CN206394888U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN206394888U CN206394888U CN201621396664.5U CN201621396664U CN206394888U CN 206394888 U CN206394888 U CN 206394888U CN 201621396664 U CN201621396664 U CN 201621396664U CN 206394888 U CN206394888 U CN 206394888U
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- unmanned plane
- camera device
- control plate
- plate
- ultrasonic probe
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Abstract
The utility model provides a kind of unmanned plane, is related to unmanned air vehicle technique field.Unmanned plane includes flying control plate, electric tuned plate, heat sink, ultrasonic probe, light stream camera device and fan.Heat sink has the first side and second side being oppositely arranged.Fly control plate to set on the first side.Electric tuned plate, which is arranged on, flies side of the control plate away from heat sink.Fly control plate to electrically connect with electric tuned plate.Ultrasonic probe and light stream camera device are electrically connected with flying control plate.Ultrasonic probe is oppositely arranged on the second side with fan.Light stream camera device is arranged on ultrasonic probe.The center of gravity of the unmanned plane is substantially centered, and unmanned plane is vibrated small, balance and stability during flight preferably, so as to improve shooting effect of the unmanned plane during flight.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, in particular to a kind of unmanned plane.
Background technology
At present, the features such as unmanned plane has maneuverability because of it, reaction speed is fast, is widely used to civilian, scientific research very
To numerous areas such as military affairs, national defence, its image real-time Transmission, the function of high-risk areas real-time on-site detection, are to satellite remote sensing
With the strong supplement of traditional air remote sensing.
But, existing unmanned plane general structure design is larger, and the center of gravity of unmanned plane is not located at the center of unmanned plane
Position, causing unmanned plane to be vibrated in flight course, larger, balance is poor, reduces stability when unmanned plane is shot, shadow
Ring shooting quality.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, and it is intended at least partly solve existing unmanned plane center of gravity
The technical problem of big, balance and less stable is vibrated during relatively inclined and flight.
The first technical scheme that the utility model is provided：A kind of unmanned plane includes flying control plate, electric tuned plate, heat sink, super
Sonic probe, light stream camera device and fan；The heat sink has the first side and second side being oppositely arranged；It is described to fly
Control plate is arranged in the first side；The electric tuned plate is arranged on the winged side of the control plate away from the heat sink；It is described
Fly control plate to electrically connect with the electric tuned plate；The ultrasonic probe and the light stream camera device are electrically connected with the winged control plate；
The ultrasonic probe is oppositely arranged in the second side with the fan；The light stream camera device is arranged on described super
On sonic probe.
Further, the unmanned plane also includes GPS plates, and the GPS plates are fixedly connected on one end of the electric tuned plate simultaneously
Side away from the winged control plate.
Further, the unmanned plane also include center, the center be arranged on the electric tuned plate with it is described it is winged control plate it
Between, for completely cutting off the electromagnetic interference between the electric tuned plate and the winged control plate.
Further, it is provided with the winged control plate on the first circuit splicing interface, the electric tuned plate and second circuit is set
One end on splicing interface, the center offers through hole, and the first circuit splicing interface connects with the second circuit grafting
Mouth is electrically connected to each other by the through hole.
Further, the unmanned plane also includes main camera device；Close to the one of the ultrasonic probe on the center
End is convexly equipped with main camera device fixed seat, and the main camera device is fixedly mounted in the main camera device fixed seat.
Further, the main camera device fixed seat includes at least one extension；There is shrinkage pool on the extension,
For fixing the main camera device.
Further, the unmanned plane also includes toroidal shell, and the inside of the toroidal shell has the first accommodating cavity, institute
State fly control plate, it is the electric tuned plate, the heat sink, the ultrasonic probe, the light stream camera device, the fan, described
Center and the main camera device are at least partially housed in first accommodating cavity.
Further, the unmanned plane also includes horn；The toroidal shell has the second accommodating cavity, and described second houses
Chamber is respectively formed on the opposite sides face of the toroidal shell；The horn is arranged in second accommodating cavity.
Further, the unmanned plane also includes battery；The toroidal shell has the 3rd accommodating cavity, and the described 3rd houses
Chamber is opened in side of the toroidal shell away from the main camera device；The battery is arranged in the 3rd accommodating cavity.
Further, the unmanned plane also includes the first lid, the second lid and translucent cover；The toroidal shell, which is fixed, to be connected
It is connected between first lid and second lid；The toroidal shell, the translucent cover, first lid and described
Second lid formation closing space；The winged control plate, the electric tuned plate, the heat sink, the ultrasonic probe, the light stream
Camera device, the fan, the center and the main camera device are arranged in the closing space；The translucent cover
Position is corresponding with the position of the main camera device.
Compared to existing unmanned plane, the beneficial effect for the unmanned plane that the utility model is provided is：
Fly the first side that control plate is arranged on heat sink, the electric tuned plate is arranged on the winged control plate away from the heat sink
Side, the ultrasonic probe and the fan be arranged in the second side, and the light stream camera device is arranged on
It on the ultrasonic probe, can be substantially centered the center of gravity of unmanned plane, unmanned plane is vibrated small, balance during flight
Property and stability preferably, so as to improve shooting effect of the unmanned plane during flight.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme of the utility model embodiment, it will use below required in embodiment
Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also
To obtain other related accompanying drawings according to these accompanying drawings.
The decomposition texture schematic diagram for the unmanned plane that Fig. 1 provides for the utility model embodiment.
Fig. 2 be Fig. 1 in toroidal shell structural representation.
Fig. 3 be Fig. 1 in center component decomposition texture schematic diagram.
Fig. 4 be Fig. 1 in unmanned plane assembling structure schematic diagram.
Icon：100- unmanned planes；The lids of 110- first；The lids of 120- second；130- toroidal shells；140- translucent covers；
150- batteries；160- center components；The accommodating cavities of 131- first；The accommodating cavities of 132- second；The accommodating cavities of 133- the 3rd；134- the 4th holds
Put chamber；161-GPS plates；162- electricity tuned plates；163- centers；164- flies control plate；165- heat sinks；166- ultrasonic probes；167-
Light stream camera device；168- fans；The main camera devices of 169-；170- steering wheels；171- lamp plates；172-wifi plates；The main shootings of 1631-
Device fixed seat；1632- extensions；1633- shrinkage pools；1634- through holes；1641- the first circuit splicing interfaces；The electricity of 1621- second
Road splicing interface；1651- first sides；1652- second sides.
Embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Accompanying drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that retouched
The embodiment stated is a part of embodiment of the utility model, rather than whole embodiments.Generally here described in accompanying drawing and
The component of the utility model embodiment shown can be arranged and designed with a variety of configurations.
Therefore, the detailed description of embodiment of the present utility model below to providing in the accompanying drawings is not intended to limit requirement
The scope of the present utility model of protection, but it is merely representative of selected embodiment of the present utility model.Based in the utility model
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, all
Belong to the scope of the utility model protection.
It should be noted that：Similar label and letter represents similar terms in following accompanying drawing, therefore, once a certain Xiang Yi
It is defined in individual accompanying drawing, then it further need not be defined and explained in subsequent accompanying drawing.
In description of the present utility model, it is to be understood that term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation or position relationship of the instruction such as " level ", " interior ", " outer " be based on orientation shown in the drawings or position relationship, or
It is the orientation or position relationship usually put when the utility model product is used, or those skilled in the art usually understand
Orientation or position relationship, are for only for ease of description the utility model and simplify description, rather than indicate or imply signified set
Standby or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to the utility model
Limitation.
In addition, term " first ", " second ", " the 3rd " etc. are only used for distinguishing description, and it is not intended that indicating or implying
Relative importance.
In description of the present utility model, in addition it is also necessary to which explanation, unless otherwise clearly defined and limited, term " are set
Put ", " installation ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected,
Or be integrally connected；Can be mechanical connection or electrical connection；Can be joined directly together, intermediary can also be passed through
It is indirectly connected to, can is the connection of two element internals.For the ordinary skill in the art, it can be managed with concrete condition
Solve concrete meaning of the above-mentioned term in the utility model.
The decomposition texture schematic diagram for the unmanned plane 100 that Fig. 1 provides for the utility model embodiment, refers to Fig. 1.Need
Bright, in all accompanying drawings, what the reference without arrow was referred to is entity structure, what the reference with arrow was referred to
It is empty body structure, such as hole, chamber or groove.
Present embodiments provide a kind of unmanned plane 100.Unmanned plane 100 includes the first lid 110, the second lid 120, annular
Housing 130, translucent cover 140, battery 150 and center component 160.
Toroidal shell 130 is fixedly connected between the first lid 110 and the second lid 120.Form three layers of housing of upper, middle and lower
Close-connected form, not only makes unmanned plane have a good closure and structural intergrity, and makes unmanned plane compact conformation,
The Miniaturization Design of complete machine can be realized.
Translucent cover 140 is connected across on the lid 120 of toroidal shell 130 and second.Specifically, translucent cover 140 can be using card
The connected mode of button is connected with the lid 120 of toroidal shell 130 and second.
Battery 150 is removably mounted on side of the toroidal shell 130 away from translucent cover 140.It is toroidal shell 130, transparent
Cover the 140, first lid 110 and the second lid 120 formation closing space.Center component 160 is arranged in closing space.So,
The closure of unmanned plane 100 can be improved, effectively prevents dust and moisture from entering the inside of unmanned plane 100.
Fig. 2 is the structural representation of the toroidal shell 130 in Fig. 1, refers to Fig. 2.
The inside of toroidal shell 130 has the first accommodating cavity 131, the second accommodating cavity 132, the 3rd accommodating cavity 133 and the 4th
Accommodating cavity 134.
During first accommodating cavity 131 can be through hole or groove, the present embodiment, the first accommodating cavity 131 is through hole.Center component
160 are at least partially housed in the first accommodating cavity 131.Second accommodating cavity 132 is respectively formed in the opposite sides of toroidal shell 130
On face.The horn of unmanned plane 100（Not shown in figure）In the second accommodating cavity 132.
3rd accommodating cavity 133 is opened in side of the toroidal shell 130 away from main camera device 169.3rd accommodating cavity 133 is
For battery compartment.Battery 150（Refer to Fig. 4）In the 3rd accommodating cavity 133.4th accommodating cavity 134 is formed at toroidal shell
On 130 another side, the 4th accommodating cavity 134 is steering wheel storehouse, the steering wheel 170 for accommodating unmanned plane 100（Refer to figure
4）.3rd accommodating cavity 133 is oppositely arranged with the 4th accommodating cavity 134.
The second accommodating cavity 132 is opened up in the opposite sides of toroidal shell 130, for accommodating horn, meanwhile, in toroidal shell
130 other opposite sides opens up the 3rd accommodating cavity 133 and the 4th accommodating cavity 134 respectively.3rd accommodating cavity 133 and the 4th is accommodating
Chamber 134 is respectively used to accommodate battery 150 and steering wheel 170, can effectively balance the center of gravity of unmanned plane 100, improves unmanned plane 100
The stability of flight.
Fig. 3 is the decomposition texture schematic diagram of the center component 160 in Fig. 1, refers to Fig. 3.
Center component 160 includes GPS plates 161, electric tuned plate 162, center 163, winged control plate 164, heat sink 165, ultrasonic wave
Probe 166, light stream camera device 167, fan 168 and main camera device 169.
Heat sink 165 has the first side 1651 and second side 1652 being oppositely arranged.Fly control plate 164 and be arranged on first
Sideways on 1651.Electric tuned plate 162, which is arranged on, flies side of the control plate 164 away from heat sink 165.Fly control plate 164 and the electric electricity of tuned plate 162
Connection.GPS plates 161 are fixedly connected on one end of electric tuned plate 162 and away from the side for flying control plate 164.
Center 163 be arranged on electric tuned plate 162 and fly control plate 164 between, for completely cut off electric tuned plate 162 with fly control plate 164 it
Between electromagnetic interference.Fly to be provided with a first circuit splicing interface 1641, electric tuned plate 162 on control plate 164 and be provided with one
One end on second circuit splicing interface 1621, center 163 offers a through hole 1634, the first circuit splicing interface 1641 with
Second circuit splicing interface 1621 is electrically connected to each other by through hole 1634.
One end on center 163 close to ultrasonic probe 166 is convexly equipped with main camera device fixed seat 1631, main camera device
169 are fixedly mounted in main camera device fixed seat 1631.Main camera device fixed seat 1631 includes at least one extension
1632.In the present embodiment, the quantity of extension 1632 is two, and two extensions 1632 are spaced and parallel to be set.Extension 1632
It is upper that there is shrinkage pool 1633, for fixing main camera device 169.The position of main camera device 169 and the position pair of translucent cover 140
Should.
Ultrasonic probe 166 is oppositely arranged in second side 1652 with fan 168.Fan 168 is with respect to ultrasonic probe
166 away from stating light stream camera device 167.Light stream camera device 167 is arranged on ultrasonic probe 166.The He of ultrasonic probe 166
Light stream camera device 167 is electrically connected with flying control plate 164.
The heat that heat sink 165 absorbs from winged control plate 164, the effect through passing through fan 168 can accelerate dissipating for heat
Hair, improves radiating effect.All parts in center component 160 arrange that not only compact conformation, saving are empty in the manner described above
Between, and overall center of gravity is substantially centered, and unmanned plane 100 is had good stability in flight course.
Fig. 4 is the assembling structure schematic diagram of the unmanned plane 100 in Fig. 1, refers to Fig. 4.
First lid 110, the second lid 120, toroidal shell 130 and translucent cover 140 are assembled into complete closing shell
Body, miscellaneous part is arranged at enclosure interior, can be specifically applied to using fluid sealant in the thin seam of adjacent housings connection, make nothing
Man-machine 100 have good closure.
Center 163 surrounds closing space with heat sink 165, flies control plate 164 and is contained in the closing space, can not only be right
Fly control plate 164 and play effectiveness well, and can effectively be radiated to flying control plate 164.Meanwhile, electric tuned plate 162
The outside of electric tuned plate 162 is arranged on, the electromagnetic interference not only completely cut off between winged control plate 164 and electric tuned plate 162, and also structure is tight
Gather, save space.
Unmanned plane 100 also includes lamp plate 171 and wifi plates 172.Lamp plate 171 and wifi plates 172 are separately positioned on battery 150
Both sides up and down, will not only take excessive space, and be closely located to battery 150, simple in construction, wiring is convenient.
GPS plates 161 are located at the upside of center 163, and ultrasonic probe 166, light stream camera device 167 and fan 168 are located at
The downside of center 163, main camera device 169 and steering wheel 170 are located at the left side of center 163, and battery 150 is located at the right side of center 163
Side, is capable of the center of gravity of active balance unmanned plane 100, improves the stability that unmanned plane 100 flies.
The present embodiment provide unmanned plane 100 can for quadrotor, six rotorcraft, eight-rotary wing aircraft,
12 rotor crafts etc..Even, the unmanned plane 100 can be single rotor craft.In addition, the unmanned plane 100 can also be
Fixed Wing AirVehicle or fixed-wing-rotor mixing aircraft.
The unmanned plane 100 that the present embodiment is provided, first, its housing has good closure and structural intergrity, can
Effectively prevent dust and moisture from entering inside unmanned plane 100, unmanned plane 100 is applied to various complicated, severe work
Environment.Secondly, the gravity balance of unmanned plane 100, it is possible to increase the stability when flight of unmanned plane 100 is shot, improves and shoots effect
Really.Then, main camera device 169 has the packaging protection of translucent cover 140, shooting effect is not interfered with not only, and avoid master
Camera device 169 is naked to be exposed on the external, and improves protection effect.Finally, toroidal shell 130 is fixedly connected on the He of the first lid 110
Between second lid 120, three layers of close-connected form of housing of upper, middle and lower are formed, makes unmanned plane compact conformation, can realize whole
The Miniaturization Design of machine.
Preferred embodiment of the present utility model is these are only, the utility model is not limited to, for this area
Technical staff for, the utility model can have various modifications and variations.It is all it is of the present utility model spirit and principle within,
Any modification, equivalent substitution and improvements made etc., should be included within protection domain of the present utility model.
Claims (10)
1. a kind of unmanned plane, including fly control plate, electric tuned plate, heat sink, ultrasonic probe, light stream camera device, it is characterised in that
Also include fan；The heat sink has the first side and second side being oppositely arranged；The winged control plate is arranged on described the
On one side；The electric tuned plate is arranged on the winged side of the control plate away from the heat sink；The winged control plate is adjusted with the electricity
Plate is electrically connected；The ultrasonic probe and the light stream camera device are electrically connected with the winged control plate；The ultrasonic probe with
The fan is oppositely arranged in the second side；The light stream camera device is arranged on the ultrasonic probe.
2. unmanned plane according to claim 1, it is characterised in that the unmanned plane also includes GPS plates, the GPS plates are consolidated
Surely it is connected to one end of the electric tuned plate and away from the side of the winged control plate.
3. unmanned plane according to claim 1, it is characterised in that the unmanned plane also includes center, the center is set
Between the electric tuned plate and the winged control plate, for completely cutting off the electromagnetic interference between the electric tuned plate and the winged control plate.
4. unmanned plane according to claim 3, it is characterised in that be provided with the first circuit grafting on the winged control plate and connect
Mouthful, set one end on second circuit splicing interface, the center to offer through hole on the electric tuned plate, first circuit is inserted
Connection interface is electrically connected to each other with the second circuit splicing interface by the through hole.
5. unmanned plane according to claim 3, it is characterised in that the unmanned plane also includes main camera device；In described
One end on frame close to the ultrasonic probe is convexly equipped with main camera device fixed seat, and the main camera device is fixedly mounted on institute
State in main camera device fixed seat.
6. unmanned plane according to claim 5, it is characterised in that the main camera device fixed seat is stretched including at least one
Go out portion；There is shrinkage pool, for fixing the main camera device on the extension.
7. unmanned plane according to claim 5, it is characterised in that the unmanned plane also includes toroidal shell, the annular
The inside of housing has the first accommodating cavity, the winged control plate, the electric tuned plate, the heat sink, the ultrasonic probe, described
Light stream camera device, the fan, the center and the main camera device are at least partially housed in first accommodating cavity
It is interior.
8. unmanned plane according to claim 7, it is characterised in that the unmanned plane also includes horn；The toroidal shell
With the second accommodating cavity, second accommodating cavity is respectively formed on the opposite sides face of the toroidal shell；The horn peace
In second accommodating cavity.
9. unmanned plane according to claim 7, it is characterised in that the unmanned plane also includes battery；The toroidal shell
With the 3rd accommodating cavity, the 3rd accommodating cavity is opened in side of the toroidal shell away from the main camera device；It is described
Battery is arranged in the 3rd accommodating cavity.
10. unmanned plane according to claim 7, it is characterised in that the unmanned plane also includes the first lid, the second lid
And translucent cover；The toroidal shell is fixedly connected between first lid and second lid；The toroidal shell, institute
State translucent cover, first lid and second lid formation closing space；It is described it is winged control plate, the electric tuned plate, it is described dissipate
Hot plate, the ultrasonic probe, the light stream camera device, the fan, the center and the main camera device are set
In the closing space；The position of the translucent cover is corresponding with the position of the main camera device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621396664.5U CN206394888U (en) | 2016-12-19 | 2016-12-19 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621396664.5U CN206394888U (en) | 2016-12-19 | 2016-12-19 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206394888U true CN206394888U (en) | 2017-08-11 |
Family
ID=59511861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621396664.5U Active CN206394888U (en) | 2016-12-19 | 2016-12-19 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206394888U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020001273A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市道通智能航空技术有限公司 | Heat dissipation structure and unmanned aerial vehicle |
| CN112154103A (en) * | 2019-09-24 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
-
2016
- 2016-12-19 CN CN201621396664.5U patent/CN206394888U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020001273A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市道通智能航空技术有限公司 | Heat dissipation structure and unmanned aerial vehicle |
| CN112154103A (en) * | 2019-09-24 | 2020-12-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Method for measuring forest by unmanned aerial vehicle aerial photography remote sensing Effective date of registration: 20180102 Granted publication date: 20170811 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.) Pledgor: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd.|CHONGQING ZERO INTELLIGENT CONTROL TECHNOLOGY CO.,LTD. Registration number: 2017990001217 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20221008 Granted publication date: 20170811 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.) Pledgor: CHONGQING ZERO INTELLIGENT CONTROL TECHNOLOGY CO.,LTD. Registration number: 2017990001217 |