CN104743121A - Cargo cabin component for unmanned aerial vehicle and unmanned aerial vehicle with the same - Google Patents
Cargo cabin component for unmanned aerial vehicle and unmanned aerial vehicle with the same Download PDFInfo
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- CN104743121A CN104743121A CN201510164500.3A CN201510164500A CN104743121A CN 104743121 A CN104743121 A CN 104743121A CN 201510164500 A CN201510164500 A CN 201510164500A CN 104743121 A CN104743121 A CN 104743121A
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- rechargeable battery
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Abstract
The invention discloses a cargo cabin component for an unmanned aerial vehicle and the unmanned aerial vehicle with the same. The unmanned aerial vehicle comprises a vehicle body, the vehicle body is provided with a power supply battery, the cargo cabin component is detachably arranged on the vehicle body, the cargo cabin component comprises a cargo cabin, a cabin door and a rechargeable battery, wherein the cargo cabin has an entrance and an exit, and a chamber used for loading cargoes is limited in the cargo cabin; the cabin door is arranged on the cargo cabin and used for opening or closing the exit; the rechargeable battery is arranged on the cargo cabin and comprises a charging port suitable for connecting with an external power supply, and the rechargeable battery is suitable for matching with the power supply battery to charge the power supply battery. The cargo cabin component is capable of providing enough electricity for the unmanned aerial vehicle, and the cyclic utilization rate of the cargo cabin is improved.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, particularly a kind of loading cabin assembly for unmanned plane and there is its unmanned plane.
Background technology
At present, existing express delivery industry terminal distribution system substantially all adopts manpower means of distribution, and its maximum weak point is: join goods efficiency low, join the high and user of goods cost and connect estimated time of commencing discharging and delivery period asymmetry problem.Therefore in the future unmanned plane is applied in express delivery terminal distribution system and is inevitable trend, at present, the well-known express company in the whole world also starts to pay close attention to unmanned plane deliver goods mode, and start the technical study carrying out being correlated with, but the deliver goods unmanned plane of design is at present delivered, and error is large, load carrying ability is low, need manpower to receive.
Summary of the invention
The present invention is intended to solve one of technical matters in correlation technique at least to a certain extent.For this reason, one object of the present invention is to propose a kind of loading cabin assembly for unmanned plane, and this loading cabin assembly can provide sufficient electric power for unmanned plane, and improves the loop cycle Occupation coefficient in loading cabin.
Another object of the present invention is to propose a kind of unmanned plane with above-mentioned loading cabin assembly.
According to the loading cabin assembly for unmanned plane of the present invention, described unmanned plane comprises fuselage, described fuselage is provided with supplying cell, described loading cabin assembly is removably located on described fuselage, described loading cabin assembly comprises: loading cabin, described loading cabin has import and outlet, limits the chamber for bearing goods in described loading cabin; Goods door, described goods door is located on described loading cabin and is used to open or close described outlet; Rechargeable battery, described rechargeable battery is located on described loading cabin, and described rechargeable battery has the charge port being suitable for being connected with external power supply, and described rechargeable battery is suitable for coordinating to charge to described supplying cell with described supplying cell.
According to the loading cabin assembly for unmanned plane of the present invention, by arranging goods door on loading cabin, make unmanned plane only can deliver goods, and loading cabin need not be delivered simultaneously, improve the loop cycle Occupation coefficient in loading cabin, realize the demand of express delivery dispensing, the recycling of convenient-loading cargo hold.
In addition, by arranging rechargeable battery on loading cabin, when unmanned plane works to the supplying cell charging on it, when ensureing unmanned plane work, sufficient electric power and longer cruise duration can be had.
In addition, the loading cabin assembly for unmanned plane according to the present invention can also have following additional technical characteristic:
According to one embodiment of present invention, the left and right sidewall in described loading cabin is respectively equipped with a described rechargeable battery.
According to one embodiment of present invention, the left and right sidewall in described loading cabin is respectively equipped with the holding tank for holding described rechargeable battery.
According to one embodiment of present invention, the described loading cabin assembly for unmanned plane also comprises the mounting clamp for being positioned at by described rechargeable battery in described holding tank.
According to one embodiment of present invention, each described holding tank runs through the corresponding sidewall in described loading cabin in the longitudinal direction respectively, and described mounting clamp is formed on left and right directions and above-below direction and locates corresponding described rechargeable battery.
According to one embodiment of present invention, a part for each described rechargeable battery is exposed from described holding tank in the lateral direction.
According to one embodiment of present invention, the roof of described chamber opens wide to limit described import, and the diapire of described chamber opens wide to limit described outlet.
According to one embodiment of present invention, described goods door is automatic shutter.
According to unmanned plane of the present invention, comprising: fuselage, described fuselage comprises and flies control device and supplying cell; Above-mentioned loading cabin assembly, described loading cabin assembly is removably located on described fuselage, and when described loading cabin assembly is located on described fuselage, described rechargeable battery is connected to power to described supplying cell with described supplying cell.
According to unmanned plane of the present invention, by loading cabin assembly is located on fuselage, the rechargeable battery be located on the assembly of loading cabin is connected to power to supplying cell with supplying cell, ensure that unmanned plane has the continuation of the journey of long period thus, and then unmanned plane can work with security and stability.
In addition, following additional technical characteristic can also be had according to unmanned plane of the present invention:
According to one embodiment of present invention, fly control device described in be connected to control opening or closing of described goods door with described goods door.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the loading cabin assembly according to the embodiment of the present invention;
Fig. 2 is the schematic diagram of the unmanned plane according to the embodiment of the present invention;
Fig. 3 is the front view of the first auxiliary section of mounting clamp according to the embodiment of the present invention;
Fig. 4 is the lateral plan of the first auxiliary section of mounting clamp according to the embodiment of the present invention;
Fig. 5 is the front view of the second auxiliary section of mounting clamp according to the embodiment of the present invention;
Fig. 6 is the lateral plan of the second auxiliary section of mounting clamp according to the embodiment of the present invention.
Reference numeral: loading cabin assembly 100, loading cabin 110, goods door 120, rechargeable battery 130, charge port 131, auxiliary section 140, battery snap close 132, second auxiliary section 133, first, body 141, snap close ball 142, mounting clamp buckle 143, import 101, holding tank 103, snap close draw-in groove 104, mounting clamp draw-in groove 105, ball slideway 106, snap close ring 107, unmanned plane 200, fuselage 210, supplying cell 211, flies to control device 212.
Detailed description of the invention
Be described below in detail embodiments of the invention, the example of described embodiment is shown in the drawings.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the present invention, and can not limitation of the present invention be interpreted as.
In describing the invention, it will be appreciated that, term " " center ", " longitudinal direction ", " transverse direction ", " length ", " width ", " thickness ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end " " interior ", " outward ", " cw ", " conter clockwise ", " axis ", " radial direction ", orientation or the position relationship of the instruction such as " circumference " are based on orientation shown in the drawings or position relationship, only the present invention for convenience of description and simplified characterization, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore limitation of the present invention can not be interpreted as.
In addition, term " first ", " second " only for describing object, and can not be interpreted as instruction or hint relative importance or imply the quantity indicating indicated technical characteristic.Thus, be limited with " first ", the feature of " second " can express or impliedly comprise at least one this feature.In describing the invention, the implication of " multiple " is at least two, such as two, three etc., unless otherwise expressly limited specifically.
In the present invention, unless otherwise clearly defined and limited, the term such as term " installation ", " being connected ", " connection ", " fixing " should be interpreted broadly, and such as, can be fixedly connected with, also can be removably connect, or integral; Can be mechanical connection, also can be electrical connection or each other can communication; Can be directly be connected, also indirectly can be connected by intermediary, can be the connection of two element internals or the interaction relationship of two elements, unless otherwise clear and definite restriction.For the ordinary skill in the art, above-mentioned term concrete meaning in the present invention can be understood as the case may be.
In the present invention, unless otherwise clearly defined and limited, fisrt feature second feature " on " or D score can be that the first and second features directly contact, or the first and second features are by intermediary indirect contact.And, fisrt feature second feature " on ", " top " and " above " but fisrt feature directly over second feature or oblique upper, or only represent that fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " below " and " below " can be fisrt feature immediately below second feature or tiltedly below, or only represent that fisrt feature level height is less than second feature.
Below in conjunction with accompanying drawing 1 to accompanying drawing 3, the loading cabin assembly 100 for unmanned plane according to the embodiment of the present invention is described in detail.
First it should be noted that, unmanned plane 200 comprises fuselage 210, and fuselage 210 is provided with supplying cell 211, and supplying cell 211 can provide power for unmanned plane 200, and unmanned plane 200 can be worked safely and steadly.
According to the loading cabin assembly 100 for unmanned plane of the embodiment of the present invention, loading cabin 110, goods door 120 and rechargeable battery 130 can be comprised.
Wherein, as shown in Figure 1, loading cabin 110 has import 101 and outlet, limits the chamber for bearing goods in loading cabin 110.
Particularly, the roof of chamber opens wide to limit import 101, and the diapire of chamber opens wide to limit outlet.Goods to be delivered can enter into the chamber in loading cabin 110 from the import 101 in loading cabin 110, goods is being placed on after in chamber, preferably, the position at goods place is roughly the center of unmanned plane 200, no matter such unmanned plane 200 is in loading state or unladen state, its center of gravity is roughly constant, can ensure that unmanned plane 200 flies safely and smoothly thus.
Goods door 120 is located on loading cabin 110 and is used to open or close outlet.When unmanned plane 200 is in state of flight, goods door 120 closes outlet, prevents goods from dropping out in loading cabin 110; Unmanned plane 200 is when arriving client appointed place (such as, in client family), and outlet is opened by goods door 120, and goods skids off in chamber, completes the dispensing of goods.
Thus, unmanned plane 200 only can deliver goods, and need not deliver loading cabin 110 simultaneously, improves the loop cycle Occupation coefficient in loading cabin 110, realizes the demand of express delivery dispensing, the recycling of convenient-loading cargo hold 110.
Alternatively, goods door 120 can be automatic shutter.Thus, the space that goods door 120 takies when opening and closing can be reduced, 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 has the charge port 131 being suitable for being connected with external power supply, and rechargeable battery 130 is suitable for coordinating to charge to supplying cell 211 with supplying cell 211.
That is, the power of unmanned plane 200 is provided by the supplying cell 211 on fuselage 210, when loading cabin assembly 100 is placed on fuselage 210, the rechargeable battery 130 on loading cabin assembly 100 not directly for unmanned plane 200 provides power, and just charges to supplying cell 211.Thus, in the process that supplying cell 211 works at unmanned plane 200, electric power is sufficient, ensure that unmanned plane 200 has longer cruise duration, and then the flight stability of unmanned plane 200 obtains guarantee.
Alternatively, as shown in Figure 1, left and right (direction as shown in Figure 1) sidewall in loading cabin 110 is respectively equipped with a rechargeable 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 the sidewall in loading cabin 110.Thus, further increase the flying power of unmanned plane 200, realize unmanned plane 200 high efficiency dispensing within the short time in dispensing goods process, and unmanned plane 200, loading cabin 110 and rechargeable battery 130 optimization collocation, and symmetrically arranged rechargeable battery 130 can make the counterweight of loading cabin assembly 100 more balance, ensure safe, steady when loading runs of unmanned plane 200.
It should be noted that, loading cabin assembly 100 is removably located on the fuselage 210 of unmanned plane 200.When being arranged on fuselage 210 by loading cabin assembly 100, the rechargeable battery 130 on loading cabin assembly 100 can provide electric power by the supplying cell 211 on charge port 131 pairs of fuselages 210; By loading cabin assembly 100 from after unmanned plane 200 disassembles, to charge to rechargeable battery 130 in the charge port 131 external power supply can being received rechargeable battery 130.
That is, the charge port 131 on rechargeable battery 130 is unmanned plane 200 operationally rechargeable battery 130 interface of powering to supplying cell 211, is also after loading cabin assembly 100 is disassembled, interface when external power supply charges to rechargeable battery 130.
According to the loading cabin assembly 100 for unmanned plane of the embodiment of the present invention, by arranging goods door 120 on loading cabin 110, make unmanned plane 200 only can deliver goods, and loading cabin 110 need not be delivered simultaneously, improve the loop cycle Occupation coefficient in loading cabin 110, realize the demand of express delivery dispensing, the recycling of convenient-loading cargo hold 110.
In addition, by arranging rechargeable battery 130 on loading cabin 110, can charge to the supplying cell 211 on it when unmanned plane 200 works, ensureing that unmanned plane 200 has sufficient electric power and longer cruise duration when working.
In some embodiments of invention, as shown in Figure 1, the left and right sidewall in loading cabin 110 is respectively equipped with the holding tank 103 for holding rechargeable battery 130.Thus, battery can put in holding tank 103, the overall space making chamber is larger, conveniently places the larger goods of volume, and rechargeable battery 130 is placed on the stability that can also improve rechargeable battery 130 in holding tank 103 to a certain extent.
Further, loading cabin assembly 100 also comprises the mounting clamp for being positioned at by rechargeable battery 130 in holding tank 103.Rechargeable battery 130 can be positioned in holding tank 103 by this mounting clamp, and then rechargeable battery 130 can stably for unmanned plane 200 provides electric power, guarantee unmanned plane 200 in the course of the work rechargeable battery 130 can not shake, and unmanned plane 200 can stably work.
Particularly, as shown in Figure 1, each holding tank 103 runs through the corresponding sidewall in loading cabin 110 in the longitudinal direction respectively, and mounting clamp is formed on left and right directions and above-below direction and locates corresponding rechargeable battery 130.That is, rechargeable battery 130 only to move in the longitudinal direction, above-below direction and left and right directions all cannot move on loading cabin 110.Rechargeable battery 130 aging need replace time, can along the longitudinal direction rechargeable battery 130 be disassembled from loading cabin 110.
Certainly, in unmanned plane 200 flight course, namely rechargeable battery 130 is carrying out in process of charging to supplying cell 211, can be provided with one or more stop part and carry out backstop rechargeable battery 130 and move in the longitudinal direction.Thus, the stability that rechargeable battery 130 works is ensured further.
In concrete example of the present invention, as shown in figures 3 to 6, each mounting clamp comprises the first auxiliary section 140 be located in corresponding holding tank 103 and the second auxiliary section 133 be located on rechargeable battery 130, the first auxiliary section 140 in holding tank 103 is fixed on the inwall of holding tank 103, first auxiliary section 140 comprises body 141, body 141 is provided with at least one snap close ball 142, the top and bottom of body 141 are respectively equipped with mounting clamp buckle 143, each mounting clamp buckle 143 is configured to " L " shape structure and comprises the first limb and the second limb, first limb of two mounting clamp buckles 143 is connected with the top and bottom of body 141 respectively, second limb of two mounting clamp buckles 143 extends respectively toward each other.Mounting clamp draw-in groove 105 is limited between two mounting clamp buckles 143 and body 141.
As shown in Figure 5 and Figure 6, when rechargeable battery 130 is arranged on loading cabin 110, the surface towards loading cabin 110 of rechargeable battery 130 is provided with the second auxiliary section 133, second auxiliary section 133 is formed with at least one ball slideway 106, and each ball slideway 106 is provided with the snap close ring 107 corresponding with snap close ball 142.
As shown in Figure 6, the top and bottom of the second auxiliary section 133 are respectively equipped with vertical outward extending flat battery snap close 132, when rechargeable battery 130 is arranged on loading cabin 110, each battery snap close 132 is between second limb and body 141 of corresponding mounting clamp buckle 143.Thus, as shown in Figure 1, rechargeable battery 130 can only move in the longitudinal direction, and can not move up at above-below direction and right and left.
As Fig. 3 to Fig. 6 and shown in composition graphs 1, second auxiliary section 133 is engaged in mounting clamp draw-in groove 105 slidably, and each snap close ball 140 is mobile in corresponding ball slideway 106, when each snap close ball 142 is fastened in corresponding snap close ring 107, define the one-movement-freedom-degree of rechargeable battery 130.Thus, snap close ball 142 and snap close ring 107 can play positioning action, are arranged on loading cabin 110 with ensureing rechargeable battery 130 fast and stable.
Be understandable that, the number of snap close ball 142 is identical with the number of the number of ball slideway 106, snap close ring 107.When snap close ball 142 is multiple, multiple snap close ball 142 can be fastened in multiple snap close ring 107 correspondingly.
In some embodiments of the invention, as shown in Figure 1, a part for each rechargeable battery 130 is exposed in the lateral direction from holding tank 103.In other words, rechargeable battery 130 is not be placed in holding tank 103 completely, and a part for rechargeable battery 130 is exposed from holding tank 103.Thus, the centre portion of the chamber that ensure that in loading cabin 110 is on the one hand unlikely to too little, improves the volume of chamber to a certain extent; On the other hand, the Assembly &Disassembly of rechargeable battery 130 is facilitated.
Charge port 131 can be located in the part exposing holding tank 103 of corresponding rechargeable battery 130 simultaneously, thus by loading cabin assembly 100 from unmanned plane 200 lift down charge time, the part that rechargeable battery 130 exposes can with the mating shapes of charger, facilitate charger to charge to rechargeable battery 130.
In concrete example of the present invention, fuselage 210 is provided with latching system, as shown in Figure 1, rechargeable battery 130 is provided with the snap close draw-in groove 104 being suitable for coordinating with latching system, this snap close draw-in groove 104 coordinates removably be located on unmanned plane 200 by loading cabin assembly 100 with latching system, ensure that loading cabin assembly 100 is stable and be arranged on securely on unmanned plane 200.
Certainly, be appreciated that be, snap close draw-in groove 104 also can be directly arranged on the sidewall in loading cabin 110, such as, on front side wall snap close draw-in groove 104 being arranged on loading cabin 110 and rear wall.
The simple unmanned plane 200 described according to the embodiment of the present invention below.
According to the unmanned plane 200 of the embodiment of the present invention, the loading cabin assembly 100 in fuselage 210 and above-described embodiment can be comprised.
Wherein, operationally, loading cabin assembly 100 is placed on the fuselage 210 of unmanned plane 200 unmanned plane 200.Fuselage 210 comprises and flies control device 212 and supplying cell 211.Fly to control the control center that device 212 is unmanned planes 200, supplying cell 211 can provide electric power for flying control device 212.
Loading cabin assembly 100 is removably located on fuselage 210, and when loading cabin assembly 100 is located on fuselage 210, rechargeable battery 130 is connected to power to supplying cell 211 with supplying cell 211.Thus, unmanned plane 200 is in flight course, and supplying cell 211 has sufficient electricity, ensures that unmanned plane 200 has longer cruise duration.Certainly, by loading cabin assembly 100 from after unmanned plane 200 uninstalls, the supplying cell 211 on fuselage 210 still has certain electricity, can also provide electric power for unmanned plane 100.
According to the unmanned plane 200 of the embodiment of the present invention, by loading cabin assembly 100 is located on fuselage 210, rechargeable battery 130 on loading cabin assembly 100 is connected to power to supplying cell 211 with supplying cell 211, ensure that unmanned plane 200 has the continuation of the journey of long period thus, and then unmanned plane 200 can work with security and stability.
In some embodiments of the invention, fly control device 212 and be connected to control opening or closing of goods door 120 with goods door 120.Such as, when unmanned plane 200 reaches the place that client specifies, fly control device 212 and can send signal control goods door 120 and open, goods skids off from outlet; After goods has been delivered, fly control device 212 and send signal control goods door 120 and close, then unmanned plane 200 makes a return voyage or delivers next time.In concrete example of the present invention, can after unmanned plane 200 arrive the 2s in the place that client specifies, fly control device 212 and control goods door 120 and automatically open.
It should be noted that, when in above-described embodiment, the transmission of signal and rechargeable battery 130 are powered to supplying cell 211, the transmission of electric energy is all through this interface of charge port 131, and charge port 131 can be contact power interface.
The working process of the unmanned plane 200 of the embodiment of the present invention is simply described below.
First in client's Relatively centralized regions such as dwelling district, Office Area, building district, build up express delivery terminal and join freight house storehouse, and unmanned plane 200 landing platform, charging room etc.Client directly to order the goods goods by cell-phone customer terminal, after client places an order, goods storage control system directly generates order, by artificial by Container Loading in loading cabin 110, then directly loading cabin assembly 100 is delivered to the launching platform of unmanned plane 200 by loading cabin assembly 100 feedway, is coordinated with latching system by snap close draw-in groove 104 and be fixed on unmanned plane 200 with just loading cabin assembly 100.
Then, unmanned plane 200 controls the flight path control information that received of device 212 according to flying, carry out control of taking off and fly, rechargeable battery 130 in flight course on loading cabin assembly 100 can charge to the supplying cell 211 on unmanned plane 200, to ensure that supplying cell 211 has sufficient electricity.When unmanned plane 200 arrives appointed place (such as, in the family of client), flying control device 212 and can send signal control goods door 120 and open on unmanned plane 200, goods skids off from outlet, then flies control device 212 and sends signal control goods door 120 and close.Complete unmanned plane 200 after delivering and control according to flying the landing platform that device 212 is back to unmanned plane 200 again, adopt the mode of automatic or manual loading cabin assembly 100 and fuselage 210 to be triped.Unmanned plane 200 is back to launching platform and prepares work of next time providing and delivering, and loading cabin assembly 100 is transported to charging room charging, prepares at any time to join goods after completing.
In the description of this specification sheets, specific features, structure, material or feature that the description of reference term " embodiment ", " some embodiments ", " example ", " concrete example " or " some examples " etc. means to describe in conjunction with this embodiment or example are contained at least one embodiment of the present invention or example.In this manual, to the schematic representation of above-mentioned term not must for be identical embodiment or example.And the specific features of description, structure, material or feature can combine in one or more embodiment in office or example in an appropriate manner.In addition, when not conflicting, the feature of the different embodiment described in this specification sheets or example and different embodiment or example can carry out combining and combining by those skilled in the art.
Although illustrate and describe embodiments of the invention above, be understandable that, above-described embodiment is exemplary, can not be interpreted as limitation of the present invention, and those of ordinary skill in the art can change above-described embodiment within the scope of the invention, revises, replace and modification.
Claims (10)
1. for a loading cabin assembly for unmanned plane, described unmanned plane comprises fuselage, and described fuselage is provided with supplying cell, it is characterized in that, described loading cabin assembly is removably located on described fuselage, and described loading cabin assembly comprises:
Loading cabin, described loading cabin has import and outlet, limits the chamber for bearing goods in described loading cabin;
Goods door, described goods door is located on described loading cabin and is used to open or close described outlet;
Rechargeable battery, described rechargeable battery is located on described loading cabin, and described rechargeable battery has the charge port being suitable for being connected with external power supply, and described rechargeable battery is suitable for coordinating to charge to described supplying cell with described supplying cell.
2. the loading cabin assembly for unmanned plane according to claim 1, is characterized in that, the left and right sidewall in described loading cabin is respectively equipped with a described rechargeable battery.
3. the loading cabin assembly for unmanned plane according to claim 2, is characterized in that, the left and right sidewall in described loading cabin being respectively equipped with the holding tank for holding described rechargeable battery.
4. the loading cabin assembly for unmanned plane according to claim 3, is characterized in that, also comprises the mounting clamp for being positioned at by described rechargeable battery in described holding tank.
5. the loading cabin assembly for unmanned plane according to claim 4, it is characterized in that, each described holding tank runs through the corresponding sidewall in described loading cabin in the longitudinal direction respectively, and described mounting clamp is formed on left and right directions and above-below direction and locates corresponding described rechargeable battery.
6. the loading cabin assembly for unmanned plane according to claim 3, it is characterized in that, a part for each described rechargeable battery is exposed from described holding tank in the lateral direction.
7. the loading cabin assembly for unmanned plane according to claim 1, is characterized in that, the roof of described chamber opens wide to limit described import, and the diapire of described chamber opens wide to limit described outlet.
8. the loading cabin assembly for unmanned plane according to claim 1, it is characterized in that, described goods door is automatic shutter.
9. a unmanned plane, is characterized in that, comprising:
Fuselage, described fuselage comprises and flies control device and supplying cell;
Loading cabin assembly according to any one of claim 1-8, described loading cabin assembly is removably located on described fuselage, when described loading cabin assembly is located on described fuselage, described rechargeable battery is connected to power to described supplying cell with described supplying cell.
10. unmanned plane according to claim 9, is characterized in that, described in fly control device be connected to control opening or closing of described goods door with described goods door.
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| 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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| 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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| CN104743121B CN104743121B (en) | 2018-03-27 |
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