CN206417193U - A kind of multi-rotor unmanned aerial vehicle aircraft - Google Patents
A kind of multi-rotor unmanned aerial vehicle aircraft Download PDFInfo
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- CN206417193U CN206417193U CN201720016657.6U CN201720016657U CN206417193U CN 206417193 U CN206417193 U CN 206417193U CN 201720016657 U CN201720016657 U CN 201720016657U CN 206417193 U CN206417193 U CN 206417193U
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- outer shroud
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Abstract
A kind of multi-rotor unmanned aerial vehicle aircraft, include floated gyroscope, rotor, inner ring angular transducer, outer shroud, outer shroud angular transducer, outer shroud torquer, inner ring torquer and inner ring, dish-shaped six wings formula aircraft be provided centrally with control storehouse, and dish-shaped six wings formula aircraft annular inboard is provided with six flying wings, eight wide-angle cameras are provided with the exterior annular wall in the control storehouse, and eight groups of infrared lamps are provided with control Cang Waicehuanxingbi.Rotor craft, with fusiform appearance, resistance during headwind flight is set to be reduced to minimum, six groups of spiraling wings are provided with simultaneously, strengthen flying power, and the floated gyroscope travel direction set by inside is converted, make aircraft that there is good flexibility, and with wide-angle imaging function, the panoramic picture with 3D effect can be fabricated to by the editor of related software.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, is related to a kind of multi-rotor unmanned aerial vehicle aircraft, more particularly to a kind of
Multi-rotor unmanned aerial vehicle aircraft.
Background technology
Being common in four wing formula aircraft, so that it may in operability, its advantage is more than shortcoming more present the market, but inverse
It is slightly inadequate during wind flight.
For this we design it is a kind of can water conservancy diversion air-flow aircraft, and with multi-functional multi-rotor unmanned aerial vehicle flight
Device.
The content of the invention
The purpose of this utility model is to provide a kind of multi-rotor unmanned aerial vehicle aircraft, it is intended to solve existing multi-rotor unmanned aerial vehicle
Problem and shortage present on aircraft.
The technical scheme that the utility model is used is：
A kind of multi-rotor unmanned aerial vehicle aircraft, includes dish-shaped six wings formula aircraft, control storehouse, flying wing, wide-angle imaging
Head, infrared lamp, arc undercarriage, floated gyroscope, rotor, inner ring angular transducer, outer shroud, outer shroud angular transducer,
Outer shroud torquer, inner ring torquer and inner ring, dish-shaped six wings formula aircraft be provided centrally with control storehouse, and dish six
Wing formula aircraft annular inboard is provided with six flying wings, the exterior annular wall in the control storehouse and is provided with eight wide-angle imagings
Head, and be provided with control Cang Waicehuanxingbi under eight groups of infrared lamps, the control storehouse of dish-shaped six wings formula aircraft
Side is provided with floated gyroscope and rotor, inner ring angular transducer, outer shroud, outer shroud angle is provided with floated gyroscope
Sensor, outer shroud torquer, inner ring torquer and inner ring, dish-shaped six wings formula aircraft bottom setting are provided with arc and risen and fallen
Frame.
It is preferred that, it is provided with Remote controller, and Remote in the control storehouse of dish-shaped six wings formula aircraft
Controller is connected by wireless communication networks with remote controller.
It is preferred that, the floated gyroscope is connected with the Remote controller in control storehouse, and dish-shaped six wings formula
Aircraft is adjusted by the inner ring angular transducer set inside floated gyroscope with outer shroud angular transducer travel direction.
The beneficial effects of the utility model are：
This dish-shaped multi-rotor unmanned aerial vehicle aircraft, with fusiform appearance, overall aircraft is flying disk type structure, structure
Simply, handsome in appearance, fusiform appearance makes resistance during headwind flight be reduced to minimum with flying disk type structure, is provided with simultaneously
Six groups of spiraling wings, strengthen flying power, and the floated gyroscope travel direction set by inside is converted, and makes flight
Utensil has a good flexibility, and with wide-angle imaging function, can be fabricated to by the editor of related software with 3D effect
Panoramic picture.
Brief description of the drawings
Fig. 1 is rotor craft surface structure schematic diagram of the present utility model；
Fig. 2 is planar structure schematic diagram of the present utility model；
Fig. 3 is floated gyroscope structural representation of the present utility model.
In figure, 1, dish-shaped six wings formula aircraft；2nd, storehouse is controlled；3rd, flying wing；4th, wide-angle camera；5th, infrared lamp；6、
Arc undercarriage；7th, floated gyroscope；8th, rotor；9th, inner ring angular transducer；10th, outer shroud；11st, outer shroud angular transducer；
12nd, outer shroud torquer；13rd, inner ring torquer；14th, inner ring.
Embodiment
The utility model is described in detail for 1-3 and embodiment below in conjunction with the accompanying drawings：
A kind of multi-rotor unmanned aerial vehicle aircraft, includes dish-shaped six wings formula aircraft 1, control storehouse 2, flying wing 3, wide-angle
Camera 4, infrared lamp 5, arc undercarriage 6, floated gyroscope 7, rotor 8, inner ring angular transducer 9, outer shroud 10, outer shroud
Angular transducer 11, outer shroud torquer 12, inner ring torquer 13 and inner ring 14, dish-shaped six wings formula aircraft 1 are provided centrally with
Storehouse 2 is controlled, and the dish-shaped annular inboard of six wings formula aircraft 1 is provided with six flying wings 3, on the exterior annular wall for controlling storehouse 2
It is provided with eight wide-angle cameras 4, and is provided with the control exterior annular wall of storehouse 2 eight groups of infrared lamps 5, dish-shaped six wings formula flies
The lower section in the control storehouse 2 of row device 1 is provided with floated gyroscope 7 and rotor 8, inner ring angle is provided with floated gyroscope 7
Spend sensor 9, outer shroud 10, outer shroud angular transducer 11, outer shroud torquer 12, inner ring torquer 13 and inner ring 14, dish-shaped six wing
The bottom of formula aircraft 1 sets and is provided with arc undercarriage 6.
Further, Remote controller, and Remote are provided with the control storehouse 2 of dish-shaped six wings formula aircraft 1
Controller is connected by wireless communication networks with remote controller.It is replaceable dress to control the Remote controller in storehouse 2
Put, bluetooth, the wireless connection such as WIFI can be carried out to dish-shaped six wings formula aircraft 1 by changing Remote controller.
Further, floated gyroscope 7 is connected with the Remote controller in control storehouse 2, and dish-shaped six wings formula
The inner ring angular transducer 9 that aircraft 1 is set by the inside of floated gyroscope 7 is adjusted with the travel direction of outer shroud angular transducer 11
Section.Floated gyroscope 7 can voluntarily adjust the level of aircraft according to route in-flight simultaneously.
Operation principle：Remote control by remote controller to being set in the control storehouse 2 of dish-shaped six wings formula aircraft 1
Device processed sends the order of flight, and dish-shaped six wings formula aircraft 1 is raised above by flying wing 3, during flight forward, floated top
The order that spiral shell instrument 7 is sent by Remote controller, turns forward and spiraling, when wide-angle camera 4 is opened, dish six
Wing formula aircraft 1 is voluntarily adjusted to rectilinear flight by floated gyroscope 7 and adjusts the level of aircraft body.
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 (3)
1. a kind of multi-rotor unmanned aerial vehicle aircraft, include dish-shaped six wings formula aircraft (1), control storehouse (2), flying wing (3), wide
Angle camera (4), infrared lamp (5), arc undercarriage (6), floated gyroscope (7), rotor (8), inner ring angular transducer
(9), outer shroud (10), outer shroud angular transducer (11), outer shroud torquer (12), inner ring torquer (13) and inner ring (14), it is special
Levy and be：Being provided centrally with of dish-shaped six wings formula aircraft (1) controls storehouse (2), and in dish-shaped six wings formula aircraft (1) ring
It is provided with the inside of shape on six flying wings (3), the exterior annular wall of the control storehouse (2) and is provided with eight wide-angle cameras (4),
And it is provided with eight groups of infrared lamps (5), the control of dish-shaped six wings formula aircraft (1) on control storehouse (2) exterior annular wall
Floated gyroscope (7) is provided with below storehouse (2) and rotor (8), inner ring angle are provided with floated gyroscope (7) and is passed
Sensor (9), outer shroud (10), outer shroud angular transducer (11), outer shroud torquer (12), inner ring torquer (13) and inner ring (14),
Dish-shaped six wings formula aircraft (1) bottom, which is set, is provided with arc undercarriage (6).
2. a kind of multi-rotor unmanned aerial vehicle aircraft according to claim 1, it is characterised in that：Dish-shaped six wings formula flight
Remote controller is provided with the control storehouse (2) of device (1), and Remote controller passes through wireless communication networks and remote control
Controller is connected.
3. a kind of multi-rotor unmanned aerial vehicle aircraft according to claim 1 or 2, it is characterised in that：The floated gyro
Instrument (7) is connected with the Remote controller in control storehouse (2), and dish-shaped six wings formula aircraft (1) passes through floated gyro
The inner ring angular transducer (9) set inside instrument (7) is adjusted with outer shroud angular transducer (11) travel direction.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720016657.6U CN206417193U (en) | 2017-01-07 | 2017-01-07 | A kind of multi-rotor unmanned aerial vehicle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720016657.6U CN206417193U (en) | 2017-01-07 | 2017-01-07 | A kind of multi-rotor unmanned aerial vehicle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206417193U true CN206417193U (en) | 2017-08-18 |
Family
ID=59574105
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720016657.6U Expired - Fee Related CN206417193U (en) | 2017-01-07 | 2017-01-07 | A kind of multi-rotor unmanned aerial vehicle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206417193U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878710A (en) * | 2019-04-04 | 2019-06-14 | 北京零偏科技有限责任公司 | A kind of dish culvert type unmanned plane |
| CN112124590A (en) * | 2020-10-15 | 2020-12-25 | 长沙中部翼天智能装备科技有限公司 | Strong crosswind interference resistant multi-rotor unmanned aerial vehicle |
| CN113110584A (en) * | 2021-04-26 | 2021-07-13 | 福州大学 | Multi-rotor aircraft cloud background network system and control method thereof |
-
2017
- 2017-01-07 CN CN201720016657.6U patent/CN206417193U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878710A (en) * | 2019-04-04 | 2019-06-14 | 北京零偏科技有限责任公司 | A kind of dish culvert type unmanned plane |
| CN112124590A (en) * | 2020-10-15 | 2020-12-25 | 长沙中部翼天智能装备科技有限公司 | Strong crosswind interference resistant multi-rotor unmanned aerial vehicle |
| CN113110584A (en) * | 2021-04-26 | 2021-07-13 | 福州大学 | Multi-rotor aircraft cloud background network system and control method thereof |
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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: 20170818 Termination date: 20180107 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |