Double-nest device capable of taking off, landing and vertically lifting fixed-wing unmanned aerial vehicle and multi-rotor unmanned aerial vehicle

By designing the dual -machine nest device of fixed -wing drones and multi -rotor drones, the problem of tedious and stability of the drone transportation process can be solved. , Improve work efficiency and security.

CN222408616UActive Publication Date: 2025-01-28TSINGHUA UNIVERSITY
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Patent Information

Application Number
CN202421190860.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-28
Publication Date
2025-01-28
Estimated Expiration
2034-05-28

AI Technical Summary

Technical Problem

Existing drones need to be transported to designated locations through vehicles when performing missions. The process is cumbersome and time-consuming, which reduces execution efficiency. The drone is poor in stability during handling, which poses safety risks.

Method used

Design a dual -machine nest device with fixed wing drones and multi -rotor drones, including the body, lifting platform, rotating platform, and sliding platform, which can be stored at the same time. Human -machine, improving the efficiency and convenience of operation of drones.

Benefits of technology

Through the dual -machine nest device, the rapid take -off and landing and convenient operations of drones are realized, work efficiency and security, reduce manpower and time costs, and can manage multiple drones at the same time.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a double-nest device capable of taking off and landing and vertically lifting a fixed-wing unmanned aerial vehicle and a multi-rotor unmanned aerial vehicle, and relates to the field of unmanned aerial vehicles. The double-nest device comprises a compartment body, a top cover is arranged on the top of a side wall frame in an openable and closable mode, and a side door capable of being opened and closed is arranged on the side wall frame; the lifting platform is arranged in the compartment body in a lifting manner, and an operation space is arranged below the lifting platform; the rotating platform is rotatably arranged on the lifting platform, and the fixed-wing unmanned aerial vehicle is suitable for being parked on the rotating platform; and the sliding platform is arranged on the compartment body in a horizontal sliding mode, and the multi-rotor unmanned aerial vehicle is suitable for being parked on the sliding platform. The double-nest device simultaneously accommodates the fixed-wing unmanned aerial vehicle and the multi-rotor unmanned aerial vehicle, so that the working efficiency and the operation convenience of the unmanned aerial vehicle can be improved, and more monitoring requirements are met.
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Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and in particular to a double-machine nest device capable of taking off and landing vertical fixed-wing unmanned aerial vehicles and multi-rotor unmanned aerial vehicles. Background Art

[0002] Currently, most drones need to be transported to a designated location by vehicle before being moved to the ground for takeoff. This process is cumbersome and time-consuming, which reduces the efficiency of execution. At the same time, drones have poor stability during transportation, which poses a safety risk. The antenna equipment and command and control room that come with drones also need to be built on site, which wastes time and manpower costs and may also affect execution efficiency. In addition, when performing some tasks, multiple drones are often required, and how to protect and transport multiple drones is a difficult problem. Utility Model Content

[0003] The utility model aims to solve at least one of the technical problems existing in the prior art. To this end, the utility model proposes a double-nest device capable of taking off and landing a vertically-lifting fixed-wing UAV and a multi-rotor UAV, wherein the double-nest device capable of taking off and landing a vertically-lifting fixed-wing UAV and a multi-rotor UAV can accommodate the fixed-wing UAV and the multi-rotor UAV, and can improve the operating efficiency and convenience of the UAV.

[0004] According to the embodiment of the utility model, a double nest device for taking off and landing fixed-wing UAVs and multi-rotor UAVs comprises: a box body, the box body comprises a side wall frame and a top cover, the top cover is openably and closably arranged on the top of the side wall frame, and the side wall frame is provided with an openable and closable side door; a lifting platform, the lifting platform is liftably arranged in the box body, the upper part of the lifting platform is a first nest space, and the lower part of the lifting platform is an operation space; a rotating platform, the rotating platform is rotatably arranged on the lifting platform, and the fixed-wing UAV is suitable for being placed in the first nest space and parked on the rotating platform; a sliding platform, the sliding platform is horizontally slidably arranged on the box body and is arranged corresponding to the side door, the upper part of the sliding platform is a second nest space, the sliding platform slides into the box body and the side door is closed when the sliding platform is stored, and the side door is opened when the sliding platform is unfolded and the sliding platform at least partially extends out of the box body, so that the second nest space is placed outside the box body, and the multi-rotor UAV is suitable for parking in the second nest space.

[0005] According to the dual nest device for taking off and landing fixed-wing drones and multi-rotor drones of the embodiment of the utility model, fixed-wing drones and multi-rotor drones can be stored at the same time to meet more monitoring needs. The top cover can be opened and closed on the top of the side wall frame, which facilitates the entry and exit of large-sized fixed-wing drones. By setting a liftable lifting platform, it is used to drive the fixed-wing drone to rise and fall. By setting a rotatable rotating platform, it is convenient to adjust the direction of the fixed-wing drone. In the storage state, the longest dimension direction of the fixed-wing drone is consistent with the length direction of the first nest space, thereby saving space to the maximum extent and facilitating the transportation and storage of the platform. In the unfolded state, the top cover is opened from the top of the side wall frame, the lifting platform rises, and docks with the opened top cover to jointly form the take-off and landing runway of the fixed-wing drone, increase the take-off and landing runway of the fixed-wing drone, improve the safety of the fixed-wing drone taking off and landing, and also make the platform more stable and reliable in the unfolded state. In the take-off state, the rotating platform is adjusted to the second angle, so that the direction of the fixed-wing drone is consistent with the wind direction, so that the fixed-wing drone is safer when taking off, avoiding the probability of falling and loss during the take-off stage. A small-sized multi-rotor drone is placed on the side of the box, which makes rational use of the internal space of the box and facilitates picking up and inspection.

[0006] This dual-nest device provides a very convenient and wide range of application scenarios for the use of drones.

[0007] When the drone is idle, the dual nest device can be adjusted to a storage state, with the fixed-wing drone stored in the first nest space and the multi-rotor drone stored in the second nest space. The two spaces are closed to prevent the external environment from causing adverse effects on the drone, such as theft and damage. When the drone needs to be used, the dual nest device can be transported to the site of use by a vehicle. In some solutions, the dual nest device is even equipped with wheels at the bottom, which are used to push the dual nest device to the site of use. When in use, the operating space becomes higher, and the operator can move more freely and comfortably in the operating space. Especially when the operator needs to track the flight status of the drone or the data information obtained by the drone, such long-term tasks can be completed in the operating space, free from the hardships of wind and sun, and improve the comfort of the operator's drone mission.

[0008] The dual-machine nest device of the present application is not limited to the types of tasks that the drones that can be adapted can complete, and can be used for meteorological observation patrols, plant protection, equipment inspections, etc.

[0009] According to some embodiments of the utility model, the double-machine nest device also includes: a sliding guide assembly connected between the sliding platform and the car body, the sliding guide assembly including: a slide rail provided on the bottom wall of the car body, the slide rail extending along the retraction and expansion direction of the sliding platform; a sliding member provided on the sliding platform, the sliding member slidingly fitting on the slide rail; the sliding guide assembly includes at least two groups, and the two groups of sliding guide assemblies are spaced apart and distributed in a direction perpendicular to the retraction and expansion direction.

[0010] In some embodiments, the double machine nest device also includes: an inner nest body placed on the sliding platform, the inner nest body including: a nest seat; a hatch cover, the hatch cover is openably disposed on the nest seat, the second machine nest space is defined between the hatch cover and the nest seat, and the top of the second machine nest space is opened when the hatch cover is opened.

[0011] Specifically, the inner nest body is detachably arranged on the sliding platform, and the inner nest body further comprises moving wheels arranged at the bottom of the nest seat.

[0012] In some specific embodiments, the dual-nest device also includes: at least one of a first meteorological monitoring device and a second meteorological monitoring device; when the first meteorological monitoring device is included, it is arranged on the compartment body and is used to at least detect wind direction; when the second meteorological monitoring device is included, it is arranged on the inner nest body and is used to at least detect wind speed.

[0013] In some embodiments, a power socket is provided on the sliding platform, and the wires of the power socket are connected to the power supply in the car body; the wires are covered with a track chain, one end of the track chain is connected to the sliding platform and the other end is connected to the car body.

[0014] In some embodiments, the double-machine-nest device further includes: a partition cover disposed in the compartment, the partition cover being connected to the bottom wall of the compartment and being located below the lifting platform, and the sliding platform sliding into the partition cover when being stored.

[0015] In some embodiments, the double-machine nest device further includes: a blowing device, the blowing device is installed on the compartment or the lifting platform, the compartment is provided with a switch door, and when the double-machine nest device is in the storage state, the blowing device and the switch door are located on opposite sides of the first machine nest space;

[0016] The double-nest device also has a first blowing mode. In the first blowing mode, the top cover is closed, the switch door is opened, and the blowing device is turned on to blow out water droplets on the fixed-wing UAV and the lifting platform.

[0017] In some embodiments, the dual-nest device also includes: a battery disposed in the compartment, the battery serving as a power source, and the battery being capable of being connected to AC power for charging; the compartment is movable on a vehicle, and the dual-nest device also includes: a power take-off generator for being connected to a power system of the vehicle, the power take-off generator being electrically connected to the battery to transmit power to the battery.

[0018] In some embodiments, the dual-machine nest device further includes: a ladder, wherein the ladder satisfies one of the following conditions:

[0019] Scenario 1: The ladder is detachably arranged on the carriage;

[0020] Scenario 2: The ladder is arranged corresponding to the side door, one end of the ladder is slidably connected to the bottom wall of the compartment, the ladder is rotatable relative to the bottom wall, and when the side door is opened, one end of the ladder slides to the side door, and the other end is suitable for supporting the ground;

[0021] Scenario three: one end of the ladder is slidably connected to the sliding platform, and the ladder is rotatable relative to the sliding platform. When the sliding platform is unfolded, one end of the ladder slides to the edge of the sliding platform, and the other end is suitable for supporting the ground.

[0022] Additional aspects and advantages of the present invention will be given in part in the following description, and in part will become apparent from the following description, or will be learned through the practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] The above and / or additional aspects and advantages of the present invention will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0024] Figure 1 is a schematic diagram of the layout of the double-machine nest device in some embodiments of the present application in a storage state from a side view;

[0025] Figure 2 is a schematic diagram of the layout of the dual-machine nest device in some embodiments of the present application in a rearward view in a storage state;

[0026] Figure 3 is a schematic diagram of the layout of the dual-machine nest device in some embodiments of the present application in the rear-view direction when in the take-off state;

[0027] Figure 4 is a schematic diagram of the layout of the dual-machine nest device in some embodiments of the present application in a top-down direction in another take-off state;

[0028] Figure 5 is a schematic diagram of the rear view structure of the dual-machine nest device in some embodiments of the present application in the storage state;

[0029] Figure 6 is another side view of the dual-machine nest device in some embodiments of the present application in the storage state;

[0030] Figure 7 yes Figure 6 The schematic diagram of the internal structure layout of the double machine nest device in the storage state is shown;

[0031] Figure 8 It is a stereoscopic view of the inner nest body of some embodiments of the present application.

[0032] Reference numerals:

[0033] Double nest device 100,

[0034] The box body 10, the top cover 11, the side wall frame 13, the first driver 14, the switch door 15, the side door 16, the bottom wall 17, the sliding guide assembly 18, the slide rail 181, the sliding member 182, the partition cover 19,

[0035] Lifting platform 20, second driver 21,

[0036] Inner nest body 30, nest seat 31, hatch cover 32, moving wheel 33,

[0037] The first machine nest space 41, the operation space 42, the second machine nest space 43,

[0038] Sealing member 51, adapter plate 52, leak-proof bag 53,

[0039] Rotating platform 61, sliding platform 62, power socket 63, wire 64, crawler chain 65,

[0040] The first meteorological monitoring device 71, the second meteorological monitoring device 72,

[0041] Controller 80, operating table 81, blowing device 82, compartment ladder 83, storage battery 84, power generator 85, ladder 86, moving rod 901, driving swivel 902, driving motor 903,

[0042] Fixed-wing UAV 201 and multi-rotor UAV 202. DETAILED DESCRIPTION

[0043] The embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and cannot be understood as limiting the present invention.

[0044] In the description of the present utility model, it should be understood that the terms "upper", "lower", "top", "bottom", "inside", "outside", etc. indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model. In addition, features defined as "first" and "second" may explicitly or implicitly include one or more of the features. In the description of the present utility model, unless otherwise specified, "multiple" means two or more.

[0045] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0046] The following describes a dual-machine nest device 100 capable of taking off and landing a fixed-wing UAV and a multi-rotor UAV according to an embodiment of the present invention with reference to the accompanying drawings.

[0047] like Figure 1 and Figure 2 As shown, according to an embodiment of the utility model, a dual-nest device 100 capable of taking off and landing fixed-wing UAVs and multi-rotor UAVs includes: a box body 10, a lifting platform 20, a rotating platform 61, a sliding platform 62, etc.

[0048] The combination of the box body 10 and the lifting platform 20 is adopted to achieve stable placement, convenient transportation, and take-off and landing operations of the fixed-wing UAV 201 in the box body 10.

[0049] The dual-machine nest device 100 capable of taking off and landing fixed-wing drones and multi-rotor drones can be applied to a variety of scenarios requiring rapid deployment and evacuation of fixed-wing drones 201, such as environmental monitoring, meteorological monitoring, field exploration, fire rescue, post-disaster rescue, etc. In these scenarios, the fixed-wing drone 201 can quickly take off from the compartment 10, and then land in the compartment 10 after completing the mission, thereby achieving rapid transfer and improving work efficiency and safety.

[0050] The body 10 can be a rear body of a vehicle, a separate trailer body or other forms of body 10, and the body 10 can be carried and moved. In the present invention, the body 10 is described as the rear body of a vehicle, and no further description is given below.

[0051] like Figure 1-Figure 4 As shown, the box body 10 includes a side wall frame 13 and a top cover 11. The top of the side wall frame 13 is open, and the top cover 11 is openably arranged on the top of the box body 10. In this way, the potential impact of the external environment on the fixed-wing UAV 201, such as wind, rain, dust, etc., can be effectively isolated by closing the top cover 11, ensuring the safety of the fixed-wing UAV 201 during transportation or parking. At the same time, the top cover 11 can be easily opened when needed, providing convenience for the take-off and landing of the fixed-wing UAV 201, without taking the fixed-wing UAV 201 out of the box body, improving the convenience and efficiency of the operation of the fixed-wing UAV 201.

[0052] In some specific embodiments, there are two top covers 11, and the two top covers 11 are translationally connected to the top of the side wall frame 13. Each top cover 11 is movable under the drive of the first driver 14, and the top of the side wall frame 13 is closed when the two top covers 11 are spliced ​​together, and the top of the side wall frame 13 is opened when the two top covers 11 are moving away from each other. In some use cases, such as when performing maintenance and monitoring on the fixed-wing UAV 201, the top cover 11 is opened to facilitate the operator to stand on the lifting platform 20, and the lifting platform 20 does not need to be raised. Of course, the present application does not exclude the situation in which there are one or three top covers 11 in some embodiments, nor does it exclude the solution that the top cover 11 is rotatably connected or connected to the side wall frame 13 through a connecting rod assembly.

[0053] When there are two top covers 11, from the perspective of the fixed-wing UAV 201, the double-nest device 100 has a storage state and an expanded state. In the storage state, the two top covers 11 are spliced ​​together, which can tightly cover the top of the side wall frame 13, so that the compartment 10 forms a complete and closed top structure. In the expanded state, the two top covers 11 move in a direction away from each other to open the top of the side wall frame 13. This opening method is not only convenient and fast, but also can maximize the space and facilitate the lifting and lowering of the lifting platform 20. Moreover, in this opening and closing method, the first driver 14 does not need too much movement space, and the required driving torque does not need to be too large.

[0054] like Figure 1-Figure 2As shown, the lifting platform 20 is driven by the second driver 21 and can be lifted and lowered in the body 10. The first nest space 41 is above the lifting platform 20, and the operating space 42 is below the lifting platform 20. Specifically, when the fixed-wing UAV 201 needs to take off and land, the top cover 11 is opened first, and then the lifting platform 20 is raised. As the lifting platform 20 rises, the position of the first nest space 41 rises, so that the fixed-wing UAV 201 rises from the inner space of the body 10 to the outer space of the body 10. This process ensures that the fixed-wing UAV 201 can smoothly move from the protected environment (inside the body 10) to the open environment for takeoff or landing. In the unfolded state, the top cover 11 is opened, the lifting platform 20 rises, and the two top covers 11 are spliced ​​on the opposite sides of the lifting platform 20, and the top cover 11 and the lifting platform 20 together constitute the landing runway of the fixed-wing UAV 201. In this way, the top cover 11 is dual-purpose, which can be used as a protective cover and a landing runway, so that the activity space of the fixed-wing UAV 201 is increased.

[0055] In some Figure 2 In the illustrated embodiment, when the lifting platform 20 is raised, the lifting platform 20 is flush with the top cover 11 of the body 10. This arrangement enables the double-nest device 100 to form a continuous and complete plane, increasing the maneuvering space of the fixed-wing UAV 201 during takeoff and landing.

[0056] Of course, the present application does not exclude that in some solutions, the lifting platform 20 can continue to rise to a level higher than the top cover 11 of the compartment 10 to facilitate other operations.

[0057] like Figure 2-Figure 3 As shown, the double nest device 100 also includes a rotating platform 61, which is rotatably arranged on the lifting platform 20, and the fixed-wing UAV 201 is suitable for being placed in the first nest space 41 and parked on the rotating platform 61. The rotating platform 61 adjusts the orientation of the fixed-wing UAV 201 by rotating, which is conducive to the fixed-wing UAV 201 switching to the optimal take-off angle during the take-off stage. At the same time, during the landing stage of the fixed-wing UAV 201, since the landing angle is not fixed, the rotating platform 61 can adjust the angle between the fixed-wing UAV 201 and the lifting platform 20 by rotating, which is conducive to the lifting platform 20 descending back into the compartment 10.

[0058] In some embodiments, Figure 1 As shown, the dual-machine nest device 100 also includes a meteorological monitoring device for at least monitoring wind direction. By measuring the wind direction, the optimal take-off and landing directions of the fixed-wing UAV 201 during take-off and landing can be more accurately selected to avoid the negative impact of unfavorable wind directions such as side winds on the take-off and landing process. Optionally, the meteorological monitoring device includes a first meteorological monitoring device 71 provided on the cabin 10, which is used to at least monitor the wind direction. Of course, the first meteorological monitoring device 71 can also be provided at other locations.

[0059] like Figure 1 As shown, the double-machine nest device 100 further includes a controller 80, which is electrically connected to the first driver 14 of the top cover 11, the second driver 21 of the lifting platform 20, the third driver of the rotating platform 61, and the meteorological monitoring device to control the operation of the first driver 14, the second driver 21, and the third driver according to the monitoring results. The controller 80 can accurately control the operation of these drivers according to different states or requirements.

[0060] Specifically, the controller 80 can control the first driver 14 to drive the top cover 11 to open and close according to the received instructions or preset programs to meet the space requirements of the fixed-wing UAV 201 during take-off and landing. At the same time, the controller 80 can also control the second driver 21 to enable the lifting platform 20 to rise and fall smoothly, ensuring that the fixed-wing UAV 201 can obtain a sufficient height during take-off and landing. The controller 80 controls the third driver to enable the rotating platform 61 to rotate flexibly, thereby adjusting the direction and angle of the fixed-wing UAV 201. In addition, the controller 80 is also connected to the meteorological monitoring device, which can receive and process meteorological data in real time, thereby improving the accuracy of the operator's judgment on the take-off and landing environment of the fixed-wing UAV 201.

[0061] The dual-machine nest device 100 further includes an operation console 81, which is disposed in the operation space 42. The operation console 81 is a standard configuration provided in the cabin 10 to facilitate the control and monitoring of the drone. The operation console 81 can be a table itself, and the operator places the control computer on the operation console 81, or the operation console 81 itself is an integrated control console that integrates the functions of the control computer.

[0062] In the stowed state, the first nest space 41 of the double nest device 100 is protected inside the box 10, and in the unfolded state, the first nest space 41 rises outside the box 10, thereby increasing the take-off and landing space of the fixed-wing UAV 201. At the same time, as the lifting platform 20 rises, the operating space 82 in the box 10 becomes higher, providing a more spacious working area for the operator.

[0063] In some optional embodiments, the lifting platform 20 is at least partially made of light-transmitting components or a window is provided on the lifting platform 20. In this way, in the unfolded state, the light input from the lifting platform 20 can be significantly increased to illuminate the operating space 82, providing a brighter and more visible operating environment for the operator. Secondly, by increasing the light input, the operator can see the status of the fixed-wing UAV 201 on the lifting platform 20 more clearly, reducing the risk of misoperation or safety accidents caused by poor visibility, and increasing the convenience of operation.

[0064] Since the rotating platform 61 can rotate the fixed-wing UAV 201, the dual-machine nest device 100 can further have a take-off state.

[0065] like Figure 1 , Figure 4 As shown, in the storage state, the rotating platform 61 is at a first angle, and the first angle is a position where the longest dimension direction of the fixed-wing UAV 201 is consistent with the length direction of the first nest space 41. In this way, the longest dimension direction of the fixed-wing UAV 201 can be consistent with the length direction of the first nest space 41, and the fixed-wing UAV 201 can be accommodated to the greatest extent in a limited space, thereby improving its storage efficiency.

[0066] like Figure 2-Figure 3 As shown, in the unfolded state, the top cover 11 is opened from the top of the side wall frame 13 to provide sufficient space for the take-off and landing of the fixed-wing UAV 201. The lifting platform 20 rises, and the opened top cover 11 docks with the lifting platform 20, so that the top cover 11 and the lifting platform 20 together constitute the take-off and landing runway of the fixed-wing UAV 201, so that the fixed-wing UAV 201 can take off and land smoothly on the double-nest device 100 without the need for additional take-off and landing equipment.

[0067] In the take-off state, compared with the unfolded state, the rotating platform 61 rotates to a second angle, and the second angle is a position where the nose of the fixed-wing UAV 201 faces the wind direction measured by the meteorological monitoring device. That is to say, in the take-off state, the rotating platform 61 rotates the fixed-wing UAV 201 so that the nose faces the wind, which can minimize the impact of the side wind on the take-off of the fixed-wing UAV 201 and improve the stability and safety of the take-off. It should be noted that since the wind direction and wind speed are constantly changing, this second angle is not fixed, but needs to be determined based on the real-time measurement results of the meteorological monitoring device to ensure that the fixed-wing UAV 201 is consistent with the wind direction. By adjusting the second angle, the impact of the side wind on the take-off and flight of the fixed-wing UAV 201 can be effectively reduced, and the stability and safety of the fixed-wing UAV 201 can be improved.

[0068] In this application, if Figure 6 and Figure 7 As shown, a side door 16 that can be opened and closed is provided on the side wall frame 13. The double nest device 100 includes: a sliding platform 62, which can be horizontally slidably arranged on the body 10 and is arranged corresponding to the side door 16, and the upper part of the sliding platform 62 is the second nest space 43. When the sliding platform 62 is stored, it slides into the body 10 and the side door 16 is closed. When the sliding platform 62 is unfolded, the side door 16 is opened and the sliding platform 62 at least partially extends out of the body 10, so that the second nest space 43 is placed outside the body 10, and the multi-rotor drone 202 is suitable for parking in the second nest space 43.

[0069] In this way, the double nest device 100 can accommodate both the fixed-wing drone 201 and the multi-rotor drone 202, meeting more environmental monitoring needs. In addition, the multi-rotor drone 202 is relatively small in size, and is arranged on the side, which makes reasonable use of the internal space of the box 10 and is convenient for taking and checking.

[0070] According to the dual-nest device 100 of some embodiments of the present invention, the meteorological monitoring device also includes a wind speed monitoring component. When it is monitored that the current wind speed exceeds the wind speed threshold, the controller 80 controls the dual-nest device 100 to remain in the storage state.

[0071] In this way, if the wind speed in the external environment is too high and may pose a threat to the take-off of the fixed-wing UAV 201, the top cover 11 will not be opened and the fixed-wing UAV 201 will remain inside the compartment 10, thereby avoiding potential risks caused by strong winds.

[0072] According to some embodiments of the present invention, the dual-machine nest device 100, the weather monitoring device further includes a humidity monitoring component. When the current air humidity is detected to exceed the humidity threshold, the controller 80 controls the dual-machine nest device 100 to remain in the storage state.

[0073] It is understandable that air humidity is also a weather condition that may affect the normal operation of drones. Especially in the spring and summer in the south, the air humidity is very high. When the air humidity is close to 100%, a lot of water vapor will condense on the surface of the drone even if it is not raining. There is a risk of water contact for the precision electronic products on the drone. Therefore, humidity monitoring can reduce the risk of damage to the drone during use.

[0074] According to the dual-nest device 100 of some embodiments of the utility model, the meteorological monitoring device also includes a rainfall monitoring component. When the rainfall monitoring component detects that the current rainfall exceeds the rainfall threshold, the controller 80 controls the dual-nest device 100 to remain in the storage state. The introduction of the rainfall monitoring component enables the dual-nest device 100 to monitor the rainfall conditions in real time. When the rainfall monitoring component detects that the current rainfall exceeds the preset rainfall threshold, the controller 80 will respond quickly and control the dual-nest device 100 to remain in the storage state. This arrangement takes into account the adverse effects of rainfall on the take-off and landing of the UAV, and avoids the take-off and landing of the UAV under slippery or waterlogged conditions, thereby ensuring the safety of the UAV and the lifting platform 20. At the same time, it also avoids potential problems caused by excessive water ingress into the compartment 10.

[0075] According to some embodiments of the present invention, the dual-nest device 100, the weather monitoring device further includes an air pressure monitoring component. When the air pressure monitoring component detects that the current air pressure is lower than the air pressure threshold, the controller 80 controls the dual-nest device 100 to remain in the storage state.

[0076] It is known that low air pressure generally indicates unfavorable meteorological conditions, such as severe weather such as storms and typhoons. Under these weather conditions, the flight environment becomes unstable, posing a threat to the flight of the drone. Therefore, when the air pressure monitoring component detects low air pressure, the controller 80 can effectively avoid the take-off operation of the drone under severe weather conditions by controlling the dual-nest device 100 to remain in the storage state. The drone can be protected from potential damage. In addition, keeping the dual-nest device 100 in the storage state can also reduce the impact of external severe weather on the interior of the compartment 10 and the lifting platform 20 itself. Therefore, by responding to changes in air pressure in a timely manner and taking corresponding measures, the dual-nest device 100 can ensure the safety of itself and the drone.

[0077] Of course, considering the climate characteristics of different regions and the impact of various weather conditions that may be encountered when using drones on the operation of drones, the number and type of monitoring components configured on the meteorological monitoring device can be freely combined according to the local environmental characteristics. In addition to the above monitoring components, light intensity monitoring components, temperature monitoring components, etc. can also be added for combination selection.

[0078] In some optional embodiments, the dual-nest device 100 has a forced opening function. In this way, considering that the drone is already in the process of performing a flight mission, when the wind speed of the external environment exceeds the safety threshold, and / or the rainfall exceeds the rainfall threshold, and / or the air pressure monitoring component detects that the current air pressure is lower than the air pressure threshold, the operator can still choose to force the dual-nest device 100 to open to the deployed state, so as to recover the drone as soon as possible and avoid further losses or risks.

[0079] Of course, this forced opening function needs to be carried out under the premise of ensuring the safety of the operator. Therefore, in actual operation, it is necessary to unlock this function through specific operation instructions or identity verification to prevent misoperation or unauthorized operation.

[0080] Although the fixed-wing UAV 201 takes off, the fixed-wing UAV 201 only sets out when the weather conditions are better as monitored by the meteorological monitoring device. However, it is not ruled out that in some cases, the fixed-wing UAV 201 has been flying in the air for a period of time, and the weather changes suddenly and the fixed-wing UAV 201 needs to return to the double nest device 100 urgently. In some embodiments of the present application, the double nest device 100 is further improved to reduce the adverse effects of weather factors on the fixed-wing UAV 201. For example, in some embodiments, the double nest device 100 also includes: a blowing device 82, the blowing device 82 is installed on the box 10 or the lifting platform 20, and the box 10 is provided with a switch door 15. When the double nest device 100 is in the storage state, the blowing device 82 and the switch door 15 are located on opposite sides of the first nest space 41.

[0081] The double-nest device 100 also has a first blowing mode. In the first blowing mode, the top cover 11 is closed, the switch door 15 is opened, and the blowing device 82 is turned on to blow out water droplets on the fixed-wing UAV 201 and the lifting platform 20.

[0082] When the fixed-wing UAV 201 encounters rain, fog or high humidity during flight, the fixed-wing UAV 201 quickly returns to the rotating platform 61, and the double nest device 100 returns to the storage state. At this time, since the outside of the compartment 10 is in rain or fog, and the first nest space 41 is located below the top cover 11, the space is small and it is not suitable for the operator to climb onto the lifting platform 20. The double nest device 100 can be adjusted to the first blowing mode, that is, the switch door 15 is opened and the blowing device 82 is turned on. After the blowing device 82 is turned on, the high-speed airflow blows through the surface of the fixed-wing UAV 201, which can take away the water droplets on the surface of the fixed-wing UAV 201. The high-speed airflow blows through the surface of the lifting platform 20, which can take away the water droplets on the surface of the lifting platform 20, thereby blowing the water droplets on the fixed-wing UAV 201 and the lifting platform 20 in the direction of the switch door 15 and out of the compartment 10. In this way, the moisture on the fixed-wing UAV 201 and the lifting platform 20 can be removed as soon as possible, reducing the penetration of rain and water into the interior of the fixed-wing UAV 201 and causing the internal precision electronic products to be damaged by water.

[0083] For a large-sized fixed-wing UAV 201, if water droplets on the surface of the fixed-wing UAV 201 are wiped manually, the speed is slow. When the double-machine nest device 100 is adjusted to the first blowing mode, the water removal efficiency on the surface of the fixed-wing UAV 201 is very high.

[0084] Such an arrangement is beneficial to extending the service life of the fixed-wing UAV 201.

[0085] In addition, since the blowing device 82 can also blow away the water droplets on the lifting platform 20, it can prevent the water droplets from leaking downward into the operating space 42, thereby improving the protection of internal components.

[0086] In some specific embodiments, the blowing device 82 includes an air conditioner. When the air conditioner is included, the air conditioner is installed on the side wall frame 13 and arranged opposite to the switch door 15. When the lifting platform 20 is lowered to the lowest position, at least part of the air outlet of the air conditioner is located above the lifting platform 20, so that the double-machine nest device 100 can have a first blowing mode. In other words, the air conditioner can be used to blow away water on the fixed-wing UAV 201 and the lifting platform 20.

[0087] Of course, the air conditioner usually has a cooling mode, and the air conditioner can also be used to cool the operating space 42. In this way, it can cool down the internal instruments in a high temperature environment, and it can also cool down the operating space 42 in a high temperature environment to improve the comfort of the operator in the operating space 42.

[0088] In some embodiments, the air conditioner is a cooling and heating air conditioner, that is, the air conditioner has a cooling mode and a heating mode, so that a comfortable temperature can be maintained even in a low temperature environment.

[0089] In other embodiments, the air conditioner has a dehumidification mode, in which case the instant switch door 15 is closed, and the dehumidification of the air conditioner can achieve a drying process in the compartment 10.

[0090] In some specific embodiments, the blowing device 82 includes a fan, which is installed on the lifting platform 20 and is located at an end away from the switch door 15. In the first blowing mode, the top cover 11 is closed and the switch door 15 is opened, and the fan is turned on, and the fan can blow away the water on the fixed-wing UAV 201 and the lifting platform 20 from the opened switch door 15.

[0091] Of course, when the fan is set, the double nest device 100 also has a second blowing mode. In the second blowing mode, the top cover 11 is spliced ​​with the lifting platform 20, and the fan is turned on. That is to say, when the fixed-wing UAV 201 is lifted outside the compartment 10, the fan can also be turned on to quickly blow away the water droplets on the fixed-wing UAV 201 and the lifting platform 20. After blowing to a certain extent, the double nest device 100 is put into the storage state, and the fixed-wing UAV 201 is returned to the compartment 10. At this time, the top cover 11 is closed and the switch door 15 can be opened, and the fan is turned on. The fan further blows away and dries the water on the fixed-wing UAV 201 and the lifting platform 20.

[0092] In some embodiments, the dual-machine nest device 100 further includes: a battery 84 disposed in the compartment 10, and the battery 84 serves as a power source. In this way, the battery 84 stores electricity to supply the instruments in the dual-machine nest device 100, and can even be used to charge the fixed-wing UAV 201. In this way, the dual-machine nest device 100 can also be powered outdoors and on the move, without the need to borrow electricity from the outside, thereby improving the convenience of use and adaptability to the environment.

[0093] Specifically, the storage battery 84 can be connected to the mains for charging, so that when the dual-machine nest device 100 is moved to a charging station or other charging location, it can store electricity and can be recycled.

[0094] In some embodiments, the dual-engine nest device 100 further includes: a power generator 85 connected to the power system of the vehicle, and the power generator 85 is electrically connected to the battery 84 to transmit electricity to the battery 84. In other words, the vehicle itself has a complete power system, and a power generator 85 is additionally provided on this basis. The shaft of the power generator 85 rotates with the movement of the power system, and the generated electric energy is stored in the battery 84.

[0095] Usually, a charging port is provided on the battery 84. When the dual-machine nest device 100 is moved to a charging station, the charger of the charging station can be connected to the charging port on the battery 84 to store electricity in the battery 84. By setting the power generator 85, the battery 84 can be stored by the power system of the vehicle, so that charging can be achieved while driving, without frequent charging at the charging station. This structure is more convenient for the dual-machine nest device 100 that needs to be used for long distances and for a long time.

[0096] Specifically, the power take-off generator 85 can be connected to the engine of the vehicle, so that when the vehicle is in neutral (ie, the vehicle is stopped but the engine is still running), the power take-off generator 85 can generate electricity using the power of the engine, thereby improving the utilization rate of the engine output power.

[0097] The structure of the power generator 85 and the connection method with the engine are both prior art and will not be described in detail here.

[0098] According to some embodiments of the present invention, the dual-machine nest device 100, such as Figure 5 As shown, a ladder 83 is also included, which is located outside the car body 10 and is installed on the side wall frame 13. Through the ladder 83, it is convenient for operators to climb up to the top cover 11 or the lifting platform 20.

[0099] When necessary, the operator can easily climb to the top of the box 10 through the box ladder 83 to inspect the fixed-wing UAV 201 or observe the state in the air. The box ladder 83 is installed on the side wall frame 13, which is not only structurally stable but also does not take up too much space. In the unfolded state, the box ladder 83 leads to the landing runway, providing a convenient passage for the operator, fully considering the actual needs of the operator when maintaining, inspecting or observing the fixed-wing UAV 201, making the entire operation process more efficient and convenient.

[0100] When the stowage and unfolding platform forms a continuous and complete plane, it also improves the safety of operators. Compared with the traditional decentralized platform, the integrated platform can provide operators with a larger and continuous operating plane, ensuring the safety of operators during inspection and observation.

[0101] In some embodiments, Figure 2As shown, in the unfolded state, the top surfaces of the two top covers 11 are flush with the top surface of the lifting platform 20. The two top covers 11 constitute an extension platform of the lifting platform 20. This arrangement allows the two top covers 11 and the lifting platform 20 to form a continuous, flat operating surface, without having to worry about crossing different heights or uneven surfaces, thereby ensuring that the fixed-wing UAV 201 remains stable during the landing process, avoiding shaking or tilting caused by uneven surfaces or height differences, thereby preventing the fixed-wing UAV 201 from being damaged or having accidents. This extension platform of a continuous platform is particularly suitable for the take-off and landing operations of the fixed-wing UAV 201 in complex environments and severe weather conditions, and it can improve the safety and success rate of the take-off and landing of the fixed-wing UAV 201.

[0102] At the same time, this continuous and flat operating surface also provides a stable working platform for operators. Since the height of the top cover 11 is consistent with that of the lifting platform 20, operators do not need to worry about safety issues such as tripping or falling when moving or working, making them safer when inspecting, maintaining or observing the fixed-wing UAV 201, thereby improving the safety of operations.

[0103] In some embodiments, in the storage state, the two top covers 11 are connected by a seal 51. In this way, the sealing of the seam between the two top covers 11 can be achieved when the top covers 11 are closed, reducing the probability of rain leakage.

[0104] The seal 51 can provide a soft contact surface when the top cover 11 is closed, reduce the impact force, and thus protect the top cover 11 from damage, and avoid damage or deformation of the top cover 11 caused by hard contact between the two top covers 11. In addition, since the seal 51 has good shock absorption performance, it can effectively absorb these vibrations, making the closing process of the top cover 11 smoother. At the same time, it can also effectively reduce the friction between the two top covers 11 in the closed state, which helps to extend the service life of the top cover 11.

[0105] Optionally, a sealing protrusion and a sealing recess are respectively provided on the contact surfaces of the two top covers 11. When the two top covers 11 are butt-jointed, the sealing protrusion is inserted into the sealing recess, thereby improving the load-bearing capacity and the sealing performance.

[0106] In some specific embodiments, in the unfolded state, the two top covers 11 are connected to the lifting platform 20 through a seal 51. In this way, when the top cover 11 and the lifting platform 20 are docked, the sealing of the joint between the two can be achieved, reducing the probability of rain leakage.

[0107] This arrangement not only enhances the connection stability between the top cover 11 and the lifting platform 20, but also provides additional support for the lifting platform 20. In addition, the seal 51 can play a buffering role when the top cover 11 contacts the lifting platform 20. At the same time, it also helps to reduce the vibration and noise that may be generated by the lifting platform 20 during the take-off and landing of the fixed-wing UAV 201.

[0108] Optionally, a sealing protrusion and a sealing recess are respectively provided on the contact surface between the top cover 11 and the lifting platform 20. When the top cover 11 is docked with the lifting platform 20, the sealing protrusion is inserted into the sealing recess, thereby improving the load-bearing capacity and sealing performance.

[0109] In some embodiments, Figure 1 As shown, at least one of the front and rear ends of the lifting platform 20 is connected with an adapter plate 52 and a leak-proof bag 53. One end of the adapter plate 52 is rotatably connected to the edge of the lifting platform 20. In the expanded state, the other end of the adapter plate 52 is connected to the top of the side wall frame 13. In the retracted state, the adapter plate 52 is retracted onto the lifting platform 20. The leak-proof bag 53 is located below the adapter plate 52. The leak-proof bag 53 connects the lifting platform 20 and the side wall frame 13.

[0110] The adapter plate 52 can be retracted and extended by rotation. When the lifting platform 20 is retracted, the adapter plate 52 is retracted, so that the adapter plate 52 is separated from the body 10, and a gap appears at the edge of the lifting platform 20, and the lifting platform 20 is less hindered from moving up and down. When the lifting platform 20 is raised, the adapter plate 52 is unfolded, so that the adapter plate 52 is connected to the edge of the body 10. On the one hand, the area of ​​the landing runway of the fixed-wing UAV 201 can be increased, and on the other hand, the adapter plate 52 is used to fill the gap around the lifting platform 20 to reduce the risk of the operator stepping on the air after coming up, and the adapter plate 52 is overlapped to increase the overall stability of the lifting platform 20 and reduce shaking.

[0111] The leak-proof bag 53 is located below the adapter plate 52 , so that no matter the adapter plate 52 is unfolded or folded, it can catch rainwater leaking from above, reducing the damage caused by rainwater flowing into the car body 10 .

[0112] According to the double-machine nest device 100 of some embodiments of the utility model, at least one of the first drive 14 top cover 11 and the second drive 21 lifting platform 20 includes a moving rod 901, a driving swivel 902 and a driving motor 903. The moving rod 901 is movable relative to the side wall frame 13. The driving swivel 902 is rotatably arranged in the compartment 10, and the driving swivel 902 cooperates with the moving rod 901. When the driving swivel 902 rotates, the moving rod 901 is driven to move. The driving motor 903 is connected to the driving swivel 902 to drive the driving swivel 902 to rotate, and the driving motor 903 is electrically connected to the controller 80.

[0113] In some embodiments, the first driver 14 includes a moving rod 901, a driving swivel 902, and a driving motor 903. The moving rod 901 moves relative to the side wall frame 13, so that the double nest device 100 can smoothly transition between the storage state and the deployment state, thereby achieving a fast and stable storage and deployment operation.

[0114] The driving motor 903 is the power source of the driving rotator 902. It is connected to the driving rotator 902 and is responsible for driving the rotation of the driving rotator 902. When the driving rotator 902 rotates, it can drive the moving rod 901 to move, thereby driving the top cover 11 to retract and expand.

[0115] The driving motor 903 is electrically connected to the controller 80 , so that the controller 80 can control the operating state of the driving motor 903 , thereby achieving precise control of the dual-machine nest device 100 .

[0116] In other embodiments, the second driver 21 includes a moving rod 901, a driving swivel 902, and a driving motor 903. The driving motor 903 is responsible for driving the driving swivel 902 to rotate, so that the driving pile body drives the moving rod 901 to move, and one end of the moving rod 901 is connected to the lifting platform 20, thereby achieving the effect of the second driver 21 driving the lifting platform 20 to move up and down.

[0117] Alternatively, in some embodiments, the first driver 14 and the second driver 21 both use a matching structure of a moving rod 901, a driving swivel 902, and a driving motor 903 to realize the opening and closing of the top cover 11 and the lifting and lowering of the lifting platform 20. It is worth noting that the moving rod 901 and the driving swivel 902 corresponding to the top cover 11 and the lifting platform 20 can adopt the same structure, or different structures can be adopted according to actual needs.

[0118] In some embodiments, the moving rod 901 is a lead screw, the driving swivel 902 is a nut, and the driving motor 903 drives the nut to rotate through the transmission gear. The nut and the lead screw are closely matched, and the rotation of the nut drives the lead screw to move linearly, thereby realizing the lifting or opening and closing action of the double nest device 100.

[0119] Alternatively, the moving rod 901 is a rack, the driving swivel 902 is a driving gear, and the driving motor 903 drives the driving gear to rotate. The driving gear forms a meshing relationship with the rack, and the rack acts as the moving rod 901, and performs linear motion under the rotation of the driving gear. One end of the rack can be fixed on the side wall frame 13, and the other end is connected to the component that needs to be lifted or opened and closed. When the driving gear rotates under the drive of the driving motor 903, the meshing relationship between it and the rack causes the rack to perform linear motion. The movement of the rack further drives the components connected thereto to realize lifting or opening and closing actions, thereby completing the operation of the double-nest device 100. Due to the meshing mode of the rack and the driving gear, the structure has high transmission accuracy and load-bearing capacity, and can realize the smooth and reliable movement of the double-nest device 100.

[0120] In some embodiments, Figure 7 As shown, the double nest device 100 further includes: a sliding guide assembly 18 connected between the sliding platform 62 and the body 10. In this way, the smoothness of the horizontal sliding of the sliding platform 62 is improved, and through the connection between the sliding guide assembly 18 and the body 10, the sliding platform 62 can be supported and kept stable even if it extends out of the body 10.

[0121] Specifically, Figure 7 As shown, the sliding guide assembly 18 includes: a slide rail 181 provided on the bottom wall 17 of the body 10 and a sliding member 182 provided on the sliding platform 62, the slide rail 181 is extended along the contraction and expansion direction of the sliding platform 62, and the sliding member 182 is slidably fitted on the slide rail 181. Here, the sliding member 182 may include at least one of a slider, a roller, and a slide rod. In some solutions, the cross section of the sliding member 182 is a groove shape, etc., so that the torsional strength and bending strength can be improved.

[0122] Specifically, the sliding guide assembly 18 includes at least two groups, and the two groups of sliding guide assemblies 18 are spaced apart and distributed along a direction perpendicular to the retraction and extension direction, thereby improving the support reliability of the sliding platform 62 .

[0123] In some embodiments, Figure 8 As shown, the double nest device 100 further includes: an inner nest body 30 placed on the sliding platform 62, the inner nest body 30 includes: a nest seat 31 and a hatch 32, the hatch 32 is openably arranged on the nest seat 31, and a second nest space 43 is defined between the hatch 32 and the nest seat 31. When the hatch 32 is opened, the top of the second nest space 43 is opened. In this way, the inner nest body 30 is used to further protect the multi-rotor UAV 202 and fix it during transportation.

[0124] Specifically, the hatch cover 32 may be a sliding cover, or a rotating cover, etc. The hatch cover 32 may be opened and closed manually, or may be opened and closed by the driving of the fourth driving member.

[0125] For example, in some specific examples, the hatch 32 is connected to the nest seat 31 through a four-bar mechanism, so that when the hatch 32 is opened, it will not occupy the internal space of the second nest space 43, which is conducive to designing the second nest space 43 to a size that is compatible with the multi-rotor drone 202.

[0126] The fourth driving member can be a motor or a piston, etc., which is not limited here.

[0127] Furthermore, there are two hatch covers 32 , and when closed, the two hatch covers 32 are spliced ​​together to cover the second machine nest space 43 .

[0128] Furthermore, the inner nest 30 can be fixedly disposed on the sliding platform 62, or the inner nest 30 can be detachably disposed on the sliding platform 62, so that the inner nest 30 can be moved out of the carriage 10 when in use, and the use is more flexible.

[0129] Alternatively, if Figure 8 As shown, the inner nest body 30 also includes a moving wheel 33 provided at the bottom of the nest seat 31. In this way, the inner nest body 30 can be moved by pushing the inner nest body 30 after being placed on the ground. Alternatively, the inner nest body 30 also includes a driving device for driving the moving wheel 33 to rotate, such as the moving wheel 33 connected to a driving motor, so that the inner nest body 30 can move automatically.

[0130] In some embodiments, the weather monitoring device further includes: a second weather monitoring device 72, which is disposed on the inner nest body 30 and is used to detect at least the wind speed. The wind speed measured in this way is more accurate than that of a small-sized multi-rotor drone 202, and can determine whether the multi-rotor drone 202 is suitable for wind travel.

[0131] In some solutions, the meteorological monitoring device further includes: a first meteorological monitoring device 71 and a second meteorological monitoring device 72, so that the detection data is more comprehensive.

[0132] In some embodiments, Figure 7 As shown, a power socket 63 is provided on the sliding platform 62, and the wire 64 of the power socket 63 can be connected to the power supply in the compartment 10, and can be connected to the controller 80 in the compartment 10. Or the wire 64 is multi-stranded, part of which is a transmission line connected to the power supply, and part of which is a signal line connected to the controller 80. The setting of the power socket 63 can facilitate the charging and / or communication settings of the multi-rotor drone 202. In some schemes, an inner nest 30 is set on the sliding platform 62, and useful electrical devices are set on the inner nest 30. The setting of the power socket 63 can facilitate the charging and / or communication settings of the inner nest 30.

[0133] Specifically, the wire 64 is set to be long enough to avoid hindering the sliding and retracting of the sliding platform 62 .

[0134] Alternatively, if Figure 7 As shown, the wire 64 is a flexible wire, and the wire 64 is covered with a track chain 65, one end of the track chain 65 is connected to the sliding platform 62 and the other end is connected to the car body 10. In this way, the wire 64 is restricted by the track chain 65 to prevent the wire 64 from being clamped in the sliding guide assembly 18, thereby reducing the risk of the wire 64 being clamped off.

[0135] In some embodiments, Figure 7 As shown, the double nest device 100 further includes: a partition cover 19 disposed in the body 10, the partition cover 19 is connected to the bottom wall 17 of the body 10 and is located below the lifting platform 20, and the sliding platform 62 slides into the partition cover 19 when stored. The arrangement of the partition cover 19 forms an independent space in the body 10 where the sliding platform 62 is located, which is separated from the space for personnel activities in the operating space 42, thereby reducing collisions and improving protection.

[0136] For ease of use, in some solutions, the double nest device 100 further includes a ladder 86, which is used to facilitate the operator to climb onto the sliding platform 62 or to climb into the compartment 10. In some solutions, the ladder 86 is provided to facilitate the inner nest 30 to climb up and down the sliding platform 62 along the ladder.

[0137] For example, the ladder 86 can be detachably arranged on the car body 10. In other words, the ladder 86 can be carried at will, so that no matter it is used by the operating personnel or used by the inner nest body 30, the use position is very flexible.

[0138] For another example, the ladder 86 is provided corresponding to the side door 16, one end of the ladder 86 is slidably connected to the bottom wall 17 of the compartment 10, and the ladder 86 is rotatable relative to the bottom wall 17. When the side door 16 is opened, one end of the ladder 86 slides to the side door 16, and the other end is suitable for supporting the ground. In this way, it is convenient for the operator or the inner nest 30 to climb along the ladder 86 into the interior of the compartment 10 where the sliding platform 62 is located.

[0139] For example, one end of the ladder 86 is slidably connected to the sliding platform 62, and the ladder 86 is rotatable relative to the sliding platform 62. When the sliding platform 62 is unfolded, one end of the ladder 86 slides to the edge of the sliding platform 62, and the other end is suitable for supporting the ground. This makes it convenient for operators or the inner nest 30 to climb up and down the sliding platform 62 along the ladder 86.

[0140] In some optional embodiments, a slider is provided at one end of the ladder 86, and a slideway is provided on the sliding platform 62 or the bottom wall 17, and the slider is slidably matched on the slideway. This end of the ladder 86 is rotatably connected to the slider, and the other end of the ladder 86 is a free end, which is convenient for taking and placing.

[0141] Below, refer to the attached Figure 1-Figure 8 , describing a dual-machine nest device 100 according to a specific embodiment of the present application.

[0142] The double-machine nest device 100 includes a car body 10 , a lifting platform 20 , a rotating platform 61 , a sliding platform 62 , an inner nest body 30 , a first meteorological monitoring device 71 , a second meteorological monitoring device 72 , a controller 80 , and a car ladder 83 .

[0143] The compartment body 10 includes a side wall frame 13 and a top cover 11 . The top of the side wall frame 13 is open, and the top cover 11 is disposed on the top of the side wall frame 13 in an openable and closable manner.

[0144] There are two top covers 11 , and the two top covers 11 are connected to the top of the side wall frame 13 in a translationally movably manner.

[0145] In the stowed state, the two top covers 11 are spliced ​​to cover the top of the side wall frame 13, and in the unfolded state, the two top covers 11 are translated in a direction away from each other to open the top of the side wall frame 13. In the unfolded state, the top surfaces of the two top covers 11 are flush with the top surface of the lifting platform 20.

[0146] The top cover 11 is connected to the first driver 14. The lifting platform 20 is movably disposed in the body 10, and the first nest space 41 is above the lifting platform 20. The lifting platform 20 is connected to the second driver 21. The rotating platform 61 is rotatably disposed on the lifting platform 20, and the fixed-wing UAV 201 is suitable for parking on the rotating platform 61.

[0147] The sliding platform 62 is connected to the bottom wall 17 of the box body 10 and can slide horizontally to extend and retract into the box body 10. A removable inner nest 30 is arranged on the sliding platform 62, and the inner nest 30 is used to rotate the multi-rotor drone 202.

[0148] The first weather monitoring device 71 is disposed on the compartment 10 and is used to monitor at least the wind direction. The second weather monitoring device 72 is disposed on the inner compartment 30 and is used to monitor at least the wind speed.

[0149] Meteorological monitoring devices include wind speed monitoring components, rainfall monitoring components and air pressure monitoring components.

[0150] When the wind speed monitoring component detects that the current wind speed exceeds the wind speed threshold, the controller 80 controls the dual-nest device 100 to remain in the stored state.

[0151] When the rainfall monitoring component detects that the current rainfall exceeds the rainfall threshold, the controller 80 controls the dual-nest device 100 to remain in the storage state.

[0152] When the air pressure monitoring component detects that the current air pressure is lower than the air pressure threshold, the controller 80 controls the dual-nest device 100 to remain in the storage state.

[0153] The car ladder 83 is installed on the side wall frame 13, and is used for the upper end to lead to the landing runway in the unfolded state.

[0154] In the description of this specification, the description with reference to the terms "embodiment", "example", etc. means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the utility model. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner.

[0155] Although the embodiments of the present invention have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. A dual-machine nest device capable of taking off and landing fixed-wing UAVs and multi-rotor UAVs, characterized in that: include: A box body (10), the box body (10) comprising a side wall frame (13) and a top cover (11), the top cover (11) being openably and closably arranged on the top of the side wall frame (13), and the side wall frame (13) being provided with an openable and closable side door (16); A lifting platform (20), the lifting platform (20) being liftably disposed in the compartment (10), the first machine nest space (41) being located above the lifting platform (20), and the operating space (42) being located below the lifting platform (20); a rotating platform (61), the rotating platform (61) being rotatably disposed on the lifting platform (20), and the fixed-wing UAV (201) being suitable for being placed in the first nest space (41) and parked on the rotating platform (61); A sliding platform (62) is horizontally slidably arranged on the body (10) and is arranged corresponding to the side door (16); a second nest space (43) is located above the sliding platform (62); when the sliding platform (62) is stored, it slides into the body (10) and the side door (16) is closed; when the sliding platform (62) is unfolded, the side door (16) is opened and the sliding platform (62) at least partially extends out of the body (10) so that the second nest space (43) is placed outside the body (10); and the multi-rotor drone (202) is suitable for being parked in the second nest space (43).

2. The dual-machine nest device according to claim 1, characterized in that: Also includes: A sliding guide assembly (18) connected between the sliding platform (62) and the carriage (10), wherein the sliding guide assembly (18) comprises: A slide rail (181) is arranged on the bottom wall (17) of the compartment (10), and the slide rail (181) is extended along the direction of expansion and contraction of the slide platform (62); A sliding member (182) provided on the sliding platform (62), wherein the sliding member (182) is slidably engaged on the sliding rail (181); The sliding guide components (18) include at least two groups, and the two groups of sliding guide components (18) are spaced apart and distributed along a direction perpendicular to the contraction and extension direction.

3. The dual-machine nest device according to claim 1, characterized in that: Also includes: An inner nest body (30) is placed on the sliding platform (62), and the inner nest body (30) comprises: Nest seat (31); A hatch cover (32), the hatch cover (32) being arranged on the nest seat (31) in an openable and closable manner, the second nest space (43) being defined between the hatch cover (32) and the nest seat (31), and the top of the second nest space (43) being opened when the hatch cover (32) is opened.

4. The dual-machine nest device according to claim 3, characterized in that: The inner nest body (30) is detachably arranged on the sliding platform (62), and the inner nest body (30) further comprises a moving wheel (33) arranged at the bottom of the nest seat (31).

5. The dual-machine nest device according to claim 3, characterized in that: Also includes: at least one of a first meteorological monitoring device (71) and a second meteorological monitoring device (72); When the first meteorological monitoring device (71) is included, it is arranged on the vehicle body (10) and is used to at least detect the wind direction; When the second meteorological monitoring device (72) is included, it is arranged on the inner nest body (30) and is used to at least detect wind speed.

6. The dual-machine nest device according to claim 1, characterized in that: The sliding platform (62) is provided with a power socket (63), and the wires (64) of the power socket (63) are connected to the power supply and / or controller (80) in the compartment (10); The electric wire (64) is covered with a track chain (65), one end of the track chain (65) is connected to the sliding platform (62) and the other end is connected to the car body (10).

7. The dual-machine nest device according to claim 1, characterized in that: Also includes: A partition cover (19) is arranged in the compartment (10), the partition cover (19) is connected to the bottom wall (17) of the compartment (10) and is located below the lifting platform (20), and the sliding platform (62) slides into the partition cover (19) when being stored.

8. The dual-machine nest device according to claim 1, characterized in that: Also includes: a blowing device (82), the blowing device (82) being installed on the compartment (10) or the lifting platform (20), the compartment (10) being provided with a switch door (15), and when the double-machine nest device (100) is in a storage state, the blowing device (82) and the switch door (15) are located on opposite sides of the first machine nest space (41); The double-nest device (100) also has a first blowing mode. In the first blowing mode, the top cover (11) is closed, the switch door (15) is opened, and the blowing device (82) is turned on to blow out water droplets on the fixed-wing UAV (201) and the lifting platform (20).

9. The dual-machine nest device according to any one of claims 1 to 8, characterized in that: Also includes: A storage battery (84) is arranged in the compartment (10), the storage battery (84) serves as a power source, and the storage battery (84) can be connected to the mains for charging; The compartment (10) is movable on a vehicle, and the dual-engine nest device (100) further comprises: a power generator (85) for connecting to a power system of the vehicle, and the power generator (85) is electrically connected to the battery (84) to transmit electricity to the battery (84).

10. The dual-machine nest device according to any one of claims 1 to 8, characterized in that: Also includes: A ladder (86), wherein the ladder (86) satisfies one of the following conditions: Situation 1: The ladder (86) is detachably arranged on the compartment (10); Scenario 2: The ladder (86) is arranged corresponding to the side door (16), one end of the ladder (86) is slidably connected to the bottom wall (17) of the compartment (10), the ladder (86) is rotatable relative to the bottom wall (17), and when the side door (16) is opened, one end of the ladder (86) slides to the side door (16), and the other end is suitable for resting on the ground; Scenario 3: One end of the ladder (86) is slidably connected to the sliding platform (62), and the ladder (86) is rotatable relative to the sliding platform (62). When the sliding platform (62) is unfolded, one end of the ladder (86) slides to the edge of the sliding platform (62), and the other end is suitable for supporting the ground.