CN211685668U - Unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof - Google Patents
Unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof Download PDFInfo
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- CN211685668U CN211685668U CN201922484749.9U CN201922484749U CN211685668U CN 211685668 U CN211685668 U CN 211685668U CN 201922484749 U CN201922484749 U CN 201922484749U CN 211685668 U CN211685668 U CN 211685668U
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- 238000004891 communication Methods 0.000 claims description 3
- 125000004122 cyclic group Chemical group 0.000 claims 1
- 210000001503 joint Anatomy 0.000 claims 1
- 230000005611 electricity Effects 0.000 abstract description 6
- 230000008878 coupling Effects 0.000 description 15
- 238000010168 coupling process Methods 0.000 description 15
- 238000005859 coupling reaction Methods 0.000 description 15
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- 238000013461 design Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 238000010030 laminating Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
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Abstract
The utility model discloses an unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof, including cloud platform main part, support and infrared camera module, the cloud platform main part include cloud platform casing, infrared processing module and with the transmission module that infrared processing module electricity is connected, infrared processing module with transmission module locates in the cloud platform casing, and the projection interval of cloud platform casing bottom sets up, the support is located cloud platform casing below, the support is in the projection of cloud platform casing bottom is located infrared processing module with between the transmission module, infrared camera module includes the main casing body and locates the infrared camera of the main casing body, the main casing body is located the support, infrared camera with the infrared processing module electricity is connected. When the unmanned aerial vehicle cloud platform of this embodiment was carried unmanned aerial vehicle, because the whole height of unmanned aerial vehicle cloud platform is less, unmanned aerial vehicle can directly place and take off on ground.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment technical field especially relates to an unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof.
Background
At present, when designing unmanned aerial vehicle's structure, can make unmanned aerial vehicle's focus and its barycenter coincidence as far as possible to guarantee unmanned aerial vehicle's steady flight. Likewise, the design unmanned aerial vehicle cloud platform that unmanned aerial vehicle carried on also need consider centrobaric problem. Unmanned aerial vehicle cloud platform on the market generally superposes each control module and processing module (for example cloud platform control panel, data transmission module, infrared camera processing module etc.) in proper order and sets up the intermediate position in the cloud platform casing to set up the camera under, thereby make the focus of unmanned aerial vehicle cloud platform be close to its barycenter.
However, with the mode that each control module and processing module set up between two parties for the whole height of unmanned aerial vehicle cloud platform on the market is higher, and the fuselage below of unmanned aerial vehicle on the market usually establishes the undercarriage, when the unmanned aerial vehicle cloud platform is connected in the fuselage below, because the height of unmanned aerial vehicle cloud platform is greater than the length of undercarriage, the relative undercarriage of unmanned aerial vehicle cloud platform part is protrusion downwards, lead to unmanned aerial vehicle can't directly place subaerial through the undercarriage, need manual the undercarriage of holding up when taking off.
SUMMERY OF THE UTILITY MODEL
The embodiment of the utility model discloses unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof, because the whole height of unmanned aerial vehicle cloud platform is less, unmanned aerial vehicle can directly place and take off on ground.
In a first aspect, the embodiment of the utility model discloses an unmanned aerial vehicle cloud platform, including cloud platform main part, support and infrared camera module, the cloud platform main part include cloud platform casing, infrared processing module and with the transmission module that infrared processing module electricity is connected, infrared processing module with transmission module locates in the cloud platform casing, just projection interval on the cloud platform casing bottom sets up, the support is located cloud platform casing below, the support is in projection on the cloud platform casing bottom is located infrared processing module with between the transmission module, infrared camera module includes the main casing body and locates the infrared camera of the main casing body, the main casing body is located the support, infrared camera with infrared processing module electricity is connected.
As an optional implementation manner, in the embodiment of the present invention, the cradle head casing includes an upper casing and a lower casing connected to form the accommodating cavity, the lower casing is provided with a first opening, the bracket is disposed at the first opening, and the infrared processing module and the transmission module are disposed at the lower casing and located at two sides of the first opening respectively.
As an optional implementation manner, in an embodiment of the present invention, the lower casing is a convex casing, and includes a first portion, a second portion, and a third portion, the second portion and the third portion are respectively disposed on two sides of the first portion, the first opening is disposed on the first portion and located at a position where the first portion protrudes from the second portion and the third portion, the infrared processing module is disposed on the second portion, and the transmission module is disposed on the third portion.
As an optional implementation manner, in an embodiment of the present invention, the bottom surface of the lower casing is provided with a plurality of heat dissipation holes communicating with the accommodating cavity.
As an optional implementation manner, in the embodiment of the present invention, the unmanned aerial vehicle cloud platform further includes two antennas, two the antenna branch is located the both sides of cloud platform casing, and set up down, two the antenna electricity connect in transmission module.
As an optional implementation manner, in the embodiment of the present invention, the unmanned aerial vehicle pan-tilt further includes a damping component, the damping component is located at the first opening of the lower shell, and is located in the containing cavity, and the support is connected to the damping component.
As an optional implementation manner, in the embodiment of the present invention, the lower shell is close to the first opening and is convexly provided with a plurality of first connecting protrusions, and is a plurality of the first connecting protrusions are annularly arranged along the center of the first opening, the damping assembly includes an annular component and a damping component, the annular component is located above the first opening, the annular component and the first opening form a heat dissipation gap therebetween, the annular component corresponds to a plurality of the first connecting protrusions are convexly provided with a plurality of second connecting protrusions, the damping component is connected to the first connecting protrusions and the second connecting protrusions, and the bracket is connected to the annular component.
As an optional implementation manner, in the embodiment of the present invention, the unmanned aerial vehicle pan-tilt further includes a mounting seat, the size of the mounting seat matches with the size of the inner ring of the annular component, the mounting seat is located on the inner annular surface of the annular component, and the support is connected to the mounting seat.
As an optional implementation manner, in the embodiment of the present invention, the upper shell is provided with a second opening, and the second opening extends upward to form an arc-shaped connection portion.
In a second aspect, the embodiment of the utility model discloses an unmanned aerial vehicle with unmanned aerial vehicle cloud platform that first aspect is disclosed, including fuselage and above-mentioned unmanned aerial vehicle cloud platform, the unmanned aerial vehicle cloud platform connect in the fuselage.
The embodiment of the utility model provides an unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof locates in the cloud platform casing through infrared processing module and transmission module, and the projection interval in the cloud platform casing sets up, and cloud platform casing below is located to the support, and the projection on the cloud platform casing is located between infrared processing module and the transmission module for the thickness of cloud platform casing is less, thereby reduces the whole height of unmanned aerial vehicle cloud platform.
Further, damper locates the first opening part of casing down, and is located the appearance intracavity that casing and inferior valve body coupling formed, and make full use of cloud platform casing's inner space makes the support be close to cloud platform casing setting more, further reduces the whole height of unmanned aerial vehicle cloud platform.
In addition, the casing is equipped with a plurality of louvres down, for first heat dissipation design, forms the clearance between annular part and the first opening, for second heat dissipation design for outside the heat that each module (for example infrared processing module and transmission module) in the cloud platform casing produced distributes to the cloud platform casing high-efficiently, prevents that operating temperature is too high to lead to damaging the condition emergence of each module.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural view of an unmanned aerial vehicle pan-tilt disclosed in the first embodiment of the present invention;
fig. 2 is a schematic structural diagram of an unmanned aerial vehicle pan-tilt (without an upper shell) disclosed in the first embodiment of the present invention;
fig. 3 is the embodiment of the utility model provides a decomposition structure schematic diagram of unmanned aerial vehicle cloud platform discloses.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the present invention, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings. These terms are used primarily to better describe the invention and its embodiments, and are not intended to limit the indicated devices, elements or components to a particular orientation or to be constructed and operated in a particular orientation.
Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in the present invention can be understood by those of ordinary skill in the art as appropriate.
Furthermore, the terms "mounted," "disposed," "provided," "connected," and "connected" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; can be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements or components. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Furthermore, the terms "first," "second," and the like, are used primarily to distinguish one device, element, or component from another (the specific nature and configuration may be the same or different), and are not used to indicate or imply the relative importance or number of the indicated devices, elements, or components. "plurality" means two or more unless otherwise specified.
The utility model discloses an unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof, because the whole height of unmanned aerial vehicle cloud platform is less, unmanned aerial vehicle can directly place and take off on ground.
Example one
Please refer to fig. 1 to fig. 3 together, which are schematic structural diagrams of an unmanned aerial vehicle cradle head according to an embodiment of the present invention, the unmanned aerial vehicle cloud platform comprises a cloud platform main body 1, a bracket 2 and an infrared camera module 3, wherein the cloud platform main body 1 comprises a cloud platform shell 11, an infrared processing module 12 and a transmission module 13 electrically connected with the infrared processing module 12, the infrared processing module 12 and the transmission module 13 are disposed in the cradle head housing 11, and are disposed at intervals in the projection on the bottom of the cradle head housing 11, the bracket 2 is arranged below the cradle head shell 11, the projection of the bracket 2 on the bottom of the cradle head shell 11 is positioned between the infrared processing module 12 and the transmission module 13, the infrared camera module 3 includes a main housing 31 and an infrared camera 32 disposed on the main housing 31, the main housing 31 is disposed on the bracket 2, and the infrared camera 32 is electrically connected to the infrared processing module 12.
Compare each control module and the processing module of current unmanned aerial vehicle cloud platform and set up between two parties, the whole height that leads to the unmanned aerial vehicle cloud platform is higher, when carrying unmanned aerial vehicle, the height that can appear the unmanned aerial vehicle cloud platform is greater than the length of unmanned aerial vehicle foot rest and leads to unmanned aerial vehicle can't directly place the condition on ground through the foot rest, make unmanned aerial vehicle need the manual undercarriage of holding up when taking off, and the infrared processing module 12 and the transmission module 13 of the unmanned aerial vehicle cloud platform of this application set up at the projection interval of cloud platform casing 11 bottom, and the projection of support 2 in cloud platform casing 11 bottom is located between infrared processing module 12 and the transmission module 13, make cloud platform casing 11's thickness less, and then reduce the whole height of this unmanned aerial vehicle cloud platform, when unmanned aerial vehicle, unmanned aerial vehicle can directly place subaerial, need not.
Specifically, as shown in fig. 2 and fig. 3, the holder housing 11 includes an upper housing 111 and a lower housing 112 connected to form a cavity, the lower housing 112 is provided with a first opening 1a, the bracket 2 is disposed at the first opening 1a, and the infrared processing module 12 and the transmission module 13 are disposed at the lower housing 112 and are respectively located at two sides of the first opening 1 a. What can learn is, this infrared processing module 12 and this output module are located this first opening 1 a's both sides respectively, this first opening 1a is located to this support 2, can make this infrared processing module 12 and this transmission module 13's weight assignable in this support 2's both sides, make the whole focus of this unmanned aerial vehicle cloud platform be close to this cloud platform casing 11's barycenter, thereby the unmanned aerial vehicle of carrying this unmanned aerial vehicle cloud platform can steadily fly, appear rocking and lead to the poor condition of infrared camera 32's formation of image quality when avoiding flying.
In this embodiment, as shown in fig. 2, the lower housing 112 is a convex housing, and includes a first portion 11a, a second portion 11b and a third portion 11c, the second portion 11b and the third portion 11c are respectively disposed at two sides of the first portion 11a, the first opening 1a is disposed at the first portion 11a and is located at a position where the first portion 11a protrudes from the second portion 11b and the third portion 11c, the infrared processing module 12 is disposed at the second portion 11b, and the transmission module 13 is disposed at the third portion 11 c. Specifically, the upper housing 111 is a convex housing corresponding to the lower housing 112, and the first portion 11a, the second portion 11b and the third portion 11c can be integrally formed, so that the production process is simple and the production cost is low.
It can be understood that the infrared processing module 12 is disposed on the second portion 11b, the transmission module 13 is disposed on the third portion 11c, and the first portion 11a is disposed therebetween, the infrared processing module 12 and the transmission module 13 are far away from each other, so that they will not interfere with each other during operation, and the generated heat will not affect each other.
Further, in order to dissipate heat in the receiving cavity to the outside of the cradle head housing 11, a plurality of heat dissipation holes 1b communicating with the receiving cavity are formed in the bottom surface of the lower housing 112. Specifically, some of the heat dissipation holes 1b are disposed corresponding to the transmission module 13 and the infrared processing module 12, and are respectively disposed in the second portion 11b and the third portion 11c, and the remaining heat dissipation holes 1b are disposed in the first portion 11a and located between the second portion 11b and the third portion 11 c. That is to say, the heat generated by the transmission module 13 and the infrared processing module 12 can be dissipated to the outside of the cradle head shell 11 through the heat dissipation holes 1b of the third portion 11c and the heat dissipation holes 1b of the second portion 11b respectively, and can be dissipated to the outside of the cradle head shell 11 through the heat dissipation holes 1b of the first portion 11a, so that the heat dissipation performance of the unmanned aerial vehicle cradle head is better, and the situation of damage caused by overheating during operation can be avoided.
In this embodiment, in order to realize the data transmission and the receipt of unmanned aerial vehicle cloud platform, this unmanned aerial vehicle cloud platform still includes two antennas 4, and two antennas 4 divide and locate this cloud platform casing 11's both sides, and set up down, and two antennas 4 electricity connect in this transmission module 13. Specifically, the two antennas 4 may establish a communication connection with a ground controller of the unmanned aerial vehicle cradle head, so as to receive a control signal sent by the ground controller or transmit image data to the ground controller.
What can learn is that two antennas 4 locate the both sides of cloud platform casing 11, and the weight that can evenly distribute antenna 4 is in the both sides of cloud platform casing 11 for cloud platform casing 11's weight distribution is more balanced, and 11 both sides weight deviations of cloud platform casing are great and lead to the unstable condition of unmanned aerial vehicle flight can not appear. And, two antennas 4 set up downwards, can shorten antenna 4 and ground controller's transmission distance, and this unmanned aerial vehicle cloud platform can avoid antenna 4 to receive unmanned aerial vehicle's signal interference and lead to the condition emergence of transmission inefficacy when carrying unmanned aerial vehicle.
In this embodiment, as shown in fig. 2, in order to make the image quality that infrared camera 32 shot better, this unmanned aerial vehicle cloud platform still includes damper 5, and this damper 5 locates first opening 1a of this lower casing 112, and is located this appearance intracavity, and this support 2 is connected in this damper 5. This unmanned aerial vehicle cloud platform carries when unmanned aerial vehicle takes photo by plane, because unmanned aerial vehicle can produce vibrations when flying, through this damper 5, the vibrations that can avoid unmanned aerial vehicle to produce make support 2 drive infrared camera module 3 and take place vibrations, lead to infrared camera 32 to shoot the blurred condition of image picture and take place.
What can learn, the damper 5 of unmanned aerial vehicle cloud platform of this application is located cloud platform casing 11 holds the intracavity, but make full use of cloud platform casing 11's inner space, avoids damper 5 to expose outside cloud platform casing 11, and can make support 2 more be close to cloud platform casing 11 and set up, reduces the overall height of this unmanned aerial vehicle cloud platform.
Further, referring to fig. 2 and 3 again, the lower case 112 is provided with a plurality of first coupling protrusions 14 adjacent to the first opening 1a, the plurality of first coupling protrusions 14 are arranged in a ring shape along the center of the first opening 1a, the damper assembly 5 includes a ring member 51 and a damper member 52, the ring member 51 is located above the first opening 1a, a heat dissipation gap a is formed between the ring member 51 and the first opening 1a, the ring member 51 is provided with a plurality of second coupling protrusions 51a protruding corresponding to the plurality of first coupling protrusions 14, the damper member 52 is coupled to the first coupling protrusions 14 and the second coupling protrusions 51a, and the bracket 2 is coupled to the ring member 51. Specifically, the number of the first coupling protrusions 14 is 6, and the distance between two adjacent first coupling protrusions 14 is the same, the number of the second coupling protrusions 51a corresponding to the first coupling protrusions 14 is also 6, and the second coupling protrusions are evenly distributed along the circumference of the ring member 51, and the damping member 52 may be a damping ball, and is 6. It is understood that, in other embodiments, the number of the shock absorbing members 52 may be set according to actual conditions, and the number of the first coupling protrusions 14 and the second coupling protrusions 51a may also be set according to actual conditions.
What can learn, the unmanned aerial vehicle cloud platform of this application has dual heat dissipation design, first heavy heat dissipation design is equipped with a plurality of louvres 1b for this bottom surface of inferior valve casing 112, second heavy heat dissipation design forms heat dissipation clearance A for between this annular part 51 and this first opening 1a, the heat accessible that infrared processing module 12 and transmission module 13 during operation that are located this cloud platform casing 11 produced rapidly gives off outside cloud platform casing 11, prevent that operating temperature is too high to lead to damaging the condition emergence of each module.
Still further, in order to realize being connected of this support 2 and this damper 5, this unmanned aerial vehicle cloud platform still includes mount pad 6, and the size of this mount pad 6 matches with the interior ring size of this annular part 51, and this mount pad 6 is located the interior anchor ring of this annular part 51, and this support 2 is connected in this mount pad 6.
In this embodiment, the upper case 111 is provided with a second opening 1c, and the second opening 1c extends upward to form an arc-shaped connecting portion 15. Carry unmanned aerial vehicle when this unmanned aerial vehicle cloud platform is, through this arc connecting portion 15, this cloud platform casing 11 can the laminating connect in this unmanned aerial vehicle's fuselage, thereby reduce the distance between this unmanned aerial vehicle cloud platform and this fuselage, and this unmanned aerial vehicle cloud platform laminating connects in this fuselage, when unmanned aerial vehicle's framework is placed in the ground, because the length of undercarriage is far greater than the distance of unmanned aerial vehicle cloud platform bottom to fuselage, interval certain distance between the bottom of this unmanned aerial vehicle cloud platform and the bottom surface, when preventing unmanned aerial vehicle from taking off, unmanned aerial vehicle cloud platform bottom bumps with ground and leads to damaging the condition emergence of unmanned aerial vehicle cloud platform.
The embodiment of the utility model provides an unmanned aerial vehicle cloud platform locates in the cloud platform casing through infrared processing module and transmission module, and the projection interval in the cloud platform casing sets up, and cloud platform casing below is located to the support, and the projection on the cloud platform casing is located between infrared processing module and the transmission module for the thickness of cloud platform casing is less, thereby reduces the whole height of unmanned aerial vehicle cloud platform.
Further, damper locates the first opening part of casing down, and is located the appearance intracavity that casing and inferior valve body coupling formed, and make full use of cloud platform casing's inner space makes the support be close to cloud platform casing setting more, further reduces the whole height of unmanned aerial vehicle cloud platform.
In addition, the casing is equipped with a plurality of louvres down, for first heat dissipation design, forms the clearance between annular part and the first opening, for second heat dissipation design for outside the heat that each module (for example infrared processing module and transmission module) in the cloud platform casing produced distributes to the cloud platform casing high-efficiently, prevents that operating temperature is too high to lead to damaging the condition emergence of each module.
Example two
The embodiment of the utility model provides an unmanned aerial vehicle, this unmanned aerial vehicle include fuselage and the unmanned aerial vehicle cloud platform of the above-mentioned embodiment one, and this unmanned aerial vehicle cloud platform is connected in this fuselage.
The embodiment of the utility model provides an unmanned aerial vehicle, the whole height of this unmanned aerial vehicle cloud platform that unmanned aerial vehicle carried on is lower, and this unmanned aerial vehicle can place subaerial, takes off the operation, and the unmanned aerial vehicle cloud platform can not bump with ground when taking off.
The unmanned aerial vehicle cradle head and the unmanned aerial vehicle thereof disclosed by the embodiment of the utility model are introduced in detail, the principle and the implementation mode of the utility model are explained by applying an example, and the explanation of the above embodiment is only used for helping to understand the unmanned aerial vehicle cradle head and the unmanned aerial vehicle thereof and the core idea thereof; meanwhile, for the general technical personnel in the field, according to the idea of the present invention, there are changes in the specific implementation and application scope, to sum up, the content of the present specification should not be understood as the limitation of the present invention.
Claims (10)
1. An unmanned aerial vehicle cloud platform, a serial communication port, include
The cradle head main body comprises a cradle head shell, an infrared processing module and a transmission module electrically connected with the infrared processing module, wherein the infrared processing module and the transmission module are arranged in the cradle head shell and are arranged at intervals in the projection on the bottom of the cradle head shell;
the bracket is arranged below the holder shell, and the projection of the bracket on the bottom of the holder shell is positioned between the infrared processing module and the transmission module; and
the infrared camera module comprises a main shell and an infrared camera arranged on the main shell, wherein the main shell is arranged on the support, and the infrared camera is electrically connected with the infrared processing module.
2. The unmanned aerial vehicle holder of claim 1, wherein the holder housing comprises an upper housing and a lower housing connected to form a cavity, the lower housing defines a first opening, the cradle is disposed at the first opening, and the infrared processing module and the transmission module are disposed at the lower housing and located on two sides of the first opening respectively.
3. The unmanned aerial vehicle holder of claim 2, wherein the lower housing is a shell shaped like a Chinese character 'tu', and comprises a first portion, a second portion and a third portion, the second portion and the third portion are respectively disposed on two sides of the first portion, the first opening is disposed on the first portion and is located at a position where the first portion protrudes from the second portion and the third portion, the infrared processing module is disposed on the second portion, and the transmission module is disposed on the third portion.
4. The unmanned aerial vehicle holder of claim 2, wherein the bottom surface of the lower housing is provided with a plurality of heat dissipation holes communicating with the accommodating cavity.
5. An unmanned aerial vehicle holder according to any one of claims 1 to 4, wherein the unmanned aerial vehicle holder further comprises two antennas, the two antennas are respectively disposed on two sides of the holder housing and are disposed downward, and the two antennas are electrically connected to the transmission module.
6. The unmanned aerial vehicle holder of any one of claims 2 to 4, further comprising a shock absorbing assembly disposed at the first opening of the lower housing and located within the cavity, the bracket being connected to the shock absorbing assembly.
7. The unmanned aerial vehicle cloud platform of claim 6, wherein, lower casing is equipped with a plurality of first connection archs adjacent to first opening department arch, and a plurality of first connection archs are arranged along the centre of first opening is cyclic annularly, damper assembly includes annular part and shock attenuation part, annular part is located the first opening top, annular part with form the heat dissipation clearance between the first opening, annular part corresponds a plurality of first connection protruding a plurality of second connection protruding, the shock attenuation part connect in first connection protruding with the second connection protruding, leg joint in annular part.
8. An unmanned aerial vehicle holder as claimed in claim 7, wherein the unmanned aerial vehicle holder further comprises a mounting base, the size of the mounting base matches the size of the inner ring of the annular member, the mounting base is provided on the inner annular surface of the annular member, and the bracket is connected to the mounting base.
9. An unmanned aerial vehicle holder according to any one of claims 2 to 4, wherein the upper housing is provided with a second opening, and the second opening extends upwardly with an arc-shaped connecting portion.
10. An unmanned aerial vehicle comprising a fuselage and an unmanned aerial vehicle head as claimed in any one of claims 1 to 9, the unmanned aerial vehicle head being connected to the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922484749.9U CN211685668U (en) | 2019-12-30 | 2019-12-30 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922484749.9U CN211685668U (en) | 2019-12-30 | 2019-12-30 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof |
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| Publication Number | Publication Date |
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| CN211685668U true CN211685668U (en) | 2020-10-16 |
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| CN201922484749.9U Active CN211685668U (en) | 2019-12-30 | 2019-12-30 | Unmanned aerial vehicle cloud platform and unmanned aerial vehicle thereof |
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| Country | Link |
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| CN (1) | CN211685668U (en) |
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2019
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| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A kind of unmanned aerial vehicle pan tilt and its unmanned aerial vehicle Effective date of registration: 20220718 Granted publication date: 20201016 Pledgee: Guangdong Development Bank Limited by Share Ltd. Guangzhou branch Pledgor: GUANGZHOU KEII ELECTRO OPTICS TECHNOLOGY Co.,Ltd. Registration number: Y2022440000174 |
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Date of cancellation: 20230830 Granted publication date: 20201016 Pledgee: Guangdong Development Bank Limited by Share Ltd. Guangzhou branch Pledgor: GUANGZHOU KEII ELECTRO OPTICS TECHNOLOGY Co.,Ltd. Registration number: Y2022440000174 |
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Denomination of utility model: A drone gimbal and its drone Effective date of registration: 20231117 Granted publication date: 20201016 Pledgee: Guangdong Development Bank Limited by Share Ltd. Guangzhou branch Pledgor: GUANGZHOU KEII ELECTRO OPTICS TECHNOLOGY Co.,Ltd. Registration number: Y2023980065425 |
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