CN208036619U - A kind of unmanned plane for launching teargas - Google Patents
A kind of unmanned plane for launching teargas Download PDFInfo
- Publication number
- CN208036619U CN208036619U CN201820403880.0U CN201820403880U CN208036619U CN 208036619 U CN208036619 U CN 208036619U CN 201820403880 U CN201820403880 U CN 201820403880U CN 208036619 U CN208036619 U CN 208036619U
- Authority
- CN
- China
- Prior art keywords
- flight control
- teargas
- screw
- holder
- motor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of unmanned planes for launching teargas,Including drone body,The drone body includes flight control assemblies and delivery device,Accumulator is equipped in the flight control assemblies,The flight control assemblies are equipped with holder,The quantity of the holder is 4,The holder is equipped with screw one and screw two,The screw one is arranged at the top of holder,The screw two is arranged in the bottom of holder,The screw one and screw two include motor one and rotor,One end of the flight control assemblies is equipped with motor two and flabellum,The top of the flight control assemblies is equipped with connecting seat,The delivery device is arranged by connecting seat on flight control assemblies,The unmanned aerial vehicle design that teargas can be launched is novel,It is easy to operate,With good development prospect.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of unmanned plane for launching teargas.
Background technology
With the development of science and technology the application field involved by unmanned plane is also increasingly broader, for example, fire-fighting, the necks such as public security
There has been the unmanned plane that can launch teargas in domain currently on the market.But existing in the market launch teargas
A rotor is all provided only on its every strut of unmanned plane, power is more insufficient, and balance quality is relatively low, on the one hand existing to throw
Put on teargas unmanned plane the device of not helpful teargas diffusion, on the other hand it is existing launch teargas without
Man-machine upper not instruction device, increases operation difficulty.
So how to design a kind of unmanned plane for launching teargas, becoming us will currently solve the problems, such as.
Invention content
In view of the deficienciess of the prior art, the utility model aim be to provide it is a kind of launching teargas nobody
Machine, to solve the problems mentioned in the above background technology, the utility model are reasonable for structure, facilitate environmental protection.
To achieve the goals above, the utility model is to realize by the following technical solutions:One kind can launch tear-gas
The unmanned plane of gas, including drone body, the drone body include flight control assemblies and delivery device, the flight
Accumulator is equipped in control device, the flight control assemblies are equipped with holder, and the quantity of the holder is 4, the holder
It is equipped with screw one and screw two, the screw one is arranged at the top of holder, and the screw two is set
It sets in the bottom of holder, the screw one and screw two include motor one and rotor, the flight control dress
The one end set is equipped with motor two and flabellum, and the top of the flight control assemblies is equipped with connecting seat, and the delivery device passes through
Connecting seat is arranged on flight control assemblies, and the side of the delivery device is equipped with laser lamp ring and through-hole, the delivery device
Interior to be equipped with inner cavity, the interior intracavitary is equipped with teargas and injector, the injector include jet port, injection pipe and gas into
Mouthful, the jet port is arranged at the top of injection pipe, and the gas import is arranged in one end of injection pipe, the jet port setting
On through-hole.
As a kind of preferred embodiment of the utility model, as a kind of preferred embodiment of the utility model, institute
Flabellum is stated on the output shaft of motor two.
As a kind of preferred embodiment of the utility model, the accumulator by electric wire and motor one, injector,
Motor two is connected with laser lamp ring.
As a kind of preferred embodiment of the utility model, the surface of the flight control assemblies is equipped with waterproof coating.
The beneficial effects of the utility model:A kind of unmanned plane for launching teargas of the utility model, including laser
Lamp ring, screw one, holder, flabellum, motor two, connecting seat, rotor, motor one, flight control assemblies, jet port,
Delivery device, gas import, injection pipe, injector, screw two.
1. due to being respectively equipped with screw one and screw two at the top and bottom of holder, so can greatly carry
Stationarity of the high equipment in state of flight, while also providing powerful flying power.
2. motor two can drive flabellum to be rotated, the wind that flabellum is fanned out to when rotating, can help teargas into
Row diffusion, keeps the effect of the injection of teargas more preferable.
3. the light that laser lamp ring irradiates when working can play user indicative function, easy to operate, conveniently make
User uses.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structural schematic diagram of the utility model injector;
In figure:1- laser lamp ring, 2- screws one, 3- holders, 4- flabellums, 5- motor two, 6- connecting seats, 7- rotations
The wing, 8- motor one, 9- flight control assemblies, 10- jet ports, 11- delivery devices, the import of 12- gas, 13- injection pipes, 14-
Injector, 15- screws two.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
It please refers to Fig.1 to Fig. 2, the utility model provides a kind of technical solution:A kind of unmanned plane for launching teargas,
Including drone body, the drone body includes flight control assemblies 9 and delivery device 11, the flight control assemblies 9
Interior to be equipped with accumulator, the flight control assemblies 9 are equipped with holder 3, and the quantity of the holder 3 is 4, is set on the holder 3
There are screw 1 and screw 2 15, the screw 1 to be arranged in the top of holder 3, the screw 2 15
It is arranged in the bottom of holder 3, the screw 1 and screw 2 15 are described to fly including motor 1 and rotor 7
One end of row control device 9 is equipped with motor 25 and flabellum 4, and the top of the flight control assemblies 9 is equipped with connecting seat 6, described
Delivery device 11 is arranged by connecting seat 6 on flight control assemblies 9, and the side of the delivery device 11 is equipped with laser lamp ring 1
And through-hole, the delivery device 11 is interior to be equipped with inner cavity, and the interior intracavitary is equipped with teargas and injector 14, the injector 14
Including jet port 10, injection pipe 13 and gas import 12, the jet port 10 is arranged at the top of injection pipe 13, the gas into
Mouth 12 is arranged in one end of injection pipe 13, and the jet port 10 is arranged on through-hole.
As a kind of preferred embodiment of the utility model, the rotor 7 is arranged on the output shaft of motor 1.
As a kind of preferred embodiment of the utility model, the flabellum 4 is mounted on the output shaft of motor 25.
As a kind of preferred embodiment of the utility model, the accumulator passes through electric wire and motor 1, injector
14, motor 25 and laser lamp ring 1 connect.
As a kind of preferred embodiment of the utility model, the surface of the flight control assemblies 9 is equipped with waterproof coating.
Operation principle:Whether all parts for first checking for the equipment are normal, can be driven when motor 1 is powered on
Rotor 7 is rotated, so as to make the equipment fly, since the top and bottom of holder 3 are respectively equipped with one 2 He of screw
Screw 2 15 so stationarity of the equipment in state of flight can greatly be improved, while also providing powerful
Flying power, injector 14 can spray the teargas of interior intracavitary, and motor 25 can drive flabellum 4 to be rotated, fan
The wind that leaf 4 is fanned out to when rotating, can help teargas to be diffused, keep the effect of injection more preferable, due to laser lamp ring 1 and spray
Loophole 14 is in the same plane, so the light that laser lamp ring 1 irradiates when working can play indicative function to user,
Easy to operate, user-friendly, the unmanned aerial vehicle design that can launch teargas is novel, easy to operate, has good
Development prospect.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiment being appreciated that.
Claims (5)
1. a kind of unmanned plane for launching teargas, including drone body, it is characterised in that:The drone body includes
Flight control assemblies(9)And delivery device(11), the flight control assemblies(9)It is interior to be equipped with accumulator, the flight control dress
It sets(9)It is equipped with holder(3), the holder(3)Quantity be 4, the holder(3)It is equipped with screw one(2)And spiral shell
Cyclone two(15), the screw one(2)It is arranged in holder(3)Top, the screw two(15)Setting is being propped up
Frame(3)Bottom, the screw one(2)With screw two(15)It include motor one(8)And rotor(7), described
Flight control assemblies(9)One end be equipped with motor two(5)And flabellum(4), the flight control assemblies(9)Top be equipped with connect
Joint chair(6), the delivery device(11)Pass through connecting seat(6)It is arranged in flight control assemblies(9)On, the delivery device(11)
Side be equipped with laser lamp ring(1)And through-hole, the delivery device(11)Interior to be equipped with inner cavity, the interior intracavitary is equipped with teargas
And injector(14), the injector(14)Including jet port(10), injection pipe(13)With gas import(12), the jet port
(10)It is arranged in injection pipe(13)Top, the gas import(12)It is arranged in injection pipe(13)One end, the jet port
(10)It is arranged on through-hole.
2. a kind of unmanned plane for launching teargas according to claim 1, it is characterised in that:The rotor(7)If
It sets in motor one(8)Output shaft on.
3. a kind of unmanned plane for launching teargas according to claim 1, it is characterised in that:The flabellum(4)Peace
Mounted in motor two(5)Output shaft on.
4. a kind of unmanned plane for launching teargas according to claim 1, it is characterised in that:The accumulator passes through
Electric wire and motor one(8), injector(14), motor two(5)With laser lamp ring(1)Connection.
5. a kind of unmanned plane for launching teargas according to claim 1, it is characterised in that:The flight control dress
It sets(9)Surface be equipped with waterproof coating.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820403880.0U CN208036619U (en) | 2018-03-23 | 2018-03-23 | A kind of unmanned plane for launching teargas |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820403880.0U CN208036619U (en) | 2018-03-23 | 2018-03-23 | A kind of unmanned plane for launching teargas |
Publications (1)
Publication Number | Publication Date |
---|---|
CN208036619U true CN208036619U (en) | 2018-11-02 |
Family
ID=63948654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820403880.0U Active CN208036619U (en) | 2018-03-23 | 2018-03-23 | A kind of unmanned plane for launching teargas |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN208036619U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110861776A (en) * | 2019-12-17 | 2020-03-06 | 淮安航空产业研究院有限公司 | Unmanned aerial vehicle and system for throwing tear-gas shells and method for throwing tear-gas shells in human-in-loop mode |
WO2021103497A1 (en) * | 2019-11-26 | 2021-06-03 | 滨州学院 | Airflow jet-type steering unmanned aerial vehicle |
-
2018
- 2018-03-23 CN CN201820403880.0U patent/CN208036619U/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021103497A1 (en) * | 2019-11-26 | 2021-06-03 | 滨州学院 | Airflow jet-type steering unmanned aerial vehicle |
CN110861776A (en) * | 2019-12-17 | 2020-03-06 | 淮安航空产业研究院有限公司 | Unmanned aerial vehicle and system for throwing tear-gas shells and method for throwing tear-gas shells in human-in-loop mode |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP7316977B2 (en) | Weight transfer coaxial rotary wing helicopter | |
CN106143911B (en) | A kind of foldable unmanned plane that individual soldier carries, can cartridge type storage and emit | |
US20190291858A1 (en) | Unmanned aerial vehicle | |
CN208036619U (en) | A kind of unmanned plane for launching teargas | |
KR20210033104A (en) | Drone capable of adjusting propulsion direction | |
CN207311831U (en) | A kind of unmanned plane | |
CN109247686A (en) | A kind of accumulation hair dryer | |
CN209700924U (en) | A kind of unmanned plane during flying body with cage shape shielded frame | |
CN109131891A (en) | A kind of more rotor plant protection drones | |
CN108082506A (en) | Unmanned vehicle | |
CN207550505U (en) | Small-sized pilotless aircraft | |
CN207550506U (en) | Ducted propeller and small-sized pilotless aircraft | |
CN207611540U (en) | It is electronic from boat torpedo model component and its electronic from boat torpedo model | |
CN107472523A (en) | Ducted propeller and small-sized pilotless aircraft | |
CN207565823U (en) | Ultrasonic wave anti-interference structure and small-sized pilotless aircraft | |
CN109122505A (en) | A kind of bio-robot for fish pond spreading | |
CN208248495U (en) | A kind of rotor enwraped type unmanned plane | |
CN207759054U (en) | Unmanned vehicle | |
CN207565837U (en) | Radiator structure and the small-sized pilotless aircraft with the radiator structure | |
CN206618338U (en) | A kind of aircraft gun pulls target | |
CN111846191A (en) | Combined power airship | |
CN208181418U (en) | A kind of flying saucer unmanned plane | |
CN107472501A (en) | Ultrasonic wave anti-interference structure and small-sized pilotless aircraft | |
CN109515699A (en) | Quadrotor drone flight system and its method | |
CN206327570U (en) | A kind of spherical aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |