CN206885325U - Unmanned vehicle device layout structure - Google Patents
Unmanned vehicle device layout structure Download PDFInfo
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- CN206885325U CN206885325U CN201720510603.5U CN201720510603U CN206885325U CN 206885325 U CN206885325 U CN 206885325U CN 201720510603 U CN201720510603 U CN 201720510603U CN 206885325 U CN206885325 U CN 206885325U
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- holding part
- fuselage
- casing
- unmanned vehicle
- vehicle device
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Abstract
The utility model proposes a kind of unmanned vehicle device layout structure, including：Fuselage inner casing, battery structure, figure pass circuit board, communications board, main control board, receiver, and locating module；The front portion of the fuselage inner casing is provided with battery compartment, and the battery compartment is interior to accommodate the battery structure, sets the figure to pass circuit board and communications board outside the left and right sides wall of the battery compartment respectively；The figure passes circuit board and the respective side backwards to battery compartment of communications board is provided with barricade；The rear portion of the fuselage inner casing is provided with the first holding part, the second holding part and the 3rd holding part, first holding part is to the accommodating locating module, second holding part is to the accommodating receiver, to house the main control board, first holding part, the second holding part and the 3rd holding part stagger certain distance 3rd holding part on the above-below direction and fore-and-aft direction of fuselage.Reduce interfering for fuselage interior.
Description
Technical field
It the utility model is related to unmanned vehicle technical field, more particularly to a kind of unmanned vehicle device layout knot
Structure.
Background technology
Unmanned vehicle is the not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself.
Unmanned vehicle needs receiver to receive telecommand at work, it is necessary to carry out flight control, take photo by plane, navigate,
Governor circuit is flown to adjust course, posture to be controlled, and control is taken photo by plane, airborne figure transmission module, radio communication mold
The image transmitting of shooting is returned remote terminal by block, generally also sets up GPS (Globle Positioning System, global satellite
Alignment system) module carries out location navigation, also need to battery certainly to be powered, etc..
The layout of each device on existing unmanned vehicle easily produces mutual cross jamming, antenna, GPS
Deng transmitting-receiving also suffer from fuselage interior circuit influence, signal is interfered and can produce noise, causes transmitting-receiving mistake or loses
Leakage.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of unmanned vehicle device layout structure, reduces fuselage
Internal interferes.
To solve the above problems, the utility model proposes a kind of unmanned vehicle device layout structure, including：In fuselage
Shell, battery structure, figure pass circuit board, communications board, main control board, receiver, and locating module；In the fuselage
The front portion of shell is provided with battery compartment, accommodating the battery structure, the left and right sides wall of the battery compartment in the battery compartment
It is outer to set the figure to pass circuit board and communications board respectively；The figure passes the respective of circuit board and communications board
Barricade is provided with backwards to the side of battery compartment；The rear portion of the fuselage inner casing be provided with the first holding part, the second holding part and
3rd holding part, first holding part is to house the locating module, and second holding part is to the accommodating reception
Device, the 3rd holding part is to the accommodating main control board, first holding part, the second holding part and the 3rd holding part
Stagger certain distance on the above-below direction and fore-and-aft direction of fuselage.
According to one embodiment of the present utility model, the first casing and the second machine that the fuselage inner casing includes left and right and divided
Shell；First holding part, the second holding part and the 3rd equal part of holding part are formed at the inner side of first casing, another
Part forms the inner side of the second casing；First casing and the second casing docking is fixed, and first holding part, second house
Portion and the respective part of the 3rd holding part and another part close up and by the locating module, receiver and governor circuit
Plate is fixed.
According to one embodiment of the present utility model, first holding part is accommodating cavity, and the locating module is built in
In box body, the box body is fixed in the accommodating cavity.
According to one embodiment of the present utility model, rubber ring is provided with least roof or bottom wall of the accommodating cavity,
Vibration damping for the box body.
According to one embodiment of the present utility model, without metal structure in surrounding's certain distance of the locating module.
According to one embodiment of the present utility model, second holding part and the 3rd holding part include chassis and both sides
Side wall, at least side of the both sides side wall are provided with chute；The receiver or main control board slip into both sides by chute
Between side wall, and pass through the chassis supports.
According to one embodiment of the present utility model, the battery compartment is formed at first casing or the second casing.
According to one embodiment of the present utility model, first holding part is located at the top of the fuselage inner casing.
According to one embodiment of the present utility model, in addition to two omnidirectional antennas；It is located at battery on the fuselage inner casing
Bottom antenna holding part is provided with below storehouse, top antenna holding part, institute are provided with the rear portion tip position of the fuselage inner casing
State and house described two omnidirectional antennas in bottom antenna holding part and top antenna holding part respectively.
According to one embodiment of the present utility model, the radiation of the omnidirectional antenna in the top antenna holding part is most
Strong position is towards body upper, and the most strong position of radiation of the omnidirectional antenna in the bottom antenna holding part is towards under fuselage
Side.
According to one embodiment of the present utility model, in addition to fuselage cover, it is coated and fixed on the outside of the fuselage inner casing.
After adopting the above technical scheme, the utility model has the advantages that compared with prior art：
Battery structure, figure biography circuit board and communications board are the larger interference sources of fuselage interior, and three is preposition
In fore-body, and both sides set barricade, shielding action is together played to three, will disturb less main control board,
Receiver is placed in fuselage afterbody with locating module, and dislocation is arranged on upper and lower, fore-and-aft direction by several persons, ensure it is certain away from
From significantly reducing the interference of fuselage interior.
Brief description of the drawings
Fig. 1 is the structural representation of the part unmanned vehicle device layout structure of the embodiment of the utility model one；
Fig. 2 is another viewing angle constructions schematic diagram of Fig. 1 part unmanned vehicle device layout structure；
Fig. 3 is the structural representation of the unmanned vehicle device layout structure of the embodiment of the utility model one.
Description of symbols in figure：
1- fuselage inner casings, 11- battery compartments, 2- battery structures, 3- figures pass circuit board, 4- communications boards, 5- master controls
Circuit board, 6- receivers, 7- locating modules, 81,82- omnidirectional antennas, 9- fuselage covers.
Embodiment
To enable above-mentioned purpose of the present utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings to this
The embodiment of utility model is described in detail.
Many details are elaborated in the following description in order to fully understand the utility model.But this practicality is new
Type can be to be much different from other manner described here to implement, and those skilled in the art can be new without prejudice to this practicality
Similar popularization is done in the case of type intension, therefore the utility model is not limited by following public specific implementation.
Referring to Fig. 1 and Fig. 2, in one embodiment, unmanned vehicle device layout structure includes：Fuselage inner casing 1, battery
Structure 2, figure pass circuit board 3, communications board 4, main control board 5, receiver 6, and locating module 7.Certainly, nobody flies
Row device device layout structure can also include other first device parts, such as the camera lens for taking photo by plane, lens control part, motor
Deng.
Can be existing annexation in terms of electric connection, between each device, the utility model does not simultaneously lie in electricity
Improvement in terms of property connection, and it is the layout of each device.Battery structure 2 can be used for needing the device of electricity consumption to enter other
Row power supply.Figure, which passes circuit board 3, can receive image and the transmission of lens shooting, and communications board 4 can conduct electricity figure road
For the image that plate 3 transmits by scheming to pass antenna transmission to outside, outside can be the mobile terminals such as mobile phone or remote control
Device.Receiver 6 is used for receiving remote signal and being transmitted to main control board 5 or other circuit boards, such as control electricity of taking photo by plane
Road.Locating module 7 is used for realizing positioning, such as can be with GPS module etc..Connection between each device can pass through lead cabling
Connection is realized.
The front portion of fuselage inner casing 1 is provided with battery compartment 11, and battery compartment 11 is interior to accommodate battery structure 2, battery compartment 11
Figure is set to pass circuit board 3 and communications board 4 respectively outside the wall of the left and right sides.Figure passes circuit board 3 and communications board 4
Be each provided with barricade (not shown) backwards to the side of battery compartment 11.Barricade can be the metals such as aluminium, galvanized iron
Material, you can play shielding action, may also function as thermolysis.Figure is passed circuit board 3 and communications board 4 and can set with gap
Heat emission hole can also accordingly be opened up on the both sides of battery compartment 11, the both sides of battery compartment 11 by putting, so as to radiation air caused by wind regime
Stream can be entered in battery compartment 11 by gap, heat emission hole to radiate.
The rear portion of fuselage inner casing 1 is provided with the first holding part, the second holding part and the 3rd holding part (unmarked in figure, position
In the position for corresponding respectively to locating module 7, receiver 6, main control board 5), the first holding part to house locating module 7,
Second holding part is to house receiver 6, and the 3rd holding part is to accommodating main control board 5, the first holding part, the second holding part
Stagger on the above-below direction and fore-and-aft direction of fuselage certain distance with the 3rd holding part.First holding part, the second holding part
It is unlimited with the concrete form of the 3rd holding part, can be channel-shaped, cavity-like, plate shape, shelf-like etc., as long as can realize accommodating
In relevant position.First holding part, the second holding part and the 3rd holding part are on the above-below direction and fore-and-aft direction of fuselage
Stagger certain distance, reduces interference while may be such that more compact structure, the distance to stagger between each other can be according to reality
Depending on needing, reduce the space of required layout in the case where ensureing that interference is relatively low.
In the utility model embodiment, left and right directions, fore-and-aft direction, above-below direction are to be used as ginseng using unmanned vehicle
Examine thing to be defined, from fuselage angle itself, the line direction between head and tail relative position is front and back
To the line direction between the relative position of fuselage both sides is left and right directions, between fuselage roof and fuselage bottom relative position
Line direction is above-below direction.
Battery structure 2, figure biography circuit board 3 and communications board 4 are the larger interference sources of fuselage interior, before three
Put in fore-body, and barricade is set in both sides, shielding action is together played to three, less main control board will be disturbed
5th, receiver 6 is placed in fuselage afterbody with locating module 7, and by several persons, dislocation is arranged on upper and lower, fore-and-aft direction, is ensured certain
Distance, significantly reduce the interference of fuselage interior.
It is not provided with producing it is appreciated that battery structure 2, figure pass to be contemplated to be near circuit board 3 and communications board 4
First device part of raw larger interference, if but there is provided corresponding interference part, the utility model is nor affected on certainly to be to drop
The purpose interfered between these low devices.
In one embodiment, the first casing and the second casing that fuselage inner casing 1 includes left and right and divided.First holding part,
Second holding part and the 3rd equal part of holding part are formed at the inner side of the first casing, and another part is formed at the interior of the second casing
Side.First casing and the second casing docking fix, the first holding part, the second holding part and the 3rd holding part it is respective a part and
Another part closes up and fixes locating module 7, receiver 6 and main control board 5.Pass through the first casing and pair of the second casing
Connect fixation, it is possible to achieve the fixation of locating module 7, receiver 6 and main control board 5, many stationary positioned modules can be saved
7th, the parts of receiver 6 and main control board 5, assembling are more simple.
Preferably, the first holding part is accommodating cavity, locating module 7 is built in box body, and box body is fixed in accommodating cavity.Change
Yan Zhi, two of the first holding part on the first casing and the second casing be partially closed after form an accommodating cavity, closing up
The box body with locating module 7 is inserted in it before, after closing up, it is only necessary to the first casing and the second casing are fixed up,
The fixation of locating module 7 can be realized.Box body can protect locating module 7, it is also possible that fixing-stable.
More preferably, rubber ring is provided with least roof or bottom wall of accommodating cavity, the vibration damping for box body.Locating module 7
Vibration can cause the unstable and corresponding position error of signal, setting can make that locating module is more stable, positioning after rubber ring
It is more accurate.
Preferably, without metal structure in surrounding's certain distance of locating module 7.Metal structure can produce certain interference,
Because locating module 7 has been fixed via the accommodating cavity closed up, thus fixture can not needed to fix, avoid metal structure
Interference, certainly, locating module 7 can be also fixed in accommodating cavity by the spiro connecting piece of other materials to be spirally connected again, e.g. moulded
Expect the spiro connecting piece of material.
Second holding part and the 3rd holding part include chassis and both sides side wall, and at least side of both sides side wall, which is provided with, to be slided
Groove.Between receiver 6 slips into both sides side wall by the chute of the second holding part, and pass through the chassis supports of the second holding part.It is main
Between control circuit board 5 slips into both sides side wall by the chute of the 3rd holding part, and pass through the chassis supports of the 3rd holding part.Receive
Device 6 or main control board 5 can tentatively be fixed on fuselage inner casing 1 due to being between insertion chute enters both sides side wall
On, it is unlikely to easily to drop in assembling, also allows for positioning, the support force of chute can be reduced by chassis supports, avoid sliding
Damaged after groove load-bearing.
Battery compartment 11 is formed at the first casing or the second casing.Due to battery structure 2 be typically arranged to removably, with
Convenient charging, thus battery compartment 11 can be integrally formed on the first casing or is integrally formed on the second casing, just
In die sinking processing and manufacturing etc..
Preferably, the first holding part is located at the top of fuselage inner casing 1, in other words, locating module 7 is arranged on fuselage inner casing 1
Top, be more beneficial for the receiving and transmitting signal of locating module 7.
In one embodiment, unmanned vehicle device layout structure also includes two omnidirectional antennas, respectively omnidirectional antennas
Line 81 and omnidirectional antenna 82.Bottom antenna holding part is provided with the lower section of battery compartment 11 on fuselage inner casing 1, fuselage inner casing 1
Top antenna holding part is provided with the tip position of rear portion, omnidirectional is housed respectively in bottom antenna holding part and top antenna holding part
Antenna 81 and omnidirectional antenna 82.Omnidirectional antenna 81 and omnidirectional antenna 82 can be the single-frequency that working frequency range is 5.8GHz, 2.4GHz
Antenna, or collection 5.8GHz, 2.4GHz dual-band antenna, but not limited to this.Omnidirectional antenna 81 and omnidirectional antenna 82 can be made
Antenna is passed for the figure in previous embodiment.
Two omnidirectional antennas are set in fuselage, and realization is double to receive double hairs, and signal transmitting and receiving is with better function；By an omnidirectional antenna 81
It is arranged on the rear portion top of fuselage inner casing 1, another omnidirectional antenna 82 is arranged on to the front base of fuselage inner casing 1 so that two
The distance between antenna is as large as possible, almost positioned at the cornerwise corner of fuselage so that reduces interference between the two；Bottom
Omnidirectional antenna 82 is arranged on the lower section of battery compartment 11, can reduce the radiation interference of battery compartment 11 and its both sides circuit board.
Preferably, the most strong position of the radiation of the omnidirectional antenna 81 in top antenna holding part is towards body upper, position
In the most strong position of the radiation of the omnidirectional antenna 82 in bottom antenna holding part towards below fuselage.
The most strong position of the radiation of the omnidirectional antenna 81 at top, the omnidirectional antenna 82 of bottom is respectively facing it is setting up and down, can
To reduce the obstruction that fuselage is received and dispatched to aerial signal as far as possible, radiation scope can be mutually made up so that general direction is more preferable, covers
Lid scope is wider, strengthens signal transmitting and receiving.
Referring to Fig. 3, in one embodiment, unmanned vehicle device layout structure also includes fuselage cover 9, is coated and fixed
In the outside of fuselage inner casing 1.By body shell set include fuselage inner casing 1 and fuselage cover 9, can by each first device part, consolidate
Determine part etc. to be arranged on fuselage inner casing 1, and real shell of the fuselage cover 9 as fuselage, strengthen appearance consistency, it is more attractive.
Fuselage cover 9 can equally be divided into left and right two halves, and half can be spirally connected by inner side and is fixed on the first casing, and second half can
To be connected in the half.
Although the utility model is disclosed as above with preferred embodiment, it is not for limiting claim, Ren Heben
Art personnel are not being departed from spirit and scope of the present utility model, can make possible variation and modification, therefore
The scope of protection of the utility model should be defined by the scope that the utility model claims are defined.
Claims (11)
- A kind of 1. unmanned vehicle device layout structure, it is characterised in that including：Fuselage inner casing, battery structure, figure conduct electricity road Plate, communications board, main control board, receiver, and locating module；The front portion of the fuselage inner casing is provided with battery Storehouse, the battery compartment is interior to accommodate the battery structure, sets the figure to pass outside the left and right sides wall of the battery compartment respectively Circuit board and communications board；The figure pass circuit board and communications board each on the side of battery compartment Provided with barricade；The rear portion of the fuselage inner casing is provided with the first holding part, the second holding part and the 3rd holding part, and described first Holding part is to house the locating module, and second holding part to house the receiver, use by the 3rd holding part With house the main control board, first holding part, the second holding part and the 3rd holding part fuselage above-below direction and Stagger certain distance on fore-and-aft direction.
- 2. unmanned vehicle device layout structure as claimed in claim 1, it is characterised in that the fuselage inner casing includes left and right And the first casing and the second casing divided；First holding part, the second holding part and the 3rd equal part of holding part are formed at The inner side of first casing, another part form the inner side of the second casing；First casing and the second casing docking is fixed, First holding part, the second holding part and the 3rd holding part it is respective it is described a part and another part close up and will be described fixed Position module, receiver and main control board are fixed.
- 3. unmanned vehicle device layout structure as claimed in claim 2, it is characterised in that first holding part is accommodating Chamber, the locating module are built in box body, and the box body is fixed in the accommodating cavity.
- 4. unmanned vehicle device layout structure as claimed in claim 3, it is characterised in that at least roof of the accommodating cavity Or rubber ring is provided with bottom wall, the vibration damping for the box body.
- 5. unmanned vehicle device layout structure as claimed in claim 3, it is characterised in that one around the locating module Without metal structure in set a distance.
- 6. unmanned vehicle device layout structure as claimed in claim 2, it is characterised in that second holding part and the 3rd Holding part includes chassis and both sides side wall, and at least side of the both sides side wall is provided with chute；The receiver or master control Between circuit board slips into both sides side wall by chute, and pass through the chassis supports.
- 7. unmanned vehicle device layout structure as claimed in claim 2, it is characterised in that the battery compartment is formed at described First casing or the second casing.
- 8. the unmanned vehicle device layout structure as described in any one in claim 1-7, it is characterised in that described first Holding part is located at the top of the fuselage inner casing.
- 9. the unmanned vehicle device layout structure as described in any one in claim 1-7, it is characterised in that also including two Individual omnidirectional antenna；It is located on the fuselage inner casing at battery compartment lower section and is provided with bottom antenna holding part, after the fuselage inner casing Top antenna holding part is provided with portion's tip position, institute is housed respectively in the bottom antenna holding part and top antenna holding part State two omnidirectional antennas.
- 10. unmanned vehicle device layout structure as claimed in claim 9, it is characterised in that hold positioned at the top antenna The most strong position of radiation of the omnidirectional antenna in portion is put towards body upper, the omnidirectional antenna in the bottom antenna holding part The most strong position of radiation towards below fuselage.
- 11. the unmanned vehicle device layout structure as described in any one in claim 1-7, it is characterised in that also include Fuselage cover, it is coated and fixed on the outside of the fuselage inner casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720510603.5U CN206885325U (en) | 2017-05-09 | 2017-05-09 | Unmanned vehicle device layout structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720510603.5U CN206885325U (en) | 2017-05-09 | 2017-05-09 | Unmanned vehicle device layout structure |
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| Publication Number | Publication Date |
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| CN206885325U true CN206885325U (en) | 2018-01-16 |
Family
ID=61340690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
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| CN201720510603.5U Active CN206885325U (en) | 2017-05-09 | 2017-05-09 | Unmanned vehicle device layout structure |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019142676A1 (en) * | 2018-01-22 | 2019-07-25 | 京セラ株式会社 | Antenna, bicycle, display device, and unmanned aerial vehicle |
| WO2021120659A1 (en) * | 2019-12-19 | 2021-06-24 | 广州极飞科技有限公司 | Self-driving control apparatus and driverless apparatus provided with same |
| RU2777941C1 (en) * | 2019-12-19 | 2022-08-12 | Гуанчжоу Иксэркрафт Текнолоджи Ко., Лтд. | Device for controlling autonomous driving and a device for unmanned driving associated with it |
| US11970242B2 (en) | 2019-07-24 | 2024-04-30 | Kyocera Corporation | Brake lever and transmission |
-
2017
- 2017-05-09 CN CN201720510603.5U patent/CN206885325U/en active Active
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019142676A1 (en) * | 2018-01-22 | 2019-07-25 | 京セラ株式会社 | Antenna, bicycle, display device, and unmanned aerial vehicle |
| JPWO2019142676A1 (en) * | 2018-01-22 | 2021-01-14 | 京セラ株式会社 | Antennas, bicycles, displays, and unmanned aerial vehicles |
| JP7041690B2 (en) | 2018-01-22 | 2022-03-24 | 京セラ株式会社 | Antennas, bicycles, display equipment, and unmanned aerial vehicles |
| US11764479B2 (en) | 2018-01-22 | 2023-09-19 | Kyocera Corporation | Antenna, bicycle, display apparatus, and unmanned aircraft |
| US11970242B2 (en) | 2019-07-24 | 2024-04-30 | Kyocera Corporation | Brake lever and transmission |
| WO2021120659A1 (en) * | 2019-12-19 | 2021-06-24 | 广州极飞科技有限公司 | Self-driving control apparatus and driverless apparatus provided with same |
| JP2022532713A (en) * | 2019-12-19 | 2022-07-19 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| RU2777941C1 (en) * | 2019-12-19 | 2022-08-12 | Гуанчжоу Иксэркрафт Текнолоджи Ко., Лтд. | Device for controlling autonomous driving and a device for unmanned driving associated with it |
| JP7269375B2 (en) | 2019-12-19 | 2023-05-08 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| US12009569B2 (en) | 2019-12-19 | 2024-06-11 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
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