CN108750115A - Unmanned aerial vehicle puts in device - Google Patents
Unmanned aerial vehicle puts in device Download PDFInfo
- Publication number
- CN108750115A CN108750115A CN201810704163.6A CN201810704163A CN108750115A CN 108750115 A CN108750115 A CN 108750115A CN 201810704163 A CN201810704163 A CN 201810704163A CN 108750115 A CN108750115 A CN 108750115A
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- side plate
- bottom plate
- plate
- storage tank
- movable part
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- 230000008878 coupling Effects 0.000 abstract 2
- 238000010168 coupling process Methods 0.000 abstract 2
- 238000005859 coupling reaction Methods 0.000 abstract 2
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000004308 accommodation Effects 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Warehouses Or Storage Devices (AREA)
Abstract
The invention relates to an unmanned aerial vehicle throwing device, and relates to the field of unmanned aerial vehicles. The unmanned aerial vehicle is simple in structure, light in weight, easy to control and strong in reliability. The main technical scheme adopted is as follows: unmanned aerial vehicle puts in device, it includes moving part, storage tank and sets up the first coupling mechanism on the storage tank, and first coupling mechanism is used for being connected to unmanned aerial vehicle with the storage tank on. The storage box comprises a top plate, a bottom plate and side plates; the side plates comprise a first side plate, a second side plate, a third side plate and a fourth side plate which are sequentially arranged along the circumferential direction; the bottom plate comprises a first bottom plate and a second bottom plate, and one end of the first bottom plate is connected with one end of the second bottom plate through a rotating shaft; the movable piece is connected with the rotating shaft and connected with the first side plate and the third side plate through a second connecting mechanism so as to drive the first bottom plate, the second bottom plate, the first side plate and the third side plate to move during movement; the movable piece is used for closing the storage box when moving to the first position; and opening the storage compartment when moved to the second position.
Description
Technical field
The present invention relates to air vehicle technique fields, more particularly to a kind of unmanned plane delivery device.
Background technology
Unmanned plane can be used for the regional air-dropped material reached of earthward having inconvenient traffic, and there has been no molding unmanned planes at present
Throwing mechanism occurs on the market, if the existing throwing mechanism for other field is mounted on unmanned plane, due to this
The structure of class throwing mechanism is excessively complicated, and overall weight is excessive, can increase the load of unmanned plane, cause the loading capacity of unmanned plane by
It to seriously affecting, eventually leads to UAV flight's ability and is greatly reduced, more useful goods and materials, therefore, design one can not be launched
Kind is simple in structure, and weight is light, easily controllable, and highly reliable unmanned plane throwing mechanism is very necessary.
Therefore, it is necessary to provide a kind of new technical solution to overcome drawbacks described above.
Invention content
In view of this, the present invention provides a kind of unmanned plane delivery device that can effectively solve above-mentioned technical problem.
In order to achieve the above objectives, present invention generally provides following technical solutions：
The embodiment of the present invention provides a kind of unmanned plane delivery device comprising movable part, for driving the movable part
Driving mechanism, storage tank and the first bindiny mechanism being arranged on the storage tank of movement, first bindiny mechanism are used for
The storage tank is connected on unmanned plane；
The storage tank includes top plate and bottom plate and the side plate；The side plate includes arranging successively along the circumferential direction of storage tank
The first side plate, the second side plate, third side plate and the 4th side plate, and the first side plate is opposite with third side plate, the second side plate and
Four side plates are opposite；First side plate and the third side plate are connect with the top panel turns；
The bottom plate includes the first bottom plate and the second bottom plate, and the first bottom plate in the two is close to the first side plate, the second bottom
Plate is connect with one end of second bottom plate by shaft close to the third side plate, one end of first bottom plate；
The movable part connect with the shaft and is connected by the second bindiny mechanism and first side plate and third side plate
It connects, to drive first bottom plate, the second bottom plate, the first side plate and third side plate to move during exercise；
Wherein, the movable part is for when moving to first position, making the other end and described first of first bottom plate
Side plate offsets and the other end of second bottom plate offsets with the third side plate, to be closed the storage tank；With move to
When two positions, the other end of the other end and the second bottom plate that make the first bottom plate tilts down and first side plate and third
Side plate is flared out, to form the outlet of the first goods and materials between first side plate and first bottom plate and described the
The outlet of the second goods and materials is formed between three side plates and second bottom plate.
By above-mentioned technical proposal, unmanned plane delivery device of the present invention at least has the advantages that：
In technical solution provided by the invention, unmanned plane delivery device of the present invention is simple in structure, easy to use, and matter
It measures light, the load of unmanned plane will not be increased so that the larger goods and materials of quality can be carried, while its is easy to operate, Ke Yifang
Just by goods and materials launch lower section, be not in the phenomenon that gets stuck so that goods and materials launch it is more convenient.
Above description is only the general introduction of technical solution of the present invention, in order to better understand the technical means of the present invention,
And can be implemented in accordance with the contents of the specification, below with presently preferred embodiments of the present invention and after coordinating attached drawing to be described in detail such as.
Description of the drawings
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technology description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with
The structure shown according to these attached drawings obtains other attached drawings.
Fig. 1 is structural representation when a kind of storage tank for unmanned plane delivery device that one embodiment of the invention provides is closed
Figure；
Fig. 2 is structural representation when a kind of storage tank for unmanned plane delivery device that one embodiment of the invention provides is opened
Figure；
Fig. 3 is a kind of shaft and the second side plate, the dress of the 4th side plate and movable part that one embodiment of the invention provides
Distribution structure schematic diagram.
Reference numeral：1, movable part；101, via；2, driving cylinder；3, storage tank；31, top plate；32, bottom plate；321, first
Bottom plate；322, the second bottom plate；331, the first side plate；332, the second side plate；333, third side plate；334, the 4th side plate；4, turn
Axis；5, fixed frame；51, first support；52, second support；53, third holder；6, card slot；71, first connecting rod；72, second connects
Bar；73, third connecting rod；74, fourth link；8, spacing block set；10, the first goods and materials export；20, the second goods and materials export；30, it accommodates
Space；3311, the first hook；3331, the second hook；3321, the first sliding groove；3341, second sliding slot；100, unmanned plane launches dress
It sets.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiment is only a part of the embodiment of the present invention, instead of all the embodiments.Base
Embodiment in the present invention, those of ordinary skill in the art obtained without creative efforts it is all its
His embodiment, shall fall within the protection scope of the present invention.
If it is to be appreciated that related in the embodiment of the present invention directionality instruction (such as up, down, left, right, before and after ...),
Then directionality instruction be only used for explaining relative position relation under a certain particular pose (as shown in the picture) between each component,
Motion conditions etc., if the particular pose changes, directionality instruction also correspondingly changes correspondingly.
If in addition, relating to the description of " first ", " second " etc. in the embodiment of the present invention, it is somebody's turn to do " first ", " second " etc.
Description be used for description purposes only, be not understood to indicate or imply its relative importance or implicitly indicate indicated skill
The quantity of art feature." first " is defined as a result, the feature of " second " can explicitly or implicitly include at least one spy
Sign.In addition, the technical solution between each embodiment can be combined with each other, but must be with those of ordinary skill in the art's energy
It is enough realize based on, when the knot that conflicting or cannot achieve when will be understood that this technical solution occurs in the combination of technical solution
Conjunction is not present, also not the present invention claims protection domain within.
As depicted in figs. 1 and 2, a kind of unmanned plane delivery device 100 that one embodiment of the present of invention proposes comprising living
Moving part 1, driving mechanism, storage tank 3 and the first bindiny mechanism.Driving mechanism is connect with movable part 1, to drive movable part 1 to move.
First bindiny mechanism is arranged on storage tank 3.First bindiny mechanism is used to storage tank 3 being connected to unmanned plane, makes unmanned plane
The flight of storage tank 3 can be carried.
Storage tank 3 includes top plate 31, bottom plate 32 and side plate.Side plate include along storage tank 3 circumferential direction arrange successively first
Side plate 331, the second side plate 332, third side plate 333 and the 4th side plate 334.First side plate 331 is opposite with third side plate 333, the
Two side plates 332 and the 4th side plate 334 are opposite.Preferably, storage tank 3 is in cube structure.
First side plate 331 and third side plate 333 are rotatablely connected with top plate 31, are opened and closed with opposite top plate 31.Bottom
Plate 32 includes the first bottom plate 321 and the second bottom plate 322, and the first bottom plate 321 in the two is close to the first side plate 331, the second bottom
Plate 322 is close to third side plate 333.One end of first bottom plate 32 is connect with one end of the second bottom plate 322 by shaft 4.
Movable part 1 connect with shaft 4 and is connect with the first side plate 331 and third side plate 333 by the second bindiny mechanism,
To drive the first bottom plate 321, the second bottom plate 322, the first side plate 331 and third side plate 333 to move during exercise.
Wherein, movable part 1 is for when moving to first position, making the other end and 331 phase of the first side plate of the first bottom plate 321
It supports and the other end of the second bottom plate 322 offsets with third side plate 333, to be closed storage tank 3 (as shown in Figure 1)；With move to
When two positions, the other end of the other end and the second bottom plate 322 that make the first bottom plate 321 tilts down and the first side plate 331
Be flared out with third side plate 333, with formed between the first side plate 331 and the first bottom plate 321 first goods and materials outlet 10,
And the second goods and materials are formed between third side plate 333 and the second bottom plate 322 and export 20 (as shown in Figure 2).
As shown in Fig. 2, when moving to the second position due to movable part 1, the first bottom plate 321 and the second bottom plate 322 are in incline
It is ramp-like, to which the goods and materials on the first bottom plate 321 and the second bottom plate 322 can be slided along corresponding bottom plate under gravity,
And it is skidded off from the outlet of corresponding goods and materials.
In order to reduce frictional resistance of the goods and materials on the first bottom plate 321 and the second bottom plate 322, it is preferred that the first bottom plate 321
It can be embedded with ball on the second bottom plate 322.
In the technical solution of above-mentioned offer, driving mechanism can drive movable part 1 to move, and movable part 1 drives the first bottom
Plate 321, the second bottom plate 322, the first side plate 331 and third side plate 333 move, and to open and close storage tank 3, control phase
It is easy to operate to more convenient.
Further, as depicted in figs. 1 and 2, the first bindiny mechanism above-mentioned may include fixed frame 5 and be arranged in fixation
Card slot 6 on frame 5.Fixed frame 5 is arranged on the top plate 31 of storage tank 3.Card slot 6 be located at fixed frame 5 away from the one of top plate 31
Side.Storage tank 3 is connected on unmanned plane by the first bindiny mechanism by card slot 6 and snapping connection on unmanned plane.In order to carry
The connective stability of high unmanned plane and both storage tanks 3, it is preferred that above-mentioned card slot 6, which can be dovetail groove etc., has limit effect
The slot of fruit.
As depicted in figs. 1 and 2, driving mechanism above-mentioned may include driving cylinder 2.Driving cylinder 2 is arranged on fixed frame 5.
Driving cylinder 2 is connect with movable part 1, to drive movable part 1 to move to first position and the second position above-mentioned.
Above-mentioned driving cylinder 2 can be cylinder or hydraulic cylinder etc..
The quantity of driving cylinder 2 can be single or multiple, in order to mitigate the load of unmanned plane, it is preferred that the number of driving cylinder 2
Amount is one.
Further, as depicted in figs. 1 and 2, fixed frame 5 above-mentioned may include sequentially connected first support 51,
Two holders 52 and third holder 53.The first connecting portion away from one end of second support 52 and 31 upper end of top plate of first support 51
Connection.Third holder 53 is connect with the second connecting portion of 31 upper end of top plate away from one end of second support 52.First support
51, accommodation space 30 is formed between second support 52, third holder 53 and top plate 31.Driving cylinder 2 above-mentioned, which is located at, accommodates sky
Between in 30 and be arranged in second support 52.One end of aforementioned active part 1 is connect with the piston rod of driving cylinder 2, and the other end passes through
It top plate 31 and is connect with shaft 4.Wherein, when driving cylinder 2 drives movable part 1 to move, movable part 1 drives the first bottom by shaft 4
Plate 321 and the movement of the second bottom plate 322, to open and close storage tank 3.
Further, as depicted in figs. 1 and 2, spacing block set 8 can be equipped on movable part 1 above-mentioned.Spacing block set 8
In in accommodation space 30.Spacing block set 8 is used for inconsistent and in activity with top plate 31 when movable part 1 moves to first position
Part 1 moves to inconsistent with the cylinder body of driving cylinder 2 when the second position.In this example, by the spacing block set of setting 8, make work
Moving part 1 can only move between the first position and the second position, prevent movable part 1 from leading to storage tank beyond preset stroke range
3 cannot normally open and close.
Further, as shown in figure 3, movable part above-mentioned 1 can be in rod-shaped.Movable part 1 away from spacing block set 8
One end is equipped with the via 101 passed through for shaft 4.Movable part 1 is connect by the via 101 with shaft 4.Specifically, shaft 4 is logical
It crosses above-mentioned via 101 to be rotatablely connected with movable part 1, to reduce the stress concentration of shaft 4 and 1 junction of movable part.
Further, as depicted in figs. 1 and 2, the second bindiny mechanism above-mentioned may include first connecting rod 71, second connecting rod
72, third connecting rod 73 and fourth link 74.One end of first connecting rod 71 is rotatablely connected with movable part 1, first connecting rod 71 it is another
End and one end of second connecting rod 72 are rotatablely connected.One end of the other end of second connecting rod 72 and the first side plate 331 is rotatablely connected, the
Side plate 331 is rotatablely connected by its middle part and one end of top plate 31.In this example, movable part 1, first connecting rod 71, second
Connecting rod 72 and the first side plate 331 form slider-crank mechanism, and movable part 1 drives when moving along a straight line under the driving of driving cylinder 2
First side plate 331 rotates, to open and close storage tank 3.
As depicted in figs. 1 and 2, one end of aforementioned third connecting rod 73 and movable part 1 are rotatablely connected, third connecting rod 73 it is another
End and one end of fourth link 74 are rotatablely connected, and the other end of fourth link 74 is rotatablely connected with one end of third side plate 333.
Third side plate 333 is rotatablely connected by its middle part and the other end of top plate 31.Likewise, in this example, movable part 1, third connect
Bar 73, fourth link 74 and third side plate 333 form another slider-crank mechanism, and movable part 1 is straight under the driving of driving cylinder 2
Third side plate 333 is driven to rotate when line moves, to open and close storage tank 3.
Preferably, as depicted in figs. 1 and 2, one end of aforementioned first connecting rod 71 and one end of third connecting rod 73 are both connected to
On spacing block set 8, to be connect with movable part 1 by spacing block set 8.
Further, as depicted in figs. 1 and 2, aforementioned first side plate 331 has the close to one end of the first bottom plate 321
One hook 3311, to catch on the first bottom plate 321 when movable part 1 moves to first position.In this example, pass through the of setting
One hook 3311 can be such that both the first side plate 331 and the first bottom plate 321 is closed more tight and stable.
Likewise, as depicted in figs. 1 and 2, aforementioned third side plate 333 has second close to one end of the second bottom plate 322
Hook 3331, to catch on the second bottom plate 322 when movable part 1 moves to first position.Wherein, pass through the second hook of setting
3331, both third side plate 333 and the second bottom plate 322 can be made to be closed more tight and stable.
Further, as shown in figure 3, the first sliding groove 3321 can be equipped on the second side plate 332 above-mentioned.4th side plate
334 are equipped with second sliding slot 3341.One end of shaft 4 is assemblied in the first sliding groove 3321, and the other end is assemblied in second sliding slot
In 3341, to be moved along the first sliding groove 3321 and second sliding slot 3341 under the drive of movable part 1.In this example, by setting
The first sliding groove 3321 and second sliding slot 3341 set are capable of the sports limiting and guiding of countershaft 4, improve shaft 4 in movable part 1
Drive the lower stability moved.
Further, 321 and second bottom plate 322 of the first bottom plate above-mentioned with the second side plate 332 and the 4th side plate 334
It is slidably matched, is slided with the second, opposite, side plate 332 under the drive of movable part 1 and the 4th side plate 334.Specifically, the first bottom
Plate 321 is slidably matched close to the side of the second side plate 332 and the second side plate 332, and the first bottom plate 321 is close to the 4th side plate 334
Side is slidably matched with the 4th side plate 334, and both the second side plate 332 and the 4th side plate 334 can be to the movements of the first bottom plate 321
Limit makes the first bottom plate 321 open and close storage tank 3.Likewise, the second bottom plate 322 close to the side of the second side plate 332 with
Second side plate 332 is slidably matched, and the second bottom plate 322 is slidably matched close to the side of the 4th side plate 334 with the 4th side plate 334, the
Both two side plates 332 and the 4th side plate 334 can be such that the second bottom plate 322 opens and closes the sports limiting of the second bottom plate 322
Storage tank 3.
The operation principle of above-mentioned unmanned plane delivery device 100 is specifically described below：It is first turned on storage tank 3, it will
It needs the goods and materials transported to be attached in storage tank 3, is then closed storage tank 3, is blocked storage tank 3 by the card slot 6 on fixed frame 5
It connects fixed on unmanned plane.Unmanned plane carries the flight of storage tank 3 to required position.Then start driving cylinder 2, driving cylinder 2 drives
Movable part 1 moves to the second position from first position, and movable part 1 drives the first bottom plate 321 and the second bottom plate 322 by shaft 4
It tilts down, while movable part 1 drives first by first connecting rod 71, second connecting rod 72, third connecting rod 73 and fourth link 74
Side plate 331 and third side plate 333 are flared out, and the goods and materials in storage tank 3 are under the effect of gravity along 321 He of the first bottom plate
First goods and materials outlet 10 and third side plate 333 and second of second bottom plate 322 between the first side plate 331 and the first bottom plate 321
20 outflow of the second goods and materials outlet between bottom plate 322.After goods and materials are launched, driving cylinder 2 drives movable part 1 to be transported from the second position
It moves to first position, makes that the first side plate 331 offsets with the first bottom plate 321 and third side plate 333 offsets with the second bottom plate 322, with
It is closed storage tank 3.Then unmanned plane carries empty van and returns.
The foregoing is merely the preferred embodiment of the present invention, are not intended to limit the scope of the invention, every at this
Under the inventive concept of invention, using equivalent structure transformation made by description of the invention and accompanying drawing content, or directly/use indirectly
In the scope of patent protection that other related technical areas are included in the present invention.
Claims (1)
1. a kind of unmanned plane delivery device, which is characterized in that including movable part (1), for driving the movable part (1) to move
Driving mechanism, storage tank (3) and the first bindiny mechanism being arranged on the storage tank (3), first bindiny mechanism are used for
The storage tank (3) is connected on unmanned plane；
The storage tank (3) includes top plate (31), bottom plate (32) and the side plate；The side plate includes the week along storage tank (3)
To the first side plate (331), the second side plate (332), third side plate (333) and the 4th side plate (334) arranged successively, and the first side
Relatively with third side plate (333), the second side plate (332) is opposite with the 4th side plate (334) for plate (331)；First side plate (331)
It is rotatablely connected with the top plate (31) with the third side plate (333)；
The bottom plate (32) includes the first bottom plate (321) and the second bottom plate (322), and the first bottom plate (321) in the two is close
First side plate (331), the second bottom plate (322) are close to the third side plate (333), one end of first bottom plate (321) and institute
The one end for stating the second bottom plate (322) is connected by shaft (4)；
The movable part (1) connect with the shaft (4) and by the second bindiny mechanism and first side plate (331) and the
Three side plates (333) connect, with drive during exercise first bottom plate (321), the second bottom plate (322), the first side plate (331) and
Third side plate (333) moves；
Wherein, the movable part (1) for when moving to first position, make the other end of first bottom plate (321) with it is described
First side plate (331) offsets and the other end of second bottom plate (322) offsets with the third side plate (333), to be closed
State storage tank (3)；When with moving to the second position, make the other end of the other end and the second bottom plate (322) of the first bottom plate (321)
It tilts down and first side plate (331) and third side plate (333) is flared out, in first side plate (331)
The first goods and materials outlet (10) is formed between first bottom plate (321) and in the third side plate (333) and second bottom
The second goods and materials outlet (20) is formed between plate (322).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810704163.6A CN108750115B (en) | 2018-07-01 | 2018-07-01 | Unmanned aerial vehicle puts in device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810704163.6A CN108750115B (en) | 2018-07-01 | 2018-07-01 | Unmanned aerial vehicle puts in device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108750115A true CN108750115A (en) | 2018-11-06 |
| CN108750115B CN108750115B (en) | 2021-05-25 |
Family
ID=63975307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810704163.6A Active CN108750115B (en) | 2018-07-01 | 2018-07-01 | Unmanned aerial vehicle puts in device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108750115B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111629964A (en) * | 2018-12-27 | 2020-09-04 | 乐天株式会社 | Unmanned plane |
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| US20160260207A1 (en) * | 2012-07-05 | 2016-09-08 | Bernard Fryshman | Object image recognition and instant active response with enhanced application and utility |
| CN206218234U (en) * | 2016-11-15 | 2017-06-06 | 北京元一创智无人机科技有限责任公司 | A kind of multi-direction magnet handling module of straight-line |
| CN206288242U (en) * | 2016-12-27 | 2017-06-30 | 西南交通大学 | A kind of unmanned plane cargo gear, control system and its unmanned plane |
| CN206561434U (en) * | 2017-02-21 | 2017-10-17 | 深圳市瑞象科技有限公司 | The carry gripper equipment of unmanned plane |
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2018
- 2018-07-01 CN CN201810704163.6A patent/CN108750115B/en active Active
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9399295B2 (en) * | 2012-03-19 | 2016-07-26 | Macdonald, Dettwiler And Associates Inc. | Spacecraft capture mechanism |
| US20160260207A1 (en) * | 2012-07-05 | 2016-09-08 | Bernard Fryshman | Object image recognition and instant active response with enhanced application and utility |
| CN105799923A (en) * | 2016-04-28 | 2016-07-27 | 南京信息工程大学 | Four-rotor aircraft-based carrying manipulator |
| CN206218234U (en) * | 2016-11-15 | 2017-06-06 | 北京元一创智无人机科技有限责任公司 | A kind of multi-direction magnet handling module of straight-line |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111629964A (en) * | 2018-12-27 | 2020-09-04 | 乐天株式会社 | Unmanned plane |
| CN111629964B (en) * | 2018-12-27 | 2023-09-29 | 乐天集团股份有限公司 | Unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108750115B (en) | 2021-05-25 |
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