CN208291491U - A kind of formation unmanned plane performance is anti-settling to use system - Google Patents
A kind of formation unmanned plane performance is anti-settling to use system Download PDFInfo
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- CN208291491U CN208291491U CN201820681790.8U CN201820681790U CN208291491U CN 208291491 U CN208291491 U CN 208291491U CN 201820681790 U CN201820681790 U CN 201820681790U CN 208291491 U CN208291491 U CN 208291491U
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Abstract
The utility model discloses a kind of anti-settling systems of formation unmanned plane performance, including fuselage and power device, it is fixedly connected between the fuselage and power device by support rod, the top of the fuselage inner wall is fixed with main circuit board, the side inner wall bolt of the fuselage has battery group, the other side inner wall bolt of the fuselage has air pump, the outer wall interlocking of the fuselage has positioning device, the middle part interlocking of the bottom end of the fuselage has anti-settling sensing device, and the lower section of the fuselage is fixedly connected with sink preventing apparatus by screw.This kind of utility model design is reasonable, it is easy to use, by being provided with positioning device, aerial unmanned plane performance can effectively and be accurately carried out thus, by being provided with sink preventing apparatus and anti-settling sensing device, anti-settling effect, and this kind of utility model can be effectively realized thus, position positioning and communication role can also be carried out, its loss is prevented.
Description
Technical field
The utility model relates to air vehicle technique field, in particular to a kind of formation unmanned plane performance is anti-settling to use system.
Background technique
Unmanned plane is the not manned vehicle using radio robot and the presetting apparatus provided for oneself manipulation.Nobody
Machine is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition: unmanned helicopter, unmanned fixed-wing
This several major class of machine, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol.
And currently, with unmanned plane diversification, unmanned plane is also widely used in unmanned plane performance, but in the table of unmanned plane
During drilling, need accurately to position, and the technical comparison of current unmanned plane in this respect lacks, and unmanned plane sometimes
It needs to be performed near waters, is easy to cause unmanned plane to fall in water, causes to sink, without preferable anti-settling protection, tool
There is certain limitation, and on the real-time tracking of unmanned plane and position positioning, also lacks certain technology monitoring.
Utility model content
The main purpose of the utility model is to provide a kind of anti-settling systems of formation unmanned plane performance, can effectively solve
The problems in background technique.
To achieve the above object, the technical solution that the utility model is taken are as follows:
A kind of performance of formation unmanned plane is anti-settling to use system, including fuselage and power device, the fuselage and power device it
Between be fixedly connected by support rod, the top of the fuselage inner wall is fixed with main circuit board, the side inner wall bolt of the fuselage
There is battery group, the other side inner wall bolt of the fuselage has air pump, and the outer wall interlocking of the fuselage has positioning device, the machine
The middle part interlocking of the bottom end of body has anti-settling sensing device, and the lower section of the fuselage is fixedly connected with sink preventing apparatus by screw.
Further, the power device includes luggage carrier, and the end bolt of the luggage carrier has motor, described electronic
Machine is connect by rotary shaft with propeller rotational.
Further, the motor is servo motor, there are two the propeller is arranged altogether, and is symmetricly set on loading
The both ends of frame.
Further, the battery group is formed by stacking by several graphene batteries, the power device, main circuit board,
Positioning device, sink preventing apparatus and air pump are electrically connected with battery group.
Further, shutdown frame is provided on the sink preventing apparatus, the bottom end for shutting down frame is bonded with buffer gasket, institute
The air bag that is internally provided with for shutting down frame is stated, the air bag is connected to by tracheae with air pump.
Further, the bottom end for shutting down frame is provided with annular groove, and the surface for shutting down frame is covered with antirust paint.
Further, the main circuit board is PC plate structure, is provided with communication module, GPS positioning on the main circuit board
Chip and central processing unit, the central processing unit are single-chip microcontroller.
Further, the communication module is connect with external inspecting terminal wireless, and the external inspecting terminal is plate electricity
Brain, PC or mobile phone any of them.
Further, there are four the positioning device is arranged altogether, and positioning device is embedded on four side walls of fuselage, institute
The middle part interlocking for stating positioning device has camera, and the two sides of the camera are respectively arranged with laser emitter and laser sensing
Device.
Further, the surface scarfing of the anti-settling sensing device has pressure sensor and moisture sensing device, the moisture
Sensor and pressure sensor are semiconductor transducer；The output end of the positioning device and anti-settling sensing device with center
The input terminal of processor is electrically connected.
Compared with prior art, the utility model has the following beneficial effects: this kind of utility model design is reasonable, user
Just, by being provided with positioning device, using camera, laser emitter and the laser sensor in positioning device, and in center
Under the cooperation of processor and communication module, aerial unmanned plane performance can effectively and be accurately carried out thus, it is anti-settling by being provided with
Device and anti-settling sensing device, and under the data sensing of moisture sensing device and pressure sensor in anti-settling sensing device, it can
So that air pump carries out fast aeration to air bag, anti-settling effect, and this kind of utility model can be effectively realized thus, by setting
It is equipped with communication module and GPS positioning chip, position positioning and communication role can be carried out thus, prevent its loss.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model.
Fig. 2 is the structural schematic diagram of the anti-settling sensing device of the utility model.
Fig. 3 is the structural schematic diagram of the utility model main circuit board.
Fig. 4 is the structural schematic diagram of the utility model positioning device.
Fig. 5 is the structural schematic diagram of the utility model sink preventing apparatus.
Fig. 6 is the structural schematic diagram of the utility model power device.
In figure: 1, power device；2, support rod；3, main circuit board；4, fuselage；5, air pump；6, battery group；7, anti-settling dress
It sets；8, anti-settling sensing device；9, positioning device；101, luggage carrier；102, motor；103, propeller；104, rotary shaft；301,
Central processing unit；302, communication module；303, GPS positioning chip；701, buffer gasket；702, frame is shut down；703, air bag；801,
Pressure sensor；802, moisture sensing device；901, camera；902, laser emitter；903, laser sensor.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
As shown in figures 1 to 6, a kind of formation unmanned plane performance is anti-settling uses system, including fuselage 4 and power device 1, the machine
It is fixedly connected between body 4 and power device 1 by support rod 2, the top of 4 inner wall of fuselage is fixed with main circuit board 3, described
The side inner wall bolt of fuselage 4 has battery group 6, and the other side inner wall of the fuselage 4, which bolts, air pump 5, outside the fuselage 4
Wall interlocking has positioning device 9, and the middle part interlocking of the bottom end of the fuselage 4 has anti-settling sensing device 8, and the lower section of the fuselage 4 is logical
It crosses screw and is fixedly connected with sink preventing apparatus 7, the anti-settling effect of unmanned plane may be implemented thus.
Wherein, the power device 1 includes luggage carrier 101, and the end bolt of the luggage carrier 101 has motor 102, institute
It states motor 102 to be rotatablely connected by rotary shaft 104 and propeller 103, realizes the power output and direction controlling of unmanned plane.
Wherein, the motor 102 is servo motor, and there are two the total settings of the propeller 103, and is symmetricly set on load
The both ends of rack 101.
Wherein, the battery group 6 is formed by stacking by several graphene batteries, and the power device 1, is determined main circuit board 3
Position device 9, sink preventing apparatus 7 and air pump 5 are electrically connected with battery group 6, provide power source for unmanned plane, and use the longevity
Life length, cruise duration are long.
Wherein, it is provided on the sink preventing apparatus 7 and shuts down frame 702, the bottom end for shutting down frame 702 is bonded with buffer gasket
701, the shutdown frame 702 is internally provided with air bag 703, and the air bag 703 is connected to air pump 5 by tracheae, is played anti-settling
Effect.
Wherein, the bottom end for shutting down frame 702 is provided with annular groove, and the surface for shutting down frame 702 is covered with antirust paint, just
Stablize in unmanned plane and stops and prolong its service life.
Wherein, the main circuit board 3 is PC plate structure, is provided with communication module 302, GPS positioning on the main circuit board 3
Chip 303 and central processing unit 301, the central processing unit 301 are single-chip microcontroller, realize real-time tracking and position positioning, prevent
It is lost.
Wherein, the communication module 302 is connect with external inspecting terminal wireless, and the external inspecting terminal is plate electricity
Brain, PC or mobile phone any of them, achieve the purpose that backstage wireless communication surveillance, and it is control effectively and is adjusted.
Wherein, there are four the positioning device 9 is arranged altogether, and positioning device 9 is embedded on four side walls of fuselage 4, institute
The middle part interlocking for stating positioning device 9 has camera 901, and the two sides of the camera 901 are respectively arranged with 902 He of laser emitter
Laser sensor 903 further increases the accuracy of position positioning.
Wherein, the surface scarfing of the anti-settling sensing device 8 has pressure sensor 801 and moisture sensing device 802, the water
Divide sensor 802 and pressure sensor 801 is semiconductor transducer, realizes quick detection when falling over into water.
Wherein, the output end of the positioning device 9 and anti-settling sensing device 8 is electric with the input terminal of central processing unit 301
Property connection, prevent system disorders, control effectively be adjusted to equipment.
Use system, when work, pass through setting it should be noted that the utility model is that a kind of performance of formation unmanned plane is anti-settling
There is positioning device 9, using camera 901, laser emitter 902 and the laser sensor 903 in positioning device 9, and in center
Under the cooperation of processor 301 and communication module 302, aerial unmanned plane performance can effectively and be accurately carried out thus, passes through setting
There are sink preventing apparatus 7 and anti-settling sensing device 8, and moisture sensing device 802 and pressure sensor 801 in anti-settling sensing device 8
Data sensing under, can make air pump 5 to air bag 703 carry out fast aeration, can effectively realize anti-settling effect thus, and
This kind of utility model can carry out position positioning and communication by being provided with communication module 302 and GPS positioning chip 303 thus
Effect, prevents its loss.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above.Current row
The technical staff of industry is described in above embodiments and description it should be appreciated that the present utility model is not limited to the above embodiments
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (10)
1. a kind of formation unmanned plane performance is anti-settling to use system, including fuselage (4) and power device (1), it is characterised in that: the machine
It is fixedly connected between body (4) and power device (1) by support rod (2), the top of fuselage (4) inner wall is fixed with main circuit
The side inner wall bolt of plate (3), the fuselage (4) has battery group (6), and the other side inner wall bolt of the fuselage (4) has gas
It pumps (5), the outer wall interlocking of the fuselage (4) has positioning device (9), and the middle part interlocking of the bottom end of the fuselage (4) has anti-settling sense
It surveys device (8), the lower section of the fuselage (4) is fixedly connected with sink preventing apparatus (7) by screw.
2. a kind of formation unmanned plane performance according to claim 1 is anti-settling to use system, it is characterised in that: the power device
It (1) include luggage carrier (101), the end bolt of the luggage carrier (101) has motor (102), and the motor (102) passes through
Rotary shaft (104) and propeller (103) are rotatablely connected.
3. a kind of formation unmanned plane performance according to claim 2 is anti-settling to use system, it is characterised in that: the motor
It (102) is servo motor, there are two the total settings of the propeller (103), and is symmetricly set on the both ends of luggage carrier (101).
4. a kind of formation unmanned plane performance according to claim 1 is anti-settling to use system, it is characterised in that: the battery group
(6) it is formed by stacking by several graphene batteries, the power device (1), main circuit board (3), positioning device (9), sink preventing apparatus
(7) it is electrically connected with battery group (6) with air pump (5).
5. a kind of formation unmanned plane performance according to claim 1 is anti-settling to use system, it is characterised in that: the sink preventing apparatus
(7) it is provided on and shuts down frame (702), the bottom end for shutting down frame (702) is bonded with buffer gasket (701), the shutdown frame
(702) be internally provided with air bag (703), the air bag (703) are connected to by tracheae with air pump (5).
6. a kind of formation unmanned plane performance according to claim 5 is anti-settling to use system, it is characterised in that: the shutdown frame
(702) bottom end is provided with annular groove, and the surface for shutting down frame (702) is covered with antirust paint.
7. a kind of formation unmanned plane performance according to claim 1 is anti-settling to use system, it is characterised in that: the main circuit board
(3) it is PC plate structure, is provided with communication module (302), GPS positioning chip (303) and central processing on the main circuit board (3)
Device (301), the central processing unit (301) are single-chip microcontroller.
8. a kind of formation unmanned plane performance according to claim 7 is anti-settling to use system, it is characterised in that: the communication module
(302) it is connect with external inspecting terminal wireless, the external inspecting terminal is tablet computer, PC or mobile phone any of them.
9. a kind of formation unmanned plane performance according to claim 7 is anti-settling to use system, it is characterised in that: the positioning device
(9) altogether there are four settings, and positioning device (9) is embedded on four side walls of fuselage (4), the middle part of the positioning device (9)
Interlocking has camera (901), and the two sides of the camera (901) are respectively arranged with laser emitter (902) and laser sensor
(903)。
10. a kind of formation unmanned plane performance according to claim 9 is anti-settling to use system, it is characterised in that: the anti-settling sense
The surface scarfing for surveying device (8) has pressure sensor (801) and moisture sensing device (802), the moisture sensing device (802) and pressure
Power sensor (801) is semiconductor transducer；The output end of the positioning device (9) and anti-settling sensing device (8) is in
The input terminal of central processor (301) is electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820681790.8U CN208291491U (en) | 2018-05-08 | 2018-05-08 | A kind of formation unmanned plane performance is anti-settling to use system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820681790.8U CN208291491U (en) | 2018-05-08 | 2018-05-08 | A kind of formation unmanned plane performance is anti-settling to use system |
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| Publication Number | Publication Date |
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| CN208291491U true CN208291491U (en) | 2018-12-28 |
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| CN201820681790.8U Active CN208291491U (en) | 2018-05-08 | 2018-05-08 | A kind of formation unmanned plane performance is anti-settling to use system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502197A (en) * | 2018-05-08 | 2018-09-07 | 广州市科锐达光电技术有限公司 | A kind of formation unmanned plane performance is anti-settling to use system |
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2018
- 2018-05-08 CN CN201820681790.8U patent/CN208291491U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108502197A (en) * | 2018-05-08 | 2018-09-07 | 广州市科锐达光电技术有限公司 | A kind of formation unmanned plane performance is anti-settling to use system |
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Address after: 510000 Two 113 Rooms, No. 20 Guanda Road, Huangpu District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Keruida Photoelectric Technology Co., Ltd. Address before: 510000 Dongguan Village, Xinya Street, Huadu District, Guangzhou City, Guangdong Province Patentee before: Guangzhou CREE Photoelectric Technology Co., Ltd. |