CN107444608A - A kind of new unmanned plane - Google Patents
A kind of new unmanned plane Download PDFInfo
- Publication number
- CN107444608A CN107444608A CN201710121593.0A CN201710121593A CN107444608A CN 107444608 A CN107444608 A CN 107444608A CN 201710121593 A CN201710121593 A CN 201710121593A CN 107444608 A CN107444608 A CN 107444608A
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- Prior art keywords
- horn component
- component
- unmanned plane
- horn
- lower casing
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/293—Foldable or collapsible rotors or rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/83—Electronic components structurally integrated with aircraft elements, e.g. circuit boards carrying loads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
Unmanned plane the present invention relates to new unmanned plane, especially horn component retractable unmanned plane and using multi-communication mode.The horn component of the new unmanned plane of the present invention can be packed up and deployed relative to casing, so as to facilitate the transport of unmanned plane and storage；Meanwhile new unmanned plane of the invention can use the communications such as Wifi and 4G, ensure that the stability and reliability of UAV Communication.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, it is related to new unmanned plane, more particularly to horn component retractable and adopts
With the unmanned plane of multi-communication mode.
Background technology
Unmanned vehicle, abbreviation unmanned plane, be a kind of flight instruments being in developing rapidly, its have maneuverability,
Rapid reaction, unmanned flight, operation require low advantage.Unmanned plane is by carrying multiple sensors, it is possible to achieve image is real-time
Transmission, high-risk areas detecting function, it is the strong supplement of satellite remote sensing and traditional air remote sensing.At present, the use model of unmanned plane
Enclose and have spread over military, scientific research and civilian three big field, specifically electric power, communication, meteorology, agricultural, ocean, exploration, photography,
Prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism it is very wide.
But for the unmanned plane with multiple propellers, its horn component often extends out, and occupies many spaces.
Transporting with storing process, these horn components significantly increase the space-consuming of unmanned plane, are not easy to its operation and storage.
Also, these horn components also tend to easily be broken off or damage in transportation, add the damage probability of unmanned plane.
Meanwhile in the prior art, the communication mode of unmanned plane is single, when communication mode failure or signal are weaker
When, unmanned plane is out of hand, and the problems such as easily causing to crash, the safety belt to unmanned plane carrys out very big harm
In view of the drawbacks described above of prior art, there is an urgent need to a kind of new unmanned plane.
The content of the invention
It is an object of the invention to overcome shortcoming present in prior art, there is provided a kind of new unmanned plane, to solve mesh
The problems such as existing transport of preceding unmanned plane and storage inconvenience and single communication mode.
To achieve these goals, the present invention provides following technical scheme：
A kind of horn component retractable unmanned plane, it includes the lower casing to cooperate and upper lid, it is characterized in that, under described
Internal center is provided with shell and upper lid, battery component is provided with the internal center, the bottom of the internal center is set
There is internal cell underframe in order to which the battery component is arranged in the internal center, the front end of the internal center is set
There is the Power conversion board being connected with the battery component, the both sides of the internal center are respectively arranged with the first pcb board and second
Pcb board, being provided with the lower casing can be relative to its rotation in order to horn component, left front horn component, the right side before the right side packed up
Horn component and left back horn component afterwards.
Further, wherein, ultrasonic light stream component is additionally provided with the lower casing and upper lid.
Further, wherein, it is described it is right before horn component, left front horn component, it is right after horn component and left back horn
Component is connected by a rotating shaft with the lower casing respectively.
Yet further, wherein, it is described it is right before horn component, left front horn component, it is right after horn component and left back horn
A propeller is respectively arranged with component.
Again further, wherein, trim is also covered with the upper lid.
Again yet further, wherein, the top of the internal center is provided with damping box.
Moreover, wherein, the front lower portion of the lower casing is provided with three axle heads.
In addition, the present invention also provides a kind of unmanned plane using multi-communication mode, it includes the lower casing and upper of mutual cooperation
Lid, it is characterized in that, internal center is provided with the lower casing and upper lid, battery component is provided with the internal center, it is described
The bottom of internal center is provided with internal cell underframe in order to which the battery component is arranged in the internal center, described
The front end of internal center is provided with the Power conversion board being connected with the battery component, and the both sides of the internal center are set respectively
There are the first pcb board and the second pcb board, Wifi modular assemblies are additionally provided with below the internal cell underframe, the lower casing
Rear end lower is additionally provided with 4G modular assemblies.
Further, wherein, multiple horn components are installed on the lower casing.
Further, wherein, be provided with the lower casing horn component before the right side, left front horn component, it is right after horn group
Part and left back horn component.
Yet further, wherein, it is described it is right before horn component, left front horn component, it is right after horn component and left back horn
Component is arranged on the lower casing in a manner of it can be rotated relative to the lower casing in order to pack up.
Again further, wherein, it is described it is right before horn component, left front horn component, it is right after horn component and left back machine
Arm component is connected by a rotating shaft with the lower casing respectively.
Again yet further, wherein, it is described it is right before horn component, left front horn component, it is right after horn component and left back machine
A corresponding feathering or inverse oar are respectively arranged with arm component.
Moreover, the front lower portion of the lower casing is provided with three axle heads.
Compared with existing unmanned plane, new unmanned plane of the invention has following advantageous effects：
1st, it has multiple horn components, and is both provided with propeller on each horn component, and flight performance is stronger, more may be used
Control.
2nd, its horn component can be packed up and deployed relative to fuselage, so, facilitate the transport and storage of unmanned plane, together
When, the damage probability of unmanned plane can be reduced.
3rd, it uses two kinds of communication modes of Wifi and 4G, in a kind of communication mode failure or weaker signal, can switch
To another communication mode, it can be ensured that the safety of unmanned plane.
Brief description of the drawings
Fig. 1 is the exploded view of the new unmanned plane of the present invention.
Fig. 2 is schematic diagram of the new unmanned plane of the present invention when horn component is in deployed condition.
Fig. 3 is schematic diagram of the new unmanned plane of the present invention when horn component is in collapsed state.
Embodiment
The present invention is further described with reference to the accompanying drawings and examples, and the content of embodiment is not as the guarantor to the present invention
Protect the limitation of scope.
Fig. 1 shows the exploded view of the new unmanned plane of the present invention.As shown in figure 1, the new unmanned plane of the present invention includes
The lower casing 1 and upper lid 2 of mutual cooperation.The fuselage of lower casing 1 and upper lid 2 the composition unmanned plane.In the present invention, the lower casing 1
It can be linked together between upper lid 2 by modes such as screws.
Internal center 3 is provided with the lower casing 1 and upper lid 2.Battery component 5 is provided with the internal center 3.It is described
Battery component 5 is used to need electric parts to provide electric power to each of unmanned plane.In the present invention, the battery component 5 can be
Battery.It is described in order to which the battery component 5 is arranged on that the bottom of the internal center 3 is provided with internal cell underframe 4
In internal center 3.The internal cell underframe 4 can be connected by modes such as screws with the internal center 3, in order to by institute
Battery component 5 is stated to be fixed therein.
The front end of the internal center 3 is provided with the Power conversion board 6 being connected with the battery component 4.The power supply turns
Fishplate bar 6 is used for each switching needed between electric parts for realizing the battery component 4 and unmanned plane, so as to pass through the battery
Component 4 provides electric power for each parts of unmanned plane.
The both sides of the internal center 3 are respectively arranged with the first pcb board 7 and the second pcb board 8.The He of first pcb board 7
Second pcb board 8 carries many critical functions of unmanned plane, the avoiding obstacles by supersonic wave of unmanned plane, flies control, GPS, horizontal stage electric machine, phase
Machine and light stream all be unable to do without the pcb board 8 of the first pcb board 7 and second.
In the present invention, it is preferred to the top of the internal center 3 is provided with damping box 18.Pass through the damping box 18
It can be its damping, prevent from vibrating the influence to sensor elements such as the IMU in it.
It is highly preferred that ultrasonic light stream component 10 is additionally provided with the lower casing 1 and upper lid 2.The ultrasonic light stream component 10
For realizing the fixed high and light stream positioning of ultrasonic wave for unmanned plane, stereo-picture-collaborative work is formed.
Specifically, the ultrasonic light stream component 10 includes ultrasonic sub-component and light stream sub-component.The ultrasonic sub-component utilizes
Ultrasonic wave detects the height of unmanned plane and ground, and it includes supersonic generator, ultrasonic receiver and ultrasonic converter.When
When the sound wave that sonotrode is sent out runs into ground, these sound waves will be reflected back, and at this moment just be connect using ultrasonic wave
The sound wave that device receives to be reflected back is received, then recycles sound wave converter that the sound wave reflected is changed into other letters
Number.
The light stream sub-component is used for the light stream positioning for realizing unmanned plane.Light stream is a kind of apparent fortune of brightness of image pattern
It is dynamic, the change of image is expressed, because it contains the information of target motion, therefore the position of target can be used to determine.
Moreover it is preferred that it is also covered with trim 16 on the upper lid 2.The one side of trim 16 can be nobody
Machine provides extraneous adornment, is on the other hand easy to spray some advertisements or logo or slogan etc..
In the present invention, multiple horn components are installed on the lower casing 1.It can be provided with each horn component
One propeller.So, the unmanned plane during flying ability of multiple propeller more, and control it is more convenient.
In the present invention, it is preferred to be provided with four horn components on the lower casing 1, be respectively it is right before horn component 12,
Horn component 14 and left back horn component 15 behind left front horn component 13, the right side.
In the present invention, it is described it is right before horn component 12, left front horn component 3, it is right after horn component 14 and left back horn
Component 15 is arranged on the lower casing 1 in a manner of it can be rotated relative to the lower casing 1 in order to pack up.
So, when needing to use unmanned plane, as shown in Fig. 2 horn component 12, left front horn component 3, the right side before the right side
Horn component 14 and left back horn component 15 are in deployed condition afterwards, in order to propeller rotational mounted thereto, so as to just
In the flight of unmanned plane.When needing to transport and storing unmanned plane, as shown in figure 3, horn component 12, left front horn before the right side
Horn component 14 and left back horn component 15 are in collapsed state behind component 3, the right side, consequently facilitating its transport and storage, and can drop
The impaired probability of low each horn component.
In the present invention, it is preferred to it is described it is right before horn component 12, left front horn component 13, it is right after the and of horn component 14
Left back horn component 5 is connected by a rotating shaft 17 with the lower casing 1 respectively.So, before needing to pack up or deploy the right side
Horn component 12, left front horn component 13, it is right after horn component 14 and during left back horn component 5, it is only necessary to make it is described it is right before machine
Arm component 12, left front horn component 13, it is right after horn component 14 and left back horn component 5 by the rotating shaft 17 relative to described
Lower casing 1 rotates.
It is highly preferred that the rotating shaft 17 includes self-locking mechanism.So, horn component 12, left front horn before by the right side
Component 13, it is right after horn component 14 and left back horn component 5 deploy in place or after packing up in place, to realize by the self-locking mechanism
It is described it is right before horn component 12, left front horn component 13, it is right after horn component 14 and left back horn component 5 fixation.
In addition, in the present invention, the unmanned plane employs multi-communication mode.So, in a kind of communication mode failure or
When signal is weaker, another communication mode can be switched to, it can be ensured that the safety of unmanned plane.
Specifically, Wifi modular assemblies 9 are additionally provided with below the internal cell underframe 4.The Wifi modular assemblies 9
For receiving focus number biography and figure biography data and being sent by Wifi.Pass through the Wifi modular assemblies 9, it is possible to achieve nothing
Radio communication between the man-machine terminal with control connects, and is easy to by controlling terminal to realize at the control and Image Communication of unmanned plane
Reason.In the present invention, the Wifi modular assemblies can use the wifi moulds of work of nature observation and control technology Co., Ltd of Shenzhen production
Block.
The rear end lower of the lower casing 1 is additionally provided with 4G modular assemblies 11.The 4G modular assemblies 11 are used for by 4G's
Mode realizes unmanned plane and controls the radio communication between terminal to connect, and is easy to the control by controlling terminal to realize unmanned plane.
In the present invention, for the ease of realizing the switching of two kinds of communication modes so that the control preferential Wifi of terminal leads to
Letter mode is established data with unmanned plane and is connected；When Wifi letter mode signal intensities are less than predetermined threshold value, 4G communication modes are enabled
Data are established with unmanned plane to be connected.
The present invention on unmanned plane by setting 4G modular assemblies and Wifi modular assemblies, and the selection to communication mode is excellent
First level is configured, and overcomes the problem of UAV Communication mode is single in the prior art, realizes unmanned plane and control terminal
Communication connection, can free switching communication mode, effective guarantee unmanned plane and control in different distance, varying environment
The communication stability and reliability of terminal processed.
Finally, in the present invention, it is preferred to, as shown in Figures 2 and 3, the front lower portion of the lower casing 1 is provided with three axle heads
19.By the three axles head 19, the unmanned plane can be enable easily to carry camera, be easy to take pictures and record a video.
Wherein it is preferred to binocular avoidance is realized by the binocular camera being connected with the three axles head 19.Meanwhile
The shooting of unmanned plane is also to be realized by the binocular camera.
The above embodiment of the present invention is only intended to clearly illustrate example of the present invention, and is not to the present invention
Embodiment restriction.For those of ordinary skill in the field, can also make on the basis of the above description
Other various forms of changes or variation.Here all embodiments can not be exhaustive.Every skill for belonging to the present invention
Row of the obvious changes or variations that art scheme is extended out still in protection scope of the present invention.
Claims (14)
1. a kind of horn component retractable unmanned plane, it includes the lower casing (1) to cooperate and upper lid (2), it is characterized in that, institute
State and internal center (3) is provided with lower casing (1) and upper lid (2), battery component (5) is provided with the internal center (3), it is described
The bottom of internal center (3) is provided with internal cell underframe (4) in order to which the battery component (5) is arranged in the inside
In frame (3), the front end of the internal center (3) is provided with the Power conversion board (6) being connected with the battery component (5), described
The both sides of internal center (3) are respectively arranged with the first pcb board (7) and the second pcb board (8), and being provided with the lower casing (1) can phase
For its rotation in order to horn component (12) before the right side packed up, left front horn component (13), it is right after horn component (14) and a left side
Horn component (15) afterwards.
2. horn component retractable unmanned plane according to claim 1, it is characterized in that, the lower casing (1) and upper lid (2)
Inside it is additionally provided with ultrasonic light stream component (10).
3. horn component retractable unmanned plane according to claim 2, it is characterized in that, horn component before the right side
(12), horn component (14) and left back horn component (15) pass through a rotating shaft (17) respectively behind left front horn component (13), the right side
It is connected with the lower casing (1).
4. horn component retractable unmanned plane according to claim 3, it is characterized in that, horn component before the right side
(12), it is respectively arranged with a spiral on horn component (14) and left back horn component (15) behind left front horn component (13), the right side
Oar.
5. the horn component retractable unmanned plane according to any one of claim 1-4, it is characterized in that, the upper lid
(2) trim (16) is also covered with.
6. the horn component retractable unmanned plane according to any one of claim 1-5, it is characterized in that, in the inside
The top of frame (3) is provided with damping box (18).
7. horn component retractable unmanned plane according to claim 6, it is characterized in that, under the front end of the lower casing (1)
Portion is provided with three axle heads (19).
8. a kind of unmanned plane using multi-communication mode, it includes the lower casing (1) to cooperate and upper lid (2), it is characterized in that, institute
State and internal center (3) is provided with lower casing (1) and upper lid (2), battery component (5) is provided with the internal center (3), it is described
The bottom of internal center (3) is provided with internal cell underframe (4) in order to which the battery component (5) is arranged in the inside
In frame (3), the front end of the internal center (3) is provided with the Power conversion board (6) being connected with the battery component (5), described
The both sides of internal center (3) are respectively arranged with the first pcb board (7) and the second pcb board (8), under the internal cell underframe (4)
Face is additionally provided with Wifi modular assemblies (9), and the rear end lower of the lower casing (1) is additionally provided with 4G modular assemblies (11).
9. the unmanned plane according to claim 8 using multi-communication mode, it is characterized in that, it is provided with the lower casing (1)
Multiple horn components.
10. the unmanned plane according to claim 9 using multi-communication mode, it is characterized in that, it is provided with the lower casing (1)
Horn component (12) before the right side, left front horn component (13), it is right after horn component (14) and left back horn component (15).
11. the unmanned plane according to claim 10 using multi-communication mode, it is characterized in that, horn component before the right side
(12), left front horn component (13), it is right after horn component (14) and left back horn component (15) with can be relative to the lower casing (1)
The mode for rotating to pack up is arranged on the lower casing (1).
12. the unmanned plane according to claim 11 using multi-communication mode, it is characterized in that, horn component before the right side
(12), horn component (14) and left back horn component (15) pass through a rotating shaft (17) respectively behind left front horn component (13), the right side
It is connected with the lower casing (1).
13. the unmanned plane using multi-communication mode according to any one of claim 8-12, it is characterized in that, before the right side
It is respectively arranged with behind horn component (12), left front horn component (13), the right side on horn component (14) and left back horn component (15)
One corresponding feathering or inverse oar.
14. the unmanned plane according to claim 13 using multi-communication mode, it is characterized in that, the front end of the lower casing (1)
Bottom is provided with three axle heads (19).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710121593.0A CN107444608A (en) | 2017-03-02 | 2017-03-02 | A kind of new unmanned plane |
| PCT/CN2018/077717 WO2018157833A1 (en) | 2017-03-02 | 2018-03-01 | Novel unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710121593.0A CN107444608A (en) | 2017-03-02 | 2017-03-02 | A kind of new unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107444608A true CN107444608A (en) | 2017-12-08 |
Family
ID=60486250
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710121593.0A Pending CN107444608A (en) | 2017-03-02 | 2017-03-02 | A kind of new unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN107444608A (en) |
| WO (1) | WO2018157833A1 (en) |
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| CN108263636A (en) * | 2018-01-25 | 2018-07-10 | 数字鹰电子（湖北）有限公司 | Multipurpose is tethered at unmanned plane |
| WO2018157833A1 (en) * | 2017-03-02 | 2018-09-07 | 亿航智能设备（广州）有限公司 | Novel unmanned aerial vehicle |
| CN109956043A (en) * | 2017-12-26 | 2019-07-02 | 广州亿航智能技术有限公司 | Flight instruments |
| CN114326820A (en) * | 2022-02-09 | 2022-04-12 | 西安羚控电子科技有限公司 | Unmanned aerial vehicle flight monitoring method and system |
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| CN109110101A (en) * | 2018-09-21 | 2019-01-01 | 广西云瑞科技有限公司 | A kind of novel plant protection unmanned plane |
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| CN108263636A (en) * | 2018-01-25 | 2018-07-10 | 数字鹰电子（湖北）有限公司 | Multipurpose is tethered at unmanned plane |
| CN108263636B (en) * | 2018-01-25 | 2022-04-12 | 绍兴柯斯卡信息技术有限公司 | Multipurpose mooring unmanned aerial vehicle |
| CN114326820A (en) * | 2022-02-09 | 2022-04-12 | 西安羚控电子科技有限公司 | Unmanned aerial vehicle flight monitoring method and system |
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| WO2018157833A1 (en) | 2018-09-07 |
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