CN214986011U - Unmanned aerial vehicle horn beta structure - Google Patents
Unmanned aerial vehicle horn beta structure Download PDFInfo
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- CN214986011U CN214986011U CN202121311991.7U CN202121311991U CN214986011U CN 214986011 U CN214986011 U CN 214986011U CN 202121311991 U CN202121311991 U CN 202121311991U CN 214986011 U CN214986011 U CN 214986011U
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- aerial vehicle
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle horn folding structure, which comprises an unmanned aerial vehicle body, one side of the unmanned aerial vehicle body is provided with a horn accommodating groove and an elastic piece accommodating groove, the inner side of the horn accommodating groove is provided with a turning horn and an extending horn, the top side of the extending horn is provided with a lifting device, one side of the unmanned aerial vehicle body is provided with a fixed limiting hole, one side of the turning horn is provided with a guide limiting groove and a guide limiting column, one side of the guide limiting column is provided with a guide limiting spring, the inner side of the elastic piece accommodating groove is provided with an elastic piece, one side of the elastic piece is provided with a plurality of elastic bodies, the top side of the turning horn is provided with an extending fixing hole, the top side of the extending horn is provided with a sliding fixing piece, one sides of the unmanned aerial vehicle body and the turning horn are both provided with a guide connecting groove and a guide connecting plate, the unmanned aerial vehicle horn folding structure is simple and ingenious in structure, and can be folded conveniently and quickly, the unfolding stability is high, and the storage is portable.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle horn beta structure.
Background
Unmanned aircraft, abbreviated "drone" and abbreviated "UAV", is an unmanned aircraft that is operated by a radio remote control device and self-contained programmed control means, or autonomously by an onboard computer, either completely or intermittently, and is often more suited to tasks that are too "fool, dirty, or dangerous" than a manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and 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 developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Present civilian unmanned aerial vehicle, unmanned aerial vehicle's horn most of structures as an organic whole can not extend the operation, also does not possess folding function, harms unmanned aerial vehicle easily when removing the transportation, and unmanned aerial vehicle carries inconveniently, and horn poor stability, therefore, we have designed an unmanned aerial vehicle horn beta structure.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving and having current civilian unmanned aerial vehicle among the prior art, unmanned aerial vehicle's horn most of structures as an organic whole can not extend the operation, does not possess folding function yet, harms unmanned aerial vehicle easily when removing the transportation, and unmanned aerial vehicle carries inconveniently, the shortcoming of horn poor stability, and the unmanned aerial vehicle horn beta structure who provides.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle horn folding structure is designed, comprising an unmanned aerial vehicle body, a lifting device and an elastic body, wherein the bottom side of the unmanned aerial vehicle body is fixedly connected with a supporting leg, one side of the unmanned aerial vehicle body is fixedly provided with a horn accommodating groove, the inner side of the horn accommodating groove is fixedly provided with an elastic part accommodating groove, the top of the inner side of the horn accommodating groove is rotatably connected with a turnover horn through a rotating shaft, one side of the turnover horn is slidably connected with an extension horn, the top side of the extension horn is fixedly provided with a lifting device, a fixed limiting hole is fixedly arranged at one side of the unmanned aerial vehicle body and at the position opposite to the horn accommodating groove, one side of the turnover horn is fixedly provided with a guide limiting groove, the inner side of the guide limiting groove is slidably connected with a guide limiting column, one side of the guide limiting column is fixedly provided with a guide limiting spring, and one side of the guide limiting spring is abutted against one side of the guide limiting groove, the inboard in groove is accomodate to the elastic component rotates through the pivot to be connected and is equipped with the elastic component, the fixed a plurality of elastomers that are equipped with in one side of elastic component, one side of elastomer offsets with one side in the groove is accomodate to the elastic component, the top side of upset horn is fixed and is equipped with two and extends the fixed orifices, the top side sliding connection who extends the horn is equipped with the sliding fixing spare, the equal fixed direction spread groove that is equipped with in one side of unmanned aerial vehicle body and upset horn, the inboard sliding connection of direction spread groove is equipped with the direction connecting plate.
Preferably, both sides of upset horn all are fixed and are equipped with the direction spout, the inboard sliding connection of direction spout is equipped with the direction slider, one side fixed connection of direction slider is in one side of extending the horn.
Preferably, the fixed anticreep spout that is equipped with in the inboard of direction spacing groove, the inboard sliding connection of anticreep spout is equipped with the anticreep slider, one side fixed connection of anticreep slider is in one side of the spacing post of direction.
Preferably, the elastic member is arranged in a wedge-shaped sixty-degree structure.
Preferably, the guide limiting column is matched with the fixed limiting hole, and one side, far away from the overturning machine arm, of the guide limiting column is arranged in a chamfering structure.
Preferably, the support leg is a shock-absorbing support frame member.
The utility model provides a pair of unmanned aerial vehicle horn beta structure, beneficial effect lies in: the overturning machine arm, the extending fixing hole, the sliding fixing piece, the guiding chute and the guiding slide block are arranged, the extending machine arm is pulled to enable the guiding slide block to move in the guiding chute on the overturning machine arm, when the extending machine arm moves to a specified position, the sliding fixing piece enters the extending fixing hole to provide a fixing function between the overturning machine arm and the extending machine arm, the overturning machine arm is pushed into the machine arm accommodating groove after the overturning machine arm and the extending machine arm contract together by arranging the machine arm accommodating groove, the fixing limiting hole, the guiding limiting groove, the guiding limiting column and the guiding limiting spring, then the guiding limiting column is extruded by the wall of the machine arm accommodating groove to enable the guiding limiting column to enter the guiding limiting groove, when the overturning machine arm and the extending machine arm are pushed to the specified position, the guiding limiting spring in the guiding limiting groove pushes the guiding limiting column into the fixing limiting hole so as to complete the accommodating operation, provide a convenient folding function to the horn, folding convenient and fast of accomodating, through setting up direction spread groove, direction connecting plate, when upset horn expandes with unmanned aerial vehicle body level, promote the direction connecting plate and remove in the direction spread groove to provide a fixed function to upset horn and unmanned aerial vehicle body, folding upset stability improves, this unmanned aerial vehicle horn beta structure, simple structure is ingenious, folding convenient and fast, it is high to expand stability, it is portable to accomodate.
Drawings
Fig. 1 is a schematic view of a front axial measurement structure of an unmanned aerial vehicle arm folding structure provided by the utility model;
fig. 2 is a schematic view of a front cut-away axial measurement structure of an unmanned aerial vehicle arm folding structure provided by the utility model;
fig. 3 is a schematic side cut-away axial measurement structure diagram of an unmanned aerial vehicle arm folding structure provided by the utility model;
fig. 4 is the utility model provides a structural schematic diagram of A in unmanned aerial vehicle horn beta structure's side dissection axle survey.
In the figure: 1 unmanned aerial vehicle body, 2 supporting legs, 3 grooves are accomodate to the horn, 4 grooves are accomodate to the elastic component, 5 upset horns, 6 extend the horn, 7 elevating gear, 8 fixed spacing holes, 9 direction spacing grooves, 10 direction spacing posts, 11 direction spacing springs, 12 elastic component, 13 elastomers, 14 extension fixed orificess, 15 sliding fixing spare, 16 direction spread groove, 17 direction connecting plate, 18 direction spouts, 19 direction sliders, 20 anticreep spouts, 21 anticreep sliders.
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.
Referring to fig. 1-4, an unmanned aerial vehicle horn folding structure comprises an unmanned aerial vehicle body 1, a lifting device 7 and an elastic body 13, wherein a supporting leg 2 is fixedly connected to the bottom side of the unmanned aerial vehicle body 1, a horn accommodating groove 3 is fixedly arranged on one side of the unmanned aerial vehicle body 1, an elastic member accommodating groove 4 is fixedly arranged on the inner side of the horn accommodating groove 3, a turning horn 5 is rotatably connected to the top of the inner side of the horn accommodating groove 3 through a rotating shaft, an extending horn 6 is slidably connected to one side of the turning horn 5, the lifting device 7 is fixedly arranged on the top side of the extending horn 6, a fixing limiting hole 8 is fixedly arranged on one side of the unmanned aerial vehicle body 1 and at a position opposite to the horn accommodating groove 3, a guiding limiting groove 9 is fixedly arranged on one side of the turning horn 5, a guiding limiting column 10 is slidably connected to the inner side of the guiding limiting groove 9, a guiding limiting spring 11 is fixedly arranged on one side of the guiding limiting column 10, one side of direction limiting spring 11 is inconsistent with one side of direction spacing groove 9, the inboard that groove 4 was accomodate to the elastic component is rotated through the pivot and is connected and be equipped with elastic component 12, one side of elastic component 12 is fixed and is equipped with a plurality of elastomers 13, one side of elastomer 13 is inconsistent with one side that groove 4 was accomodate to the elastic component, the fixed orifices 14 that extends in top side of upset horn 5 is equipped with two, the top side sliding connection that extends horn 6 is equipped with sliding fixture 15, one side of unmanned aerial vehicle body 1 and upset horn 5 is all fixed and is equipped with direction spread groove 16, the inboard sliding connection of direction spread groove 16 is equipped with direction connecting plate 17.
Specifically, both sides of the overturning machine arm 5 are fixedly provided with guide sliding grooves 18, the inner sides of the guide sliding grooves 18 are connected with guide sliding blocks 19 in a sliding manner, and one sides of the guide sliding blocks 19 are fixedly connected to one side of the extending machine arm 6.
Specifically, the inner side of the guide limiting groove 9 is fixedly provided with an anti-falling chute 20, the inner side of the anti-falling chute 20 is connected with an anti-falling sliding block 21 in a sliding manner, and one side of the anti-falling sliding block 21 is fixedly connected to one side of the guide limiting column 10.
Specifically, the elastic member 12 is arranged in a wedge-shaped sixty-degree structure.
Specifically, the guide limiting column 10 is matched with the fixed limiting hole 8, and one side, away from the overturning machine arm 5, of the guide limiting column 10 is in a chamfer structure.
Specifically, the support leg 2 is adopted as a shock-absorbing support frame member.
When the utility model is used, the turning machine arm 5, the extending machine arm 6, the extending fixing hole 14, the sliding fixing piece 15, the guiding chute 18 and the guiding slide block 19 are arranged, the extending machine arm 6 is pulled to enable the guiding slide block 19 to move in the guiding chute 18 on the turning machine arm 5, when the extending machine arm 6 moves to a specified position, the sliding fixing piece 15 enters the extending fixing hole 14 to provide a fixing function between the turning machine arm 5 and the extending machine arm 6, the turning machine arm 5 is pushed into the machine arm accommodating groove 3 after the turning machine arm 5 and the extending machine arm 6 are contracted together, then the guiding limit column 10 is extruded by the groove wall of the machine arm accommodating groove 3, the guiding limit column 10 enters the guiding limit groove 9 and is pushed to the specified position, spacing spring 11 of direction in the direction spacing groove 9 pushes into fixed spacing hole 8 with the spacing post 10 of direction, in order to accomplish and accomodate the operation, provide a convenient folding function to the horn, folding convenient and fast of accomodating, through setting up direction spread groove 16, direction connecting plate 17, when upset horn 5 expandes with unmanned aerial vehicle body 1 level, promote direction connecting plate 17 and remove in direction spread groove 16, thereby provide a fixed function to upset horn 5 and unmanned aerial vehicle body 1, folding upset stability improves, this unmanned aerial vehicle horn beta structure, moreover, the steam generator is simple in structure, folding convenient and fast, it is high to expand stability, it is portable to accomodate.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle horn folding structure comprises an unmanned aerial vehicle body (1), a lifting device (7) and an elastic body (13), and is characterized in that a supporting leg (2) is fixedly connected to the bottom side of the unmanned aerial vehicle body (1), a horn accommodating groove (3) is fixedly arranged on one side of the unmanned aerial vehicle body (1), an elastic piece accommodating groove (4) is fixedly arranged on the inner side of the horn accommodating groove (3), a turnover horn (5) is rotatably connected to the top of the inner side of the horn accommodating groove (3) through a rotating shaft, an extension horn (6) is slidably connected to one side of the turnover horn (5), the lifting device (7) is fixedly arranged on the top side of the extension horn (6), a fixed limiting hole (8) is fixedly arranged on one side of the unmanned aerial vehicle body (1) and at a position opposite to the horn accommodating groove (3), a guide limiting groove (9) is fixedly arranged on one side of the turnover horn (5), the inner side of the guide limiting groove (9) is connected with a guide limiting column (10) in a sliding manner, one side of the guide limiting column (10) is fixedly provided with a guide limiting spring (11), one side of the guide limiting spring (11) is in contact with one side of the guide limiting groove (9), the inner side of the elastic part accommodating groove (4) is connected with an elastic part (12) in a rotating manner through a rotating shaft, one side of the elastic part (12) is fixedly provided with a plurality of elastic bodies (13), one side of each elastic body (13) is in contact with one side of the elastic part accommodating groove (4), the top side of the overturning machine arm (5) is fixedly provided with two extension fixing holes (14), the top side of the extension machine arm (6) is connected with a sliding fixing part (15) in a sliding manner, one side of the unmanned aerial vehicle body (1) and one side of the overturning machine arm (5) is fixedly provided with a guide connecting groove (16), the inner side of the guide connecting groove (16) is provided with a guide connecting plate (17) in a sliding connection way.
2. The unmanned aerial vehicle horn beta structure of claim 1, characterized in that, the both sides of upset horn (5) are all fixed and are equipped with guide chute (18), the inboard sliding connection of guide chute (18) is equipped with guide slider (19), one side fixed connection of guide slider (19) is in the one side of extending horn (6).
3. The unmanned aerial vehicle horn beta structure of claim 1, characterized in that, the inboard of direction spacing groove (9) is fixed and is equipped with anticreep spout (20), the inboard sliding connection of anticreep spout (20) is equipped with anticreep slider (21), one side fixed connection of anticreep slider (21) is in the one side of direction spacing post (10).
4. The folding structure of unmanned aerial vehicle horn of claim 1, characterized in that, the elastic member (12) is arranged in a wedge-shaped sixty-degree structure.
5. The folding structure of the unmanned aerial vehicle horn of claim 1, characterized in that the guiding limiting post (10) is matched with the fixing limiting hole (8), and one side of the guiding limiting post (10) far away from the overturning horn (5) is arranged in a chamfer structure.
6. An unmanned aerial vehicle horn beta structure of claim 1, characterized in that, the supporting leg (2) adopts as shock-absorbing supporting frame member.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121311991.7U CN214986011U (en) | 2021-06-11 | 2021-06-11 | Unmanned aerial vehicle horn beta structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121311991.7U CN214986011U (en) | 2021-06-11 | 2021-06-11 | Unmanned aerial vehicle horn beta structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986011U true CN214986011U (en) | 2021-12-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121311991.7U Expired - Fee Related CN214986011U (en) | 2021-06-11 | 2021-06-11 | Unmanned aerial vehicle horn beta structure |
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| CN (1) | CN214986011U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114750945A (en) * | 2022-03-24 | 2022-07-15 | 辽宁警察学院 | Deformable water-air dual-purpose unmanned aerial vehicle and control method thereof |
-
2021
- 2021-06-11 CN CN202121311991.7U patent/CN214986011U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114750945A (en) * | 2022-03-24 | 2022-07-15 | 辽宁警察学院 | Deformable water-air dual-purpose unmanned aerial vehicle and control method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220419 Address after: 230000 room 307, West Building 3, Yulan community, Shicheng community and neighborhood committee, Longgang Economic Development Zone, Yaohai District, Hefei City, Anhui Province Patentee after: Wang Chunlin Address before: 230000 No.1 Liangyuan Road, Hefei City, Anhui Province Patentee before: ANHUI TECHNICAL College OF INDUSTRY AND ECONOMY |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211203 |