WO2024061147A1 - 货舱及包含其的无人机 - Google Patents

货舱及包含其的无人机 Download PDF

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Publication number
WO2024061147A1
WO2024061147A1 PCT/CN2023/119321 CN2023119321W WO2024061147A1 WO 2024061147 A1 WO2024061147 A1 WO 2024061147A1 CN 2023119321 W CN2023119321 W CN 2023119321W WO 2024061147 A1 WO2024061147 A1 WO 2024061147A1
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WO
WIPO (PCT)
Prior art keywords
rule
accordance
cargo hold
amended
hatch
Prior art date
Application number
PCT/CN2023/119321
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English (en)
French (fr)
Inventor
田瑜
代春旭
Original Assignee
峰飞航空科技(昆山)有限公司
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Application filed by 峰飞航空科技(昆山)有限公司 filed Critical 峰飞航空科技(昆山)有限公司
Publication of WO2024061147A1 publication Critical patent/WO2024061147A1/zh

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/12—Releasing
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Definitions

  • the utility model relates to the field of unmanned aerial vehicles, and in particular to a cargo cabin and an unmanned aerial vehicle containing the same.
  • the utility model aims to provide a cargo hold and a UAV including the cargo hold, which has good safety and high integration and can well protect the delivery mechanism when in use.
  • the utility model provides a cargo cabin, which is used in unmanned aerial vehicles and includes:
  • the line delivery and take-up mechanism specifically includes:
  • a friction wheel configured to be able to abut or disengage from the winch wheel.
  • the power transmission unit includes:
  • a steering gear is connected to the steering gear connecting rod and is used to drive the steering gear connecting rod;
  • the line delivery and take-up mechanism further includes:
  • the power transmission unit further includes a spring, which is sleeved on the sliding rod to provide restoring force for the winch.
  • the wire releasing and retracting mechanism further includes a wheel frame, and the wheel frame is used to support the winch.
  • the hatch also includes an optional stop hinge, which is installed on the hatch and used to keep the hatch in a corresponding position after it is opened.
  • the hatch further comprises a rebound hinge, which is connected to the hatch and is used for closing the hatch.
  • the cargo hold also includes a normally closed electromagnetic lock.
  • the electromagnetic lock When the electromagnetic lock is powered on, the electromagnetic lock will demagnetize and the cargo will slide out of the hatch using gravity.
  • the utility model also provides a UAV, comprising the cargo hold as described above, wherein the cargo hold further comprises a plurality of fuselage connection points for connecting with the fuselage of the UAV.
  • the cargo cabin provided by the utility model is equipped with a wire delivery and take-up mechanism.
  • the driving devices for the wire delivery and take-up will be separated from each other to protect the driving devices and avoid damage due to excessive gravity of the cargo during unloading. The instantaneous force is too large and damages the protective drive device.
  • FIG1 is a schematic diagram of the structure of the cargo hold provided by the utility model
  • Figure 2 is a schematic structural diagram of the cargo hold provided by the utility model
  • Figure 3 is a schematic diagram of the line delivery and take-up mechanism provided by the utility model
  • FIG4 is a partial enlarged view of the line-casting and retrieving mechanism provided by the present invention.
  • Figure 5 is a top view of the winch and the friction wheel of the wire delivery and take-up mechanism provided by the utility model in contact;
  • FIG. 6 is a top view of the winch wheel and the friction wheel of the wire delivery and take-up mechanism separated according to the present invention.
  • connection should be understood in a broad sense.
  • it can be a fixed connection or a removable connection.
  • Detachable connection it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium; it can be an internal connection between two components.
  • connection should be understood in specific situations.
  • the first feature being “above” or “below” the second feature may include direct contact between the first and second features, or may include the first and second features being in direct contact with each other. Features are not in direct contact but through other features between them.
  • the terms “above”, “above” and “above” a first feature on a second feature include the first feature being directly above and diagonally above the second feature, or simply mean that the first feature is higher in level than the second feature.
  • “Below”, “under” and “under” the first feature is the second feature includes the first feature being directly below and diagonally below the second feature, or simply means that the first feature is less horizontally than the second feature.
  • the utility model provides a cargo cabin, which is specifically applied to a drone.
  • the cargo cabin specifically includes a hatch 700, and the hatch 700 is connected to the cargo compartment of the drone;
  • the cargo hold 700 also includes a line release and take-up mechanism 600, which is located in the cargo hold of the drone.
  • the wire launching and retracting mechanism 600 specifically includes a power transmission unit 200 connected to the winch 300 and a friction wheel 400.
  • the friction wheel 400 is configured to be able to abut or disengage from the winch 300 to protect the motor, etc. Line driver devices.
  • the wire delivery and take-up mechanism 600 is also equipped with a wheel frame 301 for supporting the winch 300.
  • the power transmission unit 200 of the present launching and retracting mechanism 600 also includes a steering gear 201 connected to the steering gear link 202, and the steering gear 201 is used to drive the steering gear link 202;
  • the power transmission unit 200 also includes a sliding rod 203. One end of the sliding rod 203 is connected to the steering gear connecting rod 202, and the end of the sliding rod 203 away from the steering gear connecting rod 202 is connected to the winch 300.
  • the power transmission unit 200 also includes a spring 204.
  • the spring 204 is sleeved on the sliding rod 203, and its purpose is to provide restoring force for the winch 300.
  • the wire delivery and take-up mechanism 600 of the cargo compartment provided by the present utility model specifically includes a motor 500, which is used to drive the rotation of the friction wheel 400.
  • the winch 300 in the utility model can be made of a variety of materials.
  • the winch 300 is preferably made of polyurethane material, which has the characteristics of wear resistance, chemical erosion resistance, high strength, high elasticity, and low pressure resistance. , strong shock absorption, tear resistance, radiation resistance, high load-bearing and shock absorption and buffering and other good properties.
  • Polyurethane wheels have excellent sound-absorbing properties. The wheels produce no noise during movement and can achieve a silent effect.
  • the friction wheel 400 in the present invention is also made of polyurethane material, and the reasons will not be repeated here.
  • the steering gear 201 controls the rotation of the steering gear connecting rod 202, which drives the sliding rod 203 to translate and overcome the thrust of the spring 204, thus driving the winch 300 to separate from the friction wheel 400.
  • the winch 300 and the friction wheel 400 are separated, , the winch 300 will become a free-rotating state.
  • the release and take-up mechanism 600 is in a free pay-off state.
  • the load mass may be too large, which may cause a large instantaneous impact force.
  • the winch 300 and the friction wheel 400 Separated from each other, no impact will be caused to the friction wheel 400 at this time, thereby protecting the motor connected to the friction wheel 400 .
  • the steering gear 201 starts again, the sliding rod 203 is pushed by the rotation of the steering gear connecting rod 202, the winch 300 recovers under the action of the spring 204 and re-contacts with the friction wheel 400, and then drives and friction The motor connected to the wheel 400 rotates, driving the winch wheel 300 to rotate.
  • the ropes provided on the winch 300 are preferably Kevlar ropes. Kevlar ropes have better tensile properties and can carry larger loads.
  • the hatch 700 also includes an optional stop hinge 710.
  • the optional stop hinge 710 is installed on the hatch 700 and is used to keep the hatch 700 in any position after it is opened, so as to facilitate the operation of the staff.
  • the hatch 700 also includes a rebound hinge 720, which is connected to the hatch 700 and is used for closing the hatch 700.
  • the rebound hinge 720 can provide a certain torque to the hatch 700, so as to return the hatch 700 to its original position after the cargo is dropped.
  • the cargo compartment also includes a normally closed electromagnetic lock.
  • the flight control system sends an operating signal to the steering gear 201, and the steering gear 201 controls the rotation of the steering gear link 202.
  • the sliding rod 203 overcomes the thrust of the spring 204, thereby driving the winch 300 to separate from the friction wheel 400.
  • the winch 300 and the friction wheel 400 are separated, the winch 300 will become a free-rotating state.
  • the release and recovery The wire mechanism 600 is in a free releasing state.
  • the electromagnetic lock is energized.
  • the electromagnetic lock will be demagnetized at this time, and the cargo will slide out of the cabin under the action of gravity using the releasing and taking up mechanism 600.
  • Door 700 since the winch wheel 300 and the friction wheel 400 are separated from each other, will not cause impact to the friction wheel 400 at this time, thus protecting the motor connected to the friction wheel 400 .
  • the flight control system sends a signal to the steering gear 201 again, and the steering gear 201 starts again.
  • the sliding rod 203 is pushed by the rotation of the steering gear connecting rod 202, and the winch 300 is driven by the spring 204. It recovers and comes into contact with the friction wheel 400 again, and then drives the motor connected to the friction wheel 400 to rotate, driving the winch wheel 300 to rotate.
  • the release and take-up mechanism 600 will retract the rope to complete the aerial delivery task.
  • This embodiment provides an unmanned aerial vehicle, including a cargo hold as described above.
  • the cargo hold also includes several fuselage connection points 730 for connecting to the fuselage of the unmanned aerial vehicle.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

一种应用于无人机的货舱，该货舱包括舱门（700），舱门连接于无人机货舱；货舱还包括投放收线机构（600），投放收线机构包括与绞轮（300）连接的动力传动单元（200）和摩擦轮（400），摩擦轮（400）能够抵接或脱离绞轮（300），投放收线机构位于货舱内。此外还涉及一种包括该货舱的无人机。该技术方案能够使投放收线的驱动器件互相脱离，避免因卸货时货物的重力过大造成的瞬时力过大，从而保护驱动器件。

Description

货舱及包含其的无人机 技术领域
[根据细则26改正 20.11.2023]
本实用新型涉及无人机领域，尤其涉及一种货舱及包含其的无人机。
 背景技术
[根据细则26改正 20.11.2023]
在无人机投放货物过程中，通常由于货物的重量会比较重，在投放货物的过程中，由于瞬时力过大，会对投放机构造成损坏，因此需要将投放机构保护起来，为此有必要设计一款无人机在卸货时能够保护投放机构的货舱。
[根据细则26改正 20.11.2023]
实用新型内容
[根据细则26改正 20.11.2023]
本实用新型目的在于提供一种货舱及包含其的无人机，安全性好，集成度高，在使用时能良好地保护投放机构。
[根据细则26改正 20.11.2023]
为达此目的，本实用新型采用以下技术方案：
[根据细则26改正 20.11.2023]
本实用新型提供一种货舱，应用于无人机，包括：
[根据细则26改正 20.11.2023]
舱门，所述舱门连接于所述无人机货舱；
[根据细则26改正 20.11.2023]
投放收线机构，所述投放收线机构位于所述货舱内。
[根据细则26改正 20.11.2023]
作为优选，所述投放收线机构具体包括：
[根据细则26改正 20.11.2023]
动力传动单元，所述动力传动单元连接于绞轮；
[根据细则26改正 20.11.2023]
摩擦轮，所述摩擦轮配置为能够抵接或脱离所述绞轮。
[根据细则26改正 20.11.2023]
作为优选，所述动力传动单元包括：
[根据细则26改正 20.11.2023]
舵机，所述舵机连接于舵机连杆且用于驱动所述舵机连杆；
[根据细则26改正 20.11.2023]
滑杆，所述滑杆的一端连接于所述舵机连杆，所述滑杆远离所述舵机连杆的一端连接于所述绞轮。
[根据细则26改正 20.11.2023]
作为优选，所述投放收线机构还包括：
[根据细则26改正 20.11.2023]
电机，所述电机用于驱动所述摩擦轮转动。
[根据细则26改正 20.11.2023]
作为优选，所述动力传动单元还包括弹簧，所述弹簧套接于所述滑杆上，为所述绞轮提供恢复力。
[根据细则26改正 20.11.2023]
作为优选，所述投放收线机构还包括轮架，所述轮架用于支撑所述绞轮。
[根据细则26改正 20.11.2023]
作为优选，所述舱门还包括任意停铰链，所述任意停铰链安装于所述舱门上，用于保持舱门打开后保持相应位置。
[根据细则26改正 20.11.2023]
作为优选，所述舱门还包括回弹铰链，所述回弹铰链连接于所述舱门上，用于舱门的关闭。
[根据细则26改正 20.11.2023]
作为优选，所述货舱还包括常闭型电磁锁，当所述电磁锁通电时，所述电磁锁会消磁，货物利用重力滑出所述舱门。
[根据细则26改正 20.11.2023]
本实用新型还提供了一种无人机，包括如上所述的货舱，所述货舱还包括若干个机身连接点，用于与无人机机身相连接。
[根据细则26改正 20.11.2023]
本实用新型的有益效果：
[根据细则26改正 20.11.2023]
本实用新型所提供的货舱，其具备投放收线机构，在使用的过程中，会将投放收线的驱动器件互相脱离从而起到保护驱动器件的作用，避免因卸货时货物的重力过大造成的瞬时力过大从而损坏保护驱动器件。
 附图说明
[根据细则26改正 20.11.2023]
图1是本实用新型所提供的货舱的结构示意图；
[根据细则26改正 20.11.2023]
图2是本实用新型所提供的货舱的结构示意图；
[根据细则26改正 20.11.2023]
图3是本实用新型所提供的投放收线机构的示意图；
[根据细则26改正 20.11.2023]
图4是本实用新型所提供的投放收线机构的局部放大图；
[根据细则26改正 20.11.2023]
图5是本实用新型所提供的投放收线机构的绞轮与摩擦轮相抵接的俯视图；
[根据细则26改正 20.11.2023]
图6是本实用新型所提供的投放收线机构的绞轮与摩擦轮相分离的俯视图。
 具体实施方式
[根据细则26改正 20.11.2023]
下面结合附图和实施方式进一步说明本实用新型的技术方案。可以理解的是，此处所描述的具体实施例仅仅用于解释本实用新型，而非对本实用新型的限定。另外还需要说明的是，为了便于描述，附图中仅示出了与本实用新型相关的部分而非全部。
[根据细则26改正 20.11.2023]
在本实用新型的描述中，需要说明的是，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”应做广义理解，例如，可以是固定连接，也可以是可拆卸连接；可以是机械连接，也可以是电连接；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。对于本领域的普通技术人员而言，可以具体情况理解上述术语在本实用新型中的具体含义。
[根据细则26改正 20.11.2023]
在本实用新型中，除非另有明确的规定和限定，第一特征在第二特征之“上”或之“下”可以包括第一和第二特征直接接触，也可以包括第一和第二特征不是直接接触而是通过它们之间的另外的特征接触。而且，第一特征在第二特征“之上”、“上方”和“上面”包括第一特征在第二特征正上方和斜上方，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”包括第一特征在第二特征正下方和斜下方，或仅仅表示第一特征水平高度小于第二特征。
[根据细则26改正 20.11.2023]
在本实施例的描述中，术语“上”、“下”、“右”、等方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述和简化操作，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实用新型的限制。此外，术语“第一”、“第二”仅仅用于在描述上加以区分，并没有特殊的含义。
[根据细则26改正 20.11.2023]
实施例1：
[根据细则26改正 20.11.2023]
如图1-图3所示，本实用新型提供了一种货舱，该货舱具体应用到无人机上，该货舱具体包括了舱门700，该舱门700连接于无人机的货舱上；
[根据细则26改正 20.11.2023]
进一步地，该货舱700还包括有投放收线机构600，投放收线机构600位于无人机的货舱内。
[根据细则26改正 20.11.2023]
具体地，投放收线机构600具体包括连接于绞轮300的动力传动单元200以及摩擦轮400，具体地，该摩擦轮400配置为能够抵接或脱离绞轮300，用于实现保护电机等收线驱动器件。投放收线机构600还配置有一轮架301，用于支撑绞轮300。
[根据细则26改正 20.11.2023]
参照图4-图6所示，本投放收线机构600，其动力传动单元200还包括有连接于舵机连杆202上的舵机201，该舵机201用于驱动舵机连杆202；除此之外，该动力传动单元200还包括有一滑杆203，该滑杆203的一端连接于舵机连杆202，而该滑杆203远离舵机连杆202的一端连接于绞轮300。
[根据细则26改正 20.11.2023]
值得注意的是，动力传动单元200还包括有弹簧204，弹簧204套接于滑杆203上，其目的是为绞轮300提供恢复力。
[根据细则26改正 20.11.2023]
进一步地，本实用新型所提供货舱的投放收线机构600，具体还包括有电机500，该电机500用于驱动摩擦轮400的转动。
[根据细则26改正 20.11.2023]
本实用新型中的绞轮300，可以采用多种材料制成，在本申请中，优选为聚氨酯材料制成的绞轮300，具备耐磨耗、耐化学侵蚀、高强度、高弹性、耐低压、吸震性强、耐撕裂，耐辐射，高承载和减震缓冲等良好性能。聚氨酯轮具备优良的吸音特性，轮子在运动过程中不产生噪音，可达到静音结果。同理，本实用新型中的摩擦轮400也同样采用聚氨酯材料制成，理由在此不再赘述。
[根据细则26改正 20.11.2023]
使用时，舵机201控制舵机连杆202旋转，此时带动滑杆203平动，并且克服弹簧204的推力，从而带动绞轮300脱离摩擦轮400，当绞轮300和摩擦轮400脱离后，绞轮300会变为自由转动状态，此时投放收线机构600处于自由放线状态，放线时由于负载质量过大从而可能造成瞬时的冲击力较大，由于绞轮300和摩擦轮400互相分离，此时并不会对摩擦轮400造成冲击，从而保护与摩擦轮400相连接的电机。待负载完全放出后，舵机201再次启动，滑杆203在舵机连杆202的转动下被推动，绞轮300在弹簧204的作用下恢复并与摩擦轮400重新相接触，而后驱动与摩擦轮400相连接的电机旋转，带动绞轮300旋转。特别地，绞轮300上设置的绳索，优选采用凯夫拉绳索，凯夫拉绳索的抗拉性能较好，可以承载较大的载荷。
[根据细则26改正 20.11.2023]
继续参照图1-图3可知，舱门700还包括任意停铰链710，任意停铰链710安装于舱门700上，用于保持舱门700打开后保持在任意位置，方便工作人员操作。
[根据细则26改正 20.11.2023]
进一步地，舱门700还包括回弹铰链720，回弹铰链720连接于舱门700上，用于舱门700的关闭，回弹铰链720可以给舱门700提供一定的扭矩，可完成货物投放后舱门700的归位。
[根据细则26改正 20.11.2023]
值得注意的是，货舱还包括有常闭型电磁锁，使用时，当无人机需要卸货时，飞控系统给舵机201发送运行信号，舵机201便控制舵机连杆202旋转，此时带动滑杆203平动，并且克服弹簧204的推力，从而带动绞轮300脱离摩擦轮400，当绞轮300和摩擦轮400脱离后，绞轮300会变为自由转动状态，此时投放收线机构600处于自由放线状态，此时便给电磁锁通电，因为是常闭型电磁锁，此时电磁锁会消磁，货物便在重力的作用下利用投放收线机构600滑出所述舱门700，由于绞轮300和摩擦轮400互相分离，此时并不会对摩擦轮400造成冲击，从而保护与摩擦轮400相连接的电机。待货物完全滑出后，飞控系统再次给舵机201发送信号，舵机201再次启动，此时滑杆203在舵机连杆202的转动下被推动，绞轮300在弹簧204的作用下恢复并与摩擦轮400重新相接触，而后驱动与摩擦轮400相连接的电机旋转，带动绞轮300旋转。投放收线机构600便将绳索回收，完成空中投放任务。
[根据细则26改正 20.11.2023]
实施例2：
[根据细则26改正 20.11.2023]
本实施例提供了一种无人机，包括如上面所描述的货舱，货舱还包括若干个机身连接点730，用于与无人机机身相连接。
[根据细则26改正 20.11.2023]
显然，本实用新型的上述实施例仅仅是为了清楚说明本实用新型所作的举例，而并非是对本实用新型的实施方式的限定。对于所属领域的普通技术人员来说，在上述说明的基础上还可以做出其它不同形式的变化或变动。这里无需也无法对所有的实施方式予以穷举。凡在本实用新型的精神和原则之内所作的任何修改、等同替换和改进等，均应包含在本实用新型权利要求的保护范围之内。

Claims (10)

  1. [根据细则26改正 20.11.2023]
    一种货舱，应用于无人机，其特征在于，包括：
    舱门，所述舱门连接于所述无人机货舱；
    投放收线机构，所述投放收线机构位于所述货舱内。
  2. [根据细则26改正 20.11.2023]
    根据权利要求1所述的货舱，其特征在于，所述投放收线机构具体包括：
    动力传动单元，所述动力传动单元连接于绞轮；
    摩擦轮，所述摩擦轮配置为能够抵接或脱离所述绞轮。
  3. [根据细则26改正 20.11.2023]
    根据权利要求2所述的货舱，其特征在于，所述动力传动单元包括：
    舵机，所述舵机连接于舵机连杆且用于驱动所述舵机连杆；
    滑杆，所述滑杆的一端连接于所述舵机连杆，所述滑杆远离所述舵机连杆的一端连接于所述绞轮。
  4. [根据细则26改正 20.11.2023]
    根据权利要求3所述的货舱，其特征在于，所述投放收线机构还包括：电机，所述电机用于驱动所述摩擦轮转动。
  5. [根据细则26改正 20.11.2023]
    根据权利要求4所述的货舱，其特征在于，所述动力传动单元还包括弹簧，所述弹簧套接于所述滑杆上，为所述绞轮提供恢复力。
  6. [根据细则26改正 20.11.2023]
    根据权利要求4所述的货舱，其特征在于，所述投放收线机构还包括轮架，所述轮架用于支撑所述绞轮。
  7. [根据细则26改正 20.11.2023]
    根据权利要求1所述的货舱，其特征在于，所述舱门还包括任意停铰链，所述任意停铰链安装于所述舱门上，用于保持舱门打开后保持相应位置。
  8. [根据细则26改正 20.11.2023]
    根据权利要求1所述的货舱，其特征在于，所述舱门还包括回弹铰链，所述回弹铰链连接于所述舱门上，用于舱门的关闭。
  9. [根据细则26改正 20.11.2023]
    根据权利要求1所述的货舱，其特征在于，所述货舱还包括常闭型电磁锁，当所述电磁锁通电时，所述电磁锁会消磁，货物利用重力滑出所述舱门。
  10. [根据细则26改正 20.11.2023]
    一种无人机，包括如权利要求1-9任一项所述的货舱，其特征在于，所述货舱还包括若干个机身连接点，用于与无人机机身相连接。
PCT/CN2023/119321 2022-09-19 2023-09-18 货舱及包含其的无人机 WO2024061147A1 (zh)

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