WO2018018841A1 - 无人机货舱 - Google Patents

无人机货舱 Download PDF

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Publication number
WO2018018841A1
WO2018018841A1 PCT/CN2016/112937 CN2016112937W WO2018018841A1 WO 2018018841 A1 WO2018018841 A1 WO 2018018841A1 CN 2016112937 W CN2016112937 W CN 2016112937W WO 2018018841 A1 WO2018018841 A1 WO 2018018841A1
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WO
WIPO (PCT)
Prior art keywords
horizontal portion
driving device
cargo
tripod
inclined portion
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Application number
PCT/CN2016/112937
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English (en)
French (fr)
Inventor
雷鹏涛
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顺丰科技有限公司
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Filing date
Publication date
Application filed by 顺丰科技有限公司 filed Critical 顺丰科技有限公司
Publication of WO2018018841A1 publication Critical patent/WO2018018841A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U60/00—Undercarriages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons

Definitions

  • the present disclosure relates generally to logistics transportation, and more particularly to the field of logistics transportation using drones, and more particularly to unmanned cargo bays.
  • the cargo drones of the logistics drones are mostly simple cargo structures, and are directly screwed to the drones or tied to the drones.
  • the loading and unloading of such cargo tanks is very troublesome, and it is time-consuming and laborious to manually disassemble the cargo boxes and goods.
  • a drone cargo tank comprising: a set of tripod plates arranged in parallel, the top of the tripod plate being connected by a top plate; and the lower part of the tripod plate is provided with unloading a device, the unloading device includes a horizontal portion and an inclined portion; the horizontal portion is connected between the parallel stand plates, and a parallel arrangement of the stand plate, the top plate and the horizontal portion is formed a cargo receiving space; the horizontal portion is coupled to the first driving device and is capable of conveying cargo toward or away from the inclined portion; the inclined portion is coupled to the second driving device, and one end of the inclined portion is opposite to the horizontal The portion rotates, the other end of the inclined portion is in releasable contact with the ground, and the first driving device and the second driving device are both connected to the same control system.
  • the horizontal portion includes a conveyor belt and a set of rotating wheels, the conveyor belt is tensioned on the rotating wheel, the rotating wheel is connected to the first driving device, and the rotating wheel is disposed in parallel
  • the tripod plates are rotatably coupled to the tripod plates.
  • the horizontal portion includes a plurality of first roller bodies arranged side by side, and each of the first roller bodies is respectively provided with a pulley, and each of the pulleys and a foot at a corresponding position
  • the shelf is rotatably connected, and each of the pulleys on the same side is tensioned with a belt, and at least one of the first roller bodies is coupled to the first driving device.
  • the horizontal portion includes a plurality of first roller bodies arranged side by side, and each of the first roller bodies is respectively provided with a sprocket at both ends, and each of the sprocket wheels is rotatably connected with a tripod plate at a corresponding position.
  • Each of the sprockets on the same side is tensionably provided with a chain, and at least one of the first roller bodies is connected to the first driving device.
  • the inclined portion comprises a support frame, and a plurality of second roller bodies arranged side by side disposed between the support frames, the support frame being connected to the second driving device, one end of the support frame being opposite Rotating at the horizontal portion, the other end of the support frame is releasably in contact with the ground.
  • the support frame is rotatably connected to the horizontal portion through a rotating shaft connected to the second driving device, and the horizontal portion is provided with a limiting block at an end close to the rotating shaft, and the rotating shaft and the limiting block can be Released.
  • the rotating shaft is provided with a circular arc-shaped slit
  • the slit includes a first circular arc surface, and a first positioning surface and a second positioning surface on both sides of the first circular arc surface
  • the block is provided with a second arc surface that cooperates with the shape of the first arc surface, and the first positioning surface and the second positioning surface are disengageable from the limiting block.
  • a baffle is provided on a side away from the inclined portion, the baffle being disposed at a corner position.
  • the baffle is coupled between the top plate and the stand plate, and/or the baffle is coupled between the stand plate and a first drum body remote from the inclined portion.
  • each of the tripod plates is provided with a battery compartment on a side facing away from the cargo receiving space, and the battery body can be placed in the battery compartment.
  • FIG. 1 shows a drone cargo hold in accordance with an embodiment of the present application when the inclined portion is fully opened Schematic diagram of the structure
  • FIG. 2 is a schematic view showing the structure of a cargo compartment of a drone according to an embodiment of the present application when the inclined portion is completely closed;
  • FIG. 3 is a schematic structural view showing a rear view of a cargo tank of a drone according to an embodiment of the present application
  • FIG. 4 is a schematic structural view of a unloading device of a drone cargo hold when the inclined portion is completely closed according to an embodiment of the present application;
  • Figure 5 shows an enlarged view of a portion A in Figure 4.
  • FIG. 6 is a schematic view showing the structure of a unloading device of a drone cargo hold when the inclined portion is completely closed according to an embodiment of the present application;
  • Fig. 7 shows an enlarged view of a portion B in Fig. 6.
  • the unmanned cargo hold includes: a set of tripod plates 1 arranged in parallel, and the top of the stand plate 1 is connected by the top plate 2.
  • the lower portion of the tripod plate 1 is provided with a unloading device, and the unloading device includes a horizontal portion 3 and an inclined portion 4, and the horizontal portion 3 is connected between the parallel stand plates 1.
  • a cargo accommodating space 5 is formed between the tripod plate 1, the top plate 2 and the horizontal portion 3 which are arranged in parallel, thereby realizing the integrated design of the cargo compartment and the tripod plate of the drone.
  • the horizontal portion 3 is connected to the first driving device so that the horizontal portion 3 can convey the cargo toward or away from the inclined portion 4 by the driving of the first driving device.
  • the inclined portion is connected to the fourth second driving means, so that one end of the inclined portion 4 is rotatable relative to the horizontal portion by the driving of the second driving means, so that the cargo accommodating space 5 is opened or closed. Tilt when the cargo accommodation space 5 is opened The other end of the portion 4 is in contact with the ground; and when the cargo accommodating space 5 is closed, the contact between the other end of the inclined portion 4 and the ground is released.
  • both the first driving device and the second driving device are connected to the same control system, so that the first driving device and the second driving device can be manipulated by the control system to realize automatic control of the unloading device.
  • the unmanned cargo hold can be fixed to the lower part of the drone's frame.
  • the operator can place the goods on the horizontal portion 3 and operate the first drive unit through the control system.
  • the horizontal portion 3 is caused to convey the goods in a direction away from the inclined portion 4 so that the goods reach the center position of the cargo accommodating space 5.
  • the second drive device can be operated by the control system so that the inclined portion 4 is rotated toward the horizontal portion 3 to close the cargo accommodating space 5 as shown in FIG.
  • the second driving device can be operated remotely by the control system, so that the inclined portion 4 rotates away from the horizontal portion 3 and contacts the ground at one end of the inclined portion. Stop the second drive unit from running. Then, the first drive device can be operated by the control system such that the horizontal portion 3 conveys the cargo toward the inclined portion 4. At the same time, when the cargo approaches the inclined portion 4, it will slide down the inclined portion to the ground under the action of gravity, thereby completing the automatic unloading, as shown in FIG.
  • the unmanned cargo hold is provided with a baffle 7 on a side away from the inclined portion 4, and the baffle 7 is disposed at a corner position of the unmanned cargo hold, and the baffle can be connected to the top plate 2 and Between the tripod plates 1, it is also possible to be connected between the stand plate 1 and the first drum body away from the inclined portion.
  • the arrangement of the baffles 7 serves to limit the cargo located in the cargo accommodating space 5 from slipping out of the cargo accommodating space during loading or delivery.
  • each of the tripod boards is provided with a battery compartment 6 on a side facing away from the cargo accommodating space 5, and the battery body 6 can be placed in the battery compartment 6, so that when the battery body in the use of the passenger compartment of the drone is exhausted, The battery body located in the battery compartment can be replaced.
  • the horizontal portion includes a conveyor belt and a set of rotating wheels, and the conveyor belt is tensioned on the rotating wheel.
  • the rotating wheel is coupled to the first driving device, and the first driving device can drive the rotating wheel to rotate, thereby driving the conveyor belt and conveying the cargo.
  • the rotating wheel is disposed between the parallelly arranged tripod plates and is rotatably connected with the tripod plate, so that the rotating wheel can control the driving belt to be driven toward or away from the inclined portion by rotation, thereby completing the unloading or loading of the cargo.
  • the horizontal portion includes a plurality of first drum bodies 10 arranged side by side, and each of the first drum bodies 10 is provided with a pulley 9 at each end thereof, and each pulley 9 is at a corresponding position.
  • the tripod plates are rotatably connected, and the belts 8 are tensioned on the respective pulleys on the same side, and at least one of the first drum bodies is connected to the first driving device 11.
  • a belt transmission form is formed between the pulley and the belt, and the first driving device can drive the rotation of the first roller body connected thereto, and the rotation of the first roller body causes the pulley to drive the tensioned belt to move, while the belt moves while Further driving the other first roller bodies that are not connected to the first driving device also rotates, thereby realizing the synchronous rotation of the first rolling bodies arranged side by side.
  • the goods located in the cargo accommodating space can be moved toward or away from the inclined portion by the rotational movement of the first drum body.
  • the horizontal portion may also be a plurality of first roller bodies arranged side by side, and each of the first roller bodies is respectively provided with a sprocket at each end thereof, and each sprocket is rotatably connected with the tripod plate at the corresponding position, the same side
  • Each of the sprockets is tensioned with a chain, and at least one of the first roller bodies is coupled to the first driving device.
  • a chain transmission form is formed between the sprocket and the chain
  • the first driving device can drive the rotation of the first roller body connected thereto, and the rotation of the first roller body causes the sprocket to drive the tensioned chain to move, the chain moves
  • the other first roller bodies that are not connected to the first driving device are further driven to rotate, thereby realizing the synchronous rotation of the first rolling bodies arranged side by side.
  • the goods located in the cargo accommodating space can be moved toward or away from the inclined portion by the rotational movement of the first drum body.
  • the inclined portion includes a support frame 12, and a plurality of second drum bodies 13 disposed side by side may be disposed between the support frames 12.
  • the support frame 12 is coupled to the second drive unit 14 such that one end of the support frame 12 is rotatable relative to the horizontal portion by the second drive unit 14. When the support frame is rotated away from the horizontal portion and the other end of the support frame is in contact with the ground, the inclined portion can slide the supply therefrom.
  • the other end of the support frame When the cargo is unloaded or loaded, the other end of the support frame can no longer be in contact with the ground, that is, the other end of the support frame is released from contact with the ground, rotates toward the horizontal portion, and locks when rotated to be perpendicular to the horizontal portion (eg, Figure 2 and Figure 6) to close the cargo accommodation space.
  • the inclined portion can also be a plate surface structure, and the cargo can be slid down by the surface of the plate by the action of gravity.
  • the support frame 12 passes through the second driving device 14
  • the connected rotating shaft 15 is rotatably connected to the horizontal portion, and the horizontal portion is provided with a limiting block 19 at one end near the rotating shaft.
  • the rotating shaft 15 is provided with a circular arc-shaped slit, and the slit includes a first circular arc surface 16, and a first positioning surface 18 and a second positioning surface 17 on both sides of the first circular arc surface.
  • the limiting block 19 is provided with a second circular arc surface 20 matched with the shape of the first circular arc surface 16, so that during the rotation of the rotating shaft, the first circular arc surface 16 can cooperate with the second circular arc surface 20, so that The rotation process is smoother. As shown in FIG.
  • the second driving device 14 drives the rotating shaft 15 to rotate the support frame 12 away from the horizontal portion.
  • the first positioning surface 18 abuts the limiting block 19
  • the support frame 12 does not continue to rotate, and this At the same time, the inclined portion is also in contact with the ground and is fully opened.
  • the second driving device 14 drives the rotating shaft 15 to rotate the support frame 12 toward the horizontal portion, and the relationship between the first positioning surface 18 and the limiting block 19 is released.
  • FIG. 6 and FIG. 7 when the second positioning surface 17 abuts the limiting block 19, the support frame 12 no longer continues to rotate and is maintained at a position perpendicular to the horizontal portion to prevent the cargo from being transported. Sliding down.

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  • Aviation & Aerospace Engineering (AREA)
  • Loading Or Unloading Of Vehicles (AREA)
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Abstract

一种无人机货舱，包括一组平行设置的脚架板（1），脚架板（1）的顶部由顶板（2）连接；脚架板（1）的下部设有卸货装置，卸货装置包括水平部（3）和倾斜部（4）；水平部（3）连接于平行的脚架板（1）之间，平行设置的脚架板（1）、顶板（2）和水平部（3）之间形成了货物容纳空间；水平部（3）与第一驱动装置连接，并可朝向或背离倾斜部（4）传送货物；倾斜部（4）与第二驱动装置连接，倾斜部（4）的一端可相对于水平部（3）转动，倾斜部（4）的另一端与地面可解除式接触，第一驱动装置和第二驱动装置均与同一控制系统连接。该无人机货舱能够自动装卸货物，操作简单方便。

Description

无人机货舱 技术领域
本公开一般涉及物流运输，具体涉及使用无人机的物流运输领域，尤其涉及无人机货舱。
背景技术
目前，物流无人机货舱多为简易的货舱结构，并且直接采用螺钉连接至无人机上，或者捆绑至无人机上。这种货舱的装卸十分麻烦，需要人为手动拆装货箱和货物，费时费力。
发明内容
鉴于现有技术中的上述缺陷或不足，期望提供一种能够自动卸载的无人机货舱。
根据本公开提供了一种无人机货舱，所述无人机货舱包括：一组平行设置的脚架板，所述脚架板的顶部由顶板连接；所述脚架板的下部设有卸货装置，所述卸货装置包括水平部和倾斜部；所述水平部连接于平行的所述脚架板之间，平行设置的所述脚架板、所述顶板和所述水平部之间形成了货物容纳空间；所述水平部与第一驱动装置连接，并可朝向或背离所述倾斜部传送货物；所述倾斜部与第二驱动装置连接，所述倾斜部的一端可相对于所述水平部转动，所述倾斜部的另一端与地面可解除式接触，所述第一驱动装置和所述第二驱动装置均与同一控制系统连接。
优选地，所述水平部包括传送带和一组旋转轮，所述传送带张紧设置在所述旋转轮上，所述旋转轮与所述第一驱动装置连接，所述旋转轮设置在平行设置的所述脚架板之间并与所述脚架板转动连接。
优选地，所述水平部包括多个并排设置的第一滚筒体，每个所述第一滚筒体两端分别设有皮带轮，每个所述皮带轮与对应位置处的脚 架板转动连接，同一侧的各个所述皮带轮上张紧设有皮带，至少一个所述第一滚筒体与所述第一驱动装置连接。
优选地，所述水平部包括多个并排设置的第一滚筒体，每个所述第一滚筒体两端分别设有链轮，每个所述链轮与对应位置处的脚架板转动连接，同一侧的各个所述链轮上张紧设有链条，至少一个所述第一滚筒体与所述第一驱动装置连接。
优选地，所述倾斜部包括支撑架，和设置在所述支撑架之间的多个并排设置的第二滚筒体，所述支撑架与第二驱动装置连接，所述支撑架的一端可相对于所述水平部转动，所述支撑架的另一端与地面可解除式接触。
优选地，所述支撑架通过与第二驱动装置连接的转轴与所述水平部转动连接，所述水平部在靠近所述转轴的一端设有限位块，所述转轴与所述限位块可解除式相抵。
优选地，所述转轴上设有圆弧形的切口，所述切口包括第一圆弧面，和位于所述第一圆弧面两侧的第一定位面和第二定位面，所述限位块上设有与所述第一圆弧面形状相配合的第二圆弧面，所述第一定位面和所述第二定位面与所述限位块可解除式相抵。
优选地，在远离所述倾斜部的一侧设有挡板，所述挡板设置在拐角位置处。
优选地，所述挡板连接于所述顶板与所述脚架板之间，和/或所述挡板连接于所述脚架板与远离所述倾斜部的第一滚筒体之间。
优选地，每个所述脚架板在背离所述货物容纳空间的一侧设有电池舱，电池本体可放置在所述电池舱内。
根据本申请的无人机货舱，由于设置了卸货装置，因此能够实现自动卸载货物。
附图说明
通过阅读参照以下附图所作的对非限制性实施例所作的详细描述，本申请的其它特征、目的和优点将会变得更明显：
图1出示了根据本申请实施例的无人机货舱在倾斜部完全打开时 的结构示意图；
图2出示了根据本申请实施例的无人机货舱在倾斜部完全关闭时的结构示意图；
图3出示了根据本申请实施例的无人机货舱的后视角的结构示意图；
图4出示了根据本申请实施例的无人机货舱在倾斜部完全关闭时的卸货装置的结构示意图；
图5出示了图4中的A部放大图；
图6出示了根据本申请实施例的无人机货舱在倾斜部完全关闭时的卸货装置的结构示意图；以及
图7出示了图6中的B部放大图。
具体实施方式
下面结合附图和实施例对本申请作进一步的详细说明。可以理解的是，此处所描述的具体实施例仅仅用于解释相关发明，而非对该发明的限定。另外还需要说明的是，为了便于描述，附图中仅示出了与发明相关的部分。
需要说明的是，在不冲突的情况下，本申请中的实施例及实施例中的特征可以相互组合。下面将参考附图并结合实施例来详细说明本申请。
请参考图1-图7，其示出了根据本申请实施例的无人机货舱的技术方案。如图1-图3所示，无人机货舱包括：一组平行设置的脚架板1，脚架板1的顶部由顶板2连接。脚架板1的下部设有卸货装置，卸货装置包括水平部3和倾斜部4，水平部3连接于平行的脚架板1之间。平行设置的脚架板1、顶板2和水平部3之间形成了货物容纳空间5，从而实现了无人机货舱与脚架板一体化设计。水平部3与第一驱动装置连接，从而通过第一驱动装置的驱动，水平部3可以向着朝向或背离倾斜部4的方向传送货物。倾斜部与4第二驱动装置连接，从而通过第二驱动装置的驱动，倾斜部4的一端可相对于水平部转动，实现打开或者关闭货物容纳空间5。在货物容纳空间5打开时，倾斜 部4的另一端与地面接触；而当货物容纳空间5关闭时，倾斜部4的另一端与地面之间的接触被解除。优选地，第一驱动装置和第二驱动装置均与同一控制系统连接，从而可以通过控制系统来操控第一驱动装置和第二驱动装置，实现对卸货装置的自动化控制。这样，无人机货舱可以固定在无人机的机架下部，当在发货地装载货物时，操作人员可以将货物放置在水平部3上，并通过控制系统操控第一驱动装置运行，从而使得水平部3向着背离倾斜部4的方向传送货物，以便货物到达货物容纳空间5的中心位置处。接着，可以通过控制系统操控第二驱动装置运行，从而使得倾斜部4朝向水平部3转动，以便关闭货物容纳空间5，如图2所示。当无人机到达收货地点后，需要卸载货物，此时，可以通过控制系统远程操作第二驱动装置运行，从而使得倾斜部4背离水平部3转动，并在倾斜部的一端与地面接触后，停止第二驱动装置运行。接着，可以通过控制系统操控第一驱动装置运行，以使得水平部3向着朝向倾斜部4的方向传送货物。与此同时，当货物靠近至倾斜部4时，会在重力的作用下，沿着倾斜部下滑到地面，从而完成自动卸货，如图1所示。
进一步优选地，如图3所示，无人机货舱在远离倾斜部4的一侧设有挡板7，挡板7设置在无人机货舱的拐角位置处，挡板可以连接于顶板2与脚架板1之间，也可以连接于脚架板1与远离倾斜部的第一滚筒体之间。挡板7的设置起到了对位于货物容纳空间5内的货物的限位作用，防止其在装载或送货过程中从货物容纳空间内滑出。
进一步优选地，每个脚架板在背离货物容纳空间5的一侧设有电池舱6，电池舱6内可以放置电池本体，这样，当无人机货舱使用中的电池本体电量耗尽时，可以更换位于电池舱内的电池本体。
本申请的无人机货舱在上述技术方案的基础上还可以是：
水平部包括传送带和一组旋转轮，传送带张紧设置在旋转轮上。旋转轮与第一驱动装置连接，第一驱动装置可以驱动旋转轮转动，从而带动传送带传动并输送货物。旋转轮设置于平行设置的脚架板之间，并与脚架板转动连接，这样，旋转轮可以通过转动而控制传动带朝向或背离倾斜部传动，从而完成货物的卸载或装载。
优选地，如图4和图6所示，水平部包括多个并排设置的第一滚筒体10，每个第一滚筒体10两端分别设有皮带轮9，每个皮带轮9与对应位置处的脚架板转动连接，同一侧的各个皮带轮上张紧设有皮带8，至少一个第一滚筒体与第一驱动装置11连接。这样，皮带轮和皮带之间形成带传动形式，第一驱动装置可以驱动与其连接的第一滚筒体转动，而该第一滚筒体的转动会使得皮带轮带动张紧的皮带运动，皮带运动的同时又进一步带动其他的不与第一驱动装置连接的第一滚筒体也随之转动，从而实现了各个并排设置的第一滚动体的同步转动。位于货物容纳空间内的货物可以在第一滚筒体的转动运动作用下朝向或者背离倾斜部运动。
进一步优选地，水平部也可以是多个并排设置的第一滚筒体，每个第一滚筒体两端分别设有链轮，每个链轮与对应位置处的脚架板转动连接，同一侧的各个链轮上张紧设有链条，至少一个第一滚筒体与第一驱动装置连接。这样，链轮和链条之间形成链传动形式，第一驱动装置可以驱动与其连接的第一滚筒体转动，而该第一滚筒体的转动会使得链轮带动张紧的链条运动，链条运动的同时又进一步带动其他的不与第一驱动装置连接的第一滚筒体也随之转动，从而实现了各个并排设置的第一滚动体的同步转动。位于货物容纳空间内的货物可以在第一滚筒体的转动运动作用下朝向或者背离倾斜部运动。
本申请的无人机货舱在上述技术方案的基础上还可以是：
如图4和图6所示，倾斜部包括支撑架12，支撑架12之间可以设有多个并排设置的第二滚筒体13。其中，支撑架12与第二驱动装置14连接，从而在第二驱动装置14的驱动下，支撑架12的一端可相对于水平部转动。当支撑架背离水平部转动，并且支撑架的另一端与地面接触时，倾斜部可以供货物从其上滑落。而当货物卸载或者装载之后，支撑架的另一端可以不再与地面接触，即支撑架的另一端解除与地面的接触，朝向水平部转动，并在转动到与水平部垂直时锁止(如图2和图6所示)，以关闭货物容纳空间。当然，倾斜部也可以为板面结构，货物可以通过重力的作用由板面滑下。
优选地，如图5和图7所示，支撑架12通过与第二驱动装置14 连接的转轴15与水平部转动连接，水平部在靠近转轴的一端设有限位块19。转轴15上设有圆弧形的切口，切口包括第一圆弧面16，和位于第一圆弧面两侧的第一定位面18和第二定位面17。限位块19上设有与第一圆弧面16形状相配合的第二圆弧面20，这样在转轴的转动过程中，第一圆弧面16可以与第二圆弧面20配合，使得转动过程更加顺畅。如图4和图5所示，第二驱动装置14驱动转轴15以使得支撑架12背离水平部转动，当第一定位面18与限位块19相抵时，支撑架12不在继续转动，而此时，倾斜部也与地面接触，并完全打开。而当货物装载或者卸载完成后，第二驱动装置14驱动转轴15以使得支撑架12朝向水平部转动，第一定位面18与限位块19之间的相抵关系解除。如图6和图7所示，当第二定位面17与限位块19相抵时，支撑架12不再继续转动，并保持在与水平部相垂直的位置处，以防止货物在运输中的滑落。
以上描述仅为本申请的较佳实施例以及对所运用技术原理的说明。本领域技术人员应当理解，本申请中所涉及的发明范围，并不限于上述技术特征的特定组合而成的技术方案，同时也应涵盖在不脱离所述申请构思的情况下，由上述技术特征或其等同特征进行任意组合而形成的其它技术方案。例如上述特征与本申请中公开的(但不限于)具有类似功能的技术特征进行互相替换而形成的技术方案。

Claims (10)

  1. 一种无人机货舱，所述无人机货舱包括：一组平行设置的脚架板，所述脚架板的顶部由顶板连接；所述脚架板的下部设有卸货装置，所述卸货装置包括水平部和倾斜部；所述水平部连接于平行的所述脚架板之间，平行设置的所述脚架板、所述顶板和所述水平部之间形成了货物容纳空间；所述水平部与第一驱动装置连接，并可朝向或背离所述倾斜部传送货物；所述倾斜部与第二驱动装置连接，所述倾斜部的一端可相对于所述水平部转动，所述倾斜部的另一端与地面可解除式接触，所述第一驱动装置和所述第二驱动装置均与同一控制系统连接。
  2. 根据权利要求1所述的无人机货舱，其特征在于，所述水平部包括传送带和一组旋转轮，所述传送带张紧设置在所述旋转轮上，所述旋转轮与所述第一驱动装置连接，所述旋转轮设置在平行设置的所述脚架板之间并与所述脚架板转动连接。
  3. 根据权利要求1所述的无人机货舱，其特征在于，所述水平部包括多个并排设置的第一滚筒体，每个所述第一滚筒体两端分别设有皮带轮，每个所述皮带轮与对应位置处的脚架板转动连接，同一侧的各个所述皮带轮上张紧设有皮带，至少一个所述第一滚筒体与所述第一驱动装置连接。
  4. 根据权利要求1所述的无人机货舱，其特征在于，所述水平部包括多个并排设置的第一滚筒体，每个所述第一滚筒体两端分别设有链轮，每个所述链轮与对应位置处的脚架板转动连接，同一侧的各个所述链轮上张紧设有链条，至少一个所述第一滚筒体与所述第一驱动装置连接。
  5. 根据权利要求1至4中任一项权利要求所述的无人机货舱，其 特征在于，所述倾斜部包括支撑架，和设置在所述支撑架之间的多个并排设置的第二滚筒体，所述支撑架与第二驱动装置连接，所述支撑架的一端可相对于所述水平部转动，所述支撑架的另一端与地面可解除式接触。
  6. 根据权利要求5所述的无人机货舱，其特征在于，所述支撑架通过与第二驱动装置连接的转轴与所述水平部转动连接，所述水平部在靠近所述转轴的一端设有限位块，所述转轴与所述限位块可解除式相抵。
  7. 根据权利要求6所述的无人机货舱，其特征在于，所述转轴上设有圆弧形的切口，所述切口包括第一圆弧面，和位于所述第一圆弧面两侧的第一定位面和第二定位面，所述限位块上设有与所述第一圆弧面形状相配合的第二圆弧面，所述第一定位面和所述第二定位面与所述限位块可解除式相抵。
  8. 根据权利要求1至4中任一项权利要求所述的无人机货舱，其特征在于，在远离所述倾斜部的一侧设有挡板，所述挡板设置在拐角位置处。
  9. 根据权利要求8所述的无人机货舱，其特征在于，所述挡板连接于所述顶板与所述脚架板之间，和/或所述挡板连接于所述脚架板与远离所述倾斜部的第一滚筒体之间。
  10. 根据权利要求1至4中任一项权利要求所述的无人机货舱，其特征在于，每个所述脚架板在背离所述货物容纳空间的一侧设有电池舱，电池本体可放置在所述电池舱内。
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