CN206031792U - Unmanned plane sprays and dispels device - Google Patents
Unmanned plane sprays and dispels device Download PDFInfo
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- CN206031792U CN206031792U CN201620984210.3U CN201620984210U CN206031792U CN 206031792 U CN206031792 U CN 206031792U CN 201620984210 U CN201620984210 U CN 201620984210U CN 206031792 U CN206031792 U CN 206031792U
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- container
- micropump
- unmanned plane
- nozzle
- dispersed
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Abstract
The utility model discloses an unmanned plane sprays and dispels device, including container and the intercommunication that is used for saving irritability liquid the container spray the piece, spray including the micropump and the nozzle that are used for driving liquid ejection that connect gradually, certain angle slant below is set to the nozzle, the container upper end is equipped with the coupling mechanism who is used for connecting the unmanned aerial vehicle bottom three at least, the micropump is through wiring harness connection unmanned aerial vehicle's the control unit. Through setting up the container to the piece is sprayed in the setting, and a micropump that will spray and unmanned aerial vehicle's the control unit is connected, utilizes unmanned aerial vehicle's transmission signal itself to implement control to the micropump, thereby the spraying of control irritability liquid and simultaneously because the setting of the inclination of nozzle can directly upset people's face during assurance irritability liquid ejection, thereby reaches and dispel the effect.
Description
Technical field
This utility model is related to security appliance field, and device is dispersed in more particularly to a kind of unmanned plane injection.
Background technology
In recent years, safety problem has become China or even global hot issue, how to improve safety precaution water
Level that is flat and solving safety problem, also becomes problem demanding prompt solution in industry.And unmanned air vehicle technique, then can be considered as
Solve an important tool of safety problem.
At present, with the maturation of unmanned air vehicle technique, unmanned plane has carried out substantial amounts of application in each industrial circle.But
Instantly technical grade unmanned plane, still has that application mode is single, is only capable of realizing the effect of image transmitting, based on this, how
The application level of unmanned plane is improved, becomes unmanned plane industry problem demanding prompt solution instantly.
Utility model content
The technical problems to be solved in the utility model is, for existing unmanned air vehicle technique, how to improve unmanned plane application
Level.
This utility model solves the technical scheme adopted by its technical problem：
Device is dispersed in a kind of injection of UAV system, including for storing the container of excitant liquid and connect the container
Spraying pack unit, the spraying pack unit include the micropump and nozzle for driving liquid ejection being sequentially connected, and nozzle is arranged to necessarily
The oblique lower section of angle, the container upper end are provided with least three for connecting the bindiny mechanism of unmanned motor spindle, the micropump
The control unit of unmanned plane is connected by wire harness.
Further, the bindiny mechanism includes connecting rod and the screw being arranged in the connecting rod, accordingly unmanned plane
Bottom is provided with the screw being adapted.
Further, the container is provided with the inlet for injecting excitant liquid, is provided with close at the inlet
Capping.
Further, the spraying pack unit is threaded connection with the container.
Further, the upper vessel portion is provided with depressed part, for accommodating the photographic head part of unmanned plane.
Implement UAV system injection of the present utility model and disperse device, have the advantages that：By arranging container, and
Spraying pack unit is set, and the micropump of spraying pack unit is connected with the control unit of unmanned plane, believed using the transmission of unmanned plane itself
Number micropump is implemented to control, so as to control the sprinkling of excitant liquid, and simultaneously as the angle of inclination of nozzle is arranged, it is ensured that
Excitant liquid can directly stimulate face when spraying, and disperse effect so as to reach.
Description of the drawings
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or accompanying drawing to be used is briefly described needed for description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, before creative labor is not paid
Put, can be with according to these other accompanying drawings of accompanying drawings acquisition.
Fig. 1 is the planar structure block diagram that device one embodiment is dispersed in the injection of this utility model UAV system；
Fig. 2 is the right side structural representation that device is dispersed in the injection of UAV system shown in Fig. 1.
Specific embodiment
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only this utility model a part of embodiment, rather than whole
Embodiment.Based on the embodiment in this utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of this utility model protection.
Referring to Fig. 1 and Fig. 2, in one embodiment that device is dispersed in the injection of this utility model UAV system, including container 1
With spraying pack unit 2.Container 1 is used for storing excitant liquid, such as capsicum solution.Concrete is not made to the shape of container 1 in the present embodiment
Limit, can be variously-shaped for disc, cuboid etc., such structure change still falls into protection domain of the present utility model
Within.The container 1 is provided with the inlet 4 for injecting excitant liquid, is provided with closure at the inlet 4.
Used as the further optimization to the present embodiment, 1 top of the container is provided with depressed part 5, for accommodating unmanned plane
Photographic head part.Preferably the depressed part 5 is in hemisphere, so as to facilitate photographic head to rotate to 1 sunken inside of container.
Spraying pack unit 2 connects the container 1, and it is miniature for drive liquid to spray that the spraying pack unit 2 includes being sequentially connected
Pump and nozzle, nozzle arrange angled side obliquely, it is preferable that the setting direction of nozzle is using arriving in 10 with level angle
70 degree of angle is advisable.
In the present embodiment, 1 upper end of the container is provided with three bindiny mechanisms 3 for connecting unmanned motor spindle, described
Bindiny mechanism 3 includes connecting rod and the screw being arranged in the connecting rod, and accordingly unmanned motor spindle is provided with the spiral shell being adapted
Hole.In other embodiments, it would however also be possible to employ the mode of buckle draw-in groove is attached, so as to reaching the effect of Quick Release quick change.Institute
State micropump by wire harness connect unmanned plane control unit, realize then realize by using the remote control unit of unmanned plane it is right
The control of micropump.
Used as the further optimization to the present embodiment, the spraying pack unit 2 is threaded connection with the container 1, is reached close
Envelope effect prevents effusion.
Implement UAV system injection of the present utility model and disperse device, have the advantages that：By arranging container 1,
And spraying pack unit 2 is set, and the micropump of spraying pack unit 2 is connected with the control unit of unmanned plane, using the biography of unmanned plane itself
Defeated signal is implemented to control to micropump, so as to control the sprinkling of excitant liquid, and simultaneously as the angle of inclination of nozzle is arranged,
Face can directly be stimulated when ensureing that excitant liquid sprays, effect is dispersed so as to reach.
Preferred embodiment of the present utility model is the foregoing is only, it is not to limit this utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent substitution and improvements made etc. should be included in this utility model
Protection domain within.
Claims (5)
1. device is dispersed in a kind of UAV system injection, it is characterised in that included：For storing the container of excitant liquid and connecting
The spraying pack unit of the container, the spraying pack unit include the micropump and nozzle for driving liquid ejection being sequentially connected, nozzle
Angled side obliquely is set, and the container upper end is provided with least three for connecting the bindiny mechanism of unmanned motor spindle,
The micropump connects the control unit of unmanned plane by wire harness.
2. device is dispersed in UAV system injection according to claim 1, it is characterised in that the bindiny mechanism includes connection
Bar and the screw being arranged in the connecting rod, accordingly unmanned motor spindle be provided with the screw being adapted.
3. device is dispersed in UAV system injection according to claim 1, it is characterised in that the container is provided with for noting
Enter the inlet of excitant liquid, at the inlet, be provided with closure.
4. device is dispersed in UAV system injection according to claim 1, it is characterised in that the spraying pack unit and the container
It is threaded connection.
5. device is dispersed in the UAV system injection according to any one of claim 1 to 4, it is characterised in that the appearance
Device top is provided with depressed part, for accommodating the photographic head part of unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620984210.3U CN206031792U (en) | 2016-08-30 | 2016-08-30 | Unmanned plane sprays and dispels device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620984210.3U CN206031792U (en) | 2016-08-30 | 2016-08-30 | Unmanned plane sprays and dispels device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031792U true CN206031792U (en) | 2017-03-22 |
Family
ID=58303838
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620984210.3U Active CN206031792U (en) | 2016-08-30 | 2016-08-30 | Unmanned plane sprays and dispels device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206031792U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107092269A (en) * | 2017-06-20 | 2017-08-25 | 江苏蒲公英无人机有限公司 | A kind of night convoy unmanned plane and its method of work |
| CN108010598A (en) * | 2017-12-27 | 2018-05-08 | 上海格拉曼国际消防装备有限公司 | A kind of device for realizing low latitude sprinkling multicomponent depressor |
-
2016
- 2016-08-30 CN CN201620984210.3U patent/CN206031792U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107092269A (en) * | 2017-06-20 | 2017-08-25 | 江苏蒲公英无人机有限公司 | A kind of night convoy unmanned plane and its method of work |
| CN108010598A (en) * | 2017-12-27 | 2018-05-08 | 上海格拉曼国际消防装备有限公司 | A kind of device for realizing low latitude sprinkling multicomponent depressor |
| CN108010598B (en) * | 2017-12-27 | 2023-07-21 | 上海格拉曼国际消防装备有限公司 | Device for realizing low-altitude spraying of multiple groups of partial pressure preparations |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |