CN207601629U - A kind of unmanned plane during flying device of automatic dodging fixed obstacle - Google Patents
A kind of unmanned plane during flying device of automatic dodging fixed obstacle Download PDFInfo
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- CN207601629U CN207601629U CN201721839278.3U CN201721839278U CN207601629U CN 207601629 U CN207601629 U CN 207601629U CN 201721839278 U CN201721839278 U CN 201721839278U CN 207601629 U CN207601629 U CN 207601629U
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- control module
- unmanned plane
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- infrared
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Abstract
The utility model provides a kind of unmanned plane during flying device of automatic dodging fixed obstacle, wherein, control module (l) and power plant module (2) are respectively provided with six equilateral sides, pin end is provided on the side of control module (l), female connector is provided on the side of power plant module (2), pin end is provided with positive contact, negative contact terminal and communication line contact with corresponding in female connector；Anticollision component (3) is arranged in control module (l), passes through signal wire and power cord link control module (1)；Anticollision component (3) perceives fixed obstacle by infrared ray, and passes through signal wire and the perceptual signal is passed to control module (1) and obtains the flight signal that control module (1) is transmitted；And the infrared ray direction according to flight signal control motor driving detecting head is consistent with the heading of unmanned plane.The utility model, can be to avoid unmanned plane collision obstacle by increasing anticollision component (3) on the basis of existing unmanned plane.
Description
Technical field
The utility model is related to unmanned plane field, more particularly, to a kind of unmanned plane during flying of automatic dodging fixed obstacle
Device.
Background technology
UAV abbreviation unmanned plane (Unmanned Aerial Vehicle, abbreviation UAV) is a kind of using nothing
The not manned aircraft that line electrical remote control equipment and the presetting apparatus provided for oneself manipulate.With the fast development of unmanned air vehicle technique, nothing
It is man-machine to be widely used in the industries such as city management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.
After observation scope of the unmanned plane Yi Dan disengaging controllers, often touched in flight course with barrier
It hits, is damaged so as to cause unmanned plane.
Utility model content
The purpose of this utility model be directed to presently, there are the problem of, provide a kind of automatic dodging fixed obstacle nobody
Machine aircraft, the aircraft being capable of automatic identification and avoiding barriers in flight course.
The purpose of this utility model is achieved through the following technical solutions：
The purpose of this utility model is to provide a kind of unmanned plane during flying device of automatic dodging fixed obstacle, including：
Control module, power plant module and anticollision component；
The control module and power plant module are respectively provided with six equilateral sides, and public access is provided on the side of control module
Head, is provided with female connector on the side of power plant module, pin end with it is corresponding in female connector be provided with positive contact, cathode touches
Head and communication line contact；
Anticollision component is arranged in control module, passes through signal wire and power cord link control module；Anticollision component leads to
It crosses infrared ray and perceives fixed obstacle, and pass through signal wire and the perceptual signal is passed into control module and obtains control module
The flight signal of transmission；And according to the infrared ray direction of flight signal control motor driving detecting head and the flight side of unmanned plane
To consistent.
It is highly preferred that the anticollision component includes：
Detecting head, bulb, swingle, motor and microcontroller；
The detecting head is arranged in bulb, and the bulb is fixed on swingle, and the swingle is by being arranged on control
Bearings in module, and driven and rotated by motor；The motor signal end connection microcontroller, microcontroller and nobody
Control module connection on machine, obtains the heading of unmanned plane, and pass through switch control unit and control motor by signal wire
Direction of rotation and rotation angle.
It is highly preferred that the detecting head includes：
First infrared signal lamp and the second infrared signal lamp；
The first infrared signal lamp is transversely arranged in bulb, and infrared head is leant out to bulb outside；
The second infrared signal lamp is vertically arranged in bulb, and infrared head is leant out to bulb top.
The utility model compared with prior art, has as follows it can be seen from above-mentioned the technical solution of the utility model
Technique effect：
The utility model can be collided to avoid unmanned plane and be hindered by increasing anticollision component 3 on the basis of existing unmanned plane
Hinder object.
Description of the drawings
Fig. 1 is the structure diagram of the utility model embodiment one；
Fig. 2 is the structure diagram of the anticollision component in the utility model.
In attached drawing：
Control module l, power plant module 2, anticollision component 3；First infrared signal lamp 31, the second infrared signal lamp 32, bulb
33rd, swingle 34, motor 35.
Specific embodiment
In order to which those skilled in the art is made to more fully understand the technical solution of the application, below with reference to attached drawing to this reality
It is described in further details with novel.
The orientation such as upper, lower, left, right, front and rear in present specification term be based on position relationship shown in the drawings and
It establishes.Attached drawing is different, then corresponding position relationship is also possible to change therewith, therefore cannot be interpreted as with this to protecting model
The restriction enclosed.
In the utility model, belonging to " installation ", " connected ", " connecting ", " connection ", " fixation " etc. should be interpreted broadly, example
Such as, can be fixedly connected or be detachably connected or be integrally connected or be mechanically connected, also may be used
To be electrical connection or can be in communication with each other or be directly connected to or be indirectly connected with by intermediary, Ke Yishi
The interaction relationship of unicom or two components inside two components.For the ordinary skill people of this field
For member, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.
Embodiment one
The utility model embodiment one provides a kind of unmanned plane during flying device of automatic dodging fixed obstacle, and structure is as schemed
Shown in 1 and Fig. 2, including：Including control module l, power plant module 2 and anticollision component 3.
Control module l and power plant module 2 are respectively provided with six equilateral sides, and each side is both provided with positive and negative anodes contact
And communication line contact, control module l are connected with 2 side of power plant module by matched pin and box sub, and while connecting completes
The connection of positive contact, negative contact terminal and communication line contact；Anticollision component 3 is two, is separately positioned on the upper of control module l
Lower two sides, by line connection control module 1, to receive the flight signal of the transmission of control module 1, and according to the flight signal control
The infrared ray direction of motor driving detecting head processed is consistent with the heading of unmanned plane.
The concrete structure of modules or component is as follows with function：
Control module l therein is regular hexagonal prism structure, is provided with circuit board, and IMU surveys are welded on the circuit board
It controls unit and flies control computing unit.Be both provided with pin end on each side wall of control module l, the pin end from the central position to
It is disposed with positive contact, negative contact terminal and signal wire contact outside.Above-mentioned IMU measurement and control units are used to perceive the inertia of unmanned plane
Navigation data, and by the inertial navigation data to winged control computing unit；Fly control computing unit and pass through circuit and above-mentioned pin end phase
It is logical.The also embedded suction block that is magnetic on each side wall of control module 1, to be attracted above-mentioned power plant module 2.
Power supply unit is also equipped in above-mentioned control module 1, which is all on entire unmanned plane during flying device
Module provides power.
Above-mentioned power plant module 2 is also regular hexagonal prism structure, and the side wall length of side of the power plant module 2 and above-mentioned control module 1
The side wall length of side it is consistent, can ideally to be docked with above-mentioned control module 1.Each side of above-mentioned power plant module 2 is all provided with
Female connector is equipped with, shape is corresponding with the pin end on control module l side walls so that power plant module 2 can be fast with control module l
Speed is plugged in together.Be disposed with outward from the central position on female connector female connector positive contact, female connector negative contact terminal and
Female connector signal wire contact, and position is corresponded with the contact in control module 1.
The middle part of above-mentioned power plant module 2 has circular cavity, connects girt strip on the inner wall of above-mentioned power plant module 2, the rib
Beam extends to cavity center portion, and connects rotary shaft by fixing sleeve, and blade is fixed in rotary shaft.
In order to make the connection that can be more consolidated between power plant module 2 and control module l, also set on the side wall of the power plant module 2
Multiple iron blocks are equipped with, the iron block is corresponding with the multiple magnetic suction blocks set on control module l side walls.
The structure of above-mentioned anticollision component 3 as shown in Fig. 2, including：First infrared signal lamp 31, the second infrared signal lamp 32,
Bulb 33, swingle 34, motor 35 and microcontroller.
First infrared signal lamp 31 is transversely arranged in bulb 33, and infrared head is leant out to 33 outside of bulb.
Second infrared signal lamp 32 is vertically arranged in bulb 33, and infrared head is leant out to 33 top of bulb.
Bulb 33 is used for arranging infrared signal lamp, is fixed on swingle 34, the swingle 34 is by being arranged on control mould
Bearings on block 1, and driven by motor 35 rotatable.The signal output end of the signal end connection microcontroller of motor 35,
Control module l connections on the signal input part and unmanned plane of microcontroller obtain the nothing of the transmission of control module 1 by signal wire
Man-machine heading information, and the direction of rotation by switch control unit control motor 35 and rotation angle, so that first
The heading of the infrared probe real-time tracking unmanned plane of infrared signal lamp 31.
Above-described embodiment is illustrated so that anticollision component 3 is two as an example, but the utility model is not limited to
This, which can also be one, be arranged on above control module 1 or following.
Above-mentioned control module 1 can be made of ARM chips or other chips form.
The operation principle of the utility model is as follows：
During unmanned plane during flying, control module l carries out operation according to the flight information received, and true according to operation result
Determine the location information of unmanned plane and the heading of unmanned plane.
For control module l by the heading real-time Transmission of unmanned plane to the controller of anticollision component 3, controller passes through signal
The operating of line traffic control motor drives the ball motion on swingle so that the first infrared signal lamp being transversely arranged in bulb
The heading of 31 interception unmanned planes.
When the first infrared signal lamp 31 and the second infrared signal lamp 32 are detected with barrier, then perceptual signal is sent out
To control module 1, control module 1 controls the flight of unmanned plane according to perceptual signal, to avoid unmanned plane collision obstacle.
Compared with prior art, the utility model can be kept away by increasing anticollision component 3 on the basis of existing unmanned plane
Exempt from unmanned plane collision obstacle.
Although the utility model has been described by way of example and in terms of the preferred embodiments, embodiment does not limit the utility model.Not
It is detached from the spirit and scope of the utility model, any equivalence changes done or retouching, also belongs to the guarantor of the utility model
Protect range.Therefore the scope of protection of the utility model should be using the content that claims hereof is defined as standard.
Claims (3)
1. a kind of unmanned plane during flying device of automatic dodging fixed obstacle, which is characterized in that the unmanned plane during flying device includes：
Control module (1), power plant module (2) and anticollision component (3)；
The control module (1) and power plant module (2) are respectively provided with six equilateral sides, are set on the side of control module (1)
There is pin end, female connector is provided on the side of power plant module (2), pin end is touched with the anode that is provided with corresponding in female connector
Head, negative contact terminal and communication line contact；
Anticollision component (3) is arranged in control module (1), passes through signal wire and power cord link control module (1)；Anticollision structure
Part (3) perceives fixed obstacle by infrared ray, and passes through signal wire and the perceptual signal is passed to control module (1) and is obtained
Obtain the flight signal that control module (1) is transmitted；And according to the flight signal control motor driving detecting head infrared ray direction with
The heading of unmanned plane is consistent.
2. the unmanned plane during flying device of a kind of automatic dodging fixed obstacle according to claim 1, which is characterized in that described
Anticollision component (3) includes：
Detecting head, bulb (33), swingle (34), motor (35) and microcontroller；
The detecting head is arranged in bulb (33), and the bulb (33) is fixed on swingle (34), the swingle (34)
By the bearings being arranged in control module (1), and driven and rotated by motor (35)；The signal end connection of the motor (35)
Microcontroller, microcontroller are connect with the control module (1) on unmanned plane, and the heading of unmanned plane is obtained by signal wire,
And direction of rotation and the rotation angle of motor (35) are controlled by switch control unit.
A kind of 3. unmanned plane during flying device of automatic dodging fixed obstacle according to claim 2, which is characterized in that the spy
Gauge head includes：
First infrared signal lamp (31) and the second infrared signal lamp (32)；
The first infrared signal lamp (31) is transversely arranged in bulb (33), and infrared head is leant out to bulb (33) outside；
The second infrared signal lamp (32) is vertically arranged in bulb (33), and infrared head is leant out to bulb (33) top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721839278.3U CN207601629U (en) | 2017-12-25 | 2017-12-25 | A kind of unmanned plane during flying device of automatic dodging fixed obstacle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721839278.3U CN207601629U (en) | 2017-12-25 | 2017-12-25 | A kind of unmanned plane during flying device of automatic dodging fixed obstacle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207601629U true CN207601629U (en) | 2018-07-10 |
Family
ID=62766658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721839278.3U Active CN207601629U (en) | 2017-12-25 | 2017-12-25 | A kind of unmanned plane during flying device of automatic dodging fixed obstacle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207601629U (en) |
-
2017
- 2017-12-25 CN CN201721839278.3U patent/CN207601629U/en active Active
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