CN211442779U - Unmanned aerial vehicle nacelle and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle nacelle and unmanned aerial vehicle Download PDFInfo
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- CN211442779U CN211442779U CN202020927668.1U CN202020927668U CN211442779U CN 211442779 U CN211442779 U CN 211442779U CN 202020927668 U CN202020927668 U CN 202020927668U CN 211442779 U CN211442779 U CN 211442779U
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Abstract
The application relates to unmanned air vehicle technical field especially relates to an unmanned aerial vehicle nacelle and unmanned aerial vehicle, and the unmanned aerial vehicle nacelle includes: the cabin body is internally provided with a containing space, one end of the cabin body is provided with a cabin door, and the other end of the cabin body is connected to the unmanned aerial vehicle; the cabin door and the cabin body are connected through the connecting component. It is thus clear that the unmanned aerial vehicle nacelle that this application provided has the nacelle of large capacity, can once only transport a plurality of parcels, transports efficiently, and the nacelle can hold the parcel of different sizes, shape, and application scope is wide, and the practicality is extremely strong.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle nacelle and an unmanned aerial vehicle.
Background
With the continuous progress of society, the network retail amount of China is the first world in seven years continuously in 2019, and when air freight is started, the logistics industry enters the air-ground integrated era from the land. However, in the face of rapidly increasing logistics demand, the last kilometer of distribution efficiency has become a cost bottleneck of the logistics industry, the end distribution cost accounts for 30% of the total cost of the logistics industry, a large amount of social resources are consumed in the last kilometer, and for this phenomenon, unmanned aerial vehicle distribution is gradually applied to end distribution.
SUMMERY OF THE UTILITY MODEL
An object of this application is to provide an unmanned aerial vehicle nacelle and unmanned aerial vehicle to solve the adoption supporter that exists to a certain extent and transport the parcel among the prior art, not only inefficiency, and the parcel and the poor technical problem of the matching effect of supporter.
The application provides an unmanned aerial vehicle nacelle, include: the unmanned aerial vehicle comprises a cabin body, a cabin body and a control system, wherein the cabin body is provided with a containing space for containing articles, one end of the cabin body is provided with a cabin door, and the other end of the cabin body is connected to the unmanned aerial vehicle;
a connecting member through which the hatch and the cabin body are connected.
In the above technical solution, further, the accommodating space is a hollow cylindrical structure inside the cabin body, the hatch door is disposed at an opening of the first end of the cabin body, and the hatch door can move relative to the opening of the first end of the cabin body for unloading goods.
In any of the above technical solutions, further, the cabin door includes a first load-bearing door and a second load-bearing door, and the first load-bearing door and the second load-bearing door can move away from or close to each other to expose or close off the first end opening of the cabin.
In any of the above technical solutions, further, a first side wall of the first carrying door is provided with a first connecting groove, and a second side wall of the first carrying door, which is opposite to the first side wall of the first carrying door, is provided with a second connecting groove;
the first side wall of the second bearing door is provided with a third connecting groove, and the second side wall of the second bearing door, which is opposite to the first side wall of the second bearing door, is provided with a fourth connecting groove.
In any of the above technical solutions, further, the door further includes a first elastic member and a second elastic member;
one end of the first elastic piece is connected with the first connecting groove, and the other end of the first elastic piece is connected with the third connecting groove;
one end of the second elastic piece is connected with the second connecting groove, and the other end of the second elastic piece is connected with the fourth connecting groove, so that the first bearing door and the second bearing door always have a movement trend of being close to each other.
In any of the above technical solutions, further, a third side wall of the first loading door, which is located between the first side wall and the second side wall, is provided with a first connection portion;
a second connecting part is arranged on a third side wall of the second bearing door between the first side wall and the second side wall;
the first end of the cabin body is provided with a third connecting portion and a fourth connecting portion, wherein the third connecting portion faces the first connecting portion, and the fourth connecting portion faces the second connecting portion.
In any of the above technical solutions, further, the connecting member includes a first spring pin and a second spring pin;
the first spring pin shaft penetrates through the first connecting part and the third connecting part, a first fixing part is arranged at one end of the first spring pin shaft, and a first locking part is arranged at the other end of the first spring pin shaft;
the second spring pin shaft penetrates through the second connecting portion and the fourth connecting portion, a second fixing piece is arranged at one end of the second spring pin shaft, and a second locking piece is arranged at the other end of the second spring pin shaft.
In any of the above technical solutions, further, the first load-bearing door and the second load-bearing door have a flat plate structure, and a plurality of rib plates are disposed on one sides of the first load-bearing door and the second load-bearing door facing the outside of the cabin.
In any one of the above technical solutions, further, the cabin body and the second end opposite to the first end opening of the cabin body are provided with a limiting part, and the limiting part is used for being connected to the unmanned aerial vehicle.
The application also provides an unmanned aerial vehicle, which comprises the unmanned aerial vehicle nacelle and the nacelle frame in any technical scheme; the fuselage of arranging unmanned aerial vehicle in is erect to the nacelle, and the spacing portion of unmanned aerial vehicle nacelle is connected with the nacelle frame, therefore, the unmanned aerial vehicle that this application provided has all beneficial technological effects of this unmanned aerial vehicle nacelle, here, no longer gives unnecessary details.
Compared with the prior art, the beneficial effect of this application is:
the application provides an unmanned aerial vehicle nacelle includes: the cabin body, hatch door and connecting elements, wherein, the hatch door sets up in a tip of the cabin body, specifically, the hatch door sets up in the bottom opening part of the cabin body, and the hatch door can dismantle with the cabin body through connecting elements and be connected, be convenient for maintain and safeguard, the cabin body with be provided with the relative other end of one end of hatch door, specifically, the top of the cabin body is connected to unmanned aerial vehicle.
The application provides an unmanned aerial vehicle nacelle is in the use, according to different models, the specific size of the cabin body is set for to the bearing capacity of the unmanned aerial vehicle of type, put into the inside of the cabin body with goods (like express delivery parcel) from the top of the cabin body, then start unmanned aerial vehicle, transport the goods to the destination by unmanned aerial vehicle, after arriving the destination, the hatch door is opened, the goods can fall out in can following the cabin body, accomplish unmanned transportation of goods, the hatch door of following is closed, unmanned aerial vehicle and this unmanned aerial vehicle nacelle return and take place.
It is thus clear that the unmanned aerial vehicle nacelle that this application provided has the nacelle of large capacity, can once only transport a plurality of parcels, transports efficiently, and the nacelle can hold the parcel of different sizes, shape, and application scope is wide, and the practicality is extremely strong.
The utility model provides an unmanned aerial vehicle, including the aforesaid unmanned aerial vehicle nacelle, therefore, once only can hold a plurality of parcels through this unmanned aerial vehicle nacelle, show the transportation efficiency that improves the goods, and can avoid the unmanned aerial vehicle flight in-process goods to drop, the condition of losing, have stronger practicality.
Drawings
In order to more clearly illustrate the detailed description of the present application or the technical solutions in the prior art, the drawings needed to be used in the detailed description of the present application or the prior art description will be briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative efforts.
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle pod according to an embodiment of the present application;
fig. 2 is a schematic structural diagram of a cabin of an unmanned aerial vehicle pod according to an embodiment of the present application;
fig. 3 is a schematic structural view of a hatch door of a pod of the unmanned aerial vehicle provided by an embodiment of the present application;
fig. 4 is a schematic structural diagram of a first spring pin of an unmanned aerial vehicle pod according to an embodiment of the present application;
fig. 5 is a schematic structural diagram of a pod rack of a drone provided by an embodiment of the present application.
Reference numerals:
1-cabin body, 101-first end, 102-second end, 103-limiting part, 2-cabin door, 201-first load-bearing door, 202-second load-bearing door, 203-first connecting groove, 204-second connecting groove, 205-third connecting groove, 206-fourth connecting groove, 207-ribbed plate, 3-nacelle frame, 301-sliding rail, 302-fastening piece, 4-first spring pin shaft, 401-first fastening piece, 402-first locking pin, 403-first tension spring, 404-first fastening piece, 5-second spring pin shaft, 6-first connecting part, 7-second connecting part, 8-third connecting part, 10-first elastic part.
Detailed Description
The technical solutions of the present application will be described clearly and completely with reference to the accompanying drawings, and it should be understood that the described embodiments are only some embodiments of the present application, but not all embodiments.
The components of the embodiments of the present application, generally described and illustrated in the figures herein, can be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the present application, presented in the accompanying drawings, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application.
All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
In the description of the present application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present application. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present application, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present application can be understood in a specific case by those of ordinary skill in the art.
The drone pod and drone according to some embodiments of the present application are described below with reference to fig. 1-5.
Referring to fig. 1-5, embodiments of the present application provide a drone pod comprising: the unmanned aerial vehicle comprises a cabin body 1, wherein one end of the cabin body 1 is provided with a cabin door 2, and the other end of the cabin body 1 is connected to the unmanned aerial vehicle; the connecting component, the hatch door 2 and the cabin body 1 are connected through the connecting component.
Further, the cabin body 1 has a hollow cylindrical structure, the hatch 2 is disposed at the opening of the first end 101 of the cabin body 1, and the hatch 2 is movable relative to the opening of the first end 101 of the cabin body 1 for unloading goods.
The application provides an unmanned aerial vehicle nacelle includes: cabin body 1, hatch door 2 and connecting elements, wherein, hatch door 2 sets up in a tip of the cabin body 1, specifically, hatch door 2 sets up in the cabin body 1 according to the bottom opening part under the state shown in fig. 2, and hatch door 2 can dismantle with the cabin body 1 through connecting elements and be connected, the maintenance and the maintenance of being convenient for, the cabin body 1 with be provided with the opposite other end of one end of hatch door 2, specifically, the top of the cabin body 1 according to the state shown in fig. 2 is connected to unmanned aerial vehicle.
The application provides an unmanned aerial vehicle nacelle is in the use, according to different models, the specific size of cabin body 1 is set for to the bearing capacity of the unmanned aerial vehicle of type, put into the inside of cabin body 1 from the top of cabin body 1 with goods (like express delivery parcel), then start unmanned aerial vehicle, transport the goods to the destination by unmanned aerial vehicle, after arriving the destination, hatch door 2 opens, the goods can be followed and fallen out in the cabin body 1, the unmanned transportation of completion goods, hatch door 2 closes afterwards, unmanned aerial vehicle and this unmanned aerial vehicle nacelle return and take place.
It is thus clear that the unmanned aerial vehicle nacelle that this application provided has the nacelle of large capacity, can once only transport a plurality of parcels, transports efficiently, and the nacelle can hold the parcel of different sizes, shape, and application scope is wide, and the practicality is extremely strong.
In one embodiment of the present application, preferably, as shown in fig. 1 to 3, the hatch door 2 comprises a first load-bearing door 201 and a second load-bearing door 202, the first load-bearing door 201 and the second load-bearing door 202 being movable away from or towards each other to expose or close the opening of the first end 101 of the cabin 1.
In this embodiment, the first load-bearing door 201 and the second load-bearing door 202 are symmetrically disposed and slidably connected to the edge of the first end 101 of the cabin body 1, when the two doors gradually move away from each other until the cabin door 2 is completely opened, the cargo in the cabin body 1 can fall out, and when the two doors gradually move close to each other until the cabin door 2 is closed, the cargo can be loaded on the load-bearing surface inside the cabin body 1, it should be noted that the cabin door 2 is provided with a switch for controlling the cabin door 2 to be opened and closed, the switch may be an electromagnet in a specific form, and of course, without being limited thereto, the electromagnet is powered on or off to control the opening and closing processes of the cabin door 2.
In one embodiment of the present application, preferably, as shown in fig. 1 to 3, a first side wall of the first load door 201 is provided with a first connection groove 203, and a second side wall of the first load door 201 opposite to the first side wall of the first load door 201 is provided with a second connection groove 204;
a first sidewall of the second load door 202 is provided with a third coupling groove 205, and a second sidewall of the second load door 202 opposite to the first sidewall of the second load door 202 is provided with a fourth coupling groove 206.
Further, the door 2 also comprises a first elastic element 10 and a second elastic element;
one end of the first elastic member 10 is connected to the first connection groove 203, and the other end of the first elastic member 10 is connected to the third connection groove 205;
one end of the second elastic member is connected to the second connection groove 204, and the other end of the second elastic member is connected to the fourth connection groove 206, so that the first load-bearing door 201 and the second load-bearing door 202 always have a movement tendency close to each other.
In this embodiment, the first elastic member 10 and the second elastic member may be tension springs, one end of the first connecting groove 203 far from the third connecting groove 205 is provided with a first fixing portion, one end of the third connecting groove 205 far from the first connecting groove 203 is provided with a second fixing portion, one end of the first elastic member 10 is connected to the first fixing portion, the other end of the first elastic member 10 is connected to the second fixing portion, one end of the second connecting groove 204 far from the fourth connecting groove 206 is provided with a third fixing portion, one end of the fourth connecting groove 206 far from the second connecting groove 204 is provided with a fourth fixing portion, one end of the second elastic member is connected to the third fixing portion, the other end of the second elastic member is connected to the fourth fixing portion, and the first elastic member 10 and the second elastic member are always in a stretched state, so that the first load door 201 and the second load door 202 always have a tendency to move close to each other without the action of a third party's force applying component, avoid unmanned aerial vehicle to open at flight in-process hatch door 2 unusually, lead to the goods to drop and lose, and first connecting groove 203 is "one" style of calligraphy with third connecting groove 205 and arranges, second connecting groove 204 is "one" style of calligraphy with fourth connecting groove 206 and arranges, can form accommodation space respectively in order to hold first elastic component 10 and second elastic component on the one hand, on the other hand can also play the direction to first elastic component 10 and second elastic component, the effect of support.
In one embodiment of the present application, preferably, as shown in fig. 1 to 4, a third side wall between the first side wall and the second side wall of the first carrying door 201 is provided with the first connection portion 6, and the third side wall of the first carrying door 201 is provided at an opposite side of the first carrying door 201 from the second carrying door 202;
a second connection portion 7 is disposed at a third sidewall between the first sidewall and the second sidewall of the second carrying door 202, and the third sidewall of the second carrying door 202 is disposed at an opposite side of the second carrying door 202 from the first carrying door 201;
the first end 101 of the cabin 1 is provided with a third connection portion 8 and a fourth connection portion, wherein the third connection portion 8 is arranged facing the first connection portion 6 and the fourth connection portion is arranged facing the second connection portion 7.
Further, the connecting member comprises a first spring pin 4 and a second spring pin 5;
the first spring pin shaft 4 penetrates through the first connecting part 6 and the third connecting part 8, one end of the first spring pin shaft 4 is provided with a first fixing part 404, and the other end of the first spring pin shaft 4 is provided with a first locking part 401;
the second spring pin shaft 5 penetrates through the second connecting portion 7 and the fourth connecting portion, a second fixing piece is arranged at one end of the second spring pin shaft 5, and a second locking piece is arranged at the other end of the second spring pin shaft 5.
In this embodiment, the first connecting portion 6 is provided with a first through hole, the third connecting portion 8 is provided with a second through hole, the first through hole is communicated with the second through hole, the first spring pin 4 comprises a first locking pin 402 and a first tension spring 403 sleeved on the first locking pin 402, one end of the first spring pin 4 penetrates through the first through hole and the second through hole in sequence and then is locked by a first locking member 401, the first locking member 401 can be a pin cap, the pin cap and the first locking pin 402 can be in threaded connection, one end of the first locking pin 402 far away from the pin cap is provided with a first fixing member 404, the first fixing member 404 has a metal sheet structure, the surface area of the metal sheet structure is larger than the area of the first through hole/the second through hole, so that the first spring pin 4 penetrates through the first through hole and the second through hole and is locked by the pin cap, at this time, the first tension spring 403 is in a light-weight compression state, and in the same way, the second spring pin 5 is arranged in the same way as the, do not do too much and describe, setting through first spring pin axle 4 and second spring pin axle 5, can lock hatch door 2 and cabin body 1 along with unmanned aerial vehicle flight in-process at this unmanned aerial vehicle nacelle, avoid opening unusually at flight in-process hatch door 2 and lead to the goods to drop, lose, can also strengthen the location effect between hatch door 2 and the cabin body 1, compensate cabin body 1 to a certain extent, the surplus is rocked to hatch door 2, avoid rocking or cabin body 1 in cabin body 1 at flight in-process goods, the stationarity that directly influences the flight of unmanned aerial vehicle is rocked in the emergence of hatch door 2.
In one embodiment of the present application, preferably, as shown in fig. 1 to 3, the first and second load-bearing doors 201 and 202 have a flat plate structure, and a plurality of ribs 207 are provided on the sides of the first and second load-bearing doors 201 and 202 facing the outside of the cabin 1.
In this embodiment, a plurality of ribs 207 are disposed on the outer side surfaces of the first load-bearing door 201 and the second load-bearing door 202, a plurality of the ribs 207 are disposed at intervals along a first direction, another plurality of the ribs 207 are disposed at intervals along a second direction, and the first direction can be perpendicular to the second direction, so that the first load-bearing door 201 and the second load-bearing door 202 can have a strong load-bearing capacity without being too thick, and the weight of the cabin door 2 is reduced as much as possible on the premise of ensuring the load-bearing capacity.
In one embodiment of the application, preferably, as shown in fig. 1 and 5, the opening of the second end 102 of the nacelle 1 opposite to the opening of the first end 101 of the nacelle 1 is used for loading cargo, and the second end 102 of the nacelle 1 is provided with a limiting portion 103, the limiting portion 103 being used for connecting to a drone.
In this embodiment, the opening of the second end 102 of the cabin 1, that is, the upper end of the cabin 1 in the state shown in fig. 2, is provided with a limiting portion 103, the limiting portion 103 protrudes outward from the edge of the port of the second end 102 of the cabin 1, the connection portion of the unmanned aerial vehicle with the cabin 1, such as a nacelle frame 3 described below, is formed with a slide rail 301, the limiting portion 103 can be slidably connected to the slide rail 301, during this process, the slide rail 301 plays a good guiding role, and the protrusion can be set on the slide rail 301, after the protrusion is assembled with the slide rail 301, the cabin 1 and the nacelle frame 3 are locked by a fastener 302, so that the unmanned aerial vehicle nacelle can fly together with the unmanned aerial vehicle, and simultaneously the cabin 1 is prevented from falling off during the flight of the unmanned aerial vehicle, wherein the fastener 302 can be a common screw or bolt, preferably, the fastener 302 selected in this embodiment has the same structure as the first spring pin 4/, can enough lock cabin body 1 and nacelle frame 3, can also improve the stability of unmanned aerial vehicle flight in-process, and the opening of the second end 102 of the cabin body 1 is provided with the apron, the apron can be dismantled with the cabin body 1 and be connected, if sliding connection, fastener are connected etc. of course, the apron also can set up in nacelle frame 3, the apron can cover the second end 102 opening of the cabin body 1 when this unmanned aerial vehicle nacelle flies along with unmanned aerial vehicle, can avoid the goods impaired at special weather such as sleet.
Embodiments of the present application further provide an unmanned aerial vehicle (not shown in the figures), including the unmanned aerial vehicle pod and pod rack described in any of the above embodiments; the fuselage of placing unmanned aerial vehicle in is erect to the nacelle, and the spacing portion of unmanned aerial vehicle nacelle is connected with the nacelle frame, specifically, and accessible fasteners such as fastener can dismantle the connection between spacing portion and the nacelle frame, therefore, the unmanned aerial vehicle that this application provided has all beneficial technological effects of this unmanned aerial vehicle nacelle, here, no longer gives unnecessary details.
Finally, it should be noted that: the above embodiments are only used for illustrating the technical solutions of the present application, and not for limiting the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present application.
Claims (10)
1. An unmanned aerial vehicle pod, comprising:
the cabin body is provided with a containing space for containing articles, one end of the cabin body is provided with a cabin door, and the other end of the cabin body is connected to the unmanned aerial vehicle;
a connecting member through which the hatch and the cabin body are connected.
2. The unmanned aerial vehicle pod of claim 1 wherein the receiving space is an internally hollow cylindrical structure, the door being disposed at an opening at the first end of the body, the door being movable relative to the opening at the first end of the body for unloading cargo.
3. The drone pod of claim 2 wherein the door includes a first load door and a second load door that are movable away from or toward each other to expose or block the first end opening of the pod.
4. The unmanned aerial vehicle pod of claim 3 wherein a first side wall of the first load door is provided with a first attachment slot, and a second side wall of the first load door opposite the first side wall of the first load door is provided with a second attachment slot;
the first side wall of the second bearing door is provided with a third connecting groove, and the second side wall of the second bearing door, which is opposite to the first side wall of the second bearing door, is provided with a fourth connecting groove.
5. The drone pod of claim 4 wherein the door further comprises a first resilient member and a second resilient member;
one end of the first elastic piece is connected with the first connecting groove, and the other end of the first elastic piece is connected with the third connecting groove;
one end of the second elastic piece is connected with the second connecting groove, and the other end of the second elastic piece is connected with the fourth connecting groove, so that the first bearing door and the second bearing door always have a movement trend of being close to each other.
6. The unmanned aerial vehicle pod of claim 4 wherein a third side wall of the first load door between the first side wall and the second side wall is provided with a first connection;
a second connecting part is arranged on a third side wall of the second bearing door between the first side wall and the second side wall;
the first end of the cabin body is provided with a third connecting portion and a fourth connecting portion, wherein the third connecting portion faces the first connecting portion, and the fourth connecting portion faces the second connecting portion.
7. The unmanned aerial vehicle pod of claim 6, wherein the connection member comprises a first spring pin and a second spring pin;
the first spring pin shaft penetrates through the first connecting part and the third connecting part, a first fixing part is arranged at one end of the first spring pin shaft, and a first locking part is arranged at the other end of the first spring pin shaft;
the second spring pin shaft penetrates through the second connecting portion and the fourth connecting portion, a second fixing piece is arranged at one end of the second spring pin shaft, and a second locking piece is arranged at the other end of the second spring pin shaft.
8. The drone pod of claim 3 wherein the first and second load doors have a flat panel construction and a plurality of ribs are provided on a side of the first and second load doors facing the exterior of the nacelle.
9. The drone pod of any one of claims 1 to 7 wherein a second end of the nacelle body opposite the first end opening of the nacelle body is provided with a stop portion for connection to the drone.
10. An unmanned aerial vehicle comprising a pod rack and the unmanned aerial vehicle pod of any of claims 1 to 9; the pod frame is arranged on the unmanned aerial vehicle body, and the limiting part of the unmanned aerial vehicle pod is connected with the pod frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020927668.1U CN211442779U (en) | 2020-05-28 | 2020-05-28 | Unmanned aerial vehicle nacelle and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020927668.1U CN211442779U (en) | 2020-05-28 | 2020-05-28 | Unmanned aerial vehicle nacelle and unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN211442779U true CN211442779U (en) | 2020-09-08 |
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| CN202020927668.1U Active CN211442779U (en) | 2020-05-28 | 2020-05-28 | Unmanned aerial vehicle nacelle and unmanned aerial vehicle |
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