技术领域technical field
本发明涉及无人机技术领域，特别涉及一种用于无人机的载货舱组件及具有其的无人机。The invention relates to the technical field of unmanned aerial vehicles, in particular to a cargo compartment assembly for an unmanned aerial vehicle and an unmanned aerial vehicle with the same.
背景技术Background technique
目前，现有快递业终端配送体系基本全部采用人力配送方式，其最大的不足之处在于：配货效率低、配货成本高和用户接货时间与送货时间不对称问题。因此将来无人机应用在快递终端配送体系是必然的趋势，目前，全球知名的快递公司也开始关注无人机送货方式，并开始进行相关的技术研究，但目前设计的送货无人机投递误差大、载重量低、需要人力收货。At present, the existing terminal distribution system of the express delivery industry basically adopts the manual distribution method. Its biggest shortcomings are: low distribution efficiency, high distribution cost, and asymmetrical delivery time and receiving time. Therefore, the application of drones in the delivery system of express delivery terminals in the future is an inevitable trend. At present, world-renowned express companies have also begun to pay attention to the delivery methods of drones, and have begun to conduct related technical research, but the delivery drones currently designed The delivery error is large, the load capacity is low, and manpower is required to receive the goods.
发明内容Contents of the invention
本发明旨在至少在一定程度上解决相关技术中的技术问题之一。为此，本发明的一个目的在于提出一种用于无人机的载货舱组件，该载货舱组件可以为无人机提供充足的电力，且提高了载货舱的周期循环使用率。The present invention aims to solve one of the technical problems in the related art at least to a certain extent. Therefore, an object of the present invention is to provide a cargo compartment assembly for an unmanned aerial vehicle, which can provide sufficient power for the unmanned aerial vehicle and improve the cycle utilization rate of the cargo compartment.
本发明的另一个目的在于提出一种具有上述载货舱组件的无人机。Another object of the present invention is to provide an unmanned aerial vehicle having the above-mentioned cargo compartment assembly.
根据本发明的用于无人机的载货舱组件，所述无人机包括机身，所述机身上设有供电电池，所述载货舱组件可拆卸地设在所述机身上，所述载货舱组件包括：载货舱，所述载货舱具有进口和出口，所述载货舱内限定出用于承载货物的腔室；货门，所述货门设在所述载货舱上用于打开或关闭所述出口；充电电池，所述充电电池设在所述载货舱上，所述充电电池具有适于与外部电源相连的充电口，所述充电电池适于与所述供电电池配合以对所述供电电池充电。According to the cargo compartment assembly for a drone of the present invention, the drone includes a fuselage, the fuselage is provided with a power supply battery, and the cargo compartment assembly is detachably arranged on the fuselage, so The cargo compartment assembly includes: a cargo compartment, the cargo compartment has an inlet and an outlet, and a chamber for carrying goods is defined in the cargo compartment; a cargo door, the cargo door is arranged on the cargo compartment for opening or close the outlet; a rechargeable battery, the rechargeable battery is arranged on the cargo compartment, the rechargeable battery has a charging port suitable for connecting with an external power supply, and the rechargeable battery is suitable for cooperating with the power supply battery to The power supply battery is charged.
根据本发明的用于无人机的载货舱组件，通过在载货舱上设置货门，使得无人机可以只投递货物，而不必同时投递载货舱，提高了载货舱的周期循环使用率，实现快递配送的需求，方便载货舱的回收再利用。According to the cargo compartment assembly for unmanned aerial vehicle of the present invention, by setting the cargo door on the cargo compartment, the drone can only deliver the goods without having to deliver the cargo compartment at the same time, which improves the cycle utilization rate of the cargo compartment and realizes The demand for express delivery facilitates the recycling and reuse of the cargo compartment.
此外，通过在载货舱上设置充电电池，可以在无人机工作时对其上的供电电池充电，保证无人机工作时具有充足的电力以及较长的续航时间。In addition, by setting the rechargeable battery on the cargo compartment, the power supply battery on the drone can be charged when it is working, so as to ensure that the drone has sufficient power and a long battery life when it is working.
另外，根据本发明的用于无人机的载货舱组件还可以具有如下附加的技术特征：In addition, the cargo compartment assembly for UAV according to the present invention can also have the following additional technical features:
根据本发明的一个实施例，所述载货舱的左右侧壁上分别设有一个所述充电电池。According to an embodiment of the present invention, one rechargeable battery is provided on the left and right side walls of the cargo compartment respectively.
根据本发明的一个实施例，所述载货舱的左右侧壁上分别设有用于容纳所述充电电池的容纳槽。According to an embodiment of the present invention, accommodating slots for accommodating the rechargeable batteries are respectively provided on the left and right side walls of the cargo compartment.
根据本发明的一个实施例，所述用于无人机的载货舱组件还包括用于将所述充电电池定位在所述容纳槽内的安装夹。According to an embodiment of the present invention, the cargo compartment assembly for an unmanned aerial vehicle further includes a mounting clip for positioning the rechargeable battery in the receiving slot.
根据本发明的一个实施例，每个所述容纳槽在前后方向上分别贯穿所述载货舱的相应的侧壁，所述安装夹被构造成在左右方向和上下方向上定位相应的所述充电电池。According to an embodiment of the present invention, each of the accommodating slots runs through the corresponding side walls of the cargo compartment in the front and rear directions, and the mounting clips are configured to position the corresponding charging slots in the left and right directions and in the up and down directions. Battery.
根据本发明的一个实施例，每个所述充电电池的一部分在左右方向上从所述容纳槽露出。According to an embodiment of the present invention, a part of each of the rechargeable batteries is exposed from the receiving groove in the left-right direction.
根据本发明的一个实施例，所述腔室的顶壁敞开以限定出所述进口，所述腔室的底壁敞开以限定出所述出口。According to an embodiment of the present invention, the top wall of the chamber is open to define the inlet, and the bottom wall of the chamber is open to define the outlet.
根据本发明的一个实施例，所述货门为自动卷帘门。According to an embodiment of the present invention, the cargo door is an automatic rolling door.
根据本发明的无人机，包括：机身，所述机身包括飞控装置和供电电池；上述的载货舱组件，所述载货舱组件可拆卸地设在所述机身上，所述载货舱组件设在所述机身上时，所述充电电池与所述供电电池相连以向所述供电电池供电。According to the UAV of the present invention, it includes: a fuselage, the fuselage includes a flight control device and a power supply battery; the above-mentioned cargo compartment assembly, which is detachably arranged on the fuselage, and When the cargo compartment assembly is arranged on the fuselage, the rechargeable battery is connected to the power supply battery to supply power to the power supply battery.
根据本发明的无人机，通过将载货舱组件设在机身上，设在载货舱组件上的充电电池与供电电池相连以向供电电池供电，由此保证无人机具有较长时间的续航，进而无人机可以安全稳定地工作。According to the unmanned aerial vehicle of the present invention, by setting the cargo compartment assembly on the fuselage, the rechargeable battery arranged on the cargo compartment assembly is connected with the power supply battery to supply power to the power supply battery, thereby ensuring that the unmanned aerial vehicle has a longer battery life , and then the UAV can work safely and stably.
另外，根据本发明的无人机还可以具有如下附加的技术特征：In addition, the drone according to the present invention can also have the following additional technical features:
根据本发明的一个实施例，所述飞控装置与所述货门相连以控制所述货门的打开或关闭。According to an embodiment of the present invention, the flight control device is connected with the cargo door to control the opening or closing of the cargo door.
附图说明Description of drawings
图1是根据本发明实施例的载货舱组件的示意图；1 is a schematic diagram of a cargo compartment assembly according to an embodiment of the present invention;
图2是根据本发明实施例的无人机的示意图；Fig. 2 is a schematic diagram of an unmanned aerial vehicle according to an embodiment of the present invention;
图3是根据本发明实施例的安装夹的第一配合部的主视图；Fig. 3 is a front view of a first fitting part of a mounting clip according to an embodiment of the present invention;
图4是根据本发明实施例的安装夹的第一配合部的侧视图；Fig. 4 is a side view of a first matching portion of a mounting clip according to an embodiment of the present invention;
图5是根据本发明实施例的安装夹的第二配合部的主视图；5 is a front view of a second matching portion of the mounting clip according to an embodiment of the present invention;
图6是根据本发明实施例的安装夹的第二配合部的侧视图。Fig. 6 is a side view of a second fitting portion of the mounting clip according to an embodiment of the present invention.
附图标记：载货舱组件100，载货舱110，货门120，充电电池130，充电口131，电池锁扣132，第二配合部133，第一配合部140，本体141，锁扣滚珠142，安装夹卡扣143，进口101，容纳槽103，锁扣卡槽104，安装夹卡槽105，滚珠滑道106，锁扣环107，无人机200，机身210，供电电池211，飞控装置212。Reference signs: cargo compartment assembly 100, cargo compartment 110, cargo door 120, rechargeable battery 130, charging port 131, battery lock 132, second matching part 133, first matching part 140, body 141, locking ball 142, Mounting clip buckle 143, inlet 101, receiving slot 103, locking slot 104, mounting clip slot 105, ball slideway 106, locking ring 107, drone 200, fuselage 210, power supply battery 211, flight control device 212.
具体实施方式Detailed ways
下面详细描述本发明的实施例，所述实施例的示例在附图中示出。下面通过参考附图描述的实施例是示例性的，旨在用于解释本发明，而不能理解为对本发明的限制。Embodiments of the invention are described in detail below, examples of which are illustrated in the accompanying drawings. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.
在本发明的描述中，需要理解的是，术语“中心”、“纵向”、“横向”、“长度”、“宽度”、“厚度”、“上”、“下”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”“内”、“外”、“顺时针”、“逆时针”、“轴向”、“径向”、“周向”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本发明和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本发明的限制。In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " Back", "Left", "Right", "Vertical", "Horizontal", "Top", "Bottom", "Inner", "Outer", "Clockwise", "Counterclockwise", "Axial", The orientation or positional relationship indicated by "radial", "circumferential", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying the referred device or element Must be in a particular orientation, be constructed in a particular orientation, and operate in a particular orientation, and therefore should not be construed as limiting the invention.
此外，术语“第一”、“第二”仅用于描述目的，而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此，限定有“第一”、“第二”的特征可以明示或者隐含地包括至少一个该特征。在本发明的描述中，“多个”的含义是至少两个，例如两个，三个等，除非另有明确具体的限定。In addition, the terms "first" and "second" are used for descriptive purposes only, and cannot be interpreted as indicating or implying relative importance or implicitly specifying the quantity of indicated technical features. Thus, the features defined as "first" and "second" may explicitly or implicitly include at least one of these features. In the description of the present invention, "plurality" means at least two, such as two, three, etc., unless otherwise specifically defined.
在本发明中，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”、“固定”等术语应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或成一体；可以是机械连接，也可以是电连接或彼此可通讯；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通或两个元件的相互作用关系，除非另有明确的限定。对于本领域的普通技术人员而言，可以根据具体情况理解上述术语在本发明中的具体含义。In the present invention, unless otherwise clearly specified and limited, terms such as "installation", "connection", "connection" and "fixation" should be understood in a broad sense, for example, it can be a fixed connection or a detachable connection , or integrated; can be mechanically connected, can also be electrically connected or can communicate with each other; can be directly connected, can also be indirectly connected through an intermediary, can be the internal communication of two components or the interaction relationship between two components, Unless expressly defined otherwise. Those of ordinary skill in the art can understand the specific meanings of the above terms in the present invention according to specific situations.
在本发明中，除非另有明确的规定和限定，第一特征在第二特征“上”或“下”可以是第一和第二特征直接接触，或第一和第二特征通过中间媒介间接接触。而且，第一特征在第二特征“之上”、“上方”和“上面”可是第一特征在第二特征正上方或斜上方，或仅仅表示第一特征水平高度高于第二特征。第一特征在第二特征“之下”、“下方”和“下面”可以是第一特征在第二特征正下方或斜下方，或仅仅表示第一特征水平高度小于第二特征。In the present invention, unless otherwise clearly specified and limited, the first feature may be in direct contact with the first feature or the first and second feature may be in direct contact with the second feature through an intermediary. touch. Moreover, "above", "above" and "above" the first feature on the second feature may mean that the first feature is directly above or obliquely above the second feature, or simply means that the first feature is higher in level than the second feature. "Below", "beneath" and "beneath" the first feature may mean that the first feature is directly below or obliquely below the second feature, or simply means that the first feature is less horizontally than the second feature.
下面结合附图1至附图3对根据本发明实施例的用于无人机的载货舱组件100进行详细描述。The cargo compartment assembly 100 for an unmanned aerial vehicle according to an embodiment of the present invention will be described in detail below with reference to FIG. 1 to FIG. 3 .
首先需要说明的是，无人机200包括机身210，机身210上设有供电电池211，供电电池211可以为无人机200提供动力，使得无人机200能够安全、稳定地工作。Firstly, it should be noted that the UAV 200 includes a fuselage 210, and the fuselage 210 is provided with a power supply battery 211. The power supply battery 211 can provide power for the UAV 200, so that the UAV 200 can work safely and stably.
根据本发明实施例的用于无人机的载货舱组件100，可以包括载货舱110、货门120以及充电电池130。The cargo compartment assembly 100 for a drone according to the embodiment of the present invention may include a cargo compartment 110 , a cargo door 120 and a rechargeable battery 130 .
其中，如图1所示，载货舱110具有进口101和出口，载货舱110内限定出用于承载货物的腔室。Wherein, as shown in FIG. 1 , the cargo compartment 110 has an inlet 101 and an outlet, and a chamber for carrying cargo is defined in the cargo compartment 110 .
具体地，腔室的顶壁敞开以限定出进口101，腔室的底壁敞开以限定出出口。待投递的货物可以从载货舱110的进口101进入到载货舱110内的腔室中，货物在放置在腔室内后，优选地，货物所在的位置大致是无人机200的中心位置，这样无人机200不论是处于载货状态或是卸货状态，其重心大致不变，由此可以保证无人机200安全、平稳地飞行。Specifically, the top wall of the chamber is open to define the inlet 101 and the bottom wall of the chamber is open to define the outlet. The goods to be delivered can enter the chamber in the cargo compartment 110 from the entrance 101 of the cargo compartment 110. After the goods are placed in the chamber, preferably, the position of the goods is roughly the center of the drone 200, so that no No matter whether the man-machine 200 is in a loading state or an unloading state, its center of gravity remains roughly the same, thus ensuring the safe and stable flight of the UAV 200 .
货门120设在载货舱110上用于打开或关闭出口。无人机200处于飞行状态时，货门120关闭出口，防止货物从载货舱110内掉出；无人机200在到达客户指定地点时(例如，客户家中)，货门120将出口打开，货物从腔室内滑出，完成货物的配送。A cargo door 120 is provided on the cargo compartment 110 for opening or closing an exit. When the UAV 200 is in the flying state, the cargo door 120 closes the exit to prevent the goods from falling out of the cargo compartment 110; Slide out from the chamber to complete the distribution of goods.
由此，无人机200可以只投递货物，而不必同时投递载货舱110，提高了载货舱110的周期循环使用率，实现快递配送的需求，方便载货舱110的回收再利用。As a result, the UAV 200 can only deliver goods without delivering the cargo compartment 110 at the same time, which improves the cycle utilization rate of the cargo compartment 110 , fulfills the demand for express delivery, and facilitates the recycling and reuse of the cargo compartment 110 .
可选地，货门120可以为自动卷帘门。由此，可以降低货门120在开闭时占用的空间，使货门120的打开和关闭更加便捷。Optionally, the cargo door 120 may be an automatic rolling door. Thus, the space occupied by the cargo door 120 when opening and closing can be reduced, making the opening and closing of the cargo door 120 more convenient.
如图1和图2所示，充电电池130设在载货舱110上，充电电池130具有适于与外部电源相连的充电口131，充电电池130适于与供电电池211配合以对供电电池211充电。As shown in Figures 1 and 2, the rechargeable battery 130 is arranged on the cargo compartment 110, the rechargeable battery 130 has a charging port 131 suitable for being connected to an external power source, and the rechargeable battery 130 is suitable for cooperating with the power supply battery 211 to charge the power supply battery 211 .
也就是说，无人机200的动力是由机身210上的供电电池211提供的，在载货舱组件100置于机身210上时，载货舱组件100上的充电电池130并不直接为无人机200提供动力，而只是对供电电池211充电。由此，供电电池211在无人机200工作的过程中电力充足，保证了无人机200具有较长的续航时间，进而无人机200的飞行稳定性得到了保障。That is to say, the power of the UAV 200 is provided by the power supply battery 211 on the fuselage 210. When the cargo compartment assembly 100 is placed on the fuselage 210, the rechargeable battery 130 on the cargo compartment assembly 100 is not directly used The human-machine 200 provides power, but only charges the power supply battery 211 . Therefore, the power supply battery 211 has sufficient power during the working process of the UAV 200, which ensures that the UAV 200 has a longer battery life, and thus the flight stability of the UAV 200 is guaranteed.
可选地，如图1所示，载货舱110的左右(如图1所示的方向)侧壁上分别设有一个充电电池130。也就是说，载货舱110上设有两块充电电池130，且两块充电电池130相对设置在载货舱110的侧壁上。由此，进一步提高了无人机200的续航能力，实现无人机200自身在配送货物过程中的短时间内高效率配送，以及无人机200、载货舱110和充电电池130最优化配置，且对称设置的充电电池130可以使载货舱组件100的配重更加平衡，保证无人机200在载货运行时的安全、平稳。Optionally, as shown in FIG. 1 , a rechargeable battery 130 is respectively provided on the left and right (direction shown in FIG. 1 ) side walls of the cargo compartment 110 . That is to say, two rechargeable batteries 130 are arranged on the cargo compartment 110 , and the two rechargeable batteries 130 are arranged on the side walls of the cargo compartment 110 opposite to each other. As a result, the battery life of the UAV 200 is further improved, and the UAV 200 itself is delivered with high efficiency in a short period of time in the process of delivering goods, as well as the optimal configuration of the UAV 200, the cargo compartment 110 and the rechargeable battery 130, Moreover, the symmetrically arranged rechargeable batteries 130 can make the counterweight of the cargo compartment assembly 100 more balanced, ensuring the safety and stability of the drone 200 when it is carrying cargo.
需要说明的是，载货舱组件100可拆卸地设在无人机200的机身210上。在将载货舱组件100安装在机身210上时，载货舱组件100上的充电电池130可以通过充电口131对机身210上的供电电池211提供电力；在将载货舱组件100从无人机200上拆卸下来后，可以将外部电源接到充电电池130的充电口131上以对充电电池130进行充电。It should be noted that the cargo compartment assembly 100 is detachably arranged on the fuselage 210 of the UAV 200 . When the cargo compartment assembly 100 is installed on the fuselage 210, the rechargeable battery 130 on the cargo compartment assembly 100 can provide power to the power supply battery 211 on the fuselage 210 through the charging port 131; After the battery 200 is disassembled, an external power source can be connected to the charging port 131 of the rechargeable battery 130 to charge the rechargeable battery 130 .
也就是说，充电电池130上的充电口131既是无人机200在工作时充电电池130向供电电池211供电的接口，也是在载货舱组件100被拆卸后，外部电源对充电电池130充电时的接口。That is to say, the charging port 131 on the rechargeable battery 130 is not only an interface for the rechargeable battery 130 to supply power to the power supply battery 211 when the drone 200 is working, but also an interface for the external power supply to charge the rechargeable battery 130 after the cargo compartment assembly 100 is disassembled. interface.
根据本发明实施例的用于无人机的载货舱组件100，通过在载货舱110上设置货门120，使得无人机200可以只投递货物，而不必同时投递载货舱110，提高了载货舱110的周期循环使用率，实现快递配送的需求，方便载货舱110的回收再利用。According to the cargo compartment assembly 100 for unmanned aerial vehicles in the embodiment of the present invention, by setting the cargo door 120 on the cargo compartment 110, the drone 200 can only deliver the cargo without delivering the cargo compartment 110 at the same time, which improves the cargo compartment. The cycle utilization rate of 110 meets the needs of express delivery and facilitates the recycling and reuse of the cargo compartment 110.
此外，通过在载货舱110上设置充电电池130，可以在无人机200工作时对其上的供电电池211充电，保证无人机200工作时具有充足的电力以及较长的续航时间。In addition, by setting the rechargeable battery 130 on the cargo compartment 110, the power supply battery 211 on it can be charged when the UAV 200 is working, so as to ensure that the UAV 200 has sufficient power and a long battery life when it is working.
在发明的一些实施例中，如图1所示，载货舱110的左右侧壁上分别设有用于容纳充电电池130的容纳槽103。由此，电池可以地放入到容纳槽103内，使得腔室的整体空间更大，方便放置体积较大的货物，且充电电池130放置在容纳槽103内还可以在一定程度上提高充电电池130的稳定性。In some embodiments of the invention, as shown in FIG. 1 , accommodating slots 103 for accommodating rechargeable batteries 130 are respectively provided on the left and right side walls of the cargo compartment 110 . Thus, the battery can be safely put into the receiving groove 103, so that the overall space of the chamber is larger, and it is convenient to place larger goods, and the rechargeable battery 130 can also be placed in the receiving groove 103 to a certain extent. 130 stability.
进一步地，载货舱组件100还包括用于将充电电池130定位在容纳槽103内的安装夹。该安装夹可以将充电电池130定位在容纳槽103内，进而充电电池130可以稳定地为无人机200提供电力，保证无人机200在工作过程中充电电池130不会发生晃动，无人机200可以稳定地工作。Further, the cargo compartment assembly 100 also includes mounting clips for positioning the rechargeable battery 130 in the receiving slot 103 . The mounting clip can position the rechargeable battery 130 in the receiving groove 103, and then the rechargeable battery 130 can stably provide power for the drone 200, ensuring that the rechargeable battery 130 of the drone 200 will not shake during the working process, and the drone 200 can work stably.
具体地，如图1所示，每个容纳槽103在前后方向上分别贯穿载货舱110的相应的侧壁，安装夹被构造成在左右方向和上下方向上定位相应的充电电池130。也就是说，充电电池130在载货舱110上只可以在前后方向上移动，在上下方向和左右方向上都是不可以移动的。在充电电池130老化需要替换时，可以沿前后方向将充电电池130从载货舱110上拆卸下来。Specifically, as shown in FIG. 1 , each accommodating groove 103 runs through corresponding sidewalls of the cargo compartment 110 in the front-rear direction, and the mounting clip is configured to position the corresponding rechargeable battery 130 in the left-right direction and up-down direction. That is to say, the rechargeable battery 130 can only move in the front-back direction on the cargo compartment 110 , and cannot move in the up-down direction and left-right direction. When the rechargeable battery 130 is aging and needs to be replaced, the rechargeable battery 130 can be detached from the cargo compartment 110 along the front and rear directions.
当然，在无人机200飞行过程中，即充电电池130在对供电电池211进行充电过程中，可以设置有一个或多个止挡件来止挡充电电池130在前后方向上移动。由此，进一步保证充电电池130工作的稳定性。Of course, during the flight of the UAV 200 , that is, when the rechargeable battery 130 is charging the power supply battery 211 , one or more stoppers may be provided to stop the rechargeable battery 130 from moving forward and backward. Thus, the stability of the operation of the rechargeable battery 130 is further ensured.
在本发明的具体示例中，如图3-图6所示，每个安装夹包括设在相应的容纳槽103内的第一配合部140和设在充电电池130上的第二配合部133，容纳槽103内的第一配合部140固定在容纳槽103的内壁上，第一配合部140包括本体141，本体141上设有至少一个锁扣滚珠142，本体141的上端和下端分别设有安装夹卡扣143，每个安装夹卡扣143构造为“L”形结构且包括第一肢和第二肢，两个安装夹卡扣143的第一肢分别与本体141的上端和下端相连，两个安装夹卡扣143的第二肢分别朝向彼此延伸。两个安装夹卡扣143与本体141之间限定出安装夹卡槽105。In a specific example of the present invention, as shown in FIGS. 3-6 , each mounting clip includes a first matching portion 140 disposed in the corresponding receiving groove 103 and a second matching portion 133 disposed on the rechargeable battery 130 , The first matching part 140 in the receiving groove 103 is fixed on the inner wall of the receiving groove 103. The first matching part 140 includes a main body 141. Clip buckle 143, each installation clip buckle 143 is configured as an "L"-shaped structure and includes a first limb and a second limb, the first limbs of the two installation clip buckles 143 are respectively connected to the upper end and the lower end of the body 141, The second limbs of the two mounting clip buckles 143 respectively extend towards each other. A mounting clip groove 105 is defined between the two mounting clip buckles 143 and the body 141 .
如图5和图6所示，充电电池130安装在载货舱110上时，充电电池130的朝向载货舱110的表面上设有第二配合部133，第二配合部133上形成有至少一个滚珠滑道106，且每个滚珠滑道106上设有与锁扣滚珠142对应的锁扣环107。As shown in Figures 5 and 6, when the rechargeable battery 130 is installed on the cargo compartment 110, the surface of the rechargeable battery 130 facing the cargo compartment 110 is provided with a second mating portion 133, and at least one ball is formed on the second mating portion 133. slideways 106 , and each ball slideway 106 is provided with a locking ring 107 corresponding to the locking balls 142 .
如图6所示，第二配合部133的上端和下端分别设有竖直向外延伸的平板状的电池锁扣132，在充电电池130安装在载货舱110上时，每个电池锁扣132位于相应的安装夹卡扣143的第二肢和本体141之间。由此，如图1所示，充电电池130只能在前后方向上移动，而不能在上下方向和左右方向上移动。As shown in FIG. 6 , the upper end and the lower end of the second matching portion 133 are respectively provided with flat plate-shaped battery locks 132 extending vertically outward. When the rechargeable battery 130 is installed on the cargo compartment 110 , each battery lock 132 It is located between the second limb of the corresponding mounting clip buckle 143 and the body 141 . Therefore, as shown in FIG. 1 , the rechargeable battery 130 can only move in the front-back direction, but cannot move in the up-down direction and left-right direction.
如图3至图6并结合图1所示，第二配合部133可滑动地配合在安装夹卡槽105内，且每个锁扣滚珠140在相应的滚珠滑道106内移动，当每个锁扣滚珠142卡设在对应的锁扣环107内时，限定了充电电池130的移动自由度。由此，锁扣滚珠142与锁扣环107可以起到定位作用，保证充电电池130快速稳定地安装在载货舱110上。3 to 6 and shown in conjunction with FIG. 1 , the second matching portion 133 is slidably fitted in the installation clamping groove 105 , and each lock ball 140 moves in the corresponding ball slideway 106 , when each When the locking balls 142 are engaged in the corresponding locking rings 107 , the freedom of movement of the rechargeable battery 130 is limited. Thus, the locking ball 142 and the locking ring 107 can play a positioning role, ensuring that the rechargeable battery 130 is quickly and stably installed on the cargo compartment 110 .
可以理解的是，锁扣滚珠142的数目与滚珠滑道106的数目、锁扣环107的数目相同。当锁扣滚珠142为多个时，多个锁扣滚珠142可以一一对应地卡设在多个锁扣环107内。It can be understood that the number of locking balls 142 is the same as the number of ball slides 106 and the number of locking rings 107 . When there are multiple locking balls 142 , the multiple locking balls 142 can be locked in the multiple locking rings 107 one by one.
在本发明的一些实施例中，如图1所示，每个充电电池130的一部分在左右方向上从容纳槽103中露出。换言之，充电电池130并不是完全置于容纳槽103内，充电电池130的一部分从容纳槽103中露出。由此，一方面保证了载货舱110内的腔室的中间部分不至于太小，在一定程度上提高了腔室的容积；另一方面，方便充电电池130的安装和拆卸。In some embodiments of the present invention, as shown in FIG. 1 , a part of each rechargeable battery 130 is exposed from the receiving groove 103 in the left-right direction. In other words, the rechargeable battery 130 is not completely placed in the receiving groove 103 , and a part of the rechargeable battery 130 is exposed from the receiving groove 103 . Thus, on the one hand, it is ensured that the middle part of the chamber in the cargo compartment 110 is not too small, and the volume of the chamber is increased to a certain extent; on the other hand, the installation and removal of the rechargeable battery 130 is facilitated.
同时可以将充电口131设在相应的充电电池130的露出容纳槽103的部分上，从而在将载货舱组件100从无人机200上拿下来进行充电时，充电电池130露出的部分可以与充电器的形状相匹配，方便充电器对充电电池130充电。At the same time, the charging port 131 can be set on the part of the corresponding rechargeable battery 130 that exposes the accommodating groove 103, so that when the cargo compartment assembly 100 is removed from the drone 200 for charging, the exposed part of the rechargeable battery 130 can be used for charging. The shape of the rechargeable battery 130 is matched with the charger, so that the charger can charge the rechargeable battery 130 conveniently.
在本发明的具体示例中，机身210上设有锁扣装置，如图1所示，充电电池130上设有适于与锁扣装置配合的锁扣卡槽104，该锁扣卡槽104与锁扣装置配合以将载货舱组件100可拆卸地设在无人机200上，保证载货舱组件100稳定牢靠地安装在无人机200上。In a specific example of the present invention, a locking device is provided on the body 210. As shown in FIG. Cooperate with the locking device to detachably set the cargo compartment assembly 100 on the drone 200 to ensure that the cargo compartment assembly 100 is stably and securely installed on the drone 200 .
当然，可以理解得是，锁扣卡槽104也可以直接设在载货舱110的侧壁上，例如将锁扣卡槽104设置在载货舱110的前侧壁和后侧壁上。Of course, it can be understood that the locking slot 104 can also be directly provided on the side wall of the cargo compartment 110 , for example, the locking slot 104 is provided on the front side wall and the rear side wall of the cargo compartment 110 .
下面简单描述根据本发明实施例的无人机200。The drone 200 according to the embodiment of the present invention is briefly described below.
根据本发明实施例的无人机200，可以包括机身210和上述实施例中的载货舱组件100。The UAV 200 according to the embodiment of the present invention may include a fuselage 210 and the cargo compartment assembly 100 in the above embodiments.
其中，无人机200在工作时，载货舱组件100置于无人机200的机身210上。机身210包括飞控装置212和供电电池211。飞控装置212是无人机200的控制中心，供电电池211可以为飞控装置212提供电力。Wherein, when the UAV 200 is working, the cargo compartment assembly 100 is placed on the fuselage 210 of the UAV 200 . The fuselage 210 includes a flight control device 212 and a power supply battery 211 . The flight control device 212 is the control center of the UAV 200 , and the power supply battery 211 can provide power for the flight control device 212 .
载货舱组件100可拆卸地设在机身210上，载货舱组件100设在机身210上时，充电电池130与供电电池211相连以向供电电池211供电。由此，无人机200在飞行过程中，供电电池211具有充足的电量，保证无人机200具有较长的续航时间。当然，在将载货舱组件100从无人机200上卸载掉后，机身210上的供电电池211仍然具有一定的电量，还可以为无人机100提供电力。The cargo compartment assembly 100 is detachably disposed on the fuselage 210 . When the cargo compartment assembly 100 is disposed on the fuselage 210 , the rechargeable battery 130 is connected to the power supply battery 211 to supply power to the power supply battery 211 . Therefore, during the flight of the UAV 200, the power supply battery 211 has sufficient power to ensure that the UAV 200 has a longer battery life. Of course, after the cargo compartment assembly 100 is unloaded from the UAV 200 , the power supply battery 211 on the fuselage 210 still has a certain amount of power and can also provide power for the UAV 100 .
根据本发明实施例的无人机200，通过将载货舱组件100设在机身210上，载货舱组件100上的充电电池130与供电电池211相连以向供电电池211供电，由此保证无人机200具有较长时间的续航，进而无人机200可以安全稳定地工作。According to the unmanned aerial vehicle 200 of the embodiment of the present invention, by setting the cargo compartment assembly 100 on the fuselage 210, the rechargeable battery 130 on the cargo compartment assembly 100 is connected with the power supply battery 211 to supply power to the power supply battery 211, thereby ensuring that no one The unmanned aerial vehicle 200 has a longer battery life, and then the unmanned aerial vehicle 200 can work safely and stably.
在本发明的一些实施例中，飞控装置212与货门120相连以控制货门120的打开或关闭。例如，在无人机200到达了客户指定的地点时，飞控装置212可以发出信号控制货门120打开，货物从出口滑出；货物投递完成后，飞控装置212发出信号控制货门120关闭，然后无人机200返航或者进行下一次投递。在本发明的具体示例中，可以在无人机200到达客户指定的地点的2s后，飞控装置212控制货门120自动打开。In some embodiments of the present invention, the flight control device 212 is connected with the cargo door 120 to control the opening or closing of the cargo door 120 . For example, when the UAV 200 arrives at the place designated by the customer, the flight control device 212 can send a signal to control the cargo door 120 to open, and the goods will slide out from the exit; after the delivery of the goods is completed, the flight control device 212 will send a signal to control the cargo door 120 to close. , and then the UAV 200 returns or delivers the next time. In a specific example of the present invention, the flight control device 212 may control the cargo door 120 to open automatically 2 seconds after the UAV 200 arrives at the place designated by the customer.
需要说明的是，上述实施例中信号的传递和充电电池130向供电电池211供电时电能的传递都经过充电口131这个接口，充电口131可以为触点式电源接口。It should be noted that in the above embodiment, the transmission of signals and the transmission of electric energy when the rechargeable battery 130 supplies power to the power supply battery 211 all pass through the interface of the charging port 131 , and the charging port 131 can be a contact power interface.
下面简单描述本发明实施例的无人机200的工作过程。The following briefly describes the working process of the drone 200 in the embodiment of the present invention.
首先在居民区、办公区、楼宇区等客户相对集中区域内建成快递终端配货仓库，以及无人机200起降平台、充电间等。客户可通过手机客户端直接订购商品货物，客户下单后，货物存储控制系统直接生成订单，由人工将货物装载至载货舱110中，然后通过载货舱组件100输送装置直接将载货舱组件100输送至无人机200的起飞平台，通过锁扣卡槽104与锁扣装置配合以将将载货舱组件100固定在无人机200上。First of all, in residential areas, office areas, building areas and other areas where customers are relatively concentrated, express delivery terminal distribution warehouses, as well as 200 take-off and landing platforms for drones, charging rooms, etc. will be built. Customers can directly order commodities through the mobile phone client. After the customer places an order, the cargo storage control system directly generates an order, and the goods are manually loaded into the cargo compartment 110, and then the cargo compartment assembly 100 is directly transported by the cargo compartment assembly 100 conveying device. To the take-off platform of the UAV 200 , the cargo compartment assembly 100 is fixed on the UAV 200 by cooperating with the locking device through the locking slot 104 .
然后，无人机200根据飞控装置212已接收的飞行路径控制信息，进行起飞和飞行控制，在飞行过程中载货舱组件100上的充电电池130可以对无人机200上的供电电池211进行充电，以保证供电电池211具有充足的电量。在无人机200到达指定地点时(例如，客户的家中)，无人机200上的飞控装置212可以发出信号控制货门120打开，货物从出口滑出，然后飞控装置212发出信号控制货门120关闭。完成投递后无人机200再根据飞控装置212回至无人机200的降落平台，采用自动或手动的方式将载货舱组件100与机身210解扣。无人机200返回至起飞平台准备下一次配送工作，载货舱组件100被输送至充电间充电，完成后随时准备配货。Then, the UAV 200 performs take-off and flight control according to the flight path control information received by the flight control device 212. Charging to ensure that the power supply battery 211 has sufficient power. When the drone 200 arrives at a designated place (for example, the customer's home), the flight control device 212 on the drone 200 can send a signal to control the cargo door 120 to open, and the goods slide out from the exit, and then the flight control device 212 sends a signal to control The cargo door 120 is closed. After the delivery is completed, the UAV 200 returns to the landing platform of the UAV 200 according to the flight control device 212 , and automatically or manually releases the cargo compartment assembly 100 from the fuselage 210 . The UAV 200 returns to the take-off platform to prepare for the next distribution work, and the cargo compartment assembly 100 is transported to the charging room for charging, and is ready for distribution at any time after completion.
在本说明书的描述中，参考术语“一个实施例”、“一些实施例”、“示例”、“具体示例”、或“一些示例”等的描述意指结合该实施例或示例描述的具体特征、结构、材料或者特点包含于本发明的至少一个实施例或示例中。在本说明书中，对上述术语的示意性表述不必须针对的是相同的实施例或示例。而且，描述的具体特征、结构、材料或者特点可以在任一个或多个实施例或示例中以合适的方式结合。此外，在不相互矛盾的情况下，本领域的技术人员可以将本说明书中描述的不同实施例或示例以及不同实施例或示例的特征进行结合和组合。In the description of this specification, descriptions referring to the terms "one embodiment", "some embodiments", "example", "specific examples", or "some examples" mean that specific features described in connection with the embodiment or example , structure, material or characteristic is included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the described specific features, structures, materials or characteristics may be combined in any suitable manner in any one or more embodiments or examples. In addition, those skilled in the art can combine and combine different embodiments or examples and features of different embodiments or examples described in this specification without conflicting with each other.
尽管上面已经示出和描述了本发明的实施例，可以理解的是，上述实施例是示例性的，不能理解为对本发明的限制，本领域的普通技术人员在本发明的范围内可以对上述实施例进行变化、修改、替换和变型。Although the embodiments of the present invention have been shown and described above, it can be understood that the above embodiments are exemplary and should not be construed as limiting the present invention, those skilled in the art can make the above-mentioned The embodiments are subject to changes, modifications, substitutions and variations.
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510164500.3ACN104743121B (en) | 2015-04-08 | 2015-04-08 | Cargo compartment assembly for unmanned aerial vehicle and unmanned aerial vehicle having same |
| Application Number | Priority Date | Filing Date | Title |
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| CN201510164500.3ACN104743121B (en) | 2015-04-08 | 2015-04-08 | Cargo compartment assembly for unmanned aerial vehicle and unmanned aerial vehicle having same |
| Publication Number | Publication Date |
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| CN104743121Atrue CN104743121A (en) | 2015-07-01 |
| CN104743121B CN104743121B (en) | 2018-03-27 |
| Application Number | Title | Priority Date | Filing Date |
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| CN201510164500.3AExpired - Fee RelatedCN104743121B (en) | 2015-04-08 | 2015-04-08 | Cargo compartment assembly for unmanned aerial vehicle and unmanned aerial vehicle having same |
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| CN (1) | CN104743121B (en) |
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