CN109319104A - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN109319104A CN109319104A CN201710647952.6A CN201710647952A CN109319104A CN 109319104 A CN109319104 A CN 109319104A CN 201710647952 A CN201710647952 A CN 201710647952A CN 109319104 A CN109319104 A CN 109319104A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- antenna
- antenna module
- shell
- fuselage body
- 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.)
- Pending
Links
- 230000013011 mating Effects 0.000 claims description 17
- 108090000565 Capsid Proteins Proteins 0.000 claims description 13
- 238000004891 communication Methods 0.000 abstract description 5
- 238000013461 design Methods 0.000 abstract description 4
- 238000009434 installation Methods 0.000 description 13
- 239000007788 liquid Substances 0.000 description 5
- 239000000758 substrate Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 3
- 238000009423 ventilation Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/285—Aircraft wire antennas
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Details Of Aerials (AREA)
Abstract
The invention 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 set 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 invention belongs to unmanned plane technical field of structures more particularly to a kind of unmanned planes.
Background technique
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.Unmanned plane antenna is one of the significant components of unmanned plane, and effect is to transmit information, positioning etc. during unmanned plane during flying
Deng.But in existing technology, unmanned plane base station generally sets up higher, and when unmanned plane low-latitude flying, antenna cannot be fine
Ground and base station communication.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes, it is intended to solve antenna and base when existing unmanned plane low-latitude flying
The bad problem of the communication stood.
The present invention solves in this way: a kind of unmanned plane, including fuselage body and is fixedly connected in the fuselage body
Antenna module, the antenna module is obliquely set on the fuselage body, and the transmitting terminal of the antenna module is towards remote
The direction of side and top surface from the fuselage body.
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, there are two the antenna modules, 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 formed with connecting plate, and the both ends of the connection shell are fixedly connected on the fuselage body through the connecting plate,
The connection shell phase is obliquely installed the connecting plate, and two antenna modules are set on the two connection shells.
Further, the antenna module is paster antenna, is equipped with mounting groove on each connection shell inner wall, described
Chip aerial limit is accommodated in the mounting groove, and two chip aerials 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 housings positioned at the procapsid two sides, the front housing
Body is fixed on the top of the two connection shells, and two upper housings cover two antenna modules.
Further, the upper housing is located at the top of the procapsid, and the top of the upper housing is equipped with opening, described
Top cover is also detachably connected on upper housing, the lid covers the opening.
Further, the top of the upper housing is equipped with mating groove, and the opening runs through the mating groove, the cover board magnetic
Property is connected on the mating groove.
The technical effect that unmanned plane provided by the invention has compared with the prior art are as follows: by the way that antenna module is opposite
It is obliquely installed in fuselage body, and the antenna module is connected on fuselage body, while the transmitting terminal of antenna module is towards far
The direction of side and top surface from the fuselage body is arranged, so that unmanned plane can carry out well in low-latitude flying with base station
Communication.
Detailed description of the invention
It to describe the technical solutions in the embodiments of the present invention more clearly, below will be to embodiment or description of the prior art
Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only of the invention some
Embodiment for those of ordinary skill in the art without any creative labor, can also be according to these
Attached drawing obtains other attached drawings.
Fig. 1 is the overall structure stereogram of unmanned plane provided in an embodiment of the present invention.
Fig. 2 is the structure chart of unmanned plane provided in an embodiment of the present invention, and wherein housing unit is by explosive decomposition.
Fig. 3 is unmanned plane provided in an embodiment of the present invention from the perspective view for looking up direction visual angle.
Fig. 4 is the structure chart that shell is connected in unmanned plane provided in an embodiment of the present invention.
Fig. 5 is the structure chart of base enclosure ontology in unmanned plane provided in an embodiment of the present invention.
Fig. 6 be in unmanned plane provided in an embodiment of the present invention installing frame in one direction on structure chart.
Fig. 7 is the structure chart on another direction of installing frame in unmanned plane provided in an embodiment of the present invention.
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 rack 142, end plate 1421, the first side plate 1422, mating groove
14211, the second side plate 1423, crossed beam trunking 14231, the installation installation of through slot 144, second of protection department 1424, partition 143, first it is logical
Slot 145, rolling assembly 144, limit assembly 145, plug-assembly 146, first install through slot 147, second and install through slot 148；
Horn 2, housing unit 3, installation shell 31, connection shell 311, attachment beam 312, mounting plate 3111, mounting groove 3112,
Based shell 32, base enclosure ontology 321, top cover 322, procapsid 3211, upper housing 3212, mounting hole 3213, mating groove 3214, magnet ring
3215, ventilation duct 3210；
Undercarriage 4, Power Component 5, liquid storage container 6, battery part 7.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
It should be noted that it can be directly another when element is referred to as " being fixed on " or " being set to " another element
On one element or indirectly 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 ", "upper", "lower", "front", "rear", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "top", "bottom" "inner", "outside" is that orientation based on the figure or position are closed
System, is merely for convenience of description of the present invention and simplification of the description, rather than the device or element of indication or suggestion meaning must have
Specific orientation is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.
In addition, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include one or more of the features.In the description of the present invention, the meaning of " plurality " is two or more,
Unless otherwise specifically defined.
Attached drawing 1 is please referred to shown in Fig. 7, in embodiments of the present invention, provide a kind of unmanned plane, including fuselage 1 and along this
The outwardly extending multiple horns 2 of fuselage 1 are connected on the fuselage 1 and are in the housing unit 3 of streamline curved surface, are connected to the fuselage 1
Bottom and the undercarriage 4 for being used to that the unmanned plane to be protected to rise and fall, are also connected to the Power Component 5 of 2 end of horn, are connected to the machine
Liquid storage container 6 and battery part 7 on body 1, and electricity adjust component and control system.It is separate that the Power Component 5 is fixed on the horn 2
The end of 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 interior is suitable for
Article to be sprayed or to be transported is contained, which is fixed on fuselage 1 to provide power, control system for Power Component 5
System is fixed on fuselage 1, for controlling the flight attitude of the aircraft.
The fuselage 1 is connected on the fuselage body 10 including fuselage body 10, the housing unit 3 simultaneously, and the shell
It is also connected with antenna module on component 3, which is obliquely set 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 design in this way can be suitble 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 ontology 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 shell 31 being connected on the fuselage body 10, the peace
Dress shell 31 include the connection shell 311 being obliquely installed relative to the fuselage body 10 namely this connection shell 311 is inclined is connected to
On the fuselage body 10.The mounting groove 3112 that 311 inner wall of connection shell is concavely provided with for antenna module limit connection, and
With the top plate of the fuselage body 10 in first angle when the antenna module is connected on the mounting groove 3112, which is
30 °~70 °.Design can guarantee that the signal area covering of antenna module is wider in this way.
The unmanned plane designed above includes the connection shell 311 being obliquely installed relative to fuselage body 10 by installation shell 31,
And it is concavely provided with the mounting groove 3112 for antenna module limit connection in the inner wall of connection shell 311, and then can be by antenna
Component is connected in the installation shell 31, so that antenna module be avoided to be mounted on, fuselage body 10 is outer and long-term exposed and then easy quilt
Damage.With the top plate of fuselage body 10 in 30 °~70 ° when antenna module is connected on mounting groove 3112 simultaneously, 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 embodiments of the present invention, the both ends of the connection shell 311 are each formed with connection
Plate 3111, the connecting plate 3111 can be fixedly connected on the top plate 11 of the fuselage body 10, and then the both ends warp of the connection shell 311
The connecting plate 3111 is fixedly connected on the top plate 11, and design in this way can guarantee the connection shell 311 on the fuselage body 10
The stability of connection.
In embodiments of the present invention, the fuselage body 10 include top plate 11, bottom plate 12 and middle roll-over 13, the top plate 11 with
Bottom plate 12 is oppositely arranged, and middle roll-over 13 is set between top plate 11 and bottom plate 12 and connect 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 embodiments of the present invention, which is chip aerial or bar antenna, chip aerial limit
It is accommodated in the mounting groove 3112.In order to guarantee concealment effect of the antenna module in housing unit 3, which is arranged
Slabbing antenna, and the chip aerial can be contained in the mounting groove 3112, on the one hand conceal the antenna module in this way,
Simultaneously because antenna module is inclined to set with the connection shell 311, the signal area coverage of antenna module thereby may be ensured that
It is unaffected.
Specifically, as shown in Fig. 2, in embodiments of the present invention, which includes two and be connected to the fuselage sheet
Connection shell 311 on body 10 and it is connected to the attachment beam between two connection shells 311 and for being connected on 1 shell of fuselage
312, two connection shells 311 are oppositely arranged.The chip aerial is respectively connected in two connection shells 311 simultaneously, and two should
It is oppositely arranged between chip aerial.
Since connection shell 311 itself can form shield effectiveness to the signal of chip aerial, but it is pairs of and be spaced apart
Two chip aerials can make up the influence due to the connection shield effectiveness of shell 311 itself to signal area coverage well.
Specifically, as shown in Figure 2 and Figure 5, in embodiments of the present invention, which further includes being connected to the installation
The based shell 32 of 31 top of shell, the based shell 32 include base enclosure ontology 321 and the top cover being connected on the base enclosure ontology 321
322, the based shell 321 is for covering two antenna modules, and the base enclosure ontology 321 is including procapsid 3211 and along the procapsid
The ventilation duct 3210 that 3211 two sides extend rearwardly to form is also connected with and 3210 phase of ventilation duct on 1 shell of fuselage
Pair electronic device.
Specifically, as shown in figure 5, in embodiments of the present invention, the upper end of the procapsid 3211 backward and upwardly extends shape
At there is upper housing 3212, the quantity of the upper housing 3212 is two, and two upper housings 3212 are for covering two days
Line component namely the procapsid 3211 and upper housing 3212 are integrated, and the upper housing 3212 is to be located at the procapsid
3211 top, the top cover 322 in Fluid Surface is also connected on the upper housing 3212, being additionally provided on the upper housing 3212 can
For the mating groove 3214 of the top cover 322 connection.
In embodiments of the present invention, the top of upper housing 3212 opens up a mating groove 3214 to accommodate cover board, mating groove
The structure matching of 3214 shape structure top covers 322 is arranged, and specifically, the shape of mating groove 3214 is matched with the shape of top cover 322 to be set
It sets, the depth of mating groove 3214 and the thickness matching of top cover 322 are arranged, and top cover 322 is removably connected to base enclosure ontology 321 matches
Close slot 3214 at, the bottom surface of the top cover 322 is downward, at the same the mounting hole 3213 week along be above formed with for the top cover 322
The mating groove 3214 that inner wall abuts, and 322 magnetic attracting of top cover is connected in the mating groove 3214.
In the present embodiment, it is previously provided with magnet ring in the mating groove 3214, is preset with metal magnetic conducting material on the top cover 322
Material, and then the top cover 322 first passes through locating shaft and is located by connecting on the mounting hole 3213, to be pre-positioned, the then top cover
322 magnetic attractings are connected to the top cover 322 in the mating groove 3214.
Specifically, as shown in Figure 6 and Figure 7, in embodiments of the present invention, installing frame is also connected on the fuselage body 10
14, which includes for being connected on the fuselage body 10 and for connecting the fixed frame 141 of liquid storage cabinet 6 and connection
Mounting rack 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 face of the extension 14232
On be also recessed with for limit connection plug component 146 on connecting line crossed beam trunking 14231.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 rack 142 is also upward
It is extended with protection department 1424.
In embodiments of the present invention, which is connected on the fuselage body 10, which is connected to this
On fixed frame 141, it is also connected between the mounting rack 142 and fixed frame 141 every beam 143.The fixed frame 141, mounting rack 142 with
And it can be integrally formed every beam 143.Wherein, which includes substrate 1411 and two inclinations opposite from the substrate 1411
The first extension board 1412 and the second extension board 1413 tiltedly extended.The substrate 1411 is connect with roll-over 13 in this, this first
Extension board 1412 and the second extension board 1413 are along the V-shaped setting in the two sides of the substrate 1411, while 1412 He of the first extension board
Perforation is equipped on second extension board 1413.The mounting rack 142 includes opposite the first side plate 1422 and the second side plate 1423, with
And it is connected to the end plate 1421 on 1423 end face of first side plate 1422 and the second side plate.First side plate 1422 deviates from the end plate
1421 side connects the end of first extension board 1412, which should away from the connection of the side of the end plate 1421
The upper end of the end of second extension board 1413, first side plate 1422 and the second side plate 1423 upwardly extends to form the protection department
1424.The installing frame 14 limits mounting groove, and should be connected between first side plate 1422 and the second side plate 1423 every beam 143 will
The mounting groove interval is divided into the first installation through slot 147 and the second installation through slot 148.The battery part 7 can be installed on the second installation
On through slot 148, which can be installed on the first installation through slot 147.
In embodiments of the present invention, which further includes rolling assembly 144, limit assembly 145 and plug-assembly
146.The rolling assembly 144 is linked in the first installation through slot 147, and for the liquid storage container 6 that is slidably connected.The limit group
Part 145 is fixed in the second installation through slot 148, and for locking the battery part 7.The plug-assembly 146 be connected to this second
It installs in through slot 148, and is electrically connected for battery part 7 with fuselage 1.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (10)
1. a kind of 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 set 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.
2. unmanned plane as described in claim 1, it is characterised in that: the antenna module and the fuselage body are in first jiao
Degree, the first angle are 30 °~70 °.
3. unmanned plane as described in claim 1, it is characterised in that: the antenna module is paster antenna or bar antenna.
4. unmanned plane as described in any one of claims 1-3, it is characterised in that: there are two the antenna modules, two days
Line component is oppositely arranged.
5. the unmanned plane as described in right 4, it is characterised in that: the unmanned plane further includes housing unit, the housing unit packet
Two connection shells are included, the both ends of each connection shell are formed with connecting plate, and the both ends of the connection shell are fixed through the connecting plate
It is connected on the fuselage body, the connection shell phase is obliquely installed the connecting plate, and two antenna modules are set to two
On the connection shell.
6. the unmanned plane as described in right 5, it is characterised in that: the antenna module is paster antenna, in each connection shell
Mounting groove is equipped on wall, the chip aerial limit is accommodated in the mounting groove, and two chip aerials are oppositely arranged.
7. the unmanned plane as described in right 5, it is characterised in that: the housing unit further includes based shell, and the based shell is fixed
In the top of the two connection shells, the based shell covers two antenna modules.
8. the unmanned plane as described in right 7, it is characterised in that: the based shell include procapsid and be located at the procapsid two sides
Two upper housings, the procapsid be fixed on two it is described connection shells tops, two upper housings cover two antenna modules.
9. unmanned plane described in right 8, it is characterised in that: the upper housing is located at the top of the procapsid, the upper casing
The top of body is equipped with opening, and top cover is also detachably connected on the upper housing, and the lid covers the opening.
10. the unmanned plane as described in right 7, it is characterised in that: the top of the upper housing is equipped with mating groove, and the opening runs through
The mating groove, the cover board are magnetically coupled on the mating groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710647952.6A CN109319104A (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710647952.6A CN109319104A (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109319104A true CN109319104A (en) | 2019-02-12 |
Family
ID=65246018
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710647952.6A Pending CN109319104A (en) | 2017-08-01 | 2017-08-01 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109319104A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110171559A (en) * | 2019-06-21 | 2019-08-27 | 深圳市中天迅通信技术股份有限公司 | A kind of unmanned plane and its control method |
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|---|---|---|---|---|
| JPH0550991A (en) * | 1991-08-26 | 1993-03-02 | Nippon Hoso Kyokai <Nhk> | Mobile reception apparatus mounted on aircraft |
| CN1557039A (en) * | 2001-09-28 | 2004-12-22 | ס�ѵ�����ҵ��ʽ���� | Radio wave lens antenna apparatus |
| US20050212711A1 (en) * | 2003-11-28 | 2005-09-29 | Takaya Ogawa | Lens antenna apparatus |
| CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
| US20170115660A1 (en) * | 2015-10-23 | 2017-04-27 | Parrot Drones | Drone having a support housing an antenna |
| US20170168481A1 (en) * | 2015-12-14 | 2017-06-15 | Gopro, Inc. | User interface for orienting antennas |
| JP2017121008A (en) * | 2015-12-28 | 2017-07-06 | Kddi株式会社 | Communication relay device |
| CN207346086U (en) * | 2017-08-01 | 2018-05-11 | 广州极飞科技有限公司 | A kind of unmanned plane |
-
2017
- 2017-08-01 CN CN201710647952.6A patent/CN109319104A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0550991A (en) * | 1991-08-26 | 1993-03-02 | Nippon Hoso Kyokai <Nhk> | Mobile reception apparatus mounted on aircraft |
| CN1557039A (en) * | 2001-09-28 | 2004-12-22 | ס�ѵ�����ҵ��ʽ���� | Radio wave lens antenna apparatus |
| US20050212711A1 (en) * | 2003-11-28 | 2005-09-29 | Takaya Ogawa | Lens antenna apparatus |
| US20170115660A1 (en) * | 2015-10-23 | 2017-04-27 | Parrot Drones | Drone having a support housing an antenna |
| CN106785357A (en) * | 2015-10-23 | 2017-05-31 | 鹦鹉无人机股份有限公司 | Unmanned plane with the support for accommodating antenna |
| US20170168481A1 (en) * | 2015-12-14 | 2017-06-15 | Gopro, Inc. | User interface for orienting antennas |
| JP2017121008A (en) * | 2015-12-28 | 2017-07-06 | Kddi株式会社 | Communication relay device |
| CN205418056U (en) * | 2016-03-29 | 2016-08-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle of unmanned aerial vehicle shell and applied this unmanned aerial vehicle shell |
| CN207346086U (en) * | 2017-08-01 | 2018-05-11 | 广州极飞科技有限公司 | A kind of unmanned plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110171559A (en) * | 2019-06-21 | 2019-08-27 | 深圳市中天迅通信技术股份有限公司 | A kind of unmanned plane and its control method |
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