CN207550497U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN207550497U CN207550497U CN201721046160.5U CN201721046160U CN207550497U CN 207550497 U CN207550497 U CN 207550497U CN 201721046160 U CN201721046160 U CN 201721046160U CN 207550497 U CN207550497 U CN 207550497U
- Authority
- CN
- China
- Prior art keywords
- shell
- unmanned plane
- connection
- antenna
- antenna module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Details Of Aerials (AREA)
Abstract
The utility model belongs to unmanned plane technical field of structures, a kind of unmanned plane is provided and includes fuselage body and antenna module, housing unit is connected on the fuselage body, the housing unit includes based shell and is fixedly connected below the based shell and is used to support the connection shell of the based shell, the connection shell is fixedly connected on the fuselage body, and the antenna module is fixedly connected on the connection shell；Design can be solved the problems, such as in existing unmanned plane since antenna transmitting terminal connection structure complexity causes whole interior space layout unreasonable in this way.
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 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.One of the significant components of unmanned plane antenna for unmanned plane, effect are to transmit information, positioning etc. during unmanned plane during flying
Deng.But antenna transmitting terminal connection structure is complicated in existing technology, and existing unmanned plane internal space layout is unreasonable.
Utility model content
The purpose of this utility model is to provide a kind of unmanned planes, it is intended to solve in existing unmanned plane since antenna emits
The problem of end connection structure complexity causes whole interior space layout unreasonable.
The utility model solves in this way：A kind of unmanned plane, including fuselage body and antenna module, the fuselage body
On be connected with housing unit, the housing unit includes based shell and is fixedly connected below the based shell and is used to support institute
The connection shell of based shell is stated, the connection shell is fixedly connected on the fuselage body, and the antenna module is fixedly connected on institute
It states on connection shell.
Further, the antenna module is fixedly connected on the inside of the connection shell.
Further, it is obliquely installed between the antenna module and the fuselage body.
Further, for the antenna module with the fuselage body in first angle, the first angle is 30 °~70 °.
Further, the antenna module is paster antenna or bar antenna.
Further, the quantity of the connection shell is two, and two connection shells are oppositely arranged, each connection
The both ends of shell are formed with connecting plate, and the both ends of the connection shell are fixedly connected on through the connecting plate on the fuselage body, institute
It states connection shell phase to be obliquely installed the connecting plate, there are one the antenna module, two institutes for connection on each connection shell
Antenna module is stated to be oppositely arranged.
Further, the antenna module is paster antenna, and mounting groove is equipped on each connection shell inner wall, described
Paster antenna limiting is accommodated 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 on upper shell, the head cover covers the opening.
Further, the top of the upper shell is equipped with mating groove, and the opening is 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 on housing unit
The setting of shell is connected, while antenna module is connected in the connection shell, and then completes the support connection of antenna module.Together
When, which is connected on fuselage body, and the connection shell can also support the based shell, and then interior in a limited space
The support of based shell and the installation of antenna module are completed simultaneously, so that the internal structure of unmanned plane is more compact and closes
Reason.
Description of the drawings
It, 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, the accompanying drawings in the following description is 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 ontology 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, cooperation
Slot 14211, the second side plate 1423, crossed beam trunking 14231, protection department 1424, partition board 143, first installation straight slot 144, second install
Straight slot 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 ontology 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.
Specific 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, the present invention is further described in detail.It should be appreciated that specific embodiment described herein is only used to explain
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 set to " 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 instructions 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 description the utility model and simplifies description rather than instruction or imply that signified device or element 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.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include one or more this feature." multiple " are meant that two or two in the description of the present invention,
More than, unless otherwise specifically defined.
Attached drawing 1 is please referred to shown in Fig. 7, in the utility model embodiment, a kind of unmanned plane is provided, 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 and electricity on the fuselage 1 adjust component and control system.The Power Component 5 is fixed on the machine
End of the arm 2 far from the fuselage 1, effect are to provide power to the flight of unmanned plane.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 unmanned plane further includes fuselage body 10 and the antenna module being fixedly connected on the fuselage body 10, the fuselage sheet
Housing unit 3 is connected on body, which includes based shell 32 and be connected to below the based shell and be used to support the base
The connection shell 311 of housing 32, the connection shell 311 are connected on the fuselage body 10, which is fixedly connected on the connection
On shell 311, such as the inside of the connection shell 311.
The unmanned plane designed in this way by connecting the setting of shell 311 on housing unit 3, while antenna module is connected to
In the connection shell 311, and then complete the support connection of antenna module.Meanwhile the connection shell 311 is connected to fuselage body 10
On, and the connection shell 311 can also support the based shell 32, and then interior in a limited space while complete based shell 32
Support and the installation of antenna module, so that the internal structure of unmanned plane is more compact and reasonable.
In the present embodiment simultaneously, which is obliquely set on the fuselage body 10, and the antenna module
Transmitting terminal be directed away from the side of the fuselage body 10 and the direction of top surface, in this way design unmanned plane low latitude can be suitble to fly
Row.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
On the upper surface of the fuselage body 10, and the antenna module is connected between the housing unit 3 and the fuselage body 10；It can be with
Antenna module is protected by housing unit 3.The housing unit 3 includes the installation housing 31 being connected on the fuselage body 10,
The connection shell 311 is inclined to be connected on the fuselage body 10.311 inner wall of connection shell is concavely provided with to be consolidated for the antenna module
Surely the mounting groove 3112 connected, and when the antenna module is connected on the mounting groove 3112 with the top plate of the fuselage body 10
In first angle, which is 30 °~70 °.Design can ensure that the signal area covering of antenna module is wider in this way.
In the present embodiment, the connection shell 311 being obliquely installed relative to fuselage body 10 is included by installation housing 31, and
And the mounting groove 3112 being fixedly connected for antenna module is concavely provided in the inner wall for connecting shell 311, and then can be by antenna sets
Part is connected in the installation housing 31, so as to avoid antenna module outer and long-term exposed mounted on fuselage body 10 and then easily be damaged
It is bad.With the top plate of fuselage body 10 in 30 °~70 ° when antenna module is connected on mounting groove 3112 simultaneously, so that nobody
Machine can carry out good communication in low-latitude flying with base station.
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, the connecting plate 3111 can be fixedly connected on the top plate 11 of the fuselage body 10, and then the connection shell 311
Both ends are fixedly connected on through the connecting plate 3111 on the top plate 11, and design in this way can ensure the connection shell 311 in the fuselage sheet
The stability connected on body 10.
In the utility model embodiment, which includes top plate 11, bottom plate 12 and middle roll-over 13, the top
Plate 11 is oppositely arranged with bottom plate 12, and middle roll-over 13 is set between top plate 11 and bottom plate 12 and connects with the top plate 11 and bottom plate 12
It connects, which 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, the antenna module be paster antenna or bar antenna, the paster antenna
Limiting is accommodated 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, on the one hand conceal the antenna in this way
Component simultaneously because antenna module is inclined to set with the connection shell 311, thereby may be ensured that the signal of antenna module covers
Capping product is unaffected.
Specifically, as shown in Fig. 2, in the utility model embodiment, which is connected to the machine including two
It connection shell 311 on body ontology 10 and is connected between two connection shells 311 and for being connected to the company on 1 housing of fuselage
Beam 312 is connect, two connection shells 311 are oppositely arranged.Simultaneously the paster antenna, and two are respectively connected in 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 pairs of and be spaced apart
Two paster antennas can be made up well due to influence of connection shell 311 shield effectiveness to signal area coverage itself.
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 31 top of housing is installed, which includes base enclosure ontology 321 and the top being connected on the base enclosure ontology 321
Lid 322, for covering two antenna modules, which includes procapsid 3211 and along the front housing based shell 321
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
It stretches and is formed with upper shell 3212, the quantity of the upper shell 3212 is two, and two upper shells 3212 are for covering two
The antenna module namely the procapsid 3211 and upper shell 3212 are integrated, 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 on the upper shell 3212, is additionally provided on 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 322, matches
Close the structure matching setting of 3214 shape structure head cover 322 of slot, specifically, the shape of mating groove 3214 and the shape of head cover 322
With setting, the depth of mating groove 3214 is set with the thickness matching of head cover 322, and head cover 322 is detachably connected with base enclosure ontology 321
At mating groove 3214, the bottom surface of the head cover 322 is downward, at the same the mounting hole 3213 week along be above 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 in the mating groove 3214, metal magnetic conducting material is preset on 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, it in the utility model embodiment, is also associated with installing on the fuselage body 10
Frame 14, the installing frame 14 include for being connected on the fuselage body 10 and for connecting the fixed frame 141 of liquid storage babinet 6 and connecting
It is connected on the mounting bracket 142 on the fixed frame 141 and for connecting battery part 7.
In the present embodiment, which is outward extended with extension 14232, the end of the extension 14232
It is also recessed on face for the connecting line crossed beam trunking 14231 on limiting connection plug component 146.The connecting line is connected to this and crosses line
And accelerated ageing exposed to avoid the connecting line or it can be damaged in slot 14231.In addition, the upper end of the mounting bracket 142 also to
On be 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
It 142 and can be integrally formed every beam 143.Wherein, which includes substrate 1411 and opposite from the substrate 1411
The first extension board 1412 and the second extension board 1413 that both sides are obliquely extended.The substrate 1411 is connect with roll-over in this 13,
The V-shaped setting in both sides of first extension board 1412 and second extension board 1413 along the 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 that is 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.The limiting
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 (11)
1. a kind of unmanned plane, it is characterised in that：Including fuselage body and antenna module, housing group is connected on the fuselage body
Part, the housing unit include based shell and are fixedly connected below the based shell and are used to support the connection of the based shell
Shell, the connection shell are fixedly connected on the fuselage body, and the antenna module is fixedly connected on the connection shell.
2. unmanned plane as described in claim 1, it is characterised in that：The antenna module is fixedly connected on the interior of the connection shell
Side.
3. unmanned plane as described in claim 1, it is characterised in that：It tilts and sets between the antenna module and the fuselage body
It puts.
4. unmanned plane as claimed in claim 3, it is characterised in that：The antenna module is in first jiao with the fuselage body
Degree, the first angle are 30 °~70 °.
5. unmanned plane as claimed in claim 4, it is characterised in that：The antenna module is paster antenna or bar antenna.
6. such as claim 1-5 any one of them unmanned planes, it is characterised in that：The quantity of the connection shell is two, and two
A connection shell is oppositely arranged, and the both ends of each connection shell are formed with connecting plate, described in the both ends warp of the connection shell
Connecting plate is fixedly connected on the fuselage body, and the connection shell phase is obliquely installed the connecting plate, each company
The antenna module, two antenna modules to be oppositely arranged there are one connections on body contact.
7. unmanned plane as claimed in claim 6, it is characterised in that：The antenna module be paster antenna, each connection
Mounting groove is equipped on shell inner wall, the paster antenna limiting is accommodated in the mounting groove, and two paster antennas are opposite
Setting.
8. unmanned plane as claimed in claim 6, 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.
9. unmanned plane as claimed in claim 8, 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.
10. unmanned plane as claimed in claim 9, 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 on the upper shell, and the head cover covers the opening.
11. unmanned plane as claimed in claim 10, it is characterised in that：The top of the upper shell is equipped with mating groove, described to open
Mouth is magnetically coupled to through the mating groove, the head cover on the mating groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721046160.5U CN207550497U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Applications Claiming Priority (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 |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720954870.1U Division CN207346086U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207550497U true CN207550497U (en) | 2018-06-29 |
Family
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 After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720954870.1U Active CN207346086U (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN207550497U (en) |
Families Citing this family (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
Also Published As
| Publication number | Publication date |
|---|---|
| CN207346086U (en) | 2018-05-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2019119198A1 (en) | Radar and movable apparatus having same | |
| AU2018310402B2 (en) | Unmanned aerial vehicle | |
| US11343924B2 (en) | Unmanned aerial vehicle and avionics system thereof | |
| WO2020135639A1 (en) | Unmanned aerial vehicle base station and unmanned aerial vehicle communication system | |
| CN207550497U (en) | A kind of unmanned plane | |
| CN108767435A (en) | Antenna and unmanned vehicle | |
| CN209776822U (en) | three-dimensional laser radar collection system based on unmanned aerial vehicle | |
| CN207346069U (en) | It is a kind of for the installing frame of unmanned plane, rack and unmanned plane | |
| CN207060375U (en) | A kind of unmanned plane | |
| CN107792352A (en) | A kind of six rotor wing unmanned aerial vehicles | |
| CN109319104A (en) | A kind of unmanned plane | |
| CN207346087U (en) | A kind of unmanned plane | |
| CN206528630U (en) | Power is set with and unmanned vehicle | |
| CN205044993U (en) | Carry formula interferometer that goes up to air | |
| WO2018076471A1 (en) | Unmanned aerial vehicle | |
| CN206394888U (en) | Unmanned plane | |
| CN207060391U (en) | A kind of unmanned plane | |
| CN213302506U (en) | Radar assembly and movable platform with same | |
| CN113511342A (en) | Electric control device and unmanned aerial vehicle | |
| CN207883896U (en) | Antenna and unmanned vehicle | |
| WO2020038369A1 (en) | Antenna and unmanned aerial vehicle | |
| CN112407279A (en) | Modular patrol and use unmanned aerial vehicle | |
| CN216269956U (en) | Plant protection unmanned aerial vehicle | |
| CN206265281U (en) | A kind of integral type unmanned plane frame | |
| CN216684893U (en) | Top door double waterproof mechanism of unmanned aerial vehicle airport |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| 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. |