CN104743121B - For unmanned plane loading cabin component and there is its unmanned plane - Google Patents
For unmanned plane loading cabin component and there is its unmanned plane Download PDFInfo
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- CN104743121B CN104743121B CN201510164500.3A CN201510164500A CN104743121B CN 104743121 B CN104743121 B CN 104743121B CN 201510164500 A CN201510164500 A CN 201510164500A CN 104743121 B CN104743121 B CN 104743121B
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- rechargeable battery
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Abstract
The invention discloses a kind of loading cabin component for unmanned plane and there is its unmanned plane, the unmanned plane includes fuselage, and the fuselage is provided with supplying cell, and loading cabin component is detachably arranged on the fuselage, and loading cabin component includes：Loading cabin, the loading cabin have inlet and outlet, the chamber for bearing goods are limited in the loading cabin；Goods door, the goods door, which is located on the loading cabin, to be used to open or close the outlet；Rechargeable battery, the rechargeable battery are located on the loading cabin, and the rechargeable battery has the charge port for being suitable to be connected with external power source, and the rechargeable battery is suitable to coordinate to charge to the supplying cell with the supplying cell.According to the loading cabin component of the present invention, the electric power of abundance can be provided for unmanned plane, and improves the loop cycle utilization rate in loading cabin.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of loading cabin component for unmanned plane and with its
Unmanned plane.
Background technology
At present, existing express delivery industry terminal distribution system is substantially all uses manpower means of distribution, its maximum weak point
It is：With goods efficiency is low, high with goods cost and user connects ETCD estimated time of commencing discharging and delivery period asymmetry problem.Therefore future, unmanned plane should
It is inevitable trend used in express delivery terminal distribution system, at present, the well-known express company in the whole world also begins to pay close attention to unmanned plane delivery
Mode, and the technical research of correlation is proceeded by, but the delivery unmanned plane delivery error designed at present is big, loading capacity is low, needs
Manpower is received.
The content of the invention
It is contemplated that at least solves one of technical problem in correlation technique to a certain extent.Therefore, the present invention
One purpose is to propose a kind of loading cabin component for unmanned plane, and the loading cabin component can provide abundance for unmanned plane
Electric power, and improve the loop cycle utilization rate in loading cabin.
It is another object of the present invention to propose a kind of unmanned plane with above-mentioned loading cabin component.
According to the loading cabin component for unmanned plane of the present invention, the unmanned plane includes fuselage, and the fuselage is provided with
Supplying cell, loading cabin component are detachably arranged on the fuselage, and loading cabin component includes：Loading cabin, it is described
Loading cabin has inlet and outlet, and the chamber for bearing goods is limited in the loading cabin；Goods door, the goods door are located at institute
State and be used to open or close the outlet on loading cabin；Rechargeable battery, the rechargeable battery is located on the loading cabin, described to fill
Battery has the charge port for being suitable to be connected with external power source, and the rechargeable battery is suitable to coordinate with to institute with the supplying cell
State supplying cell charging.
According to the loading cabin component for unmanned plane of the present invention, by setting goods door on loading cabin so that unmanned plane
Goods can be only delivered, without delivering loading cabin simultaneously, improves the loop cycle utilization rate in loading cabin, realizes that express delivery dispenses
Demand, the recycling of convenient-loading cargo hold.
In addition, by setting rechargeable battery on loading cabin, supplying cell thereon can be filled when unmanned plane works
Electricity, ensure the electric power with abundance when unmanned plane works and longer cruising time.
In addition, technical characteristic additional as follows can also be had according to the loading cabin component for unmanned plane of the present invention：
According to one embodiment of present invention, a charging electricity is respectively equipped with the left and right sidewall in the loading cabin
Pond.
According to one embodiment of present invention, it is respectively provided with the left and right sidewall in the loading cabin and accommodates the charging
The holding tank of battery.
According to one embodiment of present invention, the loading cabin component for unmanned plane also includes being used for the charging
Battery is positioned at the installation folder in the holding tank.
According to one embodiment of present invention, each holding tank extends through the loading cabin in the longitudinal direction
Corresponding side wall, the installation folder are configured to position the corresponding rechargeable battery on left and right directions and above-below direction.
According to one embodiment of present invention, a part for each rechargeable battery is in the lateral direction from the receiving
Groove exposes.
According to one embodiment of present invention, the roof of the chamber is opened wide to limit the import, the chamber
Bottom wall is opened wide to limit the outlet.
According to one embodiment of present invention, the goods door is automatic shutter.
According to the unmanned plane of the present invention, including：Fuselage, the fuselage include flying control device and supplying cell；Above-mentioned load
Cargo hold component, loading cabin component are detachably arranged on the fuselage, when loading cabin component is located on the fuselage,
The rechargeable battery is connected with the supplying cell to be powered to the supplying cell.
According to the unmanned plane of the present invention, by the way that loading cabin component is located on fuselage, the charging being located on the component of loading cabin
Battery is connected with supplying cell to be powered to supplying cell, thereby guarantees that unmanned plane has the continuation of the journey of long period, and then nobody
Machine can work with security and stability.
In addition, technical characteristic additional as follows can also be had according to the unmanned plane of the present invention：
According to one embodiment of present invention, the winged control device is connected with the goods door to control the opening of the goods door
Or close.
Brief description of the drawings
Fig. 1 is the schematic diagram of loading cabin component according to embodiments of the present invention；
Fig. 2 is the schematic diagram of unmanned plane according to embodiments of the present invention；
Fig. 3 is the front view of the first auxiliary section of installation folder according to embodiments of the present invention；
Fig. 4 is the side view of the first auxiliary section of installation folder according to embodiments of the present invention；
Fig. 5 is the front view of the second auxiliary section of installation folder according to embodiments of the present invention；
Fig. 6 is the side view of the second auxiliary section of installation folder according to embodiments of the present invention.
Reference：Loading cabin component 100, loading cabin 110, goods door 120, rechargeable battery 130, charge port 131, battery lock
Button 132, the second auxiliary section 133, the first auxiliary section 140, body 141, lock ball 142, installation folder buckle 143, import 101,
Holding tank 103, lock neck 104, installation folder neck 105, ball slideway 106, lock ring 107, unmanned plane 200, fuselage 210,
Supplying cell 211, fly control device 212.
Embodiment
Embodiments of the invention are described below in detail, the example of the embodiment is shown in the drawings.Below with reference to
The embodiment of accompanying drawing description is exemplary, it is intended to for explaining the present invention, and is not considered as limiting the invention.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " length ", " width ",
" thickness ", " on ", " under ", "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outer ", " up time
The orientation or position relationship of the instruction such as pin ", " counterclockwise ", " axial direction ", " radial direction ", " circumference " be based on orientation shown in the drawings or
Position relationship, it is for only for ease of and describes the present invention and simplify description, rather than indicates or imply that signified device or element must
There must be specific orientation, with specific azimuth configuration and operation, therefore be not considered as limiting the invention.
In addition, term " first ", " second " are only used for describing purpose, and it is not intended that instruction or hint relative importance
Or the implicit quantity for indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can be expressed or
Implicitly include at least one this feature.In the description of the invention, " multiple " are meant that at least two, such as two, three
It is individual etc., unless otherwise specifically defined.
In the present invention, unless otherwise clearly defined and limited, term " installation ", " connected ", " connection ", " fixation " etc.
Term should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integrally；Can be that machinery connects
Connect or electrically connect or can communicate each other；Can be joined directly together, can also be indirectly connected by intermediary, can be with
It is connection or the interaction relationship of two elements of two element internals, is limited unless otherwise clear and definite.For this area
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood as the case may be.
In the present invention, unless otherwise clearly defined and limited, fisrt feature can be with "above" or "below" second feature
It is that the first and second features directly contact, or the first and second features pass through intermediary mediate contact.Moreover, fisrt feature exists
Second feature " on ", " top " and " above " but fisrt feature are directly over second feature or oblique upper, or be merely representative of
Fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " can be
One feature is immediately below second feature or obliquely downward, or is merely representative of fisrt feature level height and is less than second feature.
1 the loading cabin component 100 for unmanned plane according to embodiments of the present invention is carried out to accompanying drawing 3 below in conjunction with the accompanying drawings
It is described in detail.
Firstly the need of explanation, unmanned plane 200 includes fuselage 210, and fuselage 210 is provided with supplying cell 211, power supply electricity
Pond 211 can be that unmanned plane 200 provides power so that unmanned plane 200 can safely and steadly work.
Loading cabin component 100 for unmanned plane according to embodiments of the present invention, loading cabin 110, goods door 120 can be included
And rechargeable battery 130.
Wherein, as shown in figure 1, loading cabin 110 has import 101 and outlet, limited in loading cabin 110 for carrying goods
The chamber of thing.
Specifically, the roof of chamber is opened wide to limit exit port 101, and the bottom wall of chamber is opened wide to limit outlet.Wait to throw
The goods passed can be entered in the chamber in loading cabin 110 from the import 101 in loading cabin 110, and goods is being placed in chamber
Afterwards, it is preferable that the position where goods is about the center of unmanned plane 200, and such unmanned plane 200 is whether in loading
State or unladen state, its center of gravity is substantially constant, it is possible thereby to ensure that unmanned plane 200 safely and smoothly flies.
Goods door 120, which is located on loading cabin 110, to be used to open or close outlet.When unmanned plane 200 is in state of flight, goods door
120 close outlet, prevent goods from being dropped out out of loading cabin 110；Unmanned plane 200 is when reaching client appointed place (for example, client
In family), goods door 120 will be exported and opened, and goods skids off out of chamber, completes the dispatching of goods.
Thus, unmanned plane 200 can only deliver goods, without delivering loading cabin 110 simultaneously, improve loading cabin 110
Loop cycle utilization rate, realize express delivery dispatching demand, the recycling of convenient-loading cargo hold 110.
Alternatively, goods door 120 can be automatic shutter.Thus, it is possible to reduce the sky that goods door 120 takes in opening and closing
Between, make the opening and closing of goods door 120 more convenient.
As depicted in figs. 1 and 2, rechargeable battery 130 is located on loading cabin 110, and rechargeable battery 130, which has, to be suitable to and external electrical
The connected charge port 131 in source, rechargeable battery 130 are suitable to supplying cell 211 coordinate to charge to supplying cell 211.
That is, the power of unmanned plane 200 is provided by the supplying cell 211 on fuselage 210, in loading cabin component
100 when being placed on fuselage 210, and the rechargeable battery 130 on loading cabin component 100 does not directly provide power for unmanned plane 200, and
Simply supplying cell 211 is charged.Thus, the electric power during unmanned plane 200 works of supplying cell 211 is sufficient, ensure that
Unmanned plane 200 has longer cruising time, and then the flight stability of unmanned plane 200 is ensured.
Alternatively, filled as shown in figure 1, being respectively equipped with one in left and right (direction as shown in Figure 1) side wall in loading cabin 110
Battery 130.That is, loading cabin 110 is provided with two pieces of rechargeable batteries 130, and two pieces of rechargeable batteries 130 are oppositely arranged on
In the side wall in loading cabin 110.Thus, further increase the endurance of unmanned plane 200, realize unmanned plane 200 from
High efficiency is dispensed in short time during delivery thing, and unmanned plane 200, loading cabin 110 and rechargeable battery 130 are optimized and matched somebody with somebody
Put, and symmetrically arranged rechargeable battery 130 can be such that the counterweight of loading cabin component 100 more balances, and ensure that unmanned plane 200 is carrying
It is safe, steady during shipping row.
It should be noted that loading cabin component 100 is detachably arranged on the fuselage 210 of unmanned plane 200.By loading cabin
When component 100 is arranged on fuselage 210, the rechargeable battery 130 on loading cabin component 100 can be by charge port 131 to fuselage
Supplying cell 211 on 210 provides electric power；, can be by outside after loading cabin component 100 is disassembled from unmanned plane 200
Portion's power supply is connected in the charge port 131 of rechargeable battery 130 to be charged to rechargeable battery 130.
That is, the charge port 131 on rechargeable battery 130 be both unmanned plane 200 at work rechargeable battery 130 to confession
The interface that battery 211 is powered, and after loading cabin component 100 is disassembled, when external power source charges to rechargeable battery 130
Interface.
Loading cabin component 100 for unmanned plane according to embodiments of the present invention, by setting goods door on loading cabin 110
120 so that unmanned plane 200 can only deliver goods, without delivering loading cabin 110 simultaneously, improve the cycle in loading cabin 110
Recycling rate, realize the demand of express delivery dispatching, the recycling of convenient-loading cargo hold 110.
In addition, by setting rechargeable battery 130 on loading cabin 110, can be when unmanned plane 200 works to confession thereon
Battery 211 charges, and ensures the electric power with abundance when unmanned plane 200 works and longer cruising time.
In some embodiments of invention, as shown in figure 1, being respectively provided with receiving in the left and right sidewall in loading cabin 110
The holding tank 103 of rechargeable battery 130.Thus, battery can be put into holding tank 103 so that the overall space of chamber is more
Greatly, it is convenient to place the larger goods of volume, and rechargeable battery 130 is placed in holding tank 103 and can also carried to a certain extent
The stability of high charge battery 130.
Further, loading cabin component 100 also includes being used for the installation being positioned at rechargeable battery 130 in holding tank 103
Folder.Rechargeable battery 130 can be positioned in holding tank 103 by the installation folder, and then rechargeable battery 130 can be stably nobody
Machine 200 provides electric power, and ensureing unmanned plane 200, rechargeable battery 130 will not shake in the course of the work, and unmanned plane 200 can be with
Stably work.
Specifically, as shown in figure 1, each holding tank 103 extends through the corresponding side in loading cabin 110 in the longitudinal direction
Wall, installation folder are configured to position corresponding rechargeable battery 130 on left and right directions and above-below direction.That is, charging electricity
Pond 130 may only be moved in the longitudinal direction on loading cabin 110, all be to move on above-below direction and left and right directions
's.When the aging of rechargeable battery 130 needs to replace, under can rechargeable battery 130 be dismantled from loading cabin 110 along the longitudinal direction
Come.
Certainly, in the flight course of unmanned plane 200, i.e., rechargeable battery 130 is carrying out charging process to supplying cell 211
In, one or more stop parts can be provided with carry out backstop rechargeable battery 130 and move in the longitudinal direction.Thus, further protect
Demonstrate,prove the stability that rechargeable battery 130 works.
In the specific example of the present invention, as shown in figures 3 to 6, each installation folder includes being located at corresponding holding tank 103
Interior first auxiliary section 140 and the second auxiliary section 133 being located on rechargeable battery 130, the first auxiliary section in holding tank 103
140 are fixed on the inwall of holding tank 103, and the first auxiliary section 140 includes body 141, and body 141 is provided with least one lock
Ball 142, the top and bottom of body 141 are respectively equipped with installation folder buckle 143, and each installation folder buckle 143 is configured to " L " shape
Structure and including the first limb and the second limb, the first limb of two installation folder buckles 143 top and bottom phase with body 141 respectively
Even, the second limb of two installation folder buckles 143 is respectively facing to be extended each other.Limited between two installation folder buckles 143 and body 141
Make installation folder neck 105.
As shown in Figure 5 and Figure 6, when rechargeable battery 130 is arranged on loading cabin 110, rechargeable battery 130 towards loading cabin
110 surface is provided with the second auxiliary section 133, formed with least one ball slideway 106 on the second auxiliary section 133, and each
Ball slideway 106 is provided with lock ring 107 corresponding with lock ball 142.
As shown in fig. 6, the top and bottom of the second auxiliary section 133 are respectively equipped with the flat battery to stretch out vertically
Lock 132, when rechargeable battery 130 is arranged on loading cabin 110, each battery lock 132 is located at corresponding installation folder buckle
Between 143 the second limb and body 141.Thus, as shown in figure 1, rechargeable battery 130 can only move in the longitudinal direction, without
It can be moved up in above-below direction and right and left.
If Fig. 3 is to Fig. 6 and with reference to shown in Fig. 1, the second auxiliary section 133 is slidably fit into installation folder neck 105, and
Each lock ball 140 moves in corresponding ball slideway 106, when each lock ball 142 is fastened on corresponding lock ring
When in 107, the one-movement-freedom-degree of rechargeable battery 130 is defined.Thus, positioning can be played by latching ball 142 and lock ring 107
Effect, it is arranged on loading cabin 110 with ensureing the fast and stable of rechargeable battery 130.
It is understood that the number of lock ball 142 and the number of ball slideway 106, the number phase of lock ring 107
Together.When it is multiple to latch ball 142, multiple lock balls 142 can be fastened in multiple lock rings 107 correspondingly.
In some embodiments of the invention, as shown in figure 1, a part for each rechargeable battery 130 in the lateral direction
Expose from holding tank 103.In other words, rechargeable battery 130 is not to be completely disposed in holding tank 103, the one of rechargeable battery 130
Expose from holding tank 103 part.Thus, it on the one hand ensure that the center section of the chamber in loading cabin 110 is unlikely to too small,
The volume of chamber is improved to a certain extent；On the other hand, the installation and removal of rechargeable battery 130 are facilitated.
Charge port 131 can be located on the part for exposing holding tank 103 of corresponding rechargeable battery 130 simultaneously, so as to
Loading cabin component 100 is lifted down from unmanned plane 200 charged when, the part that rechargeable battery 130 exposes can be with filling
The shape of electrical equipment matches, and facilitates charger to charge rechargeable battery 130.
In the specific example of the present invention, fuselage 210 is provided with locker, as shown in figure 1, being set on rechargeable battery 130
There is a lock neck 104 suitable for coordinating with locker, the lock neck 104 and locker coordinate with by loading cabin component
100 are detachably arranged on unmanned plane 200, ensure that loading cabin component 100 is stable and are securely arranged on unmanned plane 200.
It will of course be understood that must be, lock neck 104 can also be directly arranged in the side wall in loading cabin 110, such as will lock
Buckle card slot 104 is arranged on the front side wall and rear wall in loading cabin 110.
Unmanned plane 200 according to embodiments of the present invention is briefly described below.
Unmanned plane 200 according to embodiments of the present invention, the loading cabin component in fuselage 210 and above-described embodiment can be included
100。
Wherein, at work, loading cabin component 100 is placed on the fuselage 210 of unmanned plane 200 unmanned plane 200.Fuselage 210
Including flying control device 212 and supplying cell 211.Fly the control centre that control device 212 is unmanned plane 200, supplying cell 211 can be with
Electric power is provided to fly control device 212.
Loading cabin component 100 is detachably arranged on fuselage 210, when loading cabin component 100 is located on fuselage 210, charging
Battery 130 is connected with supplying cell 211 to be powered to supplying cell 211.Thus, unmanned plane 200 is in flight course, power supply electricity
Pond 211 has sufficient electricity, ensures that unmanned plane 200 has longer cruising time.Certainly, by loading cabin component 100 from
After being uninstalled on unmanned plane 200, the supplying cell 211 on fuselage 210 still has certain electricity, can also be unmanned plane
100 provide electric power.
Unmanned plane 200 according to embodiments of the present invention, by the way that loading cabin component 100 is located on fuselage 210, loading cabin group
Rechargeable battery 130 on part 100 is connected with supplying cell 211 to be powered to supplying cell 211, thereby guarantees that unmanned plane 200 has
There is the continuation of the journey of long period, and then unmanned plane 200 can work with security and stability.
In some embodiments of the invention, fly control device 212 be connected with goods door 120 with control the opening of goods door 120 or
Close.For example, when unmanned plane 200 reaches the place that client specifies, signal control goods door can be sent by flying control device 212
120 open, and goods skids off from outlet；After the completion of goods is delivered, winged control device 212 sends signal control goods door 120 and closed, then
Unmanned plane 200 makes a return voyage or delivered next time.In the specific example of the present invention, client can be reached in unmanned plane 200
After the 2s in the place specified, fly control device 212 and control goods door 120 to automatically open up.
It should be noted that in above-described embodiment the transmission of signal and rechargeable battery 130 to supplying cell 211 power when electricity
All by this interface of charge port 131, charge port 131 can be contact power interface for the transmission of energy.
The course of work of the unmanned plane 200 of the embodiment of the present invention is briefly described below.
Express delivery terminal is built up in client's Relatively centralized region such as residential block, Office Area, building area first and matches somebody with somebody freight house storehouse, with
And the landing platform of unmanned plane 200, charging room etc..Client can directly be ordered the goods goods by cell-phone customer terminal, after client places an order,
Goods storage control system directly generates order, by manually loading goods into loading cabin 110, then passes through loading cabin component
Loading cabin component 100 is directly delivered to the launching platform of unmanned plane 200 by 100 conveying devices, by latching neck 104 and lock
Device coordinates so that loading cabin component 100 will be fixed on unmanned plane 200.
Then, the flight path control information that unmanned plane 200 has received according to winged control device 212, is taken off and is flown
Control, the rechargeable battery 130 in flight course on loading cabin component 100 can enter to the supplying cell 211 on unmanned plane 200
Row charging, to ensure that supplying cell 211 has sufficient electricity.When unmanned plane 200 reaches appointed place (for example, client
In family), the winged control device 212 on unmanned plane 200 can send signal control goods door 120 and open, and goods skids off from outlet, then
Winged control device 212 sends signal control goods door 120 and closed.Complete unmanned plane 200 after delivering and be back to nothing further according to winged control device 212
Man-machine 200 landing platform, loading cabin component 100 is tripped with fuselage 210 by the way of automatic or manual.Unmanned plane 200
Launching platform is back to prepare to dispense work next time, loading cabin component 100 is transported to charging room charging, after the completion of it is accurate at any time
It is standby to match somebody with somebody goods.
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or the spy for combining the embodiment or example description
Point is contained at least one embodiment or example of the present invention.In this manual, to the schematic representation of above-mentioned term not
Identical embodiment or example must be directed to.Moreover, specific features, structure, material or the feature of description can be with office
Combined in an appropriate manner in one or more embodiments or example.In addition, in the case of not conflicting, the skill of this area
Art personnel can be tied the different embodiments or example and the feature of different embodiments or example described in this specification
Close and combine.
Although embodiments of the invention have been shown and described above, it is to be understood that above-described embodiment is example
Property, it is impossible to limitation of the present invention is interpreted as, one of ordinary skill in the art within the scope of the invention can be to above-mentioned
Embodiment is changed, changed, replacing and modification.
Claims (9)
1. a kind of loading cabin component for unmanned plane, the unmanned plane includes fuselage, and the fuselage is provided with supplying cell, its
It is characterised by, loading cabin component is detachably arranged on the fuselage, and loading cabin component includes：
Loading cabin, the loading cabin have inlet and outlet, and the chamber for bearing goods is limited in the loading cabin, described
The roof of chamber is opened wide to limit the import, and the bottom wall of the chamber is opened wide to limit the outlet；
Goods door, the goods door, which is located on the loading cabin, to be used to open or close the outlet；
Rechargeable battery, the rechargeable battery are located on the loading cabin, and the rechargeable battery, which has, to be suitable to be connected with external power source
Charge port, the rechargeable battery be suitable to the supplying cell coordinate with to the supplying cell charge.
2. the loading cabin component according to claim 1 for unmanned plane, it is characterised in that the left and right sides in the loading cabin
A rechargeable battery is respectively equipped with wall.
3. the loading cabin component according to claim 2 for unmanned plane, it is characterised in that the left and right sides in the loading cabin
The holding tank for accommodating the rechargeable battery is respectively provided with wall.
4. the loading cabin component according to claim 3 for unmanned plane, it is characterised in that also include being used to fill described
Battery is positioned at the installation folder in the holding tank.
5. the loading cabin component according to claim 4 for unmanned plane, it is characterised in that each holding tank is preceding
Rear extends through the corresponding side wall in the loading cabin upwards, and the installation folder is configured in left and right directions and above-below direction
The upper corresponding rechargeable battery of positioning.
6. the loading cabin component according to claim 3 for unmanned plane, it is characterised in that each rechargeable battery
A part is exposed from the holding tank in the lateral direction.
7. the loading cabin component according to claim 1 for unmanned plane, it is characterised in that the goods door is automatic curtain
Door.
A kind of 8. unmanned plane, it is characterised in that including：
Fuselage, the fuselage include flying control device and supplying cell；
Loading cabin component according to any one of claim 1-7, loading cabin component are detachably arranged in the machine
With, when loading cabin component is located on the fuselage, the rechargeable battery is connected with the supplying cell with to the confession
Electric battery powered.
9. unmanned plane according to claim 8, it is characterised in that the winged control device is connected to control with the goods door
State opening or closing for goods door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510164500.3A CN104743121B (en) | 2015-04-08 | 2015-04-08 | For unmanned plane loading cabin component and there is its unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510164500.3A CN104743121B (en) | 2015-04-08 | 2015-04-08 | For unmanned plane loading cabin component and there is its unmanned plane |
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| Publication Number | Publication Date |
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| CN104743121A CN104743121A (en) | 2015-07-01 |
| CN104743121B true CN104743121B (en) | 2018-03-27 |
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| CN201510164500.3A Active CN104743121B (en) | 2015-04-08 | 2015-04-08 | For unmanned plane loading cabin component and there is its unmanned plane |
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Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986338B (en) * | 2015-07-08 | 2017-05-03 | 谢县钢 | Rotary wing type unmanned aerial vehicle parking system for logistics distribution and application method |
| CN105139180B (en) * | 2015-09-24 | 2019-06-18 | 杭州万兴科技股份有限公司 | A kind of unmanned plane transport roof communication base station |
| CN105966620A (en) * | 2016-05-03 | 2016-09-28 | 天机智汇科技（深圳）有限公司 | Unmanned aerial vehicle system and cargo hold thereof |
| CN105923163B (en) * | 2016-06-01 | 2018-05-08 | 北京小米移动软件有限公司 | Transport shelf and unmanned plane |
| DE102016210627B4 (en) * | 2016-06-15 | 2018-07-05 | Nickel Holding Gmbh | Device for storing and transporting components and method for supplying at least one processing device with components |
| CN106114867B (en) * | 2016-07-28 | 2019-12-27 | 顺丰科技有限公司 | Unmanned aerial vehicle cargo hold |
| CN206218239U (en) | 2016-12-05 | 2017-06-06 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| DE112017006863T5 (en) * | 2017-02-17 | 2019-10-31 | Ford Global Technologies, Llc | Drone-based freight transport |
| US11186368B2 (en) * | 2017-12-21 | 2021-11-30 | Wing Aviation Llc | Methods and systems for door-enabled loading and release of payloads in an unmanned aerial vehicle (UAV) |
| CN107985599A (en) * | 2017-12-27 | 2018-05-04 | 天机智汇科技（深圳）有限公司 | Automatic load-carrying device, unmanned plane and loading cabin |
| CN108681834A (en) * | 2018-06-26 | 2018-10-19 | 北京云迹科技有限公司 | Order dispenses task creating method and generating means |
| CN111942592B (en) * | 2020-07-13 | 2022-06-24 | 李隆锦 | Multi-cabin logistics unmanned aerial vehicle transportation system |
| CN112234298A (en) * | 2020-10-19 | 2021-01-15 | 苏州博众机器人有限公司 | Battery dismounting device and robot |
| US20230202679A1 (en) * | 2021-12-27 | 2023-06-29 | Industrial Technology Research Institute | Container device and transport system of uav |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204802090U (en) * | 2015-04-08 | 2015-11-25 | 唐枫一 | A unmanned aerial vehicle that is used for unmanned aerial vehicle's cabin subassembly and have it of carrying cargo |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8948935B1 (en) * | 2013-01-02 | 2015-02-03 | Google Inc. | Providing a medical support device via an unmanned aerial vehicle |
| CN103274047A (en) * | 2013-05-31 | 2013-09-04 | 无锡同春新能源科技有限公司 | Unmanned aerial vehicle for express parcels |
| WO2014080389A2 (en) * | 2014-03-25 | 2014-05-30 | Alshdaifat, Wasfi | Autonomous ground station interfacing aerial delivery |
| CN204037896U (en) * | 2014-08-12 | 2014-12-24 | 中国航空工业经济技术研究院 | A kind of logistics depopulated helicopter |
-
2015
- 2015-04-08 CN CN201510164500.3A patent/CN104743121B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204802090U (en) * | 2015-04-08 | 2015-11-25 | 唐枫一 | A unmanned aerial vehicle that is used for unmanned aerial vehicle's cabin subassembly and have it of carrying cargo |
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