CN221184789U - Unmanned aerial vehicle model aeroplane and model ship is with screw perforating device - Google Patents
Unmanned aerial vehicle model aeroplane and model ship is with screw perforating device Download PDFInfo
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- CN221184789U CN221184789U CN202322998498.2U CN202322998498U CN221184789U CN 221184789 U CN221184789 U CN 221184789U CN 202322998498 U CN202322998498 U CN 202322998498U CN 221184789 U CN221184789 U CN 221184789U
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- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 238000004080 punching Methods 0.000 claims abstract description 15
- 230000002457 bidirectional effect Effects 0.000 abstract description 10
- 238000000034 method Methods 0.000 abstract description 10
- 230000008569 process Effects 0.000 abstract description 7
- 230000000712 assembly Effects 0.000 abstract description 3
- 238000000429 assembly Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 7
- 206010016256 fatigue Diseases 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000003028 elevating effect Effects 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses a propeller punching device for an unmanned aerial vehicle model, and relates to the technical field of propeller punching. The utility model comprises an operation round table and an L-shaped operation table arranged below the operation round table, wherein the operation round table is provided with a clamping mechanism, a rotating mechanism, a lifting mechanism and a control mechanism; the clamping mechanism comprises a clamping assembly, two fixing assemblies and a limiting assembly, wherein the clamping assembly comprises a rectangular clamping groove formed in the top of the operation round platform, a bidirectional threaded rod is rotationally installed in the rectangular clamping groove, a clamping motor is fixedly installed on the outer wall of the operation round platform, and the right end of the bidirectional threaded rod extends out of the operation round platform and is fixedly connected with an output shaft of the clamping motor. According to the utility model, the clamping mechanism is arranged, so that the arc-shaped movable block can be fixed according to the shape of the propeller when contacting the propeller in the process that the two internal thread sliding blocks are mutually close, and the clamping stability is effectively improved.
Description
Technical Field
The utility model belongs to the technical field of propeller punching, and particularly relates to a propeller punching device for an unmanned aerial vehicle model airplane.
Background
The aero model is a general term of various aircraft models, and comprises model aircrafts and other model aircrafts, the aero model activity causes people to be interested from the beginning, and thousands of years are long and short, and the main reason is that the aero model plays a very important role in the development of aviation industry and the cultivation of technological talents, wherein unmanned aerial vehicles like to operate unmanned aerial vehicles along with the development of society, unmanned aerial vehicle propellers need to punch in the processing process, the assembly is convenient, the existing unmanned aerial vehicle propellers are inconvenient in the punching processing process because of the irregular shape of the unmanned aerial vehicle propellers, the strength of the propellers is not high at the same time, the propellers are inconvenient to fix, the propellers are easy to damage, the fixing is inconvenient and easy to generate hole offset in the drilling process, the hole precision is reduced, and the operation is inconvenient.
In the related art, a screw perforating device for unmanned aerial vehicle model aeroplane and model ship is disclosed with publication number CN217192748U, which comprises a main body, fixed centre gripping through-hole has been seted up on the top of main body, fixed trampling through-hole has been seted up to the front surface of main body, the inside fixedly connected with of main body connects fixture, and the utility model is convenient for place unmanned aerial vehicle screw at the top of main body through the connection fixture that is equipped with, drives movable grip block through the effect of connection fixture and removes in the inboard of fixed centre gripping through-hole, carries out the centre gripping to the bottom surface outside of unmanned aerial vehicle screw.
The device is in the use, and it is fixed that needs the operator to step on the activity pedal just can carry out the centre gripping to the screw with the foot, and long-time manual stepping returns and makes the foot tired out of operator, if the engineering volume of punching is great, the operator will show tired out more and lead to influencing the centre gripping effect.
Disclosure of utility model
The utility model aims to provide a propeller punching device for an unmanned aerial vehicle model airplane, which solves the problem that the long-time manual stepping back causes fatigue of feet of an operator, and if the punching engineering amount is large, the operator can be more tired, so that the clamping effect is affected.
In order to solve the technical problems, the utility model is realized by the following technical scheme:
The utility model relates to a propeller perforating device for an unmanned aerial vehicle model, which comprises an operation round table and an L-shaped operation table arranged below the operation round table, wherein a clamping mechanism, a rotating mechanism, a lifting mechanism and a control mechanism are arranged on the operation round table;
The clamping mechanism comprises a clamping assembly, two fixing assemblies and a limiting assembly, wherein the clamping assembly comprises a rectangular clamping groove formed in the top of an operation round table, a bidirectional threaded rod is rotationally installed in the rectangular clamping groove, a clamping motor is fixedly installed on the outer wall of the operation round table, the right end of the bidirectional threaded rod extends out of the operation round table and is fixedly connected with an output shaft of the clamping motor, and two internal thread sliding blocks are installed on the bidirectional threaded rod in a threaded mode.
Further, the fixed subassembly is including two round bars of internal thread slider front and back respectively fixed mounting, a plurality of the round bar is the one end that keeps away from each other fixed mounting has the dead lever respectively, a plurality of the right-hand member of dead lever is articulated respectively and is installed the arc movable block.
Further, the limiting assembly comprises a round sliding rod fixedly arranged in the rectangular clamping groove, and the round sliding rod penetrates through the two inner thread sliding blocks and is in sliding connection with the two inner thread sliding blocks.
Further, rotary mechanism is including rotating axis and the rotating electrical machines of installing at L type operation panel top, the bottom and the operation round platform fixed connection of axis of rotation, fixed mounting has gear one on the output shaft of rotating electrical machines, fixed cover is equipped with gear two on the outer wall of axis of rotation, gear one and gear two phase engagement.
Further, the lifting mechanism comprises a puncher fixedly mounted on the inner wall of the top of the L-shaped operating platform, a rectangular bottom plate is arranged below the L-shaped operating platform, a hydraulic cylinder is fixedly mounted on the top of the rectangular bottom plate, and an output shaft of the hydraulic cylinder is fixedly connected with the L-shaped operating platform.
Further, the control mechanism comprises a control block fixedly installed on the top of the L-shaped operation table, and a lifting switch, a clamping switch and a rotary switch are arranged on the top of the control block.
The utility model has the following beneficial effects:
According to the utility model, the fixing assembly is arranged, so that the arc-shaped movable block can be fixed according to the shape of the screw propeller when contacting the screw propeller in the process that the two internal thread sliding blocks are mutually close, and the clamping stability is effectively improved; through setting up spacing subassembly, can make two internal thread sliders steadily remove through circular slide bar in the in-process that two internal thread sliders are close to each other, effectively improve the stability of device; through setting up rotary mechanism for can start the rotating electrical machines, the rotating electrical machines drives gear one and rotates, under the effect of gear one and gear two, drives the axis of rotation simultaneously and rotates, and the operation round platform of drive of axis of rotation rotates, can realize simultaneously that will adjust the angle to the spiral on the operation round platform and be convenient for punch; by arranging the lifting mechanism, the hydraulic cylinder can be started to drive the L-shaped operation table to integrally lift or descend, so that the height of the L-shaped operation table can be effectively adjusted according to the height of an operator, and the operator is more comfortable in operation; through setting up control mechanism for can effectively improve the convenience through each equipment on lifting switch, clamp switch and the rotary switch controlling means on the L type operation panel top control block.
Of course, it is not necessary for any one product to practice the utility model to achieve all of the advantages set forth above at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural view of a propeller perforating device for unmanned aerial vehicle model airplane of the present utility model;
Fig. 2 is a schematic top view of a propeller punching device for unmanned aerial vehicle model airplane according to the present utility model;
FIG. 3 is a schematic side view of a propeller perforating device for unmanned aerial vehicle model airplane of the present utility model;
FIG. 4 is an enlarged schematic view of the structure of FIG. 3A according to the present utility model;
Fig. 5 is a schematic diagram of a front cross-sectional structure of a propeller perforating device for unmanned aerial vehicle model airplane.
In the drawings, the list of components represented by the various numbers is as follows:
1. operating the round table; 2. a rectangular clamping groove; 3. a two-way threaded rod; 4. clamping the motor; 5. an internal thread slider; 6. an L-shaped operation table; 7. a round bar; 8. a fixed rod; 9. an arc movable block; 10. a circular slide bar; 11. a rotating shaft; 12. a rotating electric machine; 13. a first gear; 14. a second gear; 15. a puncher; 16. a rectangular bottom plate; 17. a hydraulic cylinder; 18. a control block; 19. a lifting switch; 20. a clamp switch; 21. and (3) rotating the switch.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the utility model discloses a propeller perforating device for unmanned aerial vehicle model airplane, comprising an operation round table 1 and an L-shaped operation table 6 arranged below the operation round table 1, wherein a clamping mechanism, a rotating mechanism, a lifting mechanism and a control mechanism are arranged on the operation round table 1;
The fixture comprises a clamping assembly, two fixing assemblies and a limiting assembly, wherein the clamping assembly comprises a rectangular clamping groove 2 formed in the top of an operation round table 1, a bidirectional threaded rod 3 is rotatably mounted in the rectangular clamping groove 2, a clamping motor 4 is fixedly mounted on the outer wall of the operation round table 1, the right end of the bidirectional threaded rod 3 extends out of the operation round table 1 and is fixedly connected with an output shaft of the clamping motor 4, and two internal thread sliding blocks 5 are mounted on the bidirectional threaded rod 3 in a threaded manner.
As shown in fig. 4, the fixing component includes two round bars 7 respectively fixedly installed on the front side and the back side of the internal thread slider 5, one ends of the plurality of round bars 7 far away from each other are respectively fixedly installed with a fixing bar 8, and right ends of the plurality of fixing bars 8 are respectively hinged with an arc movable block 9.
Through setting up fixed subassembly for can be in the in-process that two internal thread sliders 5 are close to each other, can fix according to the shape of screw when arc movable block 9 contacted the screw, effectively improve the stability of centre gripping.
As shown in fig. 2, the limiting component comprises a circular sliding rod 10 fixedly installed in the rectangular clamping groove 2, and the circular sliding rod 10 penetrates through the two internal thread sliding blocks 5 and is in sliding connection with the two internal thread sliding blocks 5.
Through setting up spacing subassembly for can make the steady removal of two internal thread slider 5 through the in-process that circular slide bar 10 is being close to each other at two internal thread slider 5, effectively improve the stability of device.
As shown in fig. 5, the rotating mechanism comprises a rotating shaft 11 and a rotating motor 12 rotatably installed at the top of the L-shaped operating platform 6, the bottom end of the rotating shaft 11 is fixedly connected with the operating platform 1, a first gear 13 is fixedly installed on an output shaft of the rotating motor 12, a second gear 14 is fixedly sleeved on the outer wall of the rotating shaft 11, and the first gear 13 is meshed with the second gear 14.
Through setting up rotary mechanism for can start rotating electrical machines 12, rotating electrical machines 12 drive gear one 13 and rotate, under gear one 13 and gear two 14's effect, drive axis of rotation 11 simultaneously and rotate, the operation round platform 1 of drive of axis of rotation 11 rotates, can realize simultaneously that the spiral will carry out angle adjustment on the operation round platform 1 and be convenient for punch.
As shown in fig. 5, the lifting mechanism comprises a puncher 15 fixedly mounted on the inner wall of the top of the L-shaped operating platform 6, a rectangular bottom plate 16 is arranged below the L-shaped operating platform 6, a hydraulic cylinder 17 is fixedly mounted on the top of the rectangular bottom plate 16, and an output shaft of the hydraulic cylinder 17 is fixedly connected with the L-shaped operating platform 6.
Through setting up elevating system for can start pneumatic cylinder 17, pneumatic cylinder 17 drives L type operation panel 6 wholly and rises or descend, can be according to operator's height, effectively adjust L type operation panel 6's height, let the operator more comfortable when the operation.
Wherein as shown in fig. 2, the control mechanism comprises a control block 18 fixedly installed on the top of the L-shaped operation table 6, and a lifting switch 19, a clamping switch 20 and a rotary switch 21 are arranged on the top of the control block 18.
By arranging the control mechanism, each device on the device can be controlled by the lifting switch 19, the clamping switch 20 and the rotary switch 21 on the top control block 18 of the L-shaped operating platform 6, so that convenience is effectively improved.
One specific application of this embodiment is: when in use, firstly, the lifting switch 19 on the control block 18 is pressed down, and the lifting switch 19 starts the hydraulic cylinder 17 to lift, so that the device is adjusted to a proper height; then placing the propeller on the operation round table 1, then pressing down the clamping switch 20, starting the clamping motor 4 to rotate by the clamping switch 20, driving the bidirectional threaded rod 3 to rotate by the clamping motor 4, and fixing the arc-shaped movable block 9 according to the shape of the propeller when the arc-shaped movable block 9 contacts the propeller in the process that the bidirectional threaded rod 3 drives the two internal threaded sliding blocks 5 to approach each other; after the fixing is finished, the hole can be punched, the rotary switch 21 can be pressed down in the punching process, the rotary switch 21 starts the rotary motor 12, the rotary motor 12 drives the gear I13 to rotate, under the action of the gear I13 and the gear II 14, the rotating shaft 11 is simultaneously driven to rotate, the rotating shaft 11 drives the operation round table 1 to rotate, and meanwhile, the angle adjustment of the spiral on the operation round table 1 can be realized.
In the description of the present specification, the descriptions of the terms "one embodiment," "example," "specific example," and the like, mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present utility model. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the utility model disclosed above are intended only to assist in the explanation of the utility model. The preferred embodiments are not exhaustive or to limit the utility model to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best understand and utilize the utility model. The utility model is limited only by the claims and the full scope and equivalents thereof.
Claims (6)
1. The utility model provides an unmanned aerial vehicle model aeroplane and model ship is with screw perforating device, includes operation round platform (1) and sets up L type operation panel (6) in operation round platform (1) below, its characterized in that: the operation round table (1) is provided with a clamping mechanism, a rotating mechanism, a lifting mechanism and a control mechanism;
Clamping mechanism includes clamping assembly, two fixed subassembly and spacing subassembly, the clamping assembly is including seting up rectangle grip groove (2) at operation round platform (1) top, two-way threaded rod (3) are installed in rectangle grip groove (2) internal rotation, fixed mounting has clamping motor (4) on the outer wall of operation round platform (1), the right-hand member of two-way threaded rod (3) extends to outside operation round platform (1) and with the output shaft fixed connection of clamping motor (4), two internal thread slider (5) are installed to the screw thread on two-way threaded rod (3).
2. The propeller punching device for the unmanned aerial vehicle model aeroplane and model ship according to claim 1, wherein the fixing component comprises two round bars (7) which are respectively fixedly installed on the front side and the back side of the internal thread sliding block (5), one ends, far away from each other, of a plurality of round bars (7) are respectively fixedly installed with a fixing rod (8), and the right ends of a plurality of fixing rods (8) are respectively hinged with an arc-shaped movable block (9).
3. The propeller punching device for the unmanned aerial vehicle model airplane according to claim 2, wherein the limiting component comprises a round sliding rod (10) fixedly installed in the rectangular clamping groove (2), and the round sliding rod (10) penetrates through the two inner threaded sliding blocks (5) and is in sliding connection with the two inner threaded sliding blocks (5).
4. A propeller punching device for unmanned aerial vehicle model aeroplane and model ship according to claim 3, characterized in that, rotary mechanism is including rotating shaft (11) and rotating electrical machines (12) of installing at L type operation panel (6) top of rotation, the bottom and the operation round platform (1) fixed connection of axis of rotation (11), fixed mounting has gear one (13) on the output shaft of rotating electrical machines (12), fixed cover is equipped with gear two (14) on the outer wall of axis of rotation (11), gear one (13) and gear two (14) mesh.
5. The propeller punching device for the unmanned aerial vehicle model aeroplane and model ship according to claim 4, wherein the lifting mechanism comprises a puncher (15) fixedly mounted on the inner wall of the top of the L-shaped operating platform (6), a rectangular bottom plate (16) is arranged below the L-shaped operating platform (6), a hydraulic cylinder (17) is fixedly mounted on the top of the rectangular bottom plate (16), and an output shaft of the hydraulic cylinder (17) is fixedly connected with the L-shaped operating platform (6).
6. The propeller punching device for the unmanned aerial vehicle model airplane according to claim 5, wherein the control mechanism comprises a control block (18) fixedly installed on the top of the L-shaped operation table (6), and a lifting switch (19), a clamping switch (20) and a rotary switch (21) are arranged on the top of the control block (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322998498.2U CN221184789U (en) | 2023-11-07 | 2023-11-07 | Unmanned aerial vehicle model aeroplane and model ship is with screw perforating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322998498.2U CN221184789U (en) | 2023-11-07 | 2023-11-07 | Unmanned aerial vehicle model aeroplane and model ship is with screw perforating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221184789U true CN221184789U (en) | 2024-06-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322998498.2U Active CN221184789U (en) | 2023-11-07 | 2023-11-07 | Unmanned aerial vehicle model aeroplane and model ship is with screw perforating device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221184789U (en) |
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2023
- 2023-11-07 CN CN202322998498.2U patent/CN221184789U/en active Active
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