CN220616221U - Unmanned aerial vehicle horn quick assembly disassembly structure - Google Patents
Unmanned aerial vehicle horn quick assembly disassembly structure Download PDFInfo
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- CN220616221U CN220616221U CN202322017067.3U CN202322017067U CN220616221U CN 220616221 U CN220616221 U CN 220616221U CN 202322017067 U CN202322017067 U CN 202322017067U CN 220616221 U CN220616221 U CN 220616221U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a quick dismounting structure of an unmanned aerial vehicle arm. It comprises the following steps: fuselage and horn, the inside cavity that is equipped with of fuselage, the side of fuselage be equipped with horn matched with spliced eye, be equipped with in the cavity with the main electric grafting end of spliced eye relative setting, the front end of horn is the link, the link be connected with main electric grafting end matched with vice electric grafting end, one side of link be equipped with barb form buckle and with this buckle connection's elastic sheet, the one end of elastic sheet is located the outside of spliced eye, the lateral wall of spliced eye be equipped with this buckle matched with draw-in hole or the adapter sleeve of draw-in hole installation with this buckle joint, the adapter sleeve cup joints with the link. According to the utility model, the buckle is arranged on the horn, and the clamping hole or the connecting sleeve is arranged in the plugging hole of the machine body, so that the horn can be clamped while being plugged, and the horn and the machine body are convenient to assemble and disassemble.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a quick dismounting structure of an unmanned aerial vehicle arm.
Background
Unmanned aerial vehicle on the market generally adopts a plurality of horn structures at present, for convenient quick installation horn, and the industry generally adopts grafting structure at present, like patent number is: CN201821198769.9, the name of which is: the utility model patent of a detachable horn of an unmanned aerial vehicle, wherein the horn in the patent adopts a plug-in connection structure, two ends of the plug-in connection are respectively provided with a power interface, and the plug-in connection is realized simultaneously so as to facilitate the machine body to control the rotating wing at the upper end of the horn; because of the simple plug-in structure, the horn is easy to separate from the machine body, and the reinforcing structure is arranged on the outer side of the horn in the technical scheme, and the horn is separated from the machine body; the reinforcing structure is arranged, so that the reinforcing structure needs to be detached firstly when the motor is detached, and the reinforcing structure needs to be installed on each horn when the motor is installed, and the motor is detached slowly.
Disclosure of Invention
The utility model aims to overcome the defects of the prior art and provides a rapid disassembly and assembly structure for an unmanned aerial vehicle arm, which is simple in disassembly and assembly structure and convenient to implement.
An unmanned aerial vehicle horn quick assembly disassembly structure, it includes: fuselage and horn, the inside cavity that is equipped with of fuselage, the side of fuselage be equipped with horn matched with spliced eye, be equipped with in the cavity with the main electric grafting end of spliced eye relative setting, the front end of horn is the link, the link be connected with main electric grafting end matched with vice electric grafting end, one side of link be equipped with barb form buckle and with this buckle connection's elastic sheet, the one end of elastic sheet is located the outside of spliced eye, the lateral wall of spliced eye be equipped with this buckle matched with draw-in hole or the adapter sleeve of draw-in hole installation with this buckle joint, the adapter sleeve cup joints with the link.
Further, a power supply control board is arranged in the cavity, and the main electric plug-in end is arranged on the power supply control board.
Further, the fuselage includes casing and drain pan, and the side of going up the casing is equipped with the last lug of the U-shaped of inversion, and the side of drain pan is equipped with the lower lug of U-shaped, goes up lug and lower lug concatenation and be hollow arch, protruding inside formation spliced eye, adapter sleeve and arch between be equipped with connection structure, the adapter sleeve is fixed in the spliced eye.
Further, a plurality of connecting lugs are arranged on the side face of the connecting sleeve, a side connecting hole is formed in the middle of the connecting lug, an upper protruding block is provided with an upper plug-in column extending downwards, a lower protruding block is provided with a lower plug-in column extending upwards, and the upper plug-in column and the lower plug-in column are respectively inserted into the upper end and the lower end of the side connecting hole of the connecting lug.
Further, the upper plug-in column and the lower plug-in column are respectively provided with a perforation, a connecting piece is connected between the upper protruding block and the lower protruding block, and the connecting piece penetrates through the upper plug-in column and the lower plug-in column to connect the bottom shell with the upper shell.
Further, the upper end face of the connecting sleeve is provided with a clamping hole matched with the buckle.
Further, the horn includes horn shell and lower horn shell, vice electric grafting end is connected with vice PCB board, and lower horn shell is equipped with and holds matched with jack with vice PCB board, goes up horn shell, lower horn shell all to be equipped with vice electric grafting end matched with breach.
Further, the front end of the buckle is extended with a connecting block, the front end of the connecting block is connected with a plurality of hollow connecting cylinders, the lower arm shell is provided with a base matched with the connecting cylinders, the upper arm shell is provided with a plug-in column which is plugged with the connecting cylinders, and the lower end of the plug-in column passes through the connecting cylinders to be abutted with the base; the upper arm is provided with a through hole matched with the buckle and the elastic piece; the buckle protrudes out of the upper arm shell.
Further, the rear end of the elastic sheet is provided with a convex pressing block.
Further, a spring is arranged between the elastic piece and the lower arm shell.
The utility model has the beneficial effects that: according to the utility model, the buckle is arranged on the horn, and the clamping hole or the connecting sleeve is arranged in the plugging hole of the machine body, so that the horn can be clamped while being plugged, and the horn and the machine body are convenient to assemble and disassemble.
Drawings
FIG. 1 is a schematic diagram of the present utility model.
Fig. 2 is an exploded view of the present utility model.
Fig. 3 is another exploded view of the present utility model.
Fig. 4 is an exploded view of the horn.
The reference numerals are:
1, a machine body; 2-a bump; 3-a main electrical plug; 4-an auxiliary electrical plug terminal; 5-pressing the block; 6-arm; 7-connecting lugs; 8, connecting sleeve; 9-a clamping hole; 11-a buckle; 12-elastic sheet; 13-lower arm shell; 14-upper arm shell; 15-through holes; 16-a plug-in column; 17-connecting block; 18—a connecting cylinder; 19—a secondary PCB board; 20-a base; 21-a jack; 22-upper housing; 23-upper bump; 24-upper plug-in column; 25—under bump; 26-lower plug-in column; 27-bottom shell; 28-power control board.
Description of the embodiments
The utility model is described in detail below with reference to the accompanying drawings.
Examples: see fig. 1-4; an unmanned aerial vehicle horn 6 quick assembly disassembly structure, it includes: fuselage 1 and horn 6, the inside cavity that is equipped with of fuselage 1, the side of fuselage 1 be equipped with horn 6 matched with spliced eye, be equipped with in the cavity with the relative main electric grafting end 3 that sets up of spliced eye, the front end of horn 6 is the link, the link be connected with main electric grafting end 3 matched with vice electric grafting end 4, one side of link be equipped with barb form buckle 11 and with the elastic sheet 12 that this buckle 11 is connected, the one end of elastic sheet 12 is located the outside of spliced eye, the lateral wall of spliced eye be equipped with this buckle 11 matched with draw-in hole 9 or draw-in hole install with the adapter sleeve 8 of this buckle 11 joint, adapter sleeve 8 cup joints with the link.
Compared with the prior art, the improvement points of the technical scheme are as follows: the horn 6 adopts the lock joint structure when pegging graft with fuselage 1 for the joint of horn 6 can quick joint through buckle 11 and draw-in hole 9 or adapter sleeve 8, when dismantling, needs to adopt the foreign object to press down elastic piece 12, makes buckle 11 leave draw-in hole 9, withdraws from horn 6 fast again.
See fig. 3; further, a power control board 28 is arranged in the cavity, and the main electric plug-in terminal 3 is arranged on the power control board 28.
The power supply control board 28 is arranged, so that the installation is convenient; with respect to the decentralized mounting of the main electrical plug terminals 3, no wiring structure is required.
See fig. 3; further, the machine body 1 includes an upper housing 22 and a bottom housing 27, an inverted U-shaped upper bump 23 is provided on a side surface of the upper housing 22, a U-shaped lower bump 25 is provided on a side surface of the bottom housing 27, the upper bump 23 and the lower bump 25 are spliced into a hollow protrusion 2, the protrusion 2 is internally formed with a plugging hole, a connection structure is provided between the connection sleeve 8 and the protrusion 2, and the connection sleeve 8 is fixed in the plugging hole.
For convenient connection, the side surface of the machine body 1 is provided with a hollow bulge 2 which is used for being connected with a connecting sleeve 8 and the connecting end of a machine arm 6. Meanwhile, the joint is positioned inside the bulge 2, so that external interference is avoided. The connection structure may be a socket structure and an interference fit.
Further, a plurality of connecting lugs 7 are arranged on the side face of the connecting sleeve 8, a side connecting hole is formed in the middle of the connecting lug 7, an upper protruding block 23 is provided with an upper plug-in post 24 extending downwards, a lower protruding block 25 is provided with a lower plug-in post 26 extending upwards, and the upper plug-in post 24 and the lower plug-in post 26 are respectively inserted into the upper end and the lower end of the side connecting hole of the connecting lug 7.
By arranging the side connecting lugs 7 on the side surface of the connecting sleeve 8, an upper plug-in column 24 and a lower plug-in column 26 are arranged in the convex blocks; is spliced with the connecting sleeve 8 through the upper splicing column 24 and the lower splicing column 26 and is fixed.
Further, the upper plug post 24 and the lower plug post 26 are provided with through holes, and a connecting piece is connected between the upper protruding block 23 and the lower protruding block 25 and penetrates through the upper plug post 24 and the lower plug post 26 to connect the bottom shell 27 with the upper shell 22.
The connection may be a bolt. Through the upper plug-in column 24 and the lower plug-in column 26, a connecting piece can be arranged to connect the bottom shell 27 with the upper shell 22, and the connecting sleeve 8 can be fixed. Convenient to use.
Further, the upper end face of the connecting sleeve 8 is provided with a clamping hole 9 matched with a clamping buckle 11.
See fig. 3, 4; further, the horn 6 includes an upper horn shell 14 and a lower horn shell 13, the auxiliary electric plug-in end 4 is connected with an auxiliary PCB 19, the lower horn shell 13 is provided with a jack 21 matched with the auxiliary PCB 19, and the upper horn shell 14 and the lower horn shell 13 are provided with notches matched with the auxiliary electric plug-in end 4.
For the convenience of fixing the auxiliary electric plug-in end 4, the auxiliary electric plug-in end 4 is connected with an auxiliary PCB 19, the auxiliary PCB 19 is vertically arranged, the lower end of the auxiliary PCB is inserted into a jack 21 of the lower horn 6, and the upper end of the auxiliary PCB is abutted with the upper horn shell 14.
Further, a connecting block 17 extends from the front end of the buckle 11, a plurality of hollow connecting cylinders 18 are connected to the front end of the connecting block 17, a base 20 matched with the connecting cylinders 18 is arranged on the lower arm shell 13, a plug-in column 16 plugged with the connecting cylinders 18 is arranged on the upper arm shell 14, and the lower end of the plug-in column 16 passes through the connecting cylinders 18 and is abutted with the base 20; the upper arm 6 is provided with a through hole 15 matched with the buckle 11 and the elastic piece 12; the buckle 11 protrudes from the upper arm casing 14.
The buckle 11 is separately and additionally arranged in the technical scheme, so that the buckle 11 can be replaced. The front end of buckle 11 is connected with connecting tube 18 through connecting block 17, and connecting block 17 is located the upper end of connecting tube 18, and connecting block 17 and buckle 11, elastic piece 12 are located unsettled state, therefore elastic piece 12 has elasticity, and when using, the connecting end inserts the spliced eye, and buckle 11 receives the butt of spliced eye side earlier and presses down bending deformation, and when buckle 11 gets into card hole 9, buckle 11 and elastic piece 12 reset. When the elastic piece 12 is detached, the elastic piece 12 needs to be pressed downwards, so that the buckle 11 is separated from the clamping hole 9.
Further, the rear end of the elastic sheet 12 is provided with a protruding pressing block 5.
The pressing block 5 is arranged to facilitate pressing.
Further, a spring (not shown) is provided between the elastic piece 12 and the lower arm case 13.
In order to give the elastic sheet 12 a good elasticity, a spring is therefore provided.
The foregoing is merely exemplary of the utility model, and those skilled in the art will recognize that the utility model is not limited thereto, except insofar as modifications may be made by those skilled in the art in light of the teachings of the utility model.
Claims (10)
1. An unmanned aerial vehicle horn quick assembly disassembly structure, it includes: fuselage and horn, the inside cavity that is equipped with of fuselage, the side of fuselage be equipped with horn matched with spliced eye, be equipped with in the cavity with the main electric grafting end of spliced eye relative setting, the front end of horn is the link, the link be connected with main electric grafting end matched with vice electric grafting end, its characterized in that: one side of the connecting end is provided with a barb-shaped buckle and an elastic sheet connected with the buckle, one end of the elastic sheet is positioned at the outer side of the inserting hole, the side wall of the inserting hole is provided with a clamping hole matched with the buckle or the inserting hole is provided with a connecting sleeve clamped with the buckle, and the connecting sleeve is sleeved with the connecting end.
2. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 1, wherein: the cavity is internally provided with a power supply control board, and the main electric plug-in end is arranged on the power supply control board.
3. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 1, wherein: the machine body comprises an upper shell and a bottom shell, wherein an inverted U-shaped upper protruding block is arranged on the side face of the upper shell, a U-shaped lower protruding block is arranged on the side face of the bottom shell, the upper protruding block and the lower protruding block are spliced to form a hollow protrusion, a plug hole is formed in the protrusion, a connecting structure is arranged between a connecting sleeve and the protrusion, and the connecting sleeve is fixed in the plug hole.
4. A quick release structure for an unmanned aerial vehicle horn according to claim 3, wherein: the side of adapter sleeve is equipped with a plurality of engaging lugs, and the middle part of engaging lug is equipped with the side connecting hole, upward the lug is equipped with downwardly extending's last spliced pole, and lower lug is equipped with upward extending's lower spliced pole, goes up spliced pole, lower spliced pole and inserts the side connecting hole upper end of engaging lug, lower extreme respectively.
5. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 4, wherein: the upper plug-in column and the lower plug-in column are respectively provided with a perforation, a connecting piece is connected between the upper convex block and the lower convex block, and the connecting piece penetrates through the upper plug-in column and the lower plug-in column to connect the bottom shell with the upper shell.
6. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 4, wherein: the upper end face of the connecting sleeve is provided with a clamping hole matched with the buckle.
7. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 1, wherein: the horn includes horn shell and lower horn shell, vice electric grafting end is connected with vice PCB board, and lower horn shell is equipped with and holds matched with jack with vice PCB board, goes up horn shell, lower horn shell all to be equipped with vice electric grafting end matched with breach.
8. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 7, wherein: the front end of the buckle is extended with a connecting block, the front end of the connecting block is connected with a plurality of hollow connecting cylinders, the lower arm shell is provided with a base matched with the connecting cylinders, the upper arm shell is provided with a plug-in column which is plugged with the connecting cylinders, and the lower end of the plug-in column passes through the connecting cylinders to be abutted with the base; the upper arm is provided with a through hole matched with the buckle and the elastic piece; the buckle protrudes out of the upper arm shell.
9. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 8, wherein: the rear end of the elastic sheet is provided with a convex pressing block.
10. The unmanned aerial vehicle horn quick assembly disassembly structure of claim 1, wherein: a spring is arranged between the elastic sheet and the lower arm shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322017067.3U CN220616221U (en) | 2023-07-30 | 2023-07-30 | Unmanned aerial vehicle horn quick assembly disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322017067.3U CN220616221U (en) | 2023-07-30 | 2023-07-30 | Unmanned aerial vehicle horn quick assembly disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220616221U true CN220616221U (en) | 2024-03-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322017067.3U Active CN220616221U (en) | 2023-07-30 | 2023-07-30 | Unmanned aerial vehicle horn quick assembly disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220616221U (en) |
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2023
- 2023-07-30 CN CN202322017067.3U patent/CN220616221U/en active Active
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