CN220281680U - A carry base for unmanned aerial vehicle - Google Patents
A carry base for unmanned aerial vehicle Download PDFInfo
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- CN220281680U CN220281680U CN202322071478.0U CN202322071478U CN220281680U CN 220281680 U CN220281680 U CN 220281680U CN 202322071478 U CN202322071478 U CN 202322071478U CN 220281680 U CN220281680 U CN 220281680U
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Abstract
The utility model discloses a mounting base for an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicle mounting. The utility model comprises a mounting bottom plate, a positioning component and a bearing component, wherein one side of the mounting bottom plate, which is close to the bottom, is connected with a mounting object main body through the positioning component, and the bottom of the mounting bottom plate is provided with the bearing component. The utility model is used for bearing the bottom of the mounting main body after fixing the mounting main body through the positioning component, is beneficial to being applicable to mounting main bodies with different heights through the arranged sliding rod and the second spring, is beneficial to preventing the mounting main body from falling down due to shaking of the unmanned aerial vehicle in the flying process, and is more stable to use.
Description
Technical Field
The utility model belongs to the field of unmanned aerial vehicle mounting, and particularly relates to a mounting base for an unmanned aerial vehicle.
Background
Prior art is unmanned aircraft that are operated by means of a radio remote control device and a self-contained program control device, or are operated autonomously, either entirely or intermittently, by an on-board computer. Unmanned aircraft tend to be more suitable for tasks that are too "fooled, messy, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.
The utility model discloses a Chinese patent with the application number of 202120816646.2, which relates to the field of unmanned aerial vehicle equipment and comprises a base, a fixing mechanism, an interface and a mounting mechanism, wherein the base is fixed at the bottom of the unmanned aerial vehicle; however, the mount base of the unmanned aerial vehicle is not supported by the mount base when being connected and fixed although different mount mechanisms are replaced when in use, and the mount base is easy to fall off when being only fixed by a spring during shaking in the air, so that the use is unsafe.
The present utility model has been made in view of this.
Disclosure of Invention
The utility model aims to solve the technical problem of overcoming the defects of the prior art and providing a mounting base for an unmanned aerial vehicle.
In order to solve the technical problems, the utility model adopts the basic conception of the technical scheme that:
the utility model provides a carry base for unmanned aerial vehicle, includes mounting bottom plate, locating component and bearing subassembly, one side that mounting bottom plate is close to the bottom is connected with the mount main part through locating component, mounting bottom plate bottom is provided with bearing subassembly, bearing subassembly includes the fixed plate, mounting bottom plate bottom symmetry fixed mounting has the fixed plate, the regulating tank has been seted up to the fixed plate inside, the inside sliding connection of regulating tank has the slide bar, the outside cover of slide bar is equipped with No. two springs, the slide bar bottom is connected through the connecting plate.
Optionally, slide bar top fixed mounting has the stopper, no. two spring is close to the one end and the stopper fixed connection of stopper, no. two spring keep away from the one end and the adjustment tank fixed connection of stopper.
Optionally, the locating component includes the movable tank, the movable tank has been seted up to the inside movable tank that has been installed to the mounting bottom plate, the inside rotation of movable tank is connected with two-way lead screw, the outside symmetry threaded connection of two-way lead screw has the movable block, movable block bottom symmetry fixed mounting has the locating lever, the spacing groove has been seted up to the inside one side symmetry that is close to the locating lever of mounting bottom plate, the locating tank has been seted up to the one side that the mounting main body is close to the locating lever, the locating lever extends to the locating tank inside.
Optionally, auxiliary assembly has been seted up to one side that the mounting bottom plate is close to two-way lead screw, the one end of two-way lead screw extends to dodge the inslot portion, one side that the auxiliary assembly is close to two-way lead screw is inside to be provided with auxiliary assembly.
Optionally, auxiliary assembly includes the baffle, dodge the inside eastern baffle that is connected with of groove, the baffle has been seted up to one side that is close to the baffle at mounting bottom plate top, the one end of baffle extends to inside the spout, dodge one side that the tank bottom portion is close to the baffle and seted up the draw-in groove, baffle bottom fixed mounting has the fixture block, the fixture block extends to inside the draw-in groove, mounting groove has been seted up to one side that is close to the draw-in groove inside the mounting bottom plate, mounting groove inside fixed mounting has a spring, one end fixed mounting that a spring is close to the draw-in groove has the grafting piece, grafting piece one end extends to inside the fixture block.
Optionally, an auxiliary plate is fixedly installed on one side, close to the bottom, of the baffle plate.
Optionally, a mounting seat is fixedly mounted on the top of the mounting bottom plate.
After the technical scheme is adopted, compared with the prior art, the utility model has the following beneficial effects, and of course, any product for implementing the utility model does not necessarily need to achieve all the following advantages at the same time:
1. through the bearing subassembly that sets up, will mount the back of main part through locating component for to the bearing of mount main part bottom, slide bar and No. two springs through setting up are favorable to being applicable to the not high mount main part of co-altitude, are favorable to preventing that unmanned aerial vehicle from rocking in the flight and leading to the mount main part to drop, use more stably.
2. The locating component that sets up is favorable to fixing the mount main part of equidimension not, and the auxiliary assembly that sets up in the locating component simultaneously for protect two-way lead screw, prevent that the mistake from touching and rotating two-way lead screw.
The following describes the embodiments of the present utility model in further detail with reference to the accompanying drawings.
Drawings
The drawings in the following description are only examples of embodiments from which other drawings may be derived by those skilled in the art without the exercise of inventive faculty. In the drawings:
FIG. 1 is a perspective view of an embodiment of the present utility model;
FIG. 2 is a front cross-sectional view of an embodiment of the present utility model;
FIG. 3 is a perspective view of a positioning assembly according to an embodiment of the present utility model;
FIG. 4 is a schematic view of the structure shown in FIG. 3A;
in the drawings, the list of components represented by the various numbers is as follows:
1. mounting a bottom plate; 2. a positioning assembly; 21. a moving groove; 22. a bidirectional screw rod; 23. a moving block; 24. a positioning rod; 25. a limit groove; 26. an avoidance groove; 27. an auxiliary component; 271. a baffle; 272. a chute; 273. a clamping groove; 274. a clamping block; 275. a mounting groove; 276. a first spring; 277. a plug block; 278. an auxiliary plate; 28. a positioning groove; 3. a support assembly; 31. a fixing plate; 32. an adjustment tank; 33. a slide bar; 34. a second spring; 35. a limiting block; 36. a connecting plate; 4. a mounting base; 5. and (5) mounting an object main body.
It should be noted that these drawings and the written description are not intended to limit the scope of the inventive concept in any way, but to illustrate the inventive concept to those skilled in the art by referring to the specific embodiments.
Detailed Description
The utility model will now be described in further detail with reference to the accompanying drawings.
Referring to fig. 1-4, in this embodiment, a mounting base for an unmanned aerial vehicle is provided, which includes a mounting base plate 1, a positioning assembly 2 and a supporting assembly 3, wherein one side of the mounting base plate 1 near the bottom is connected with a mounting main body 5 through the positioning assembly 2, the bottom of the mounting base plate 1 is provided with the supporting assembly 3, the supporting assembly 3 includes a fixing plate 31, the bottom of the mounting base plate 1 is symmetrically and fixedly provided with the fixing plate 31, an adjusting groove 32 is formed in the fixing plate 31, a sliding rod 33 is slidingly connected in the adjusting groove 32, a second spring 34 is sleeved on the outer side of the sliding rod 33, and the bottom of the sliding rod 33 is connected through a connecting plate 36.
The application of one aspect of the embodiment is: in use, the mount main body 5 is placed at the top of the connecting plate 36, the mount main bodies 5 with different heights are fixed through the sliding rod 33 and the second spring 34, the mount main body 5 is further fixed through the positioning assembly 2, and the unmanned aerial vehicle is prevented from falling off due to shaking in the flying process, so that the use is more stable.
A limiting block 35 is fixedly arranged at the top end of the sliding rod 33 in the embodiment, one end, close to the limiting block 35, of the second spring 34 is fixedly connected with the limiting block 35, and one end, far away from the limiting block 35, of the second spring 34 is fixedly connected with the adjusting groove 32.
The positioning assembly 2 of this embodiment includes a movable groove 21, the movable groove 21 is provided in the mounting base plate 1, the bidirectional screw 22 is rotationally connected in the movable groove 21, the outside symmetrical threaded connection of the bidirectional screw 22 has a movable block 23, the bottom of the movable block 23 is symmetrically and fixedly provided with a positioning rod 24, one side of the mounting base plate 1, which is close to the positioning rod 24, is symmetrically provided with a limiting groove 25, one side of the mounting body 5, which is close to the positioning rod 24, is provided with a positioning groove 28, and the positioning rod 24 extends into the positioning groove 28.
An auxiliary assembly 27 is arranged on one side, close to the bidirectional screw rod 22, of the mounting base plate 1 in the embodiment, one end of the bidirectional screw rod 22 extends to the inside of the avoidance groove 26, an auxiliary assembly 27 is arranged on one side, close to the bidirectional screw rod 22, of the inside of the auxiliary assembly 27, in use, through the avoidance groove 26, the bidirectional screw rod 22 is rotated, and the auxiliary assembly 27 is beneficial to protecting the bidirectional screw rod 22 inside the avoidance groove 26.
The auxiliary assembly 27 of this embodiment includes the baffle 271, dodge the inside eastern baffle 271 that is connected with of groove 26, the baffle 271 has been seted up to one side that is close to the baffle 271 at mounting bottom plate 1 top, the one end of baffle 271 extends to inside spout 272, dodge groove 26 bottom and be close to one side of baffle 271 and seted up draw-in groove 273, the clamping block 274 of fixed mounting bottom plate 1 bottom has been seted up the mounting groove 275 to the inside of draw-in groove 273, the inside fixed mounting of mounting groove 275 has a spring 276, a spring 276 is close to the one end fixed mounting of draw-in groove 273 has the grafting piece 277, grafting piece 277 one end extends to inside the clamping block 274, in use, protect bi-directional screw 22 through the baffle 271 that sets up, be favorable to the mistake to bump rotation bi-directional screw 22, the mounting groove 275 that sets up, a spring 276 and grafting piece 277 are favorable to the fixing to the clamping block 274.
An auxiliary plate 278 is fixedly mounted on one side of the baffle 271 near the bottom of the embodiment, and the baffle 271 is pushed to move upwards to slide in the chute 272 by the aid of the auxiliary plate 278, and meanwhile the baffle 271 is prevented from being separated from the chute 272.
The mount pad 4 is fixedly installed at the top of the mounting base plate 1 in this embodiment, and the mount pad 4 is beneficial to fixedly installing the mounting base plate 1 at the bottom of the unmanned aerial vehicle.
The present utility model is not limited to the above embodiments, and any person who can learn the structural changes made under the teaching of the present utility model can fall within the scope of the present utility model if the present utility model has the same or similar technical solutions. The technology, shape, and construction parts of the present utility model, which are not described in detail, are known in the art.
Claims (7)
1. The utility model provides a mount base for unmanned aerial vehicle, its characterized in that, including mount bottom plate (1), locating component (2) and bearing component (3), one side that mount bottom plate (1) is close to the bottom is connected with mount main part (5) through locating component (2), mount bottom plate (1) bottom is provided with bearing component (3), bearing component (3) include fixed plate (31), mount bottom plate (1) bottom symmetry fixed mounting has fixed plate (31), regulating groove (32) have been seted up to inside of fixed plate (31), inside sliding connection of regulating groove (32) has slide bar (33), the outside cover of slide bar (33) is equipped with No. two springs (34), slide bar (33) bottom is connected through connecting plate (36).
2. The mounting base for the unmanned aerial vehicle according to claim 1, wherein a limiting block (35) is fixedly mounted at the top end of the sliding rod (33), one end, close to the limiting block (35), of the second spring (34) is fixedly connected with the limiting block (35), and one end, far away from the limiting block (35), of the second spring (34) is fixedly connected with the adjusting groove (32).
3. The mounting base for the unmanned aerial vehicle according to claim 1, wherein the positioning assembly (2) comprises a moving groove (21), the moving groove (21) is formed in the mounting base plate (1), the bidirectional screw (22) is rotationally connected in the moving groove (21), the moving block (23) is symmetrically and threadedly connected to the outer side of the bidirectional screw (22), the positioning rod (24) is symmetrically and fixedly arranged at the bottom of the moving block (23), the limiting groove (25) is symmetrically formed in one side, close to the positioning rod (24), of the mounting base plate (1), the positioning groove (28) is formed in one side, close to the positioning rod (24), of the mounting base plate (5), and the positioning rod (24) extends into the positioning groove (28).
4. A mounting base for an unmanned aerial vehicle according to claim 3, wherein an auxiliary assembly (27) is provided on a side of the mounting base plate (1) close to the bi-directional screw (22), one end of the bi-directional screw (22) extends into the avoidance groove (26), and an auxiliary assembly (27) is provided on a side of the auxiliary assembly (27) close to the bi-directional screw (22).
5. The mount base for unmanned aerial vehicle according to claim 4, wherein the auxiliary assembly (27) comprises a baffle (271), dodge the inside eastern baffle (271) that is connected with of groove (26), mount bottom plate (1) top is close to one side of baffle (271) and has seted up baffle (271), the one end of baffle (271) extends to spout (272) inside, dodge groove (26) bottom and be close to one side of baffle (271) and seted up draw-in groove (273), baffle (271) bottom fixed mounting has fixture block (274), fixture block (274) extend to inside draw-in groove (273), mount bottom plate (1) inside is close to one side of draw-in groove (273) and has seted up mounting groove (275), inside fixed mounting has spring (276) No. one, one end fixed mounting that spring (276) is close to draw-in groove (273) has plug-in piece (277), plug-in piece (277) one end extends to inside fixture block (274).
6. A mounting base for an unmanned aerial vehicle according to claim 5, wherein the side of the flap (271) near the bottom is fixedly fitted with an auxiliary plate (278).
7. A mounting base for an unmanned aerial vehicle according to claim 1, wherein the mounting base (1) is fixedly mounted with a mounting base (4) on top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322071478.0U CN220281680U (en) | 2023-08-03 | 2023-08-03 | A carry base for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322071478.0U CN220281680U (en) | 2023-08-03 | 2023-08-03 | A carry base for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220281680U true CN220281680U (en) | 2024-01-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322071478.0U Active CN220281680U (en) | 2023-08-03 | 2023-08-03 | A carry base for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220281680U (en) |
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2023
- 2023-08-03 CN CN202322071478.0U patent/CN220281680U/en active Active
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