Three-in-one air-ground cooperative emergency management carrier for electric power material information

Abstract

The utility model provides a three-in-one air-ground cooperative emergency management carrier for electric power, material and information. The three-in-one air-ground cooperative emergency management carrier comprises a power traction headstock provided with a generator set, an emergency function carriage, an unmanned aerial vehicle used for air-ground cooperative operation and an unmanned aerial vehicle operation module arranged on a vehicle roof. The unmanned aerial vehicle is characterized in that the unmanned aerial vehicle can replace a task module and has the functions of information collection and material delivery; a command control room and an equipment operation room are arranged in the compartment, and power transmission of the air-ground cooperative emergency management carrier is properly allocated; the electric power of the whole vehicle can be optimally configured, the emergency materials stored in the vehicle can be reasonably dispatched in combination with aerial reconnaissance information, and accurate distribution of the last kilometer is carried out through the unmanned aerial vehicle. According to the utility model, mobile power supply, material storage, aerial reconnaissance and aerial delivery are integrated, the problem of disjunction of information and material dispatching in a traditional emergency mode is solved, and the cooperative efficiency and accuracy of emergency response are significantly improved.

Description

Technical Field

[0001] This utility model relates to the field of emergency command and rescue equipment technology, and in particular to an emergency vehicle that integrates mobile power supply, material storage, drone operation, information processing and intelligent dispatch functions, and can realize integrated air-ground collaborative operation. Background Technology

[0002] In emergency response to major sudden disasters, there are two core challenges: the first is the "first mile" problem of information acquisition, namely how to quickly and accurately grasp the disaster situation in areas that are difficult for ground rescue forces to reach; the second is the "last mile" problem of material distribution, namely how to accurately deliver critical materials to trapped personnel or small work units.

[0003] Currently, drones are widely used as aerial information gathering platforms, but their operations are often disconnected from ground command, power supply, and logistical support systems, resulting in limited endurance and a single mission mode. Meanwhile, traditional emergency supply transport vehicles and power supply vehicles function independently, failing to form an organic whole. A common scenario at rescue sites is that while drones locate trapped individuals, urgently needed medicines or communication equipment cannot be delivered immediately; or, large supply vehicles arrive at the assembly point but cannot efficiently distribute supplies to multiple dispersed demand points.

[0004] Therefore, existing technologies lack an integrated equipment that can deeply integrate aerial reconnaissance, air delivery, ground command, power supply, and material reserves, making it impossible to achieve true air-ground coordination and intelligent material dispatch. This results in gaps in the emergency response chain and affects overall rescue efficiency. Utility Model Content

[0005] This utility model aims to solve the problems existing in the above-mentioned background technology and provide an air-ground collaborative emergency management vehicle that integrates power material information. As a highly integrated air-ground collaborative combat unit, this emergency vehicle aims to connect the entire link of "information acquisition - decision-making and command - material scheduling - precise delivery" in emergency response.

[0006] To achieve the above objectives, the present invention adopts the following technical solution.

[0007] A three-in-one air-ground collaborative emergency management vehicle for power materials and information includes a power tractor unit and a first emergency function carriage connected to each other; the power tractor unit has a second emergency function carriage, and the second emergency function carriage contains a generator set;

[0008] The air-ground collaborative emergency management vehicle also includes a drone operation module, including:

[0009] Multiple unmanned aerial vehicle (UAV) cabins are installed on the top of the first and second emergency function carriages, respectively; each UAV cabin includes a cabin body and a door, with the door located on top of the cabin body for opening / closing the cabin body; the cabin body contains a take-off and landing platform;

[0010] Multiple drones, each drone bay is used to accommodate one drone; the drones are multi-rotor drones or compound-wing drones, equipped with electro-optical reconnaissance pods or delivery mechanisms; the delivery mechanisms are used to hold and release materials;

[0011] The first emergency function compartment also has multiple compartments for: setting up a command and control room and equipment operation room; storing emergency supplies and spare drones; storing spare batteries for drones and setting up a drone charging area with drone charging devices;

[0012] The generator set is used to provide power to the first emergency function car, the second emergency function car, the unmanned cabin, and external equipment.

[0013] Preferably, the second emergency function carriage has a main power distribution cabinet; the main power distribution cabinet is equipped with an entrance protection and isolation unit, including:

[0014] Main circuit breaker, circuit connected to generator set;

[0015] The first-level surge protection module is connected to the main circuit breaker circuit and is used to deal with voltage fluctuations and absorb surges;

[0016] A three-phase isolation transformer is connected to the primary surge protection module circuit to provide a 220V / 380V three-phase four-wire power supply.

[0017] The central controller is connected to the main circuit breaker, the primary surge protection module, and the three-phase isolation transformer.

[0018] Air-ground coordinated emergency management vehicles also include:

[0019] The first circuit is connected to the L1 phase power supply provided by the three-phase isolation transformer. The output of the first circuit is connected to the drone cabin and the drone charging device.

[0020] The second circuit is connected to the L2 phase power supply provided by the three-phase isolation transformer. The second circuit also has an online uninterruptible power supply. The output of the second circuit is connected to the equipment in the first emergency function carriage.

[0021] The third circuit is connected to the L3 phase power supply provided by the three-phase isolation transformer. The third circuit also has miniature circuit breakers, AC contactors and thermal overload relays that are interconnected. The connection terminal of the second circuit is connected to the air conditioning system of the first emergency function car and the second emergency function car.

[0022] The fourth circuit connects to the L3 phase power supply provided by the three-phase isolation transformer. The fourth circuit also has a residual current circuit breaker, which integrates overload protection, short circuit protection and residual current protection. The output of the fourth circuit connects to the lighting system and ordinary power socket of the first and second emergency function carriages.

[0023] The central controller is also connected to the first, second, third, and fourth circuits respectively, and is used to distribute the load to the first, second, third, and fourth circuits.

[0024] Preferably, the powered tractor unit and the first emergency function vehicle are mechanically connected via a saddle traction structure; the powered tractor unit has a five-wheel saddle, and the first emergency function vehicle has a traction pin that cooperates with the five-wheel saddle.

[0025] The power tractor unit and the first emergency function carriage are electrically connected via a heavy-duty multi-core power and signal composite cable bundle; the heavy-duty multi-core power and signal composite cable bundle includes a power cable, a shielded twisted pair cable, and a control signal line.

[0026] Preferably, the command and control room is used to: receive target area images transmitted back by the UAV; and send flight control signals and / or material delivery control signals to the UAV.

[0027] Preferably, a delivery box is suspended under the belly of the drone; the delivery box has an openable / closeable door; and the delivery box has a movable hook inside.

[0028] As can be seen from the technical solutions provided by the above embodiments of this utility model, this utility model provides a three-in-one air-ground collaborative emergency management vehicle integrating power, materials, and information, including: a power traction vehicle equipped with a generator set, an emergency function carriage, a drone for air-ground collaborative operations, and a drone operation module mounted on the roof. Its core lies in the fact that the drone has interchangeable mission modules, combining information collection and material delivery functions; the carriage is equipped with a command and control room and equipment operation room, and the power transmission of the air-ground collaborative emergency management vehicle has been appropriately allocated; it can not only optimize the power configuration of the entire vehicle, but also, combined with aerial reconnaissance information, rationally dispatch emergency materials stored in the vehicle, and conduct precise "last-mile" delivery via drones. This utility model integrates mobile power supply, material storage, aerial reconnaissance, and aerial delivery into a single system, solving the pain point of information and material dispatch disconnect in traditional emergency modes, and significantly improving the collaborative efficiency and accuracy of emergency response. The air-ground collaborative emergency management vehicle provided by this utility model also has the following beneficial effects:

[0029] Achieving true air-ground coordination: Seamlessly linking ground command, power supply, and warehousing ("ground") with aerial reconnaissance and delivery ("air") to form a unified, mobile combat unit, greatly enhancing the coordination and overall effectiveness of the response.

[0030] It combines power supply and dual material delivery functions: the vehicle itself serves as a mobile material forward warehouse, completing the first delivery of materials to the site; the drones equipped with the delivery module perform the "last mile" precise secondary delivery from the site to the specific demand point, solving the key problem of material distribution.

[0031] Flexible mission payload and multi-functionality: By changing mission modules, the same UAV can perform large-scale intelligence, surveillance, and reconnaissance (ISR) missions as well as point-to-point material delivery missions, greatly enhancing the tactical flexibility and efficiency of a single piece of equipment.

[0032] Intelligent dispatching and power optimization: The introduction of the central control unit makes power distribution and material dispatching no longer isolated manual operations, but an intelligent decision-making process based on real-time information and preset logic, ensuring the efficient use of energy and the accuracy of dispatching.

[0033] Additional aspects and advantages of this invention will be set forth in part in the description which follows, and will become apparent from the description or may be learned by practice of the invention. Attached Figure Description

[0034] To more clearly illustrate the technical solutions of the embodiments of this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0035] Figure 1 A structural schematic diagram of an air-ground collaborative emergency management vehicle integrating power material information, provided by this utility model;

[0036] Figure 2 A top view of the UAV operation module of a three-in-one air-ground collaborative emergency management vehicle for power material information provided by this utility model;

[0037] Figure 3 A schematic diagram of the storage state of the drone operation module of a three-in-one air-ground collaborative emergency management vehicle for power material information provided by this utility model;

[0038] Figure 4 A schematic diagram of the drone launch status of the drone operation module of a three-in-one air-ground collaborative emergency management vehicle for power materials information provided by this utility model.

[0039] Figure 5The present invention provides an energy line logic block diagram for the unmanned aerial vehicle (UAV) operation module of a three-in-one air-ground collaborative emergency management vehicle for power materials information.

[0040] In the picture:

[0041] 1. Power tractor unit 2. First emergency function compartment 21. Monitoring host 22. Main power distribution cabinet 3. Unmanned vehicle compartment 31. Cabin 32. Door 33. Take-off and landing platform 34. Unmanned vehicle 4. Second emergency function compartment Detailed Implementation

[0042] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.

[0043] Those skilled in the art will understand that, unless specifically stated otherwise, the singular forms “a,” “an,” “the,” and “the” used herein may also include the plural forms. It should be further understood that the term “comprising” as used in this specification means the presence of the stated features, integers, steps, operations, elements, and / or components, but does not exclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and / or groups thereof. It should be understood that when we say an element is “connected” or “coupled” to another element, it can be directly connected or coupled to the other element, or there may be intermediate elements. Furthermore, “connected” or “coupled” as used herein can include wireless connections or couplings. The term “and / or” as used herein includes any and all combinations of one or more of the associated listed items.

[0044] It will be understood by those skilled in the art that, unless otherwise defined, all terms used herein (including technical and scientific terms) have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. It should also be understood that terms such as those defined in general dictionaries should be understood to have the same meaning as in the context of the prior art, and should not be interpreted in an idealized or overly formal sense unless defined as herein.

[0045] To facilitate understanding of the embodiments of this utility model, the following will provide further explanation and description with reference to the accompanying drawings and several specific embodiments. These embodiments do not constitute a limitation on the embodiments of this utility model.

[0046] See Figure 1This utility model provides a three-in-one air-ground collaborative emergency management vehicle integrating power materials and information, including a powered tractor unit 1 and a first emergency function compartment 2 connected to each other. The powered tractor unit 1 has a second emergency function compartment 4, which contains a generator set. In the embodiment provided by this utility model, the powered tractor unit 1 is the power core of the platform, modified from a heavy-duty truck cab, and integrates a high-power diesel generator set (not shown in the figure) to provide a stable and reliable AC power supply for the entire platform. The heavy-duty truck cab can be a six-axle flat-head heavy-duty truck, and the space above and behind the chassis can accommodate a compartment, namely the second emergency function compartment 4 in this embodiment.

[0047] The air-ground collaborative emergency management vehicle also includes a drone operation module, including:

[0048] Multiple unmanned vehicle cabins 3 are respectively installed on the top of the first emergency function carriage 2 and the second emergency function carriage 4; each unmanned vehicle cabin 3 includes a cabin body 31 and a cabin door 32, the cabin door 32 is located on the top of the cabin body 31 and is used to open / close the cabin body 31; the cabin body 31 has a take-off and landing platform 33.

[0049] Multiple drones 34, each drone bay 3 is used to accommodate one drone 34; the drone 34 is a multi-rotor drone 34 or a compound wing drone 34, with an electro-optical reconnaissance pod and a delivery mechanism; the delivery mechanism is used to hold / release materials.

[0050] As a key component of this invention for achieving air-ground collaboration, the UAV operation module 34 preferably comprises a multi-rotor or compound-wing UAV with vertical takeoff and landing (VTOL) capabilities to adapt to takeoff and landing requirements in complex environments. Its core feature is a standardized mission mounting interface located beneath the fuselage. This interface enables rapid mounting and identification of different mission modules.

[0051] As a standard payload, the electro-optical reconnaissance pod integrates a high-definition visible light camera, an infrared thermal imager, and a laser rangefinder for all-weather disaster reconnaissance, target search, and location.

[0052] As a functional mount, the delivery unit can carry emergency supplies such as medicines, food, water, and small communication equipment, and can also deliver supplies according to instructions.

[0053] Commercially available products can be used for drones that can be equipped with interchangeable mission components and drop items.

[0054] In some preferred embodiments, the take-off and landing platform 33 inside the unmanned cabin 3 can adopt a lifting platform structure, such as... Figure 3 As shown, when the drone 34 is normally stored, the hatch 32 is closed, and the takeoff and landing platform 33 is in a low position. Figure 4As shown, when the UAV 34 takes off, the hatch 32 opens and the take-off and landing platform 33 rises. The lifting mechanism of the take-off and landing platform 33 can be based on existing technology, such as installing a small linear motor in the sub-cabin 31 to drive the lifting rod to lift and lower the take-off and landing platform 33.

[0055] In the embodiments provided by this utility model, the first emergency function carriage 2 also has multiple compartments, the number and specific layout of which are appropriately set according to actual needs, and multiple doors are opened in the first emergency function carriage 2 for personnel to enter and exit. The multiple compartments in the first emergency function carriage 2 can be used to store emergency supplies, spare drones 34, batteries required for spare drones 34, and charging devices for charging drones 34, respectively. Similarly, the command and control room and the equipment operation room are also in the first emergency function carriage 2, and are set up in the form of compartments. In a preferred embodiment, the main power distribution cabinet 22 in the equipment operation room is located on one side wall panel of the equipment operation room, and the command and control room and the equipment operation room are located in the same compartment. The command and control room is equipped with a monitoring host 21, which can display the status information of drones 34, including the returned on-site images, location information, flight path information, etc., the power supply status in the carriage, etc., and can also input commands and communicate with the outside world.

[0056] The generator set is used to provide power to the first emergency function compartment 2, the unmanned aerial vehicle compartment 3, and external equipment. The power is supplied by the generator set through a composite cable bundle, and undergoes multi-level protection, transformation, and intelligent distribution within the compartment to provide high-quality power to the unmanned aerial vehicle operation module, sensitive equipment operating area, environmental control unit, and general equipment.

[0057] In the preferred embodiment provided by this utility model, the power supply method of this air-ground coordinated emergency management vehicle includes the following three stages:

[0058] Phase 1: Main Power Supply Input and Primary Protection

[0059] The input power first passes through the inlet protection and isolation unit, which constitutes the system's primary safety defense, isolating external power grid disturbances and performing basic protection. Its core configuration is as follows:

[0060] Main circuit breaker: A four-pole molded case circuit breaker, such as the Schneider Electric Compact NSX series, is installed at the main system inlet. The main circuit breaker enables synchronous breaking and closing control of all live conductors (L1, L2, L3, N), serves as the control switch for the main power supply of the carriage, and undertakes the primary overload and short-circuit protection of the system, ensuring complete electrical isolation from external power sources during emergency shutdowns or equipment maintenance.

[0061] Primary surge protection module: Located downstream of the main circuit breaker, a primary surge protector is configured, which can be the Phoenix Contact VALVETRAB SEC series. To prevent maloperation of the upstream circuit breaker due to its potential failure short-circuit mode, a manufacturer-recommended dedicated backup protection device (such as a dedicated fuse or miniature circuit breaker) is added upstream of this protector to ensure effective protection against strong power surges from the grid side.

[0062] Phase Two: Three-Phase Balance Conversion and Electrical Isolation

[0063] This unit aims to solve the problem of three-phase current imbalance in generators caused by single-phase heavy loads, and to provide a clean and safe power supply environment for downstream loads. Its core configuration is as follows:

[0064] Three-phase isolation transformer: The 380V three-phase power supply after primary protection is transmitted to a delta-phase three-phase dry-type isolation transformer, such as the Siemens 4AP series. The transformer establishes complete electrical isolation between the primary and secondary sides, suppressing common-mode interference transmission; a neutral point is generated on the secondary side through a Y-connection, providing three independent 220V single-phase power outputs.

[0065] Phase 3: Intelligent distribution of 22 zones in the main power distribution cabinet

[0066] The 220V / 380V three-phase four-wire power supply, transformed by the isolation transformer, is led to the busbar inside the main distribution cabinet 22. Under the centralized monitoring and scheduling of the central controller (such as a Siemens SIMATIC S7-1200 series PLC), the total system load is distributed to the following four functional loops:

[0067] First Circuit (UAV Operation Module): This circuit is located on phase L1 and is designed for high-power DC power supply. It is protected by a dedicated miniature circuit breaker, with its core component being a high-power AC / DC switching power supply (such as the Mean Well RSP-3000-48). This power module converts 220V AC power to a stable 48V DC power, and on its DC output side, it is equipped with independent DC fast-acting fuses for the automatic charging device and the 32-motor driver for the hatch, achieving precise isolation of downstream equipment faults.

[0068] Second Circuit (Equipment Operating Area): This circuit is located on phase L2 and is designed for highly stable uninterruptible power supply. Under the protection of an independent miniature circuit breaker, an online uninterruptible power supply (UPS) (such as the Schneider Electric APC Smart-UPSOnline SRT series) is connected in series. This UPS provides pure sine wave power with zero switching time to all precision electronic equipment in the operating area, such as computers and data link communication modules, ensuring data security and task continuity.

[0069] The third circuit (environmental control unit): This circuit is located on phase L3 and is designed specifically for inductive loads. The protection and control link consists of miniature circuit breakers (short-circuit protection), AC contactors (whose coils are controlled by a PLC to perform start-stop operations), and thermal overload relays (motor overload protection).

[0070] Fourth Circuit (General Lighting and Auxiliary Sockets): This circuit can be installed on phase L3 or selected based on the principle of three-phase balance. It employs a single residual current circuit breaker (such as the Schneider Electric Acti9 Vigi series) integrating overload, short-circuit, and Type A (or Type AC) leakage protection functions to provide the highest level of safety protection for all lighting and general power sockets inside the vehicle. The general power sockets provide 220V power. Preferably, multiple sockets or modules are integrated to provide power for multiple users' small electrical appliances, such as mobile phones and power bank charging. Combined with external communication vehicles, it forms an emergency supply station, providing post-disaster network and communication services. This ordinary power socket can be integrated into the side of the first emergency function compartment 2 and / or the second emergency function compartment 4; it can be accessed by opening a cover on the side wall of the compartment.

[0071] The necessary frequency converters and transformers in each of the above sub-circuits can all be commercially available products.

[0072] like Figure 5 As shown, the central controller connects to the main circuit breaker, the primary surge protection module, and the three-phase isolation transformer via the main distribution cabinet 22, and controls the load distribution of the four sub-circuits via the main distribution cabinet 22. In some feasible embodiments, the central controller can be a highly stable programmable logic controller (Siemens SIMATIC S7-1214C) or an industrial computer (Advantech ARK-2250) as the intelligent brain of the platform. It is used to distribute the load to the above-mentioned sub-circuits, monitor the power parameters of each sub-circuit in real time, precisely control the on / off state of each sub-circuit according to instructions, receive sensor signals and execute corresponding operations, and display all system operating statuses on the display screen in the equipment operation room.

[0073] First emergency function carriage 2, main power distribution cabinet 22

[0074] In a preferred embodiment of this invention, a delivery box is suspended below the fuselage of the drone 34. The delivery box stores the materials to be delivered, and has an openable and closable door at the bottom. The delivery box also includes a movable hook.

[0075] When loading supplies, the drone 34 can be remotely controlled to open the container door and autonomously grab the supplies using the movable hook. After closing the door, it takes off and enters its flight path. Alternatively, the drone 34 can be loaded with supplies manually and then taken off. The command and control room in the second emergency function compartment 4 monitors the flight path of the drone 34. After reaching the target area, the location of the drop point is determined by the image transmitted back by the electro-optical reconnaissance pod. When dropping supplies, the command and control room issues instructions to the drone 34 to drop the supplies. In the preferred embodiment provided by this utility model, the drone 34 and the command and control room can communicate via radio or microwave, or the drone 34's flight path can be planned using GPS navigation. Accordingly, the command and control room is equipped with a wireless communication device (which also has network communication capabilities with the outside world), a microwave communication device, a GPS communication device, and a multi-functional display device, based on existing technology.

[0076] In a preferred embodiment of this invention, a delivery box is suspended below the belly of the drone 34. The delivery box has a box-like structure with an openable / closable door at the bottom. A movable hook is located at the top inside the box and is directly connected to the fuselage of the drone 34, with its movement directly controlled by the drone 34's controller.

[0077] In a preferred embodiment of this invention, the powered tractor unit 1 and the first emergency function vehicle compartment 2 are mechanically connected via a saddle-type traction structure. The powered tractor unit has a five-wheeled saddle, and the first emergency function vehicle compartment has a towing pin that cooperates with the five-wheeled saddle. The five-wheeled saddle and the towing pin are a complete set of equipment and can be commercially available truck parts.

[0078] In addition, the powered tractor unit 1 and the first emergency function carriage 2 are electrically connected via a heavy-duty multi-core power and signal composite cable bundle. The heavy-duty multi-core power and signal composite cable bundle includes a power cable, a shielded twisted pair cable, and a control signal line.

[0079] The air-ground coordinated emergency management vehicle provided by this utility model has the following air-ground coordinated workflow:

[0080] Deployment and Information Gathering: After the emergency vehicle arrives at the scene, the operator directs UAV 34, equipped with an "electro-optical reconnaissance pod," to take off from the UAV operation module on the roof of the vehicle to conduct reconnaissance flights over the target area. Real-time high-definition video and infrared images are transmitted back to the display screen in the equipment control room.

[0081] Intelligent dispatching and decision-making: The central control unit assists in processing the transmitted data and highlights suspected signs of life or distress signals on the map. Based on this information, operators make decisions regarding the distribution of supplies; for example, determining whether to deliver a satellite phone to point A and a first-aid kit to point B.

[0082] Mission Switching and Secondary Delivery: Drone 34 returned and landed on landing platform 33. Ground personnel, following instructions, retrieved a satellite phone from the supplies storage area, installed the "precision delivery module," and quickly changed the payload for Drone 34.

[0083] Precise Delivery: After the payload was changed, Drone 34 took off again and, under the precise control of the operator in the equipment control room, flew to the airspace above point A. After confirming the environment below through the onboard camera of Drone 34, the operator remotely controlled the delivery module to safely deliver the satellite phone to the designated location. Subsequently, Drone 34 can continue to point B to perform the next delivery mission.

[0084] Energy closed-loop and optimized power allocation: Throughout the process, UAV 34 can return to the platform for automatic charging at any time during mission breaks. The central control unit will adjust the power of other non-critical equipment appropriately based on the current operation priority, such as prioritizing the UPS power supply of the command system, while charging UAV 34, thus achieving intelligent optimization of power allocation.

[0085] Through the above process, this utility model deeply integrates the information gathering and material delivery capabilities of the UAV 34 with the vehicle's carrying, storage, power supply, and command capabilities, forming a highly efficient air-ground collaborative emergency response system of "reconnaissance-decision-dispatch-delivery-support".

[0086] In summary, this utility model provides a three-in-one air-ground collaborative emergency management vehicle integrating power, materials, and information, comprising: a power tractor equipped with a generator set, an emergency function carriage, a drone for air-ground collaborative operations, and a drone operation module mounted on the roof. Its core feature is that the drone has interchangeable mission modules, combining information gathering and material delivery functions; the carriage houses a command and control room and equipment operation room; and the power transmission of the air-ground collaborative emergency management vehicle has been appropriately allocated. It not only optimizes the power configuration of the entire vehicle but also, combined with aerial reconnaissance information, rationally dispatches emergency materials stored within the vehicle and performs precise "last-mile" delivery via drones. This utility model integrates mobile power supply, material storage, aerial reconnaissance, and aerial delivery, solving the pain point of information and material dispatch disconnect in traditional emergency models, and significantly improving the collaborative efficiency and accuracy of emergency response. The air-ground collaborative emergency management vehicle provided by this utility model also has the following beneficial effects:

[0087] Achieving true air-ground coordination: Seamlessly linking ground command, power supply, and warehousing ("ground") with aerial reconnaissance and delivery ("air") to form a unified, mobile combat unit, greatly enhancing the coordination and overall effectiveness of the response.

[0088] It combines power supply and dual material delivery functions: the vehicle itself serves as a mobile material forward warehouse, completing the first delivery of materials to the site; the drones equipped with the delivery module perform the "last mile" precise secondary delivery from the site to the specific demand point, solving the key problem of material distribution.

[0089] Flexible mission payload and multi-functionality: By changing mission modules, the same UAV can perform large-scale intelligence, surveillance, and reconnaissance (ISR) missions as well as point-to-point material delivery missions, greatly enhancing the tactical flexibility and efficiency of a single piece of equipment.

[0090] Intelligent dispatching and power optimization: The introduction of the central control unit makes power distribution and material dispatching no longer isolated manual operations, but an intelligent decision-making process based on real-time information and preset logic, ensuring the efficient use of energy and the accuracy of dispatching.

[0091] The various embodiments in this specification are described in a progressive manner. Similar or identical parts between embodiments can be referred to mutually. Each embodiment focuses on describing the differences from other embodiments. In particular, for apparatus or system embodiments, since they are basically similar to method embodiments, the description is relatively simple; relevant parts can be referred to the descriptions in the method embodiments. The apparatus and system embodiments described above are merely illustrative. The units described as separate components may or may not be physically separate. The components shown as units may or may not be physical units; that is, they may be located in one place or distributed across multiple network units. Some or all of the modules can be selected to achieve the purpose of this embodiment according to actual needs. Those skilled in the art can understand and implement this without creative effort.

[0092] The above description is merely a preferred embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this utility model should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the scope of the claims.

Claims

1. A three-in-one air-ground collaborative emergency management vehicle for power materials and information, characterized in that, It includes a power tractor unit and a first emergency function compartment connected to each other; the power tractor unit has a second emergency function compartment, which contains a generator set; The air-ground collaborative emergency management vehicle also includes a drone operation module, comprising: Multiple unmanned aerial vehicle (UAV) cabins are respectively installed on the top of the first emergency function vehicle and the second emergency function vehicle; each UAV cabin includes a cabin body and a door, the door being located on top of the cabin body for opening / closing the cabin body; the cabin body has a take-off and landing platform; Multiple drones, each drone bay is used to accommodate one drone; the drone is a multi-rotor drone or a compound-wing drone, and has an electro-optical reconnaissance pod or a delivery mechanism; the delivery mechanism is used to hold and release materials; The first emergency function compartment also has multiple compartments for: setting up a command and control room and equipment operation room; storing emergency supplies and spare drones; storing spare batteries for drones and setting up a drone charging area, which is equipped with drone charging devices; The generator set is used to provide power to the first emergency function carriage, the second emergency function carriage, the unmanned cabin, and external equipment.

2. The air-ground coordinated emergency management vehicle according to claim 1, characterized in that, The second emergency function compartment has a main power distribution cabinet; the main power distribution cabinet is equipped with an entrance protection and isolation unit, including: The main circuit breaker is connected to the generator set. A primary surge protection module is connected to the main circuit breaker circuit to cope with voltage fluctuations and absorb surges; A three-phase isolation transformer is connected to the primary surge protection module circuit to provide a 220V / 380V three-phase four-wire power supply. The central controller is connected to the main circuit breaker, the primary surge protection module, and the three-phase isolation transformer. The air-ground coordinated emergency management vehicle also includes: The first circuit is connected to the L1 phase power supply provided by the three-phase isolation transformer, and the output terminal of the first circuit is connected to the unmanned aerial vehicle cabin and the unmanned aerial vehicle charging device. The second circuit is connected to the L2 phase power supply provided by the three-phase isolation transformer, and the second circuit also has an online uninterruptible power supply; the output terminal of the second circuit is connected to the equipment in the first emergency function carriage. The third circuit is connected to the L3 phase power supply provided by the three-phase isolation transformer. The third circuit also has miniature circuit breakers, AC contactors and thermal overload relays that are interconnected. The connection terminal of the second circuit is connected to the air conditioning systems of the first emergency function car and the second emergency function car. The fourth circuit is connected to the L3 phase power supply provided by the three-phase isolation transformer. The fourth circuit also has a leakage current protection circuit breaker, which integrates overload protection, short circuit protection and leakage current protection. The output terminal of the fourth circuit is connected to the lighting system and ordinary power socket of the first emergency function car and the second emergency function car. The central controller is also connected to the first circuit, the second circuit, the third circuit and the fourth circuit respectively, and is used to distribute the load to the first circuit, the second circuit, the third circuit and the fourth circuit.

3. The air-ground coordinated emergency management vehicle according to claim 2, characterized in that, The powered tractor unit and the first emergency function vehicle are mechanically connected via a saddle traction structure; the powered tractor unit has a five-wheel saddle, and the first emergency function vehicle has a traction pin that cooperates with the five-wheel saddle. The power tractor unit and the first emergency function carriage are electrically connected via a heavy-duty multi-core power and signal composite cable bundle; the heavy-duty multi-core power and signal composite cable bundle includes a power cable, a shielded twisted pair cable, and a control signal line.

4. The air-ground coordinated emergency management vehicle according to claim 1, characterized in that, The command and control room is used to: receive target area images transmitted back by the UAV; and send flight control signals and / or material delivery control signals to the UAV.

5. The air-ground coordinated emergency management vehicle according to claim 1, characterized in that, The drone has a delivery box suspended from its underside; the delivery box has an openable / closeable door; and the delivery box has a movable hook inside.

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