CN206345013U - A kind of rotor wing unmanned aerial vehicle with kuppe - Google Patents
A kind of rotor wing unmanned aerial vehicle with kuppe Download PDFInfo
- Publication number
- CN206345013U CN206345013U CN201720016676.9U CN201720016676U CN206345013U CN 206345013 U CN206345013 U CN 206345013U CN 201720016676 U CN201720016676 U CN 201720016676U CN 206345013 U CN206345013 U CN 206345013U
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- CN
- China
- Prior art keywords
- water conservancy
- conservancy diversion
- fuselage
- cover
- aerial vehicle
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Abstract
A kind of rotor wing unmanned aerial vehicle with kuppe, include water conservancy diversion flight cover, water conservancy diversion flying wing, rotor blade, lateral deflector, fuselage, bottom flap, camera and infrared lamp, water conservancy diversion flight cover is provided with the top of the fuselage, and be respectively arranged with lateral deflector in the left and right sides on water conservancy diversion flight cover top and water conservancy diversion flight cover afterbody is provided with water conservancy diversion flying wing, the bottom of the fuselage is provided with bottom flap, and it is connected with four rotor blades in fuselage, the front end of the fuselage is provided with camera and infrared lamp, and infrared lamp is arranged at around camera in isosceles triangle.This rotor wing unmanned aerial vehicle, has installed wind-force air deflector additional, makes more to stablize and turn to flexibly during flight, and reduces windage by wind-force air deflector, the use time of battery is added, while also increasing the flight endurance of unmanned plane.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is related to a kind of rotor wing unmanned aerial vehicle with kuppe, more particularly to
A kind of rotor wing unmanned aerial vehicle with kuppe.
Background technology
In view of unmanned plane on the market, pay attention on good appearance and functionally more, but ignore the emphasis of aircraft, fly
The endurance when emphasis of device is exactly flight and flight, is how this makes unmanned plane suffered wind-force resistance in flight reduce most
It is small, it is research of the present utility model to increase stability in-flight and flexibility.
The content of the invention
The purpose of this utility model is to provide a kind of rotor wing unmanned aerial vehicle with kuppe, it is intended to solve existing rotor nobody
Problem and shortage present on machine.
The technical scheme that the utility model is used is：
A kind of rotor wing unmanned aerial vehicle with kuppe, include water conservancy diversion flight cover, water conservancy diversion flying wing, rotor blade, laterally
Water conservancy diversion flight cover is provided with the top of deflector, fuselage, bottom flap, camera and infrared lamp, the fuselage, and is being led
The left and right sides on stream flight cover top is respectively arranged with lateral deflector and water conservancy diversion flight cover afterbody is provided with water conservancy diversion flying wing,
The bottom of the fuselage is provided with bottom flap, and is connected with four rotor blades in fuselage, and the front end of the fuselage is set
There are camera and infrared lamp, and infrared lamp is arranged at around camera in isosceles triangle.
It is preferred that, the water conservancy diversion flight cover is set for arcuate stream line shape, and connects in the top left and right sides of water conservancy diversion flight cover
The lateral deflector of herringbone is connected to be provided with 120 degree of skewed frame-type water conservancy diversion flying wings with water conservancy diversion flight cover afterbody.
It is preferred that, the bottom flap is arranged on the axis of fuselage bottom in herringbone, and length is fuselage
30%.
It is preferred that, the water conservancy diversion flight cover installation settings is protruded and machine in the top of fuselage, and the front end of water conservancy diversion flight cover
Body front end 1mm.
The beneficial effects of the utility model are：
This rotor wing unmanned aerial vehicle, has installed wind-force air deflector additional, makes more to stablize and turn to flexibly during flight, and lead by wind-force
Stream device reduces windage, the use time of battery is added, while also increasing the flight endurance of unmanned plane.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is contour structures schematic diagram of the present utility model and air flow direction schematic diagram.
In figure, 1, water conservancy diversion flight cover；2nd, water conservancy diversion flying wing；3rd, rotor blade；4th, lateral deflector；5th, fuselage；6th, bottom
Flap；7th, camera；8th, infrared lamp.
Embodiment
The utility model is described in detail for 1-2 and embodiment below in conjunction with the accompanying drawings：
A kind of rotor wing unmanned aerial vehicle with kuppe, includes water conservancy diversion flight cover 1, water conservancy diversion flying wing 2, rotor blade 3, side
To deflector 4, fuselage 5, bottom flap 6, camera 7 and infrared lamp 8, the top of fuselage 5 is provided with water conservancy diversion flight cover 1,
And lateral deflector 4 is respectively arranged with the left and right sides on 1 top of water conservancy diversion flight cover and is provided with water conservancy diversion flight 1 afterbody of cover
Water conservancy diversion flying wing 2, the bottom of fuselage 5 is provided with bottom flap 6, and is connected with four rotor blades 3 in fuselage 5, fuselage 5
Front end is provided with camera 7 and infrared lamp 8, and infrared lamp 8 is arranged at around camera 7 in isosceles triangle.
Further, water conservancy diversion flight cover 1 is that arcuate stream line shape is set, and is connected in the top left and right sides of water conservancy diversion flight cover 1
The lateral deflector 4 of herringbone is connected to be provided with 120 degree of skewed frame-type water conservancy diversion flying wings 2 with water conservancy diversion flight 1 afterbody of cover.Such as
Shown in air flow direction described in Fig. 2, designed, can made with lateral deflector 4 and water conservancy diversion flying wing 2 by water conservancy diversion flight cover 1
The wind-force resistance in the front of fuselage 5 is reduced
Further, bottom flap 6 is arranged on the axis of the bottom of fuselage 5 in herringbone, and length is fuselage
30%.Air-flow is oriented to the afterbody of fuselage 5 by bottom flap 6, and bottom flap 6 collectively constitutes air-flow with water conservancy diversion flight cover 1
Flow guide system.
Further, water conservancy diversion flight 1 installation settings of cover is protruded and machine in the top of fuselage 5, and the front end of water conservancy diversion flight cover 1
The front end 1mm of body 5.Water conservancy diversion flight 1 protuberance of cover is mainly for the air-flow stress surface at the top of reduction fuselage 5.
Operation principle：Air flow guiding system is constituted with bottom flap 6 by installing water conservancy diversion flight cover 1 additional in fuselage 5, makes nothing
The man-machine stability added in flight in-flight, and by the way that air-flow is oriented into the afterbody of fuselage 5, add promotion during flight
Power.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Any modifications, equivalent substitutions and improvements made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (4)
1. a kind of rotor wing unmanned aerial vehicle with kuppe, includes water conservancy diversion flight cover (1), water conservancy diversion flying wing (2), rotor blade
(3), lateral deflector (4), fuselage (5), bottom flap (6), camera (7) and infrared lamp (8), it is characterised in that：Institute
State and water conservancy diversion flight cover (1) is provided with the top of fuselage (5), and be respectively arranged with the left and right sides on water conservancy diversion flight cover (1) top
Lateral deflector (4) and water conservancy diversion flight cover (1) afterbody is provided with water conservancy diversion flying wing (2), the bottom of the fuselage (5) is provided with
Bottom flap (6), and four rotor blades (3) are connected with fuselage (5), the front end of the fuselage (5) is provided with camera
And infrared lamp (8), and infrared lamp (8) is arranged at around camera (7) in isosceles triangle (7).
2. a kind of rotor wing unmanned aerial vehicle with kuppe according to claim 1, it is characterised in that：The water conservancy diversion flight cover
(1) set for arcuate stream line shape, and the lateral deflector of herringbone (4) is connected with the top left and right sides of water conservancy diversion flight cover (1)
It is provided with water conservancy diversion flight cover (1) afterbody in 120 degree of skewed frame-type water conservancy diversion flying wings (2).
3. a kind of rotor wing unmanned aerial vehicle with kuppe according to claim 1, it is characterised in that：The bottom flap
(6) it is arranged in herringbone on the axis of fuselage (5) bottom, and length is the 30% of fuselage.
4. a kind of rotor wing unmanned aerial vehicle with kuppe according to claim 1, it is characterised in that：The water conservancy diversion flight cover
(1) installation settings is protruded and fuselage (5) front end 1mm in the top of fuselage (5), and the front end of water conservancy diversion flight cover (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720016676.9U CN206345013U (en) | 2017-01-07 | 2017-01-07 | A kind of rotor wing unmanned aerial vehicle with kuppe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720016676.9U CN206345013U (en) | 2017-01-07 | 2017-01-07 | A kind of rotor wing unmanned aerial vehicle with kuppe |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206345013U true CN206345013U (en) | 2017-07-21 |
Family
ID=59324332
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720016676.9U Expired - Fee Related CN206345013U (en) | 2017-01-07 | 2017-01-07 | A kind of rotor wing unmanned aerial vehicle with kuppe |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206345013U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155335A (en) * | 2019-05-29 | 2019-08-23 | 东北农业大学 | A kind of plant protection drone |
| CN112357057A (en) * | 2020-10-27 | 2021-02-12 | 湖北山石智能科技有限公司 | Plant protection unmanned aerial vehicle front shroud |
| WO2023044833A1 (en) * | 2021-09-25 | 2023-03-30 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, camera mechanism and cradle head |
-
2017
- 2017-01-07 CN CN201720016676.9U patent/CN206345013U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155335A (en) * | 2019-05-29 | 2019-08-23 | 东北农业大学 | A kind of plant protection drone |
| CN112357057A (en) * | 2020-10-27 | 2021-02-12 | 湖北山石智能科技有限公司 | Plant protection unmanned aerial vehicle front shroud |
| CN112357057B (en) * | 2020-10-27 | 2022-09-09 | 湖北山石智能科技有限公司 | Plant protection unmanned aerial vehicle front shroud |
| WO2023044833A1 (en) * | 2021-09-25 | 2023-03-30 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle, camera mechanism and cradle head |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170721 Termination date: 20180107 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |