-dimensional structure diagram of part B in

[0031] Figure 10 is a schematic first-angle assembled three-dimensional structure diagram of an internal gear ring and a workpiece limiting assembly;

[0032] Figure 11 is a schematic second-angle assembled three-dimensional structure diagram of an internal gear ring and a workpiece limiting assembly.

[0033] [Reference Numerals]

[0034] 1. Milling machine body; 2. Y-axis lead screw platform; 3. X-axis lead screw platform; 4. Workpiece operation platform; 41. Clamping hole; 5. Clamping structure; 51. Base component; 511. First rotating column; 512. Second rotating column; 513. Second clamping groove; 514. Embedded column; 515. First clamping piece; 5151. First limiting section; 5152. Support section; 516. First sliding sleeve; 517. Second sliding sleeve; 518. Chute; 52. Adjusting component; 521. Adjusting sleeve; 522. Installation groove; 523. Slide bar; 524. Second clamping piece; 5241. Deformation section; 5242. Second limiting section; 525. Adjusting groove; 53. Internal gear ring; 531. Angle scale groove; 54. Workpiece limiting component; 541. External rack; 542. Adjusting limiting piece; 543. Ridge; 544. Workpiece baffle; 545. Connecting bar.

[0035] As shown in the figure, in order to clearly implement the structure of the embodiments of the present invention, specific structures and devices are marked in the figure, but this is only for illustrative needs and is not intended to limit the present invention to this specific structure, device and environment. According to specific needs, those of ordinary skill in the art can adjust or modify these devices and environments. Detailed implementation manners

[0036] The following describes in detail a cutting device and system for UAV processing provided by the present invention in conjunction with the accompanying drawings and specific embodiments. At the same time, it should be noted here that in order to make the embodiments more detailed, the following embodiments are the best and preferred embodiments. For some well-known technologies, those skilled in the art can also adopt other alternative methods for implementation; moreover, the accompanying drawings are only for more specific description of the embodiments and are not intended to specifically limit the present invention.

[0037] It should be pointed out that in the specification, terms such as "one embodiment", "embodiment", "exemplary embodiment", "some embodiments", etc. indicate that the described embodiments may include specific features, structures or characteristics, but not necessarily every embodiment includes this specific feature, structure or characteristic. In addition, when combining embodiments to describe specific features, structures or characteristics, implementing such features, structures or characteristics in combination with other embodiments (whether explicitly described or not) should be within the knowledge scope of those skilled in the relevant art.

[0038] Generally, terms can be understood at least in part from their use in the context. For example, at least in part depending on the context, the term "one or more" used herein can be used to describe any feature, structure or characteristic in a singular sense, or can be used to describe a combination of features, structures or characteristics in a plural sense. Additionally, the term "based on" can be understood as not necessarily intended to convey a set of exclusive factors, but rather, at least in part depending on the context, can allow for the existence of other factors that may not be explicitly described.

[0039] It will be understood that the terms "on", "above", and "over" in the present invention should be construed in the broadest manner such that "on" not only means "directly on" something, but also includes the meaning of being "on" something with intervening features or layers therebetween, and "above" or "over" not only means "above" or "over" something, but may also include the meaning of being "above" or "over" something with no intervening features or layers therebetween.

[0040] In addition, spatial relative terms such as "under", "below", "lower", "above", "upper", etc. may be used herein for convenience of description to describe the relationship of one element or feature to another or other elements or features, as shown in the figures. The spatial relative terms are intended to cover different orientations in the use or operation of the device in addition to the orientation depicted in the figures. The device may be oriented in other ways, and the spatial relative descriptors used herein may be interpreted accordingly.

[0041] Such as Figures 1 to 3As shown in the figure, an embodiment of the present invention provides a cutting device for drone processing, including a milling machine body 1. A Y-axis lead screw platform 2 is fixedly connected to the milling machine body 1. An X-axis lead screw platform 3 is fixedly connected to the lead screw nut of the Y-axis lead screw platform 2. The milling machine body 1, the Y-axis lead screw platform 2, and the X-axis lead screw platform 3 are all prior arts. A workpiece operation platform 4 is fixedly connected to the lead screw nut of the X-axis lead screw platform 3. The bottom of the workpiece operation platform 4 is fixedly connected to the X-axis lead screw platform 3. The workpiece operation platform 4 is used to place the drone workpiece to be processed. A number of uniformly arranged clamping holes 41 are provided on the workpiece operation platform 4. The clamping holes 41 penetrate through the workpiece operation platform 4, which is convenient for discharging the waste chips generated during the processing of the drone workpiece and at the same time provides an installation space for the clamping structure 5. The clamping structure 5 is located inside the clamping hole 41 and is detachably connected thereto. The clamping structure 5 is used to limit and clamp the drone processing parts. The irregular drone workpiece can be clamped by the clamping structure 5, and after the workpiece processing is completed, it is convenient to fixedly clamp the next workpiece to be processed. The clamping structure 5 includes a base component 51 detachably connected to the inside of the clamping hole 41. The base component 51 is used to fix the entire clamping structure 5 in the clamping hole 41. At the same time, when it is necessary to replace the processed workpiece, it can cooperate with the adjustment component 52 to release the limit on the workpiece without removing the base component 51. An adjustment component 52 is slidably connected to the base component 51. The adjustment component 52 is used to provide an installation platform for the workpiece limit component 54 and at the same time is adapted to the base component 51 to adjust the workpiece limit component 54. An internal gear ring 53 is fixedly connected to the adjustment component 52. The internal gear ring 53 is used to clamp and limit the workpiece limit component 54. The workpiece limit component 54 is clamped inside the internal gear ring 53. The workpiece limit component 54 is used to limit and fix the drone workpiece to be processed. The irregular workpiece can be cooperatively limited by a number of workpiece limit components 54 so that it will not shift during the processing.

[0042] When cutting and processing the drone workpiece, place the drone workpiece to be processed on the workpiece operation platform 4. According to the shape of the workpiece, selectively fix the clamping structure 5 on the clamping holes 41 around the workpiece. The workpiece is limited and fixed by a number of workpiece limit components 54, so as to fix the workpiece on the workpiece operation platform 4, and then carry out the processing procedure of the workpiece.

[0043] As Figure 2 and Figures 4 to 6As shown, the base assembly 51 includes a first rotating column 511 and a second rotating column 512 that are rotatably connected. The diameters of the first rotating column 511 and the second rotating column 512 are the same. The first rotating column 511 and the second rotating column 512 are rotatably connected by a rotating shaft. At both ends of the outer surface wall of the first rotating column 511, a first sliding sleeve 516 and an embedding column 514 are respectively sleeved. The length of the first sliding sleeve 516 is 1 / 4 of the length of the embedding column 514, and the diameter of the first sliding sleeve 516 is smaller than the diameter of the embedding column 514. The diameter of the embedding column 514 is slightly smaller than the diameter of the clamping hole 41. A second sliding sleeve 517 is sleeved on the outer surface wall of the second rotating column 512. The diameter of the second sliding sleeve 517 is the same as the diameter of the first sliding sleeve 516. The diameters of the first sliding sleeve 516 and the second sliding sleeve 517 are the same, so that the open end of the adjusting sleeve 521 can slide from the second sliding sleeve 517 to the first sliding sleeve 516. Four corresponding sliding grooves 518 are provided on the outer surface walls of the first sliding sleeve 516 and the second sliding sleeve 517. The sliding grooves 518 are used to be adapted to the sliding rods 523, so that while the adjusting sleeve 521 can slide on the first sliding sleeve 516 and the second sliding sleeve 517, they will not rotate relative to each other. The four sliding grooves 518 are distributed at 90° to each other. It further includes a first clamping unit for detachably connecting the embedding column 514 to the clamping hole 41. The first clamping unit is used to limit and fix the embedding column 514 in the clamping hole 41, facilitating the placement and removal of the embedding column 514.

[0044] As Figure 2 , Figure 5 and Figure 6 shown, the first clamping unit includes a first clamping piece 515 fixedly connected to the outer surface wall of the embedding column 514. The first clamping piece 515 is connected by a first limiting section 5151 and two supporting sections 5152. The first limiting section 5151 is a ring-shaped elastic sheet structure that is convex in the middle and concave on both sides. The two ends of the first limiting section 5151 are fixedly connected to the outer surface wall of the embedding column 514. The two ends of the supporting section 5152 are respectively fixedly connected to the inner surface wall of the concave section of the first limiting section 5151 and the outer surface wall of the embedding column 514 corresponding to the center of the convex section of the first limiting section 5151. The two supporting sections 5152 are symmetrically installed in the gap between the first limiting section 5151 and the embedding column 514. A first clamping groove adapted to the shape of the first clamping piece 515 is provided on the inner surface wall of the clamping hole 41. The embedding column 514 and the clamping hole 41 are adaptively clamped through the first clamping piece 515 and the first clamping groove.

[0045] When the embedding post 514 is gradually inserted into the clamping hole 41, during the insertion process of the embedding post 514, the first limiting section 5151 of the first clamping piece 515 will contact the orifice wall of the clamping hole 41, and the orifice wall will squeeze the concave section, causing it to undergo compressive deformation. When the concave section is squeezed, it will also squeeze the supporting section 5152. Since the thickness of the supporting section 5152 gradually changes from thin to thick from the middle to both ends, when the supporting section 5152 is subjected to the squeezing force, it will undergo compressive deformation until the entire first clamping piece 515 is compressed and snapped into the clamping hole 41. When it moves to the first clamping groove inside the clamping hole 41, after the two supporting sections 5152 lose the squeezing force of the hole wall, they recover their deformation, thereby driving the first limiting section 5151 to recover its deformation, and then snapping into the first clamping groove to fix the embedding post 514 in the clamping hole 41.

[0046] Such as Figure 4 And Figure 8As shown, the adjusting assembly 52 includes an adjusting sleeve 521 slidably connected to the second sliding sleeve 517. The adjusting sleeve 521 is used to provide an installation position for the inner gear ring 53 and the workpiece stop assembly 54, and can drive the inner gear ring 53 and the workpiece stop assembly 54 installed thereon to slide on the second sliding sleeve 517. The inner ring diameter of the adjusting sleeve 521 is consistent with the outer ring diameter of the first sliding sleeve 516. When the adjusting sleeve 521 slides to the outer wall of the first sliding sleeve 516, the adjusting sleeve 521 will move the first sliding sleeve 516 and the second sliding sleeve 517. The first rotating column 511 and the second rotating column 512 are wrapped inside the adjusting sleeve 521, so that the first rotating column 511 and the second rotating column 512 will not rotate and deviate. The inner surface wall of the adjusting sleeve 521 is provided with four sliding rods 523 adapted to the sliding groove 518. The sliding rods 523 are located at the lower end of the inner surface wall of the adjusting sleeve 521. The sliding rods 523 are used to slide and limit the adjusting sleeve 521 to increase the strength of the adjusting sleeve 521. At the same time, when the sliding rods 523 are located at the sliding grooves 518 on the first sliding sleeve 516 and the second sliding sleeve 517 at the same time, it can help prevent the first rotating column 511 from rotating and deviating. 11 and the second rotating column 512 are offset, and the length of the sliding rod 523 is 1 / 2 of the distance between the farthest ends of the sliding groove 518 on the first sliding sleeve 516 and the sliding groove 518 on the second sliding sleeve 517. Therefore, when the adjusting sleeve 521 slides to the uppermost end of the sliding groove 518 on the second sliding sleeve 517, the adjusting sleeve 521 will expose the first rotating column 511 and the second rotating column 512. When it is necessary to release the limit of the workpiece to be processed, it is only necessary to slide the adjusting sleeve 521 upward to expose the first rotating column 511 and the second rotating column 512, thereby bending the adjusting sleeve 521. 1, which can drive the second rotating column 512 to rotate on the first rotating column 511, so that the workpiece limiting assembly 54 on the adjusting sleeve 521 is offset, thereby releasing the limiting position with the workpiece. The outer wall of the adjusting sleeve 521 is provided with a mounting groove 522, and also includes a second clamping unit for clamping the adjusting sleeve 521 and the first sliding sleeve 516 with each other. The second clamping unit is used to increase the fixing strength between the adjusting sleeve 521 and the first sliding sleeve 516 when fixing the workpiece, so as to prevent the adjusting sleeve 521 from sliding up due to vibration during the workpiece cutting operation.

[0047] like Figure 4 , Figure 8 and Figure 9As shown, the second clamping unit includes a second clamping piece 524 fixedly connected to the inner wall of the opening end of the adjusting sleeve 521. A second clamping groove 513 is formed on the outer wall of one end of the first sliding sleeve 516 close to the embedding column 514. The adjusting sleeve 521 and the first sliding sleeve 516 are clamped together through the cooperation of the second clamping piece 524 and the second clamping groove 513. The second clamping piece 524 is connected by two deformation segments 5241 and a second limiting segment 5242. Both ends of the second limiting segment 5242 are fixedly connected to the deformation segments 5241. The other ends of the two deformation segments 5241 are fixedly connected to the inner wall of the adjusting sleeve 521. The two deformation segments 5241 are concave, the second limiting segment 5242 is convex, and the thickness of the deformation segments 5241 and the second limiting segment 5242 gradually changes from thin to thick from the middle to both sides.

[0048] When the adjusting sleeve 521 slides down in the sliding groove 518, the deformation segment 5241 will contact the outer wall of the first sliding sleeve 516, and the outer wall of the first sliding sleeve 516 will squeeze the deformation segment 5241. Since the middle of the deformation segment 5241 is thin and both ends are thick, when it is subjected to the squeezing force of the first sliding sleeve 516, it will deform inward. While deforming inward, it will pull the second limiting segment 5242 to move towards the inner wall of the adjusting sleeve 521. During the continuous sliding of the adjusting sleeve 521, after the first sliding sleeve 516 squeezes the deformation segment 5241, it will contact the second limiting segment 5242 and squeeze the second limiting segment 5242 to deform until the entire second clamping piece 524 is compressed and deformed between the adjusting sleeve 521 and the first sliding sleeve 516. When the second clamping piece 524 slides into the second clamping groove 513, it will restore its deformation, thereby clamping the adjusting sleeve 521 in the second clamping groove 513 and limiting and fixing the two.

[0049] As Figure 4 and Figure 8 shown, the internal gear ring 53 is fixedly connected to the bottom end of the installation groove 522, and there is an adjustment gap between the inner ring of the internal gear ring 53 and the inner wall of the installation groove 522. An angle marking groove 531 is formed on one side of the internal gear ring 53. The angle marking groove 531 is used to display the included angle between the two connecting bars 545, which is convenient for the staff to adjust the positions of the two workpiece baffles 544.

[0050] As Figure 3 、 Figure 4 、 Figure 9 and Figure 11As shown, the workpiece limiting component 54 includes external racks 541 symmetrically placed in the adjustment gap. The external racks 541 are engaged with the inner ring of the internal gear ring 53. One side of the external rack 541 is fixedly connected with an adjustment limiting piece 542. One end of the adjustment limiting piece 542 is fixedly connected with a connecting bar 545. One end of the connecting bar 545 is fixedly connected with a workpiece baffle 544. A convex strip 543 is fixedly connected to the top of one side of the workpiece baffle 544. An annular adjustment groove 525 adapted to the shape of the adjustment limiting piece 542 is formed at the top of the installation groove 522. The height of the adjustment groove 525 is the sum of the height of the adjustment limiting piece 542 and the height of the connecting bar 545. The height of the external rack 541, the height of the connecting bar 545 are the same as the height of the external rack 541. The height of the installation groove 522 is three times the height of the internal gear ring 53. The bottom end of the workpiece baffle 544 is in an outward-turning structure. An eight-shaped structure is formed between the two workpiece baffles 544. The bottom end of the workpiece baffle 544 is in an outward-turning shape, which can more conveniently allow the two workpiece baffles 544 to be inserted into the side corners of the drone workpiece.

[0051] When it is necessary to limit irregular workpieces, select several side corners according to the shape of the workpiece, so that fixing these side corners can fix the whole workpiece. Judge the angles of the workpiece side corners according to the workpiece drawing, and then adjust the included angle between the two workpiece baffles 544. The included angle between the two workpiece baffles 544 ranges from 10° to 260°. When adjusting the workpiece baffle 544, the staff manually pulls up the workpiece baffle 544 to disconnect the external rack 541 from the connection with the internal gear ring 53 until the adjustment limiting piece 542 moves to the top of the annular adjustment groove 525. Rotate the external rack 541 and judge the angle of the connecting bar 545 at the position of the angle scale groove 531. When it is rotated to the appropriate angle, then press down the external rack 541 to make it snap into the internal gear ring 53 and limit and fix the external rack 541. When the angles of the two workpiece baffles 544 are both adjusted, slide down the adjustment sleeve 521 to drive the two workpiece baffles 544 to move downward. During the movement, the two workpiece baffles 544 in an eight-shaped structure will snap into the side corners of the workpiece, thereby limiting the side corners of the workpiece until the adjustment sleeve 521 slides to be limited and fixed with the first sliding sleeve 516.

[0052] On the other hand, the present invention also provides a cutting system for drone processing, including the cutting device for drone processing described above, and further including a control unit, which is connected to the Y-axis lead screw platform 2, the X-axis lead screw platform 3 and the milling head motor, and is used to control the Y-axis lead screw platform 2 and the X-axis lead screw platform 3 to drive the workpiece operation platform 4 to move in the X-axis and Y-axis directions, and control the milling head motor to drive the vertical milling head to perform cutting processing on the workpiece.

[0053] The working principle of the technical solution provided by the present invention is as follows: when cutting a UAV workpiece, the UAV workpiece to be processed is placed on the workpiece operating platform 4, and the clamping structure 5 is selectively fixed on the clamping holes 41 around the workpiece according to the shape of the workpiece.

[0054] When fixing the clamping structure 5, several side angles are selected according to the shape of the workpiece, so that the workpiece can be fixed as a whole by fixing these side angles, the angle of the workpiece side angle is determined according to the workpiece drawing, and then the angle between the two workpiece baffles 544 is adjusted. When adjusting the workpiece baffle 544, the staff manually pulls the workpiece baffle 544 upward to make the outer rack 541 disengage from the connection with the inner gear ring 53 until the adjustment limit plate 542 moves to the top of the annular adjustment groove 525, rotates the outer rack 541, and determines whether the connecting strip 545 is at an angle. The angle of the mark groove 531 is adjusted. When it is rotated to a suitable angle, the outer rack 541 is pressed downward so that it is inserted into the inner gear ring 53 to limit and fix the outer rack 541. When the angles of the two workpiece baffles 544 are adjusted, the adjusting sleeve 521 is slid downward to drive the two workpiece baffles 544 to move downward. During the movement, the two workpiece baffles 544 in an eight-shaped shape will be inserted into the side angles of the workpiece, thereby limiting the side angles of the workpiece until the adjusting sleeve 521 slides to be limited and fixed with the first sliding sleeve 516.

[0055] When the adjusting sleeve 521 slides down in the sliding groove 518, the deforming section 5241 will contact the outer wall of the first sliding sleeve 516, and the outer wall of the first sliding sleeve 516 will squeeze the deforming section 5241. Since the deforming section 5241 is thin in the middle and thick at both ends, it will deform inward when subjected to the squeezing force of the first sliding sleeve 516, and at the same time, the second limiting section 5242 will be pulled toward the inner wall of the adjusting sleeve 521. Continuing the sliding movement, after the first sliding sleeve 516 squeezes the deformation section 5241, it will contact the second limiting section 5242, squeezing the second limiting section 5242 to deform until the entire second clamping piece 524 is compressed and deformed between the adjusting sleeve 521 and the first sliding sleeve 516. When the second clamping piece 524 slides to the inside of the second clamping groove 513, the deformation is restored, thereby clamping the adjusting sleeve 521 into the second clamping groove 513, and the two are limited and fixed.

[0056] The workpiece is thereby fixed on the workpiece operating platform 4, and then the workpiece processing procedure is carried out. When the workpiece processing is completed and the workpiece to be processed needs to be released from the limit, the adjusting sleeve 521 only needs to be slid up to expose the first rotating column 511 and the second rotating column 512, so as to bend the adjusting sleeve 521 to drive the second rotating column 512 to rotate on the first rotating column 511, so that the workpiece limiting assembly 54 on the adjusting sleeve 521 is offset, thereby releasing the limit on the workpiece.

[0057] The present invention covers any alternatives, modifications, equivalent methods, and solutions made within the spirit and scope of the present invention. To enable the public to thoroughly understand the present invention, specific details are described in detail in the following preferred embodiments of the present invention, and those skilled in the art can fully understand the present invention without the description of these details. In addition, well-known methods, processes, procedures, components, and circuits are not described in detail to avoid unnecessary confusion about the essence of the present invention.

[0058] The above description is only a preferred embodiment of the present invention. It should be noted that for those of ordinary skill in the art, without departing from the principle of the present invention, several improvements and refinements can be made, and these improvements and refinements should also be regarded as the protection scope of the present invention.

Claims

1. A cutting device for processing unmanned aerial vehicles, characterized in that, It includes a milling machine body (1), on which a Y-axis lead screw platform (2) is fixedly connected. A workpiece operation platform (4) is fixedly connected to the lead screw nut of the Y-axis lead screw platform (2). An X-axis lead screw platform (3) is fixedly connected to the lead screw nut of the X-axis lead screw platform (3). A number of uniformly arranged clamping holes (41) are provided on the workpiece operation platform (4). A clamping structure (5) is located inside the clamping hole (41) and is detachably connected thereto. The clamping structure (5) is used for limiting and clamping the parts of the unmanned aerial vehicle to be processed. The clamping structure (5) includes a base component (51) detachably connected inside the clamping hole (41). An adjusting component (52) is slidably connected to the base component (51). An internal gear ring (53) is fixedly connected to the adjusting component (52). A workpiece limiting component (54) is clamped inside the internal gear ring (53). The base component (51) includes a first rotating column (511) and a second rotating column (512) that are rotatably connected. At both ends of the outer surface wall of the first rotating column (511), a first sliding sleeve (516) and an embedding column (514) are respectively sleeved. The length of the first sliding sleeve (516) is 1 / 4 of the length of the embedding column (514), and the diameter of the first sliding sleeve (516) is smaller than the diameter of the embedding column (514). A second sliding sleeve (517) is sleeved on the outer surface wall of the second rotating column (512). The diameter of the second sliding sleeve (517) is the same as the diameter of the first sliding sleeve (516). Four corresponding sliding grooves (518) are provided on the outer surface walls of the first sliding sleeve (516) and the second sliding sleeve (517). The four sliding grooves (518) are distributed at 90° to each other. It further includes a first clamping unit for detachably connecting the embedding column (514) to the clamping hole (41). The adjusting component (52) includes an adjusting sleeve (521) slidably connected to the second sliding sleeve (517). Four sliding rods (523) adapted to the sliding grooves (518) are provided on the inner surface wall of the adjusting sleeve (521). The length of the sliding rod (523) is 1 / 2 of the distance between the farthest ends of the sliding grooves (518) on the first sliding sleeve (516) and the sliding grooves (518) on the second sliding sleeve (517). An installation groove (522) is provided on the outer surface wall of the adjusting sleeve (521). It further includes a second clamping unit for clamping the adjusting sleeve (521) and the first sliding sleeve (516) to each other.

2. The cutting device for UAV processing according to claim 1, characterized in that, The first clamping unit includes a first clamping piece (515) fixedly connected to the outer wall of the embedding column (514). The first clamping piece (515) is formed by connecting a first limiting section (5151) and two supporting sections (5152). The first limiting section (5151) is an annular elastic sheet structure with a convex middle and concave sides. The two ends of the first limiting section (5151) are fixedly connected to the outer wall of the embedding column (514). The two ends of the supporting section (5152) are respectively fixedly connected to the inner wall of the concave section of the first limiting section (5151) and the outer wall of the embedding column (514) corresponding to the center of the convex section of the first limiting section (5151). The two supporting sections (5152) are symmetrically installed in the gap between the first limiting section (5151) and the embedding column (514). A first clamping groove adapted to the shape of the first clamping piece (515) is formed on the inner wall of the clamping hole (41). The embedding column (514) and the clamping hole (41) are adaptively clamped through the first clamping piece (515) and the first clamping groove.

3. The cutting device for UAV processing according to claim 1, characterized in that, The second clamping unit includes a second clamping piece (524) fixedly connected to the inner wall of the open end of the adjusting sleeve (521). A second clamping groove (513) is formed on the outer wall of one end of the first sliding sleeve (516) close to the embedding column (514). The adjusting sleeve (521) and the first sliding sleeve (516) are cooperatively clamped through the second clamping piece (524) and the second clamping groove (513). The second clamping piece (524) is formed by connecting two deformation sections (5241) and a second limiting section (5242). The two ends of the second limiting section (5242) are fixedly connected with the deformation sections (5241). The other ends of the two deformation sections (5241) are fixedly connected to the inner wall of the adjusting sleeve (521). The two deformation sections (5241) are concave, and the second limiting section (5242) is convex. The thicknesses of the deformation sections (5241) and the second limiting section (5242) gradually change from thin to thick from the middle to both sides.

4. The cutting device for UAV processing according to claim 1, characterized in that, The internal gear ring (53) is fixedly connected to the bottom end of the installation groove (522), and an adjusting gap is provided between the inner ring of the internal gear ring (53) and the inner wall of the installation groove (522). An angle marking groove (531) is formed on one side of the internal gear ring (53).

5. The cutting device for UAV processing according to claim 4, characterized in that, The workpiece limiting assembly (54) includes external racks (541) symmetrically placed in the adjusting gap. The external racks (541) are clamped with the inner ring of the internal gear ring (53). One side of the external rack (541) is fixedly connected with an adjusting limiting piece (542). One end of the adjusting limiting piece (542) is fixedly connected with a connecting bar (545). One end of the connecting bar (545) is fixedly connected with a workpiece baffle (544). A convex strip (543) is fixedly connected to the top of one side of the workpiece baffle (544).

6. The cutting device for processing drones according to claim 5, wherein, An annular adjustment groove (525) adapted to the shape of the adjustment limiting piece (542) is formed at the top of the installation groove (522), and the height of the adjustment groove (525) is the sum of the height of the adjustment limiting piece (542) and the height of the connecting strip (545).

7. The cutting device for UAV processing according to claim 5, characterized in that, The height of the external rack (541), the height of the connecting strip (545) is the same as that of the external rack (541), the height of the installation groove (522) is three times the height of the internal gear ring (53), the bottom end of the workpiece baffle (544) is in an outward-turning structure, and an inverted V-shaped structure is formed between the two workpiece baffles (544).

8. A cutting system for UAV processing, comprising the cutting device for UAV processing according to any one of claims 1-7, characterized in that, It further includes: A control unit, connected to the Y-axis lead screw platform (2), the X-axis lead screw platform (3) and the milling head motor, for controlling the Y-axis lead screw platform (2) and the X-axis lead screw platform (3) to drive the workpiece operation platform (4) to move in the X-axis and Y-axis directions, and controlling the milling head motor to drive the vertical milling head to perform cutting processing on the workpiece.

Citation Information

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