CN209290711U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN209290711U CN209290711U CN201822006687.6U CN201822006687U CN209290711U CN 209290711 U CN209290711 U CN 209290711U CN 201822006687 U CN201822006687 U CN 201822006687U CN 209290711 U CN209290711 U CN 209290711U
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- unmanned plane
- horn
- foot prop
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- electricity
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Abstract
The utility model discloses a kind of unmanned plane, including fuselage, the horn component and the Power Component on horn component being connect with fuselage, electronic component is equipped in fuselage, horn component includes horn and the mounting assembly set on horn far from fuselage one end, mounting assembly includes Coupling, attachment base and foot prop, Coupling is separately connected horn and attachment base, Power Component and foot prop are separately positioned on the two sides up and down of attachment base, electric tune is installed in foot prop, electricity, which is adjusted, to be connect by the first connecting line with electronic component, Power Component is adjusted by the second connecting line and electricity and is connected, first connecting line is in horn component internal cabling, second connecting line cabling inside mounting assembly.The unmanned plane structure of the utility model is simple, rationally distributed and small in size, and can be effectively reduced the influence that Power Component adjusts electricity.
Description
Technical field
The utility model relates to unmanned vehicle technical fields, more particularly to a kind of rationally distributed unmanned plane.
Background technique
Unmanned plane be manipulated using radio robot (i.e. remote controler) and the presetting apparatus provided for oneself it is not manned
Aircraft, unmanned plane take photo by plane, survey and draw, agricultural plant protection, monitoring infectious disease, electric inspection process, the disaster relief, the fields such as movies-making have extensively
General application.
Unmanned plane includes fuselage and horn, and horn is equipped with rotor.The electric-regulating device of unmanned plane be laid out mostly in fuselage or
On the foot prop of person's horn end.When electric-regulating device is arranged on fuselage, the space on fuselage can be occupied, increases the cloth in fuselage
Office's difficulty；When electric-regulating device is arranged on the foot prop of horn end, the motor usually with driving propeller rotation is mounted on one
It rises, or is installed close to motor, so that the structure that foot prop installation motor and electricity are mediated is larger, meanwhile, motor generates when working
Heat also easily pass to electric-regulating device, influence the normal work of electric-regulating device.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, structure is simple and rationally distributed, to electric-regulating device
It influences small.
For this purpose, the utility model uses following technical scheme:
A kind of unmanned plane is provided, including fuselage, the horn component connecting with the fuselage and is set to the horn component
On Power Component, electronic component is equipped in the fuselage, the horn component includes horn and is set to the horn far from institute
The mounting assembly of fuselage one end is stated, the mounting assembly includes Coupling, attachment base and foot prop, and the Coupling is separately connected institute
Horn and the attachment base are stated, the Power Component and the foot prop are separately positioned on the two sides up and down of the attachment base, described
Electric tune is installed, the electricity, which is adjusted, to be connect by the first connecting line with the electronic component, and the Power Component passes through the in foot prop
Two connecting lines and the electricity are adjusted and are connected, first connecting line in the horn component internal cabling, second connecting line in
Cabling inside the mounting assembly.
As a kind of preferred embodiment of unmanned plane, container is offered on the foot prop, the electricity, which is adjusted, is contained in the receipts
In tank.
As a kind of preferred embodiment of unmanned plane, the foot prop is detachably connected with the attachment base, and the foot prop is close
One end of the attachment base is equipped with the first opening being connected to the container.
As a kind of preferred embodiment of unmanned plane, the side of the foot prop offers second be connected to the container and opens
Mouthful, second opening is detachably provided with the mounting shell for blocking second opening.
As a kind of preferred embodiment of unmanned plane, the electricity, which is adjusted, is arranged in the mounting shell close to the one of the container
Side.
As a kind of preferred embodiment of unmanned plane, the electricity, which is adjusted, is arranged thermal component between the mounting shell；And/or
The electricity is corresponded on the installation shell to adjust equipped with the thermal component.
It further include antenna as a kind of preferred embodiment of unmanned plane, the antenna is mounted in the foot prop, the antenna
It is connect by antenna control line with the electronic component, the antenna control line is in the horn component internal cabling.
It further include antenna as a kind of preferred embodiment of unmanned plane, the antenna is mounted on outside the foot prop, the foot prop
Above through cable-through hole is offered, the antenna is connect by antenna control line with the electronic component, and the antenna control line is worn
The cable-through hole is crossed in the horn component internal cabling.
As a kind of preferred embodiment of unmanned plane, the outer surface of the antenna is coated with sealant.
As a kind of preferred embodiment of unmanned plane, cushion is arranged far from one end of the attachment base in the foot prop.
As a kind of preferred embodiment of unmanned plane, the horn includes principal arm and the support arm that connect with the principal arm, described
Mounting assembly is set to the one end of the support arm far from the principal arm, and the Coupling includes socket part and connect with the socket part
Articulated section, the socket part is set in the end of the support arm, and the articulated section and the attachment base are hinged, the attachment base
It can be rotated around hinge axes relative to the support arm.
As a kind of preferred embodiment of unmanned plane, glue is provided between the socket part and the outer peripheral surface of the support arm.
The utility model embodiment has the beneficial effect that by setting up separately Power Component and foot prop up and down the two of attachment base
Side, and electricity is adjusted and is arranged in foot prop, the company for increasing mounting assembly can not be needed reasonably using space spacious in foot prop
The volume of joint chair can be effectively reduced the size of entire mounting assembly, while be effectively isolated to electricity reconciliation Power Component,
The heat generated when preventing Power Component from working influences the normal work that electricity is adjusted；By the connection that will connect electricity reconciliation Power Component
Line cabling inside horn component or mounting assembly, so that connecting line is not exposed, and then effectively protects connecting line.
Detailed description of the invention
The utility model is described in further detail below according to drawings and examples.
Fig. 1 is the stereoscopic schematic diagram of the unmanned plane of the utility model embodiment.
Fig. 2 is the structural schematic diagram of the support arm assembly of the utility model embodiment.
Fig. 3 is the schematic cross-sectional view of the support arm assembly of the utility model embodiment.
Fig. 4 is the stereoscopic schematic diagram of the Coupling of the utility model embodiment.
Fig. 5 is the stereoscopic schematic diagram of the attachment base of the utility model embodiment.
Fig. 6 is the first view stereo schematic diagram of the supporing shell of the utility model embodiment.
Fig. 7 is the second view stereo schematic diagram of the supporing shell of the utility model embodiment.
The electricity tune and the first visual angle schematic diagram after the assembling of mounting shell that Fig. 8 is the utility model embodiment.
The electricity tune and the second visual angle schematic diagram after the assembling of mounting shell that Fig. 9 is the utility model embodiment.
Figure 10 is that the electricity of the utility model embodiment adjusts the decomposition diagram with mounting shell.
Figure 11 is the stereoscopic schematic diagram of the radiating piece of the utility model embodiment.
In figure:
10, fuselage；
20, horn component；21, principal arm；22, support arm；23, mounting assembly；231, Coupling；2311, socket part；2312,
Articulated section；232, attachment base；2321, interconnecting piece；23211, supporting walls；23212, connection wall；2322, support portion；233, foot prop；
2330, container；2331, supporing shell；2332, mounting shell；23320, heat release hole；2333, cushion；
30, Power Component；31, motor；32, propeller；
40, electricity is adjusted；41, electricity adjusts circuit board；42, radiating piece；421, heat-conducting substrate；422, radiating part；50, antenna；60,
One connecting line.
Specific embodiment
The technical issues of to solve the utility model, the technical solution of use and the technical effect that reaches are clearer,
It is described in further detail below in conjunction with technical solution of the attached drawing to the utility model embodiment, it is clear that described reality
Applying example is only the utility model a part of the embodiment, instead of all the embodiments.Based on the embodiments of the present invention,
It is practical new to belong to this for those skilled in the art's every other embodiment obtained without creative efforts
The range of type protection.
In the description of the present invention, unless otherwise clearly defined and limited, term " connected ", " connection ", " Gu
It is fixed " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or integral；It can be mechanical connect
It connects, is also possible to be electrically connected；It can be directly connected, can also can be in two elements indirectly connected through an intermediary
The interaction relationship of the connection in portion or two elements.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
In the present invention unless specifically defined or limited otherwise, fisrt feature the "upper" of second feature or it
"lower" may include that the first and second features directly contact, and also may include that the first and second features are not direct contacts but lead to
Cross the other characterisation contact between them.Moreover, fisrt feature includes above the second feature " above ", " above " and " above "
One feature is right above second feature and oblique upper, or is merely representative of first feature horizontal height higher than second feature.First is special
Sign is directly below and diagonally below the second feature including fisrt feature under the second feature " below ", " below " and " below ", or only
Indicate that first feature horizontal height is less than second feature.
The position when nouns of locality such as the front, rear, left and right mentioned in following embodiment are according to unmanned plane normally travel is come
Description, only as description reference.
Fig. 1 to Fig. 9 is please referred to, unmanned plane provided by the embodiment of the utility model is described.Unmanned plane can be used for geographical mapping
Equal activities.Certainly, unmanned plane is not limited to use in geographical mapping, it may also be used for photography of taking photo by plane, electric inspection process, environmental monitoring and
The fields such as disaster inspection.
Unmanned plane includes fuselage 10, horn component 20 and Power Component 30.In present embodiment, unmanned plane is quadrotor
Unmanned plane, 30 quantity of Power Component are four, and four Power Components 30 are distributed in fuselage 10 by the support of horn component 20
In the rectangular area of surrounding, and each Power Component 30 is located on a vertex of rectangle.
Certainly, according to different demands, the quantity of Power Component 30 can do suitable variation, for example, Power Component 30
Quantity can be two, three, six etc., even, the quantity of Power Component 30 can be only one, correspondingly, horn group
The quantity of part 20 can also according to Power Component 30 quantity and be rationally arranged.
Referring to Fig.1, fuselage 10 is the load-bearing part of unmanned plane, and electrical mounting portion can be set on fuselage 10 or in fuselage 10,
Electric mounting portion can install and carry Anneta module, fly to control the electronics such as module, circuit main board, communication module and battery member
Part.Application field according to unmanned plane is different, and can also carry other on fuselage 10 can be realized the load of particular task, example
Such as, unmanned plane is for when taking photo by plane or surveying and drawing, fuselage 10 can be equipped with the capture apparatus for increasing steady holder；Unmanned plane is for trip of racing
When play, fuselage 10 can carry game station etc..
With continued reference to Fig. 1, horn component 20 is rotatably connected at the side of fuselage 10.Horn component 20 is used to support dynamic
Power component 30, and the connecting line between the electronic component on Power Component 30 and fuselage 10 is protected, and make Power Component 30 with pre-
Pattern is ordered to be distributed in around fuselage 10.Since horn component 20 is rotatably connected to the side of fuselage 10, horn group
Part 20 can adjust different position and state relative to fuselage 10.
Referring to figs. 1 to Fig. 3, horn component 20 includes horn and mounting assembly of the horn far from 10 one end of fuselage is arranged in
23, wherein horn includes principal arm 21 and the support arm connecting with principal arm 21 22, and mounting assembly 23 is set to support arm 22 far from principal arm 21 1
End.
The quantity of principal arm 21 is two, and two principal arms 21 are connected to the opposite two sides of fuselage 10, each principal arm 21
One end is rotatably connected on fuselage 10 by connection component, wherein connection component includes fixing seat and rotation seat, fixing seat
It is connect with fuselage 10, rotation seat is connect with principal arm 21, and fixing seat and rotation seat are pivotally connected.The other end and support arm 22 of each principal arm 21
It is connected.Each principal arm 21 connects two support arms 22.
Referring to figs. 1 to Fig. 3, two support arms 22 are coaxially disposed the two sides for being located at principal arm 21.Principal arm 21 and support arm 22 are big
Cause connection " T " shape.In present embodiment, the support arm 22 of each 21 two sides of principal arm can be shown as with integrally connected, support arm 22
End of the principal arm 21 far from fuselage 10 is fixed on by connecting lantern ring in the elongated arm of one entirety, the approximate mid-section position of support arm 22
Portion, support arm 22 are substantially vertical with principal arm 21.Further, it connects on lantern ring and offers the use being connected with principal arm 21 and support arm 22
In the via hole passed through for connecting line.
Mounting assembly 23 includes Coupling 231, attachment base 232 and foot prop 233, and Coupling 231 is separately connected 22 He of support arm
Attachment base 232, Power Component 30 and foot prop 233 are separately positioned on the two sides up and down of attachment base 232, are equipped with electricity in foot prop 233
40 are adjusted, electricity adjusts 40 to connect by the first connecting line 60 with electronic component, and Power Component 30 adjusts 40 to connect by the second connecting line and electricity
It connects, the first connecting line 60 is in 20 inside cabling of horn component, and the second connecting line is in 23 inside cabling of mounting assembly.By by power
Component 30 and foot prop 233 set up separately in the two sides up and down of attachment base 232, and adjust 40 to be arranged in foot prop 233 electricity, can be reasonably
Using space spacious in foot prop 233, the volume for increasing the attachment base 232 of mounting assembly 23 is not needed, can be effectively reduced whole
The size of a mounting assembly 23, while electricity tune 40 and Power Component 30 are effectively isolated, prevent Power Component 30 from working
When the heat that generates influence the normal work that electricity adjusts 40；By the way that the connecting line of electricity tune 40 and Power Component 30 will be connected in horn group
23 inside cabling of part 20 or mounting assembly, so that connecting line is not exposed, and then effectively protects connecting line.
In the present embodiment, Coupling 231 include it is annular in shape and at least partly structure and support arm 22 far from principal arm 21 one
The socket part 2311 that end cap is set.In order to promote the bonding strength between socket part 2311 and support arm 22, in socket part 2311 and branch
Glue is set between the outer peripheral surface of arm 22, is connected so as to be bonded between socket part 2311 and support arm 22 by glue.Pass through gluing
Mode socket part 2311 is fixed, method is simple, and avoids big using the fixed forms bring weight such as screw
The problem of.
Coupling 231 further includes articulated section 2312, and attachment base 232 and articulated section 2312 are hinged, and attachment base 232 can be around pivot joint
Axis is rotated relative to support arm 22.
Referring to Fig. 5, attachment base 232 includes interconnecting piece 2321 and support portion 2322, and interconnecting piece 2321 includes supporting walls 23211
And two connection walls 23212 extended vertically downward along 23211 two sides of supporting walls.2322 projection of support portion is in supporting walls 23211
Top, Power Component 30 is installed on 2322 on support portion.In the present embodiment, two connection walls 23212 and Coupling 231
Articulated section 2312 is pivotally connected, and further, articulated section 2312 is inserted between two connection walls 23212 and by shaft and two companies
Connect the connection of wall 23212.Certainly, in other embodiments, attachment base 232 can also be integrally formed with Coupling 231, for example be used
Plastics integrated injection molding.
Referring to figure 6 and figure 7, foot prop 233 is used for support when rising and falling as unmanned plane.Container is offered on foot prop 233
2330, the electricity that container 2330 is used to accommodate control Power Component 30 adjusts 40.
Optionally, 40 installation is adjusted for the ease of electricity, foot prop 233 is detachably connected with attachment base 232, and foot prop 233 is close
One end of attachment base 232 is equipped with the first opening being connected to container 2330.Electricity adjusts 40 can be open by first and be installed on foot prop
In 233.Alternatively, the side of foot prop 233 offers the second opening being connected to container 2330, the second opening is detachably arranged
There is the mounting shell 2332 for blocking the second opening, i.e., dismounts electricity from the side of foot prop 233 and adjust 40, do not need to dismantle entire foot prop 233.
Specifically, foot prop 233 further includes supporing shell 2331, the top of supporing shell 2331 and connection wall 23212 connect
It connects, the first opening and the second opening are provided with the top and side of supporing shell 2331 respectively, and further, electricity adjusts 40 to be fixed on
On mounting shell 2332, and it is located at mounting shell 2332 close to the side of container 2330, the lid of mounting shell 2332 is located at the second opening
To close container 2330.
Further, 0 and Figure 11, electricity adjust 40 to adjust circuit board 41 and radiating piece 42, the position of radiating piece 42 including electricity referring to Fig.1
Setting, which can be set, adjusts between circuit board 41 and mounting shell 2332 in electricity or is arranged on mounting shell 2332.Specifically, radiating piece
42 be metalwork, and radiating piece 42 includes heat-conducting substrate 421 and radiating part 422, and mounting shell 2332 offers heat release hole 23320, is dissipated
Hot portion 422 is pierced by along heat release hole 23320 and, electricity tune circuit board 41 and heat-conducting substrate fixed (being clamped herein) with mounting shell 2332
421 patch merga pass fasteners and mounting shell 2332 are fixed.Further, electricity is adjusted between circuit board 41 and heat-conducting substrate 421 also
It is provided with heat conductive silica gel.
Further, foot prop 233 further includes a cushion 2333, and cushion 2333 is set to the bottom of foot prop 233.
Power Component 30 is used to provide the power of flight for unmanned plane.Power Component 30 is installed on support portion 2322, is moved
Power component 30 includes motor 31 and the propeller 32 being connected with motor 31.Motor 31 can drive propeller 32 to rotate, in turn
Generate the power of driving unmanned plane movement.Motor 31 can be the motor of any types such as brushless motor, brush motor.
In the present embodiment, motor 31 can be electrically connected with the electronic component of fuselage 10 (like flying control module, battery etc.), real
Now rotated according to scheduled revolving speed, steering driving propeller 32.Specifically, electronic component (the control module like flying, electricity of fuselage 10
Pond etc.) it is connect by the first connecting line 60 with the electricity tune 40 in foot prop 233, electricity tune 40 passes through the second connecting line and the company of motor 31 again
It connects, wherein the first connecting line 60 and the second connecting line include power supply line and data line, one end of the first connecting line 60 and fuselage
Electronic component connection in 10, the other end are introduced to foot prop by the principal arm 21 of horn component 20 and the inside cabling of support arm 22
40 are adjusted to connect with electricity in 233, one end of the second connecting line adjusts 40 to connect with the electricity in foot prop 233, and the other end is by horn component 20
Mounting assembly 23 inside cabling, and connect with the motor 31 on support portion 2322.Connecting line is contained in horn component 20,
It can be not only effectively protected connecting line, while space can also be saved.
Further, unmanned plane further includes antenna 50, and antenna 50 can be set in the container 2330 of foot prop 233, day
Line 50 is connect by antenna control line with the electronic component in fuselage 10, antenna control line and 20 inside cabling of horn component.
Certainly, in other embodiments, the outside of foot prop 233 can also be arranged in antenna 50, open in supporing shell 2331
Equipped with the cable-through hole that is connected to inside container 2330, antenna control line after this cable-through hole in the inside of horn component 20 by walking
Line.Antenna 50 can be fixed by screws on foot prop 233.Further, the outer surface of antenna 50 is coated with sealant.
In the description of this specification, the description of reference term " embodiment " etc. means the specific spy in conjunction with the embodiment
Sign, structure, material or feature are contained at least one embodiment or example of the utility model.In the present specification, right
The schematic representation of above-mentioned term is not necessarily referring to identical embodiment.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this narrating mode of specification be only be to understand device, those skilled in the art should
It considers the specification as a whole, the technical solutions in the embodiments can also be appropriately combined, and forming those skilled in the art can
With the other embodiments of understanding.
Technical principle of the utility model has been described above with reference to specific embodiments.These descriptions are intended merely to explain this reality
With novel principle, and it cannot be construed to the limitation to scope of protection of the utility model in any way.Based on the explanation herein,
Those skilled in the art, which does not need to pay for creative labor, can associate with other specific implementation modes of this utility model,
These modes are fallen within the protection scope of the utility model.
Claims (12)
1. a kind of unmanned plane, including fuselage, the horn component being connect with the fuselage and moving on the horn component
Power component, the fuselage is interior to be equipped with electronic component, which is characterized in that the horn component includes that horn is remote with the horn is set to
Mounting assembly from described fuselage one end, the mounting assembly include Coupling, attachment base and foot prop, and the Coupling connects respectively
The horn and the attachment base are connect, the Power Component and the foot prop are separately positioned on the two sides up and down of the attachment base,
Electric tune is installed, the electricity, which is adjusted, to be connect by the first connecting line with the electronic component, and the Power Component is logical in the foot prop
It crosses the second connecting line and the electricity is adjusted and connected, first connecting line is in the horn component internal cabling, second connection
Line cabling inside the mounting assembly.
2. unmanned plane according to claim 1, which is characterized in that offer container on the foot prop, the electricity, which is adjusted, to be received
It is dissolved in the container.
3. unmanned plane according to claim 2, which is characterized in that the foot prop is detachably connected with the attachment base, institute
It states foot prop and is equipped with the first opening being connected to the container close to one end of the attachment base.
4. unmanned plane according to claim 2, which is characterized in that the side of the foot prop is offered to be connected with the container
The second logical opening, second opening are detachably provided with the mounting shell for blocking second opening.
5. unmanned plane according to claim 4, which is characterized in that the electricity, which is adjusted, to be arranged in the mounting shell close to the receipts
The side of tank.
6. unmanned plane according to claim 5, which is characterized in that the electricity, which is adjusted, is arranged radiating part between the mounting shell
Part；And/or the electricity is corresponded on the mounting shell and is adjusted equipped with the thermal component.
7. unmanned plane according to claim 1, which is characterized in that further include antenna, the antenna is mounted on the foot prop
Interior, the antenna is connect by antenna control line with the electronic component, and the antenna control line is in the horn component internal
Cabling.
8. unmanned plane according to claim 1, which is characterized in that further include antenna, the antenna is mounted on the foot prop
Outside, through cable-through hole is offered on the foot prop, the antenna is connect by antenna control line with the electronic component, the day
Line traffic control line passes through the cable-through hole in the horn component internal cabling.
9. unmanned plane according to claim 8, which is characterized in that the outer surface of the antenna is coated with sealant.
10. unmanned plane according to claim 1, which is characterized in that the foot prop is arranged far from one end of the attachment base
Cushion.
11. unmanned plane according to claim 1, which is characterized in that the horn includes principal arm and connect with the principal arm
Support arm, the mounting assembly be set to the one end of the support arm far from the principal arm, the Coupling include socket part and with institute
The articulated section of socket part connection is stated, the socket part is set in the end of the support arm, and the articulated section and the attachment base are cut with scissors
It connects, the attachment base can be rotated around hinge axes relative to the support arm.
12. unmanned plane according to claim 11, which is characterized in that between the socket part and the outer peripheral surface of the support arm
It is provided with glue.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822006687.6U CN209290711U (en) | 2018-11-29 | 2018-11-29 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822006687.6U CN209290711U (en) | 2018-11-29 | 2018-11-29 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209290711U true CN209290711U (en) | 2019-08-23 |
Family
ID=67656862
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822006687.6U Active CN209290711U (en) | 2018-11-29 | 2018-11-29 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209290711U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113353269A (en) * | 2021-07-26 | 2021-09-07 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
| EP3950491A4 (en) * | 2019-12-19 | 2022-06-15 | Guangzhou Xaircraft Technology Co., Ltd | Self-driving control apparatus and driverless apparatus provided with same |
| US12009569B2 (en) | 2019-12-19 | 2024-06-11 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
-
2018
- 2018-11-29 CN CN201822006687.6U patent/CN209290711U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3950491A4 (en) * | 2019-12-19 | 2022-06-15 | Guangzhou Xaircraft Technology Co., Ltd | Self-driving control apparatus and driverless apparatus provided with same |
| JP2022532713A (en) * | 2019-12-19 | 2022-07-19 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| JP7269375B2 (en) | 2019-12-19 | 2023-05-08 | 広州極飛科技股▲ふん▼有限公司 | Automatic operation control device and unmanned operation device equipped with it |
| AU2020408484B2 (en) * | 2019-12-19 | 2023-07-13 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
| US12009569B2 (en) | 2019-12-19 | 2024-06-11 | Guangzhou Xaircraft Technology Co., Ltd. | Self-driving control device and unmanned driving device with the same |
| CN113353269A (en) * | 2021-07-26 | 2021-09-07 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
| CN113353269B (en) * | 2021-07-26 | 2022-07-19 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 510000, No. 1, Cheng Cheng Road, Gaotang Software Park, Guangzhou, Guangdong, Tianhe District, 3A01 Patentee after: Guangzhou Jifei Technology Co.,Ltd. Address before: 510000, No. 1, Cheng Cheng Road, Gaotang Software Park, Guangzhou, Guangdong, Tianhe District, 3A01 Patentee before: Guangzhou Xaircraft Technology Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder |