CN213109803U - Unmanned aerial vehicle throwing mechanism has locking structure couple - Google Patents
Unmanned aerial vehicle throwing mechanism has locking structure couple Download PDFInfo
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- CN213109803U CN213109803U CN202022325450.1U CN202022325450U CN213109803U CN 213109803 U CN213109803 U CN 213109803U CN 202022325450 U CN202022325450 U CN 202022325450U CN 213109803 U CN213109803 U CN 213109803U
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- 238000001125 extrusion Methods 0.000 claims description 7
- 238000005266 casting Methods 0.000 claims description 6
- 238000010030 laminating Methods 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000032258 transport Effects 0.000 description 3
- 230000010354 integration Effects 0.000 description 2
- 238000005381 potential energy Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle throwing mechanism has locking structure couple, including the unmanned aerial vehicle main part, the unmanned aerial vehicle main part includes unmanned aerial vehicle, support frame and camera, and the unmanned aerial vehicle downside has all linked firmly the support frame, the inside locking mechanism that is provided with of support frame, and support frame inside inserts and be equipped with the couple, the inside third slot that has seted up of couple, and the inside inserting of third slot is equipped with the bolt pole, the inside inserting of bolt pole is equipped with the head rod, and the head rod downside links firmly on the support frame, one side that the couple was kept away from to the bolt pole slides has the slide, and the slide one side of keeping away from the bolt pole has linked firmly first spring, the one end that the slide was kept away from to first spring links firmly on the couple, and the bolt pole downside has linked firmly. The utility model discloses make unmanned aerial vehicle when transporting article, will transport article and carry out the closure transportation, transport more firm, conveying efficiency is higher, reduces the transportation risk, promotes the transportation quality, promotes economic benefits.
Description
Technical Field
The utility model relates to a couple technical field specifically is an unmanned aerial vehicle throws mechanism and has locking structure couple.
Background
Along with the progress of science and technology, the society develops constantly, in the era of the quick innovation of all kinds of machines, unmanned aerial vehicle's throwing mechanism couple when unmanned aerial vehicle transports, conveniently carries the transportation, has brought very big facility for people's life, consequently can know that present unmanned aerial vehicle throws mechanism couple and satisfies people's demand basically, but still has some problems.
The first problem is that: the hook of the traditional unmanned aerial vehicle throwing mechanism is not in a closed form generally, and objects needing to be transported are hung on the hook generally during transportation.
The second problem is that: traditional unmanned aerial vehicle camera all is usually with unmanned aerial vehicle integration, unable split, although this kind of connected mode is firm, when nevertheless the camera damages, can't change the camera, need purchase new unmanned aerial vehicle, extravagant more fund.
Therefore, there is a need for an Unmanned Aerial Vehicle (UAV) casting mechanism with a locking structure hook to solve the above problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle throws mechanism has locking structure couple to solve the problem of the unable closure of unmanned aerial vehicle couple that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a hook with a locking structure for an unmanned aerial vehicle throwing mechanism comprises an unmanned aerial vehicle main body, wherein the unmanned aerial vehicle main body comprises an unmanned aerial vehicle, a support frame and a camera, the support frame is fixedly connected to the lower side of the unmanned aerial vehicle, a locking mechanism is arranged inside the support frame to facilitate locking, a hook is inserted inside the support frame, a third opening groove is formed in the hook, a plug rod is inserted inside the third opening groove, a first connecting rod is inserted inside the plug rod, the lower side of the first connecting rod is fixedly connected to the support frame, a sliding plate slides on one side of the plug rod, away from the hook, a first spring is fixedly connected to one side of the sliding plate, away from the plug rod, one end of the first spring, away from the sliding plate, is fixedly connected to the hook, a first connecting plate is fixedly connected to the lower side of the plug rod, a second spring is fixedly connected to one side of the first connecting plate, away from the, the bolt pole upper end has linked firmly the bolt board, and the bolt pole one side of keeping away from the bolt board has linked firmly the second connecting rod, the one side that the bolt pole was kept away from to the second connecting rod has linked firmly the second connecting plate.
Preferably, a camera is arranged in the middle of the lower side of the unmanned aerial vehicle, a first open slot is formed in the camera, a quick dismounting mechanism is arranged in the first open slot, the dismounting is convenient, the inner part of the first open groove is sleeved outside the connecting block, one side of the connecting block far away from the camera is fixedly connected on the unmanned aerial vehicle, a latch block is inserted in the connecting block, one side of the latch block, which is far away from the camera, is fixedly connected with a third spring, and one end of the third spring far away from the latch block is fixedly connected on the connecting block, the other end of the latch block far away from the camera is fixedly connected with the sliding block, and one side of the sliding block far away from the pin block slides on the sliding rail, the side of the sliding rail far away from the sliding block is fixedly connected with the connecting block, and the one end that the third spring was kept away from to the bolt piece is inserted and is established in the second fluting, the second fluting outside all sets up in the camera, and the one side laminating that the third spring was kept away from to the bolt piece has the stripper plate.
Preferably, the laminating of bolt board upside has first stopper, is convenient for spacing, and the one side that the support frame was kept away from to first stopper links firmly on the head rod, is convenient for connect.
Preferably, one side of the second connecting plate, which is far away from the second connecting rod, is fixedly connected with a push block, so that the push block is convenient to push, and the push block is in a ladder shape, so that the push block is convenient to push.
Preferably, one side that the connecting block was kept away from to the slide rail has linked firmly the second stopper, is convenient for spacing, and the second stopper is kept away from one side laminating latch piece of slide rail, is convenient for connect.
Preferably, the one end that the plug block was kept away from to the stripper plate is inserted and is established in the fourth fluting, is convenient for connect, and sets up in the rubber sleeve outside the fourth fluting, is convenient for press, one side that the plug block was kept away from to the stripper plate links firmly on the rubber sleeve, is convenient for connect, and one side that the rubber sleeve is close to the camera links firmly on the camera, is convenient for connect.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the unmanned aerial vehicle throwing mechanism is provided with a hook with a locking structure, a pin rod, a first connecting rod, a sliding plate, a first spring, a second spring, a pin plate, a second connecting rod, a second connecting plate and a pushing block, when the unmanned aerial vehicle throwing mechanism needs to be transported, the pushing block is pushed to drive the second connecting plate and the second connecting rod to push the pin rod, the pin rod drives the pin plate to be inserted into a third groove, the pin is extruded to slide, the hook extrudes the first spring, the first connecting plate compresses the second spring, an article to be transported is sleeved on the hook, the pushing block is loosened, the upper end of the hook is attached to a support frame under the elastic potential energy of the first spring and the second spring, the problem that the hook of the traditional unmanned aerial vehicle throwing mechanism is not closed normally is solved, the article to be transported is usually hung on the hook during transportation, and the hook is easily influenced by external force during transportation, the problem that transported articles fall off and are inconvenient to transport is solved, so that when the unmanned aerial vehicle transports the articles, the transported articles are locked and transported, the transportation is more stable, the transportation efficiency is higher, the transportation risk is reduced, the transportation quality is improved, and the economic benefit is improved;
2. this unmanned aerial vehicle throwing mechanism has closure structure couple and is provided with the connecting block, the bolt piece, the third spring, a slide rail, stripper plate and rubber sleeve, when the camera needs the maintenance to demolish, press the rubber sleeve, drive stripper plate extrusion bolt piece, make the bolt piece under the supplementary slip of slider, slide to in the connecting block, compress the third spring, the pulling camera, it is connected with unmanned aerial vehicle's block to remove the camera, traditional unmanned aerial vehicle camera has been solved, usually all be with unmanned aerial vehicle integration, unable split, this kind of connected mode is firm, but when the camera damages, can't change the camera, need purchase new unmanned aerial vehicle, the problem of extravagant more fund, make the camera when damaging needs maintenance or change, carry out the split to unmanned aerial vehicle and camera fast, reduce the material loss, save the fund input.
Drawings
FIG. 1 is a schematic sectional view of the front view of the structure of the present invention;
FIG. 2 is a schematic front view of the structure of the present invention;
fig. 3 is an enlarged schematic view of the structure at a in fig. 1 according to the present invention;
fig. 4 is an enlarged schematic view of the structure at B in fig. 1 according to the present invention.
In the figure: 100. an unmanned aerial vehicle main body; 110. an unmanned aerial vehicle; 120. a support frame; 130. a camera; 131. a first slot; 132. a second slot; 200. a locking mechanism; 210. hooking; 211. a third slot is formed; 220. a latch rod; 221. a first connecting plate; 230. a first connecting rod; 231. a first stopper; 240. a slide plate; 250. a first spring; 260. a second spring; 270. a latch plate; 280. a second connecting rod; 290. a second connecting plate; 2010. a push block; 300. a quick disassembly and assembly mechanism; 310. connecting blocks; 320. a latch block; 321. a slider; 330. a third spring; 340. a slide rail; 341. a second limiting block; 350. a pressing plate; 360. a rubber sleeve; 361. and a fourth slot.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides an embodiment: a hook with a locking structure for an unmanned aerial vehicle throwing mechanism comprises an unmanned aerial vehicle main body 100, wherein the unmanned aerial vehicle main body 100 comprises an unmanned aerial vehicle 110, a support frame 120 and a camera 130, the support frame 120 is fixedly connected to the lower side of the unmanned aerial vehicle 110, a locking mechanism 200 convenient for locking is arranged in the support frame 120 and convenient for transportation, a hook 210 is inserted in the support frame 120, a third opening groove 211 is formed in the hook 210, a plug rod 220 is inserted in the third opening groove 211, a first connecting rod 230 is inserted in the plug rod 220, the lower side of the first connecting rod 230 is fixedly connected to the support frame 120, a sliding plate 240 slides on one side of the plug rod 220 away from the hook 210, a first spring 250 is fixedly connected to one side of the sliding plate 240 away from the plug rod 220, one end of the first spring 250 away from the sliding plate 240 is fixedly connected to the hook 210, a first connecting plate 221 is fixedly connected to the lower side of the plug rod 220, a second spring, and the end of the second spring 260 far away from the first connecting plate 221 is fixedly connected to the support frame 120, the upper end of the latch rod 220 is fixedly connected to the latch plate 270, one side of the latch rod 220 far away from the latch plate 270 is fixedly connected to a second connecting rod 280, and one side of the second connecting rod 280 far away from the latch rod 220 is fixedly connected to a second connecting plate 290.
The camera 130 is arranged in the middle of the lower side of the unmanned aerial vehicle 110, the camera 130 is internally provided with a first slot 131, the first slot 131 is internally provided with a quick dismounting mechanism 300 which is convenient to dismount and is convenient to replace, the first slot 131 is internally sleeved outside the connecting block 310, one side of the connecting block 310, which is far away from the camera 130, is fixedly connected to the unmanned aerial vehicle 110, a pin block 320 is inserted into the connecting block 310, one side of the pin block 320, which is far away from the camera 130, is fixedly connected to a third spring 330, one end of the third spring 330, which is far away from the pin block 320, is fixedly connected to the connecting block 310, one end of the pin block 320, which is far away from the camera 130, is fixedly connected to a sliding block 321, one side of the sliding block 321, which is far away from the pin block 320, is slid on a sliding rail 340, one side of the sliding rail 340, which is far away from the sliding block 321, is, and the side of the latch block 320 remote from the third spring 330 is attached with a pressing plate 350.
The first limiting block 231 convenient for limiting is attached to the upper side of the bolt plate 270, stability is enhanced, and one side, away from the support frame 120, of the first limiting block 231 is fixedly connected to the first connecting rod 230 convenient for connection, so that stability is enhanced.
One side of the second connecting plate 290, which is far away from the second connecting rod 280, is fixedly connected with a push block 2010 which is convenient to push, so that the push block 2010 is convenient to bear force, and the push block 2010 is in a trapezoid shape which is convenient to push, so that the push block 2010 is convenient to bear force.
One side of the slide rail 340 far away from the connecting block 310 is fixedly connected with a second limiting block 341 convenient for limiting, so that the stability is enhanced, and one side of the second limiting block 341 far away from the slide rail 340 is attached to the bolt block 320 convenient for connecting, so that the stability is enhanced.
One end of the extrusion plate 350, which is far away from the latch block 320, is inserted into a fourth groove 361 which is convenient to connect, stability is enhanced, the outer side of the fourth groove 361 is arranged in a rubber sleeve 360 which is convenient to press, the force is convenient to bear, one side of the extrusion plate 350, which is far away from the latch block 320, is fixedly connected to the rubber sleeve 360 which is convenient to connect, stability is enhanced, one side of the rubber sleeve 360, which is close to the camera 130, is fixedly connected to the camera 130 which is convenient to connect, and stability is enhanced.
The working principle is as follows: when transportation is needed, the pushing block 2010 is pushed to drive the second connecting plate 290 and the second connecting rod 280 to push the latch rod 220, the latch rod 220 drives the latch plate 270 to be inserted into the third opening 211, the hook 210 is extruded to slide, the hook 210 extrudes the first spring 250 to enable the first connecting plate 221 to compress the second spring 260, articles to be transported are sleeved on the hook 210, the pushing block 2010 is loosened, the upper end of the hook 210 is attached to the support frame 120 under the elastic potential energy of the first spring 250 and the second spring 260, when the camera 130 needs maintenance and removal, the rubber sleeve 360 is pressed to drive the extrusion plate 350 to extrude the latch block 320, the latch block 320 slides into the connecting block 310 under the auxiliary sliding of the sliding block 321 to compress the third spring 330, the camera 130 is pulled to remove the clamping connection between the camera 130 and the unmanned aerial vehicle 110.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides an unmanned aerial vehicle jettison mechanism has locking structure couple, includes unmanned aerial vehicle main part (100), unmanned aerial vehicle main part (100) include unmanned aerial vehicle (110), support frame (120) and camera (130), and unmanned aerial vehicle (110) downside has all linked firmly support frame (120), support frame (120) inside is provided with locking mechanism (200), its characterized in that: a hook (210) is inserted into the support frame (120), a third open slot (211) is formed in the hook (210), a pin rod (220) is inserted into the third open slot (211), a first connecting rod (230) is inserted into the pin rod (220), the lower side of the first connecting rod (230) is fixedly connected to the support frame (120), a sliding plate (240) is slid on one side of the pin rod (220) far away from the hook (210), a first spring (250) is fixedly connected to one side of the sliding plate (240) far away from the pin rod (220), one end of the first spring (250) far away from the sliding plate (240) is fixedly connected to the hook (210), a first connecting plate (221) is fixedly connected to the lower side of the pin rod (220), a second spring (260) is fixedly connected to one side of the first connecting plate (221) far away from the pin rod (220), and one end of the second spring (260) far away from the first connecting plate (221) is fixedly connected to the support frame (120), the upper end of the bolt rod (220) is fixedly connected with a bolt plate (270), one side, far away from the bolt plate (270), of the bolt rod (220) is fixedly connected with a second connecting rod (280), and one side, far away from the bolt rod (220), of the second connecting rod (280) is fixedly connected with a second connecting plate (290).
2. The unmanned aerial vehicle casting mechanism of claim 1, wherein the locking structure comprises: the middle of the lower side of the unmanned aerial vehicle (110) is provided with a camera (130), a first groove (131) is formed in the camera (130), a quick dismounting mechanism (300) is arranged in the first groove (131), the first groove (131) is sleeved outside the connecting block (310), one side, far away from the camera (130), of the connecting block (310) is fixedly connected to the unmanned aerial vehicle (110), a pin block (320) is inserted in the connecting block (310), one side, far away from the camera (130), of the pin block (320) is fixedly connected with a third spring (330), one end, far away from the pin block (320), of the third spring (330) is fixedly connected to the connecting block (310), one end, far away from the camera (130), of the pin block (320) is fixedly connected with a sliding block (321), one side, far away from the pin block (320), of the sliding block (321) slides on a sliding rail (340), one side, far away from the sliding rail (340), of the sliding block (321), is fixedly connected to the connecting block (, and one end of the plug pin block (320) far away from the third spring (330) is inserted into the second open slot (132), the outer side of the second open slot (132) is arranged in the camera (130), and one side of the plug pin block (320) far away from the third spring (330) is attached with the extrusion plate (350).
3. The unmanned aerial vehicle casting mechanism of claim 1, wherein the locking structure comprises: the bolt plate (270) is attached with a first limiting block (231) on the upper side, and one side, far away from the support frame (120), of the first limiting block (231) is fixedly connected to the first connecting rod (230).
4. The unmanned aerial vehicle casting mechanism of claim 1, wherein the locking structure comprises: one side of the second connecting plate (290), which is far away from the second connecting rod (280), is fixedly connected with a push block (2010), and the push block (2010) is in a trapezoid shape.
5. The unmanned aerial vehicle casting mechanism of claim 2, wherein the locking structure comprises: one side of the sliding rail (340) far away from the connecting block (310) is fixedly connected with a second limiting block (341), and one side of the second limiting block (341) far away from the sliding rail (340) is attached to the latch block (320).
6. The unmanned aerial vehicle casting mechanism of claim 2, wherein the locking structure comprises: one end of the extrusion plate (350) far away from the latch block (320) is inserted into the fourth slot (361), the outer side of the fourth slot (361) is arranged in the rubber sleeve (360), one side of the extrusion plate (350) far away from the latch block (320) is fixedly connected to the rubber sleeve (360), and one side of the rubber sleeve (360) close to the camera (130) is fixedly connected to the camera (130).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022325450.1U CN213109803U (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle throwing mechanism has locking structure couple |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022325450.1U CN213109803U (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle throwing mechanism has locking structure couple |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213109803U true CN213109803U (en) | 2021-05-04 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022325450.1U Expired - Fee Related CN213109803U (en) | 2020-10-19 | 2020-10-19 | Unmanned aerial vehicle throwing mechanism has locking structure couple |
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| Country | Link |
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| CN (1) | CN213109803U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859542A (en) * | 2021-10-23 | 2021-12-31 | 四川省天域航通科技有限公司 | Rescue unmanned aerial vehicle convenient to put in goods and materials |
-
2020
- 2020-10-19 CN CN202022325450.1U patent/CN213109803U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859542A (en) * | 2021-10-23 | 2021-12-31 | 四川省天域航通科技有限公司 | Rescue unmanned aerial vehicle convenient to put in goods and materials |
| CN113859542B (en) * | 2021-10-23 | 2023-06-06 | 四川省天域航通科技有限公司 | Rescue unmanned aerial vehicle convenient to throw in goods and materials |
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| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210504 |