CN207346086U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN207346086U CN207346086U CN201720954870.1U CN201720954870U CN207346086U CN 207346086 U CN207346086 U CN 207346086U CN 201720954870 U CN201720954870 U CN 201720954870U CN 207346086 U CN207346086 U CN 207346086U
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- unmanned plane
- antenna
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- antenna module
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Abstract
The utility model belongs to unmanned plane technical field of structures, a kind of unmanned plane is provided, including fuselage body and the antenna module being fixedly connected in the fuselage body, the antenna module is obliquely arranged on the fuselage body, and the transmitting terminal of the antenna module is directed away from the side of the fuselage body and the direction of top surface.Such design enables unmanned plane to carry out good communication with base station in low-latitude flying.
Description
Technical field
The utility model belongs to unmanned plane technical field of structures, more particularly to a kind of unmanned plane.
Background technology
Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and the control device of itself, such as
Unmanned helicopter, unmanned fixed-wing aircraft, unmanned gyroplane etc..In recent years, with Development of UAV, because it is with motor-driven spirit
Work, rapid reaction, unmanned flight, operation require low advantage, unmanned plane be widely used in agricultural plant protection, photography of taking photo by plane,
Electric inspection process, environmental monitoring, forest fire protection and disaster inspection, effectively overcome manned aircraft and carry out aerial work not
Foot.Unmanned plane antenna is one of significant components of unmanned plane, and it is to transmit information, positioning etc. during unmanned plane during flying that it, which is acted on,
Deng.But in existing technology, unmanned plane base station generally sets up higher, when unmanned plane low-latitude flying, antenna cannot be fine
Ground and base station communication.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, it is intended to solves antenna during existing unmanned plane low-latitude flying
With the communication of base station it is bad the problem of.
The utility model so solves：A kind of unmanned plane, including fuselage body and it is fixedly connected on the fuselage sheet
Internal antenna module, the antenna module are obliquely arranged on the fuselage body, the transmitting terminal court of the antenna module
To away from the side of the fuselage body and the direction of top surface.
Further, the antenna module and the fuselage body are in first angle, and the first angle is 30 °~70 °.
Further, the antenna module is paster antenna or bar antenna.
Further, the antenna module has two, and two antenna modules are oppositely arranged.
Further, the unmanned plane further includes housing unit, and the housing unit includes two connection shells, each company
The both ends of body contact are fixedly connected on the fuselage body formed with connecting plate, the both ends of the connection shell through the connecting plate,
The connection shell phase is obliquely installed for the connecting plate, and two antenna modules are arranged on the two connection shells.
Further, the antenna module is paster antenna, and mounting groove is equipped with each connection shell inner wall, described
Paster antenna is spacing to be contained in the mounting groove, and two paster antennas are oppositely arranged.
Further, the housing unit further includes based shell, and the based shell is fixed on the top of the two connection shells,
The based shell covers two antenna modules.
Further, the based shell includes procapsid and two upper shells positioned at the procapsid both sides, the front housing
Body is fixed on the top of the two connection shells, and two upper shells cover two antenna modules.
Further, the upper shell is located at the top of the procapsid, and the top of the upper shell is equipped with opening, described
Head cover is also detachably connected with upper shell, the head cover covers the opening.
Further, the top of the upper shell is equipped with mating groove, and the opening runs through the mating groove, the head cover magnetic
Property is connected on the mating groove.
The technique effect that unmanned plane provided by the utility model has compared with the prior art is：By by antenna module
It is obliquely installed relative to fuselage body, and the antenna module is connected on fuselage body, while the transmitting terminal court of antenna module
Set to the side away from the fuselage body and the direction of top surface, so that unmanned plane can be carried out in low-latitude flying with base station
Good communication.
Brief description of the drawings
, below will be to embodiment or the prior art in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing is briefly described needed in description, it should be apparent that, drawings in the following description are only that this practicality is new
Some embodiments of type, for those of ordinary skill in the art, without having to pay creative labor, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the overall structure stereogram for the unmanned plane that the utility model embodiment provides.
Fig. 2 is the structure chart for the unmanned plane that the utility model embodiment provides, and wherein housing unit is by explosive decomposition.
Fig. 3 is unmanned plane that the utility model embodiment provides from the stereogram for looking up direction visual angle.
Fig. 4 is the structure chart that shell is connected in the unmanned plane that the utility model embodiment provides.
Fig. 5 is the structure chart of base enclosure body in the unmanned plane that the utility model embodiment provides.
Fig. 6 be the utility model embodiment provide unmanned plane in installing frame in one direction on structure chart.
Fig. 7 be in the unmanned plane that the utility model embodiment provides installing frame along the structure chart on another direction.
Wherein, wherein, fuselage 1, fuselage body 10, top plate 11, bottom plate 12, middle roll-over 13, installing frame 14, fixed frame 141,
Substrate 1411, the first extension board 1412, the second extension board 1413, mounting bracket 142, end plate 1421, the first side plate 1422, mating groove
14211st, it is logical to install the installation of straight slot 144, second for the second side plate 1423, crossed beam trunking 14231, protection department 1424, partition plate 143, first
Groove 145, rolling assembly 144, limit assembly 145, plug-assembly 146, first install straight slot 147, second and install straight slot 148；
Horn 2, housing unit 3, installation housing 31, connection shell 311, tie-beam 312, installing plate 3111, mounting groove 3112,
Based shell 32, base enclosure body 321, head cover 322, procapsid 3211, upper shell 3212, mounting hole 3213, mating groove 3214, magnet ring
3215th, ventilation duct 3210；
Undercarriage 4, Power Component 5, liquid storage container 6, battery part 7.
Embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, is further elaborated the utility model.It should be appreciated that specific embodiment described herein is only explaining
The utility model, is not used to limit the utility model.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, it can be directly another
On one element or it is connected on another element.When an element is known as " being connected to " another element, it can
To be directly to another element or be indirectly connected on another element.
It is to be appreciated that term " length ", " width ", " on ", " under ", "front", "rear", "left", "right", " vertical ",
The orientation or position relationship of the instruction such as " level ", " top ", " bottom " " interior ", " outer " are to be closed based on orientation shown in the drawings or position
System, is for only for ease of and describes the utility model and simplified description, rather than the device or element of instruction or hint meaning are necessary
With specific orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.
In addition, term " first ", " second " are only used for description purpose, and it is not intended that instruction or hint relative importance
Or the implicit quantity for indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can be expressed or
Implicitly include one or more this feature.In the description of the utility model, " multiple " are meant that two or two
More than, unless otherwise specifically defined.
Attached drawing 1 be refer to shown in Fig. 7, in the utility model embodiment, there is provided a kind of unmanned plane, including 1 He of fuselage
Along the outwardly extending multiple horns 2 of the fuselage 1, be connected on the fuselage 1 and in streamline curved surface housing unit 3, be connected to this
1 bottom of fuselage simultaneously is used to protect the undercarriage 4 that the unmanned plane rises and falls, and is also connected to the Power Component 5 of 2 end of horn, connects
Liquid storage container 6 and battery part 7 on the fuselage 1, and electricity adjust component and control system.The Power Component 5 is fixed on the machine
End of the arm 2 away from the fuselage 1, it is to provide power to the flight of unmanned plane that it, which is acted on,.The liquid storage container 6 is equipped on fuselage 1
And it is interior suitable for containing article to be sprayed or to be transported, which is fixed on fuselage 1 dynamic to be provided for Power Component 5
Power, control system are fixed on fuselage 1, for controlling the flight attitude of the aircraft.
The fuselage 1 includes fuselage body 10 at the same time, the housing unit 3 is connected on the fuselage body 10, and the housing
Antenna module is also associated with component 3, which is obliquely arranged on the fuselage body 10, and the antenna module
Transmitting terminal is directed away from the side of the fuselage body 10 and the direction of top surface, and so design can be adapted to unmanned plane low-latitude flying.
Because general base station sets up higher, received signal quality is more preferable obliquely for antenna transmitting terminal.The housing unit 3 lid is located at the machine
On the upper surface of body body 10, and the antenna module is connected between the housing unit 3 and the fuselage body 10；It can pass through
Housing unit 3 protects antenna module.The housing unit 3 includes the installation housing 31 being connected on the fuselage body 10, the peace
Dress housing 31 includes the connection shell 311 that is obliquely installed relative to the fuselage body 10, namely this connection shell 311 is inclined is connected to
On the fuselage body 10.311 inner wall of connection shell is concavely provided with the mounting groove 3112 for the spacing connection of the antenna module, and
The top plate when antenna module is connected on the mounting groove 3112 with the fuselage body 10 is in first angle, which is
30 °~70 °.So design can ensure that the signal area covering of antenna module is wider.
The unmanned plane of design above, the connection shell 311 for including being obliquely installed relative to fuselage body 10 by installation housing 31,
And the mounting groove 3112 for the spacing connection of antenna module is concavely provided with the inner wall of connection shell 311, and then can be by antenna
Component is connected in the installation housing 31, so as to avoid antenna module from being installed on, fuselage body 10 is outer and long-term exposed and then easy quilt
Damage.Top plate when antenna module is connected on mounting groove 3112 at the same time with fuselage body 10 is in 30 °~70 °, so that nothing
It is man-machine to carry out good communication with base station in low-latitude flying.
Specifically, as shown in Figure 2 and Figure 4, in the utility model embodiment, the both ends of the connection shell 311 are each formed with
Connecting plate 3111, which can be fixedly connected on the top plate 11 of the fuselage body 10, and then the two of the connection shell 311
End is fixedly connected on the top plate 11 through the connecting plate 3111, and so design can ensure the connection shell 311 in the fuselage body
The stability connected on 10.
In the utility model embodiment, which includes top plate 11, bottom plate 12 and middle roll-over 13, the top plate
11 are oppositely arranged with bottom plate 12, and middle roll-over 13 is arranged between top plate 11 and bottom plate 12 and is connected with the top plate 11 and bottom plate 12,
The top plate 11 is located at the top of fuselage body 10, which is located at the lower part of the fuselage body 10.
Specifically, in the utility model embodiment, which is paster antenna or bar antenna, the paster antenna
It is spacing to be contained in the mounting groove 3112.In order to ensure concealment effect of the antenna module in housing unit 3, by the antenna structure
It is arranged to paster antenna, and the paster antenna can be contained in the mounting groove 3112, so on the one hand conceal the antenna
Component, simultaneously because antenna module is inclined to set with the connection shell 311, thereby may be ensured that the signal covering of antenna module
Area is unaffected.
Specifically, as shown in Fig. 2, in the utility model embodiment, which is connected to the machine including two
Connection shell 311 on body body 10 and it is connected between two connection shells 311 and the company for being connected on 1 housing of fuselage
Beam 312 is connect, two connection shells 311 are oppositely arranged.At the same time the paster antenna, and two are respectively connected with two connection shells 311
It is oppositely arranged between a paster antenna.
Since connection shell 311 itself can form the signal of paster antenna shield effectiveness, but it is paired and be spaced apart
Two paster antennas can make up due to influence of connection shell 311 shield effectiveness to signal area coverage itself well.
Specifically, as shown in Figure 2 and Figure 5, in the utility model embodiment, which, which further includes, is connected to this
The based shell 32 of the top of housing 31 is installed, which includes base enclosure body 321 and the top being connected on the base enclosure body 321
Lid 322, the based shell 321 are used to cover two antenna modules, which includes procapsid 3211 and along the front housing
The ventilation duct 3210 that the both sides of body 3211 extend rearwardly to form, is also associated with and the ventilation duct 3210 on 1 housing of fuselage
Opposite electronic device.
Specifically, as shown in figure 5, in the utility model embodiment, the upper end of the procapsid 3211 is prolonged backward and upwards
Stretch formed with upper shell 3212, the quantity of the upper shell 3212 is two, and two upper shells 3212 are used to cover two
The antenna module, namely the procapsid 3211 and upper shell 3212 are integral, and the upper shell 3212 is to be located at the front housing
The top of body 3211, the head cover 322 in Fluid Surface is also associated with the upper shell 3212, is additionally provided with the upper shell 3212
For the mating groove 3214 of the head cover 322 connection.
In the utility model embodiment, the top of upper shell 3212 opens up a mating groove 3214 to accommodate head cover, coordinates
The structure matching of 3214 shape structure head cover 322 of groove is set, specifically, the shape of mating groove 3214 and the form fit of head cover 322
Set, the depth of mating groove 3214 is set with the thickness matching of head cover 322, and head cover 322 is removably connected to base enclosure body 321
At mating groove 3214, the bottom surface of the head cover 322 is downward, at the same the mounting hole 3213 week on formed with for the head cover
The mating groove 3214 that 322 inner walls abut, and 322 magnetic attracting of head cover is connected in the mating groove 3214.
In the present embodiment, magnet ring is previously provided with the mating groove 3214, metal magnetic conducting material is preset with the head cover 322
Material, and then the head cover 322 first passes through locating shaft and is located by connecting on the mounting hole 3213, so as to be pre-positioned, the then head cover
322 magnetic attractings are on the magnet ring so that the head cover 322 is connected in the mating groove 3214.
Specifically, as shown in Figure 6 and Figure 7, in the utility model embodiment, it is also associated with installing on the fuselage body 10
Frame 14, the installing frame 14 are included for being connected to the fixed frame 141 on the fuselage body 10 and for connection liquid storage babinet 6 and connecting
It is connected on the fixed frame 141 and is used for the mounting bracket 142 for connecting battery part 7.
In the present embodiment, which is outward extended with extension 14232, the end face of the extension 14232
On be also recessed with for the connecting line crossed beam trunking 14231 on spacing connection plug component 146.The connecting line is connected to the crossed beam trunking
In 14231 can and accelerated ageing exposed to avoid the connecting line, or be damaged.In addition, the upper end of the mounting bracket 142 is also upward
It is extended with protection department 1424.
In the utility model embodiment, which is connected on the fuselage body 10, which connects
In on the fixed frame 141, it is also associated between the mounting bracket 142 and fixed frame 141 every beam 143.Fixed frame 141, the mounting bracket
142 and it can be integrally formed every beam 143.Wherein, the fixed frame 141 include substrate 1411 and from the substrate 1411 it is opposite two
Roll the first extension board 1412 and the second extension board 1413 tiltedly extended.The substrate 1411 is connected with roll-over in this 13, should
The V-shaped setting in both sides of first extension board 1412 and the second extension board 1413 along substrate 1411, while first extension board
1412 and second are equipped with perforation on extension board 1413.The mounting bracket 142 includes opposite the first side plate 1422 and the second side plate
1423, and the end plate 1421 being connected on 1422 and second side plate of the first side plate, 1423 end face.First side plate 1422 is carried on the back
Side from the end plate 1421 connects the end of first extension board 1412, which deviates from the one of the end plate 1421
Side connects the end of second extension board 1413, and the upper end of 1422 and second side plate 1423 of the first side plate upwardly extends to be formed
The protection department 1424.The installing frame 14 limits mounting groove, should be connected to 1422 and second side plate of the first side plate every beam 143
The mounting groove interval is divided into the first installation straight slot 147 and the second installation straight slot 148 between 1423.The battery part 7 can be installed
In on the second installation straight slot 148, which can be installed on the first installation straight slot 147.
In the utility model embodiment, which further includes rolling assembly 144, limit assembly 145 and plug group
Part 146.The rolling assembly 144 is linked in the first installation straight slot 147, and for the liquid storage container 6 that is slidably connected.This is spacing
Component 145 is fixed in the second installation straight slot 148, and for locking the battery part 7.The plug-assembly 146 be connected to this
In two installation straight slots 148, and it is electrically connected for battery part 7 with fuselage 1.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (9)
- A kind of 1. unmanned plane, it is characterised in that：Including fuselage body and the antenna module that is fixedly connected on the fuselage body, The antenna module is obliquely arranged on the fuselage body, and the transmitting terminal of the antenna module is directed away from the fuselage sheet The side of body and the direction of top surface, the antenna module and the fuselage body be in first angle, and the first angle is 30 °~ 70°。
- 2. unmanned plane as claimed in claim 1, it is characterised in that：The antenna module is paster antenna or bar antenna.
- 3. such as claim 1-2 any one of them unmanned planes, it is characterised in that：The antenna module has two, two days Line component is oppositely arranged.
- 4. unmanned plane as claimed in claim 3, it is characterised in that：The unmanned plane further includes housing unit, the housing group Part includes two connection shells, and the both ends of each connection shell are formed with connecting plate, and the both ends of the connection shell are through the connecting plate It is fixedly connected on the fuselage body, the connection shell phase is obliquely installed for the connecting plate, and two antenna modules are set In on the two connection shells.
- 5. unmanned plane as claimed in claim 4, it is characterised in that：The antenna module is paster antenna, each connection Mounting groove is equipped with shell inner wall, the paster antenna is spacing to be contained in the mounting groove, and two paster antennas are opposite Set.
- 6. unmanned plane as claimed in claim 4, it is characterised in that：The housing unit further includes based shell, the based shell The top of the two connection shells is fixed on, the based shell covers two antenna modules.
- 7. unmanned plane as claimed in claim 6, it is characterised in that：The based shell includes procapsid and positioned at the procapsid Two upper shells of both sides, the procapsid are fixed on the top of the two connection shells, and two upper shells cover two antenna modules.
- 8. unmanned plane as claimed in claim 7, it is characterised in that：The upper shell is located at the top of the procapsid, described The top of upper shell is equipped with opening, and head cover is also detachably connected with the upper shell, and the head cover covers the opening.
- 9. unmanned plane as claimed in claim 8, it is characterised in that：The top of the upper shell is equipped with mating groove, the opening Through the mating groove, the head cover is magnetically coupled on the mating groove.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721046160.5U CN207550497U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
| CN201720954870.1U CN207346086U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720954870.1U CN207346086U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721046160.5U Division CN207550497U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207346086U true CN207346086U (en) | 2018-05-11 |
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ID=62360503
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721046160.5U Active CN207550497U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
| CN201720954870.1U Active CN207346086U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721046160.5U Active CN207550497U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN207550497U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109319104A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | A kind of unmanned plane |
-
2017
- 2017-08-01 CN CN201721046160.5U patent/CN207550497U/en active Active
- 2017-08-01 CN CN201720954870.1U patent/CN207346086U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109319104A (en) * | 2017-08-01 | 2019-02-12 | 广州极飞科技有限公司 | A kind of unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN207550497U (en) | 2018-06-29 |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 510000 Block C, 115 Gaopu Road, Tianhe District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Jifei Technology Co.,Ltd. Address before: 510000, Guangdong, Guangzhou, Gaotang Tianhe District Software Park Road, No. 1, 3A01 Patentee before: Guangzhou Xaircraft Technology Co.,Ltd. |
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| CP03 | Change of name, title or address |