CN212099316U - Unmanned aerial vehicle horn locking mechanical system - Google Patents
Unmanned aerial vehicle horn locking mechanical system Download PDFInfo
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- CN212099316U CN212099316U CN202020723476.9U CN202020723476U CN212099316U CN 212099316 U CN212099316 U CN 212099316U CN 202020723476 U CN202020723476 U CN 202020723476U CN 212099316 U CN212099316 U CN 212099316U
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- fixedly connected
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- aerial vehicle
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle horn locking mechanism, which comprises a body, wherein the surrounding side walls of the body are provided with horns, and the outer wall of the body is provided with an annular frame; the upper surface of the annular frame is fixedly connected with a plurality of uniformly distributed L-shaped fixing plates, corresponding threaded holes are formed in the surface of the horizontal part of each L-shaped fixing plate and the upper surface of the machine body, and bolts are connected with the threaded holes in an internal thread manner; the outer wall of the annular frame is fixedly connected with a bottom plate, the upper surface of the bottom plate is fixedly connected with a plurality of groups of two first fixing rods which are uniformly distributed, the surface of the horn is provided with first through holes corresponding to the two first fixing rods, and the upper surface of the bottom plate is provided with a cover plate; the surface of the cover plate is rotatably connected with a plurality of rotating rods through bearings. The utility model discloses can conveniently carry out the dismouting to a plurality of horn simultaneously, improve dismouting efficiency, can conveniently dismantle the maintenance to an solitary horn simultaneously.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle horn locking mechanical system.
Background
Compared with the manned aircraft, the unmanned aircraft has the advantages of small volume, low cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
When the horn and the fuselage on the unmanned aerial vehicle need to be locked, the bolt is used for locking, and when the unmanned aerial vehicle is disassembled and assembled, a specific tool is used for disassembling and assembling one of the horn and the fuselage, so that the unmanned aerial vehicle is complicated and inconvenient.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the problem that when needs lock horn and fuselage on the unmanned aerial vehicle among the prior art, lock through using the bolt because of needs, when carrying out the dismouting to it, still need use specific instrument to one of them dismouting, the loaded down with trivial details inconvenience of going on, and an unmanned aerial vehicle horn locking mechanical system who provides.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle horn locking mechanism comprises a body, wherein the peripheral side walls of the body are provided with horns, and the outer wall of the body is provided with an annular frame;
the upper surface of the annular frame is fixedly connected with a plurality of uniformly distributed L-shaped fixing plates, corresponding threaded holes are formed in the surface of the horizontal part of each L-shaped fixing plate and the upper surface of the machine body, and bolts are connected with the threaded holes in an internal thread mode;
the outer wall of the annular frame is fixedly connected with a bottom plate, the upper surface of the bottom plate is fixedly connected with a plurality of groups of two first fixing rods which are uniformly distributed, first through holes corresponding to the two first fixing rods are formed in the surface of the machine arm, and a cover plate is arranged on the upper surface of the bottom plate;
the surface of the cover plate is rotatably connected with a plurality of rotating rods through bearings, the bottom ends of the rotating rods are fixedly connected with strip-shaped clamping blocks, and strip-shaped openings corresponding to the strip-shaped clamping blocks are formed in the surface of the bottom plate;
the surface of the cover plate is provided with a groove corresponding to the machine arm, and a rotary dismounting mechanism is rotationally connected in the groove.
Preferably, the upper surface of the rotating rod is fixedly connected with a rotating block.
Preferably, the rotary disassembling mechanism comprises a rotating shaft which is connected with the rotation of the side wall of the groove, the outer wall of the rotating shaft is fixedly connected with two torsion springs which are symmetrically distributed, two torsion springs are fixedly connected with one ends, back to the back, of the torsion springs and the side wall of the groove, the outer wall of the rotating shaft is fixedly connected with a connecting plate, one end, far away from the rotating shaft, of the connecting plate is connected with a sealing plate, the sealing plate is multiple, a second fixing rod is fixedly connected with the lower surface of the sealing plate, and a second through hole corresponding to the second fixing rod is formed in the surface.
Preferably, the outer wall of the sealing plate is fixedly connected with a sealing gasket.
Preferably, the lower surface of the bottom plate is fixedly connected with a limit stop corresponding to the strip-shaped fixture block.
Compared with the prior art, the utility model provides an unmanned aerial vehicle horn locking mechanical system possesses following beneficial effect:
1. this unmanned aerial vehicle horn locking mechanical system, outer wall through at the fuselage is provided with annular frame, and be provided with bottom plate and apron on annular frame, when needs lock the unmanned aerial vehicle horn, earlier on a plurality of horn cards first dead lever on the bottom plate, cover the apron on the bottom plate, seal in the second dead lever on the board inserts the second through-hole on the horn, the bar fixture block on the apron passes the bar opening on the bottom plate, rotate the turning block, the turning block drives the dwang and rotates, the dwang drives the bar fixture block and rotates, make the bar fixture block card on the bottom plate, otherwise can dismantle the horn, can conveniently carry out the dismouting to a plurality of horns simultaneously, the dismouting efficiency is improved.
2. This unmanned aerial vehicle horn locking mechanical system, through being provided with the sealing plate on the apron, when needs dismantle the maintenance to an solitary horn, rotate the sealing plate, the sealing plate drives the connecting plate and rotates, the connecting plate drives the pivot and rotates, the pivot drives torque spring and rotates, seals the plate pulling second dead lever, extracts the second dead lever from the horn, the pulling horn makes first dead lever keep away from the horn, can conveniently dismantle the maintenance to an solitary horn.
The part that does not relate to among the device all is the same with prior art or can adopt prior art to realize, the utility model discloses can conveniently carry out the dismouting to a plurality of horn simultaneously, improve dismouting efficiency, can conveniently dismantle the maintenance to an solitary horn simultaneously.
Drawings
Fig. 1 is a schematic structural view of an arm locking mechanism of an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic top view of the locking mechanism of the arm of the unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic structural view of a bottom plate of the locking mechanism of the arm of the unmanned aerial vehicle according to the present invention;
fig. 4 is the utility model provides a structural schematic diagram of unmanned aerial vehicle horn locking mechanical system A part.
In the figure: the device comprises a machine body 1, a machine arm 2, an annular frame 3, a 4L-shaped fixing plate, a bolt 5, a bottom plate 6, a first fixing rod 7, a cover plate 8, a rotating rod 9, a strip-shaped clamping block 10, a rotating block 11, a rotating shaft 12, a torsion spring 13, a connecting plate 14, a sealing plate 15, a second fixing rod 16 and a limit stop 17.
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.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.
Referring to fig. 1-4, an unmanned aerial vehicle horn locking mechanism comprises a body 1, wherein the side walls of the periphery of the body 1 are provided with horns 2, and the outer wall of the body 1 is provided with an annular frame 3;
the upper surface of the annular frame 3 is fixedly connected with a plurality of evenly distributed L-shaped fixing plates 4, corresponding threaded holes are formed in the surface of the horizontal part of each L-shaped fixing plate 4 and the upper surface of the machine body 1, and bolts 5 are connected with the threaded holes in a threaded manner;
a bottom plate 6 is fixedly connected to the outer wall of the annular frame 3, a plurality of groups of two first fixing rods 7 which are uniformly distributed are fixedly connected to the upper surface of the bottom plate 6, first through holes corresponding to the two first fixing rods 7 are formed in the surface of the horn 2, and a cover plate 8 is arranged on the upper surface of the bottom plate 6;
the surface of the cover plate 8 is rotatably connected with a plurality of rotating rods 9 through bearings, the bottom ends of the rotating rods 9 are fixedly connected with strip-shaped clamping blocks 10, and strip-shaped openings corresponding to the strip-shaped clamping blocks 10 are formed in the surface of the bottom plate 6;
the surface of the cover plate 8 is provided with a groove corresponding to the machine arm 2, and the groove is rotationally connected with a rotary dismounting mechanism.
The upper surface of dwang 9 is fixedly connected with turning block 11, can conveniently rotate dwang 9.
The rotary disassembling mechanism comprises a rotating shaft 12 which is rotatably connected with the side wall of the groove, the outer wall of the rotating shaft 12 is fixedly connected with two torsion springs 13 which are symmetrically distributed, one ends of the two torsion springs 13, which are back to the back, are fixedly connected with the side wall of the groove, the outer wall of the rotating shaft 12 is fixedly connected with a connecting plate 14, one end of the connecting plate 14, which is far away from the rotating shaft 12, is fixedly connected with sealing plates 15, a plurality of second fixing rods 16 are fixedly connected with the lower surfaces of the sealing plates 15, and second through holes corresponding to the second fixing rods 16 are formed in the.
The outer wall of the sealing plate 15 is fixedly connected with a sealing gasket, so that the sealing performance of the sealing plate 15 can be conveniently improved.
The lower surface of the bottom plate 6 is fixedly connected with a limit stop 17 corresponding to the strip-shaped fixture block 10, so that the strip-shaped fixture block 10 can be conveniently limited.
In the utility model, when the unmanned aerial vehicle arm 2 is required to be locked, a plurality of arms 2 are firstly clamped on a first fixed rod 7 on a bottom plate 6, a cover plate 8 is covered on the bottom plate 6, a second fixed rod 16 on a sealing plate 15 is inserted into a second through hole on the arm 2, a strip-shaped fixture block 10 on the cover plate 8 passes through a strip-shaped opening on the bottom plate 6, a rotating block 11 is rotated, the rotating block 11 drives a rotating rod 9 to rotate, the rotating rod 9 drives the strip-shaped fixture block 10 to rotate, so that the strip-shaped fixture block 10 is clamped on the bottom plate 6, otherwise, the arm 2 can be disassembled, a plurality of arms 2 can be conveniently and simultaneously disassembled, the disassembling efficiency is improved, when an independent arm 2 is required to be disassembled and maintained, the sealing plate 15 is rotated, the sealing plate 15 drives a connecting plate to rotate 14, the connecting plate 14 drives a rotating shaft 12 to rotate, the rotating shaft 12 drives a torsion spring 13 to rotate, the, the second fixing rod 16 is pulled out of the horn 2, the horn 2 is pulled, the first fixing rod 7 is far away from the horn 2, and the single horn 2 can be conveniently detached and maintained.
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 (5)
1. An unmanned aerial vehicle horn locking mechanism comprises a body (1), wherein the side walls of the periphery of the body (1) are provided with horns (2), and is characterized in that the outer wall of the body (1) is provided with an annular frame (3);
the upper surface of the annular frame (3) is fixedly connected with a plurality of uniformly distributed L-shaped fixing plates (4), corresponding threaded holes are formed in the surface of the horizontal part of each L-shaped fixing plate (4) and the upper surface of the machine body (1), and bolts (5) are connected with the threaded holes in an internal thread mode;
a bottom plate (6) is fixedly connected to the outer wall of the annular frame (3), a plurality of groups of two first fixing rods (7) which are uniformly distributed are fixedly connected to the upper surface of the bottom plate (6), first through holes corresponding to the two first fixing rods (7) are formed in the surface of the horn (2), and a cover plate (8) is arranged on the upper surface of the bottom plate (6);
the surface of the cover plate (8) is rotatably connected with a plurality of rotating rods (9) through bearings, the bottom ends of the rotating rods (9) are fixedly connected with strip-shaped clamping blocks (10), and strip-shaped openings corresponding to the strip-shaped clamping blocks (10) are formed in the surface of the bottom plate (6);
the surface of the cover plate (8) is provided with a groove corresponding to the machine arm (2), and a rotary dismounting mechanism is rotationally connected in the groove.
2. The unmanned aerial vehicle horn locking mechanism of claim 1, wherein a turning block (11) is fixedly connected to an upper surface of the turning rod (9).
3. The unmanned aerial vehicle horn locking mechanical system of claim 1, characterized in that, the rotatory disassembly body includes the pivot (12) of being connected with the recess lateral wall rotation, the outer wall fixedly connected with two symmetrical distribution of torsion spring (13) of pivot (12), two the one end that torsion spring (13) back to the back is connected with the lateral wall fixed connection of recess, the outer wall fixedly connected with connecting plate (14) of pivot (12), the one end fixedly connected with that the pivot (12) is kept away from in connecting plate (14) seals board (15), a plurality of the lower surface of sealing board (15) all fixedly connected with second dead lever (16), the surface of horn (2) is seted up the second through-hole corresponding with second dead lever (16).
4. The unmanned aerial vehicle horn locking mechanism of claim 3, wherein the outer wall of the sealing plate (15) is fixedly connected with a sealing gasket.
5. The unmanned aerial vehicle horn locking mechanism of claim 1 wherein the lower surface of the base plate (6) is fixedly connected with a limit stop (17) corresponding to the strip-shaped fixture block (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020723476.9U CN212099316U (en) | 2020-05-06 | 2020-05-06 | Unmanned aerial vehicle horn locking mechanical system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020723476.9U CN212099316U (en) | 2020-05-06 | 2020-05-06 | Unmanned aerial vehicle horn locking mechanical system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212099316U true CN212099316U (en) | 2020-12-08 |
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ID=73618757
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020723476.9U Expired - Fee Related CN212099316U (en) | 2020-05-06 | 2020-05-06 | Unmanned aerial vehicle horn locking mechanical system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212099316U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113353250A (en) * | 2021-07-13 | 2021-09-07 | 江苏无国界无人机科技有限公司 | Assembled unmanned aerial vehicle convenient to use |
-
2020
- 2020-05-06 CN CN202020723476.9U patent/CN212099316U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113353250A (en) * | 2021-07-13 | 2021-09-07 | 江苏无国界无人机科技有限公司 | Assembled unmanned aerial vehicle convenient to use |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20201208 |