CN206218230U - A kind of semi-ring wing plant protection unmanned plane - Google Patents
A kind of semi-ring wing plant protection unmanned plane Download PDFInfo
- Publication number
- CN206218230U CN206218230U CN201621257455.2U CN201621257455U CN206218230U CN 206218230 U CN206218230 U CN 206218230U CN 201621257455 U CN201621257455 U CN 201621257455U CN 206218230 U CN206218230 U CN 206218230U
- Authority
- CN
- China
- Prior art keywords
- wing
- semi
- unmanned plane
- plant protection
- chest
- 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.)
- Expired - Fee Related
Links
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses a kind of semi-ring wing plant protection unmanned plane, superposition is provided with medicine-chest and water pump in the waist of semi-ring wing unmanned plane, the medicine-chest is connected by pipeline with the grug transportation tube being horizontally installed on below host wing, pipeline connection between the water pump and medicine-chest and grug transportation tube, is evenly arranged with several atomizers on the grug transportation tube.The utility model has the high-adaptability and crop absorption ratio of the efficient and rotor wing unmanned aerial vehicle of plant protection fixed-wing concurrently, and the wind resistance of this aerodynamic arrangement is fine, flapping wing and very short takeoff and landing performance, can provide the parameter in terms of aerodynamic arrangement for later transporter and early warning plane.
Description
Technical field
The utility model belongs to agricultural aviation device technical field, and in particular to a kind of semi-ring wing plant protection unmanned plane.
Background technology
Nowadays plant protection aircraft be divided into it is manned and unmanned, it is manned with unmanned two kinds of agricultural aviation operations
Mode respectively has an advantage and disadvantage, and the culture that unmanned plane flies to control hand is more much lower than pilot toxigenic capacity, therefore, microminiature it is agricultural nobody
Machine can make up the deficiency of existing manned agricultural aviation, have great demand in Chinese modern agriculture, and China is at present
It is that 1.8% effect is far below other developed countries to use aerial pesticide working area.
Utility model content
In view of this, main purpose of the present utility model is to provide a kind of semi-ring wing plant protection unmanned plane.
To reach above-mentioned purpose, what the technical solution of the utility model was realized in:
The utility model embodiment provides a kind of semi-ring wing plant protection unmanned plane, in the waist of semi-ring wing unmanned plane
Superposition is provided with medicine-chest and water pump, and the medicine-chest is connected by pipeline with the grug transportation tube being horizontally installed on below host wing, described
Pipeline connection between water pump and medicine-chest and grug transportation tube, is evenly arranged with several atomizers on the grug transportation tube.
In such scheme, propulsive thrust mechanism is provided with the top of the semi-ring wing unmanned plane, the propulsive thrust mechanism includes
Duct cylinder and the blade being arranged in duct cylinder.
In such scheme, the duct cylinder is connected by pipeline with medicine-chest.
In such scheme, the duct cylinder is connected by pipeline with the air-blast atomizer for being arranged on host wing side.
In such scheme, control valve is provided with the air-blast atomizer.
In such scheme, the annular wing, the annular wing are symmetrically arranged with the host wing of the semi-ring wing unmanned plane both sides
Inside it is provided with sustainer.
Compared with prior art, the beneficial effects of the utility model:
The utility model has the high-adaptability and crop absorption ratio of the efficient and rotor wing unmanned aerial vehicle of plant protection fixed-wing concurrently, and
Very well, flapping wing and very short takeoff and landing performance can be later transporter and pre- for the wind resistance of this aerodynamic arrangement
Alert machine provides the parameter in terms of aerodynamic arrangement.
Brief description of the drawings
A kind of Fig. 1 structural representations of semi-ring wing plant protection unmanned plane for the utility model embodiment is provided.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and implementation
Example, is further elaborated to the utility model.It should be appreciated that specific embodiment described herein is only used to explain
The utility model, is not used to limit the utility model.
The utility model embodiment provides a kind of semi-ring wing plant protection unmanned plane, as shown in figure 1, being located at semi-ring wing unmanned plane 1
Waist in superposition be provided with medicine-chest 3 and water pump 1, the medicine-chest 3 is by pipeline and is horizontally installed on below host wing
Grug transportation tube 4 is connected, the pipeline connection between the water pump 1 and medicine-chest 3 and grug transportation tube 4, if being evenly arranged with the grug transportation tube 4
Dry atomizer 5.
The top of the semi-ring wing unmanned plane 1 is provided with propulsive thrust mechanism, and the propulsive thrust mechanism includes duct cylinder 6 and sets
Put the blade 7 in duct cylinder 6;The annular main lift-rising principle of the wing accelerates annular wing upper surface air velocity and derivative one for active
Part section Anda effect produces high-lift, is applied on fixed-wing unmanned plane, can be in the case of flying speed is slow
Great lift is produced, the flying speed that propulsive thrust mechanism further suppresses unmanned plane is set.
The duct cylinder 6 is connected by pipeline with medicine-chest 3, can provide pressure for medicine-chest 3
The duct cylinder 6 is connected by pipeline with the air-blast atomizer 8 for being arranged on host wing side, can control effectively spray
Gas port size, by controlling jet pipe size, causes wing both sides force unbalance, controls unmanned machine rolling.
Control valve is provided with the air-blast atomizer 8.
It is symmetrically arranged with the host wing of the both sides of semi-ring wing unmanned plane 1 in the annular wing 9, the annular wing 9 and is provided with
Sustainer.
It is used for replacing a rudder face part to pressurize agricultural chemicals for unmanned plane provides a gases at high pressure part by propulsive thrust mechanism,
The topped up with water of the medicine-chest 3 is mixed into agricultural chemicals by a certain percentage, checks that regional has fault-free, standby for takeoff;First turn on counter pushing away
Force mechanisms reach setting critical value, and the wake flow that at this moment propulsive thrust mechanism produces can be collected, and medicine-chest 3 and spray are conveyed to respectively
The air-blast atomizer 8 of gas formula rudder face pipe end.The air pressure and jet vane facial canal wall pressure power of pressure gauge display medicine-chest 3 is waited to reach mark
Quasi- value, at this moment just can manipulate unmanned plane carries out operation.
The above, preferred embodiment only of the present utility model is not intended to limit protection of the present utility model
Scope.
Claims (6)
1. a kind of semi-ring wing plant protection unmanned plane, it is characterised in that be superimposed in the waist of semi-ring wing unmanned plane and be provided with
Medicine-chest and water pump, the medicine-chest are connected by pipeline with the grug transportation tube being horizontally installed on below host wing, the water pump and medicine-chest
Pipeline connection and grug transportation tube between, is evenly arranged with several atomizers on the grug transportation tube.
2. a kind of semi-ring wing plant protection unmanned plane according to claim 1, it is characterised in that:The top of the semi-ring wing unmanned plane
Portion is provided with propulsive thrust mechanism, the blade that the propulsive thrust mechanism includes duct cylinder and is arranged in duct cylinder.
3. a kind of semi-ring wing plant protection unmanned plane according to claim 2, it is characterised in that:Duct cylinder by pipeline with
Medicine-chest is connected.
4. a kind of semi-ring wing plant protection unmanned plane according to Claims 2 or 3, it is characterised in that:The duct cylinder is by pipe
Road connects with the air-blast atomizer for being arranged on host wing side.
5. a kind of semi-ring wing plant protection unmanned plane according to claim 4, it is characterised in that:It is provided with the air-blast atomizer
Control valve.
6. a kind of semi-ring wing plant protection unmanned plane according to claim 5, it is characterised in that:The semi-ring wing unmanned plane both sides
Host wing on be symmetrically arranged with the annular wing, be provided with sustainer in the annular wing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621257455.2U CN206218230U (en) | 2016-11-23 | 2016-11-23 | A kind of semi-ring wing plant protection unmanned plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621257455.2U CN206218230U (en) | 2016-11-23 | 2016-11-23 | A kind of semi-ring wing plant protection unmanned plane |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206218230U true CN206218230U (en) | 2017-06-06 |
Family
ID=58791059
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621257455.2U Expired - Fee Related CN206218230U (en) | 2016-11-23 | 2016-11-23 | A kind of semi-ring wing plant protection unmanned plane |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206218230U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107352034A (en) * | 2017-06-14 | 2017-11-17 | 广州越城丰茂农林科技有限公司 | New golden-pomelo yellow twig Control Technology |
WO2019063942A1 (en) * | 2017-09-27 | 2019-04-04 | Drone Air Fly | Dispersion aircraft |
-
2016
- 2016-11-23 CN CN201621257455.2U patent/CN206218230U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107352034A (en) * | 2017-06-14 | 2017-11-17 | 广州越城丰茂农林科技有限公司 | New golden-pomelo yellow twig Control Technology |
WO2019063942A1 (en) * | 2017-09-27 | 2019-04-04 | Drone Air Fly | Dispersion aircraft |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN206243453U (en) | A kind of unmanned plane gas source control system | |
CN205891234U (en) | A unite efflux controlling means for helicopter rotor blade | |
CN106005396B (en) | United jet flow control device and its control method for lifting airscrew blade | |
CN106628163B (en) | A kind of supersonic speed unmanned fighter that big drag braking and VTOL can be achieved | |
CN104890858A (en) | Wing structure with active flow control mechanism | |
CN104176241A (en) | High-efficiency pneumatic layout structure of synergistic jet for high-altitude propeller and control method | |
CN104108464B (en) | A kind of double-deck rotor aircraft | |
CN206218230U (en) | A kind of semi-ring wing plant protection unmanned plane | |
CN208165247U (en) | Unmanned plane based on gas jet technique turning | |
CN109677608A (en) | Tailless flying wing coupling power aircraft | |
CN102145744B (en) | High-speed energy-saving warplane | |
CN107021235B (en) | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft | |
CN109850128A (en) | Multi-stage blowing circulation volume high-lift device and aircraft | |
CN104875887B (en) | A kind of vertical lift component and the fan rotor aircraft with it | |
CN101143622A (en) | Wingless air vehicle capable of vertical take-off and landing and its realizing method | |
RU86560U1 (en) | VERTICAL TAKEOFF AND LANDING FLIGHT | |
CN103921943A (en) | Wingtip spraying system of rotor-type aircraft and application of wingtip spraying system | |
US3025026A (en) | Supplemental flight controls for aircraft | |
CN1718507B (en) | Wind power air pressure engine air craft | |
CN205589506U (en) | Novel medicine rack is spouted in unmanned aerial vehicle pneumatics device | |
CN202464126U (en) | Rotor wing blade tip jet one-man flight vehicle | |
CN104986323A (en) | Glove vane aircraft | |
CN209852581U (en) | Ducted propeller thrust coaxial dual-rotor helicopter | |
CN208291467U (en) | A kind of double ducted fan vector power short take-off and landing devices of fixed-wing | |
GB862032A (en) | Aircraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170606 Termination date: 20191123 |
|
CF01 | Termination of patent right due to non-payment of annual fee |