Emergency command vehicle

Abstract

The utility model relates to the technical field of emergency rescue equipment, and discloses an emergency command vehicle. The emergency command vehicle comprises a compartment. The compartment comprises a compartment body, a first connecting assembly, a second connecting assembly and a third connecting assembly. The box body is provided with an opening for the medium-sized composite wing unmanned aerial vehicle to enter and exit from the box body. The first connecting assembly is arranged on the inner wall of the left side of the box body and used for being detachably connected with a left wing and a right wing of the medium-sized composite wing unmanned aerial vehicle. The second connecting assembly is arranged on the inner wall of the right side of the box body and used for being detachably connected with an empennage and a wingtip of the medium-sized composite wing unmanned aerial vehicle. The third connecting assembly is arranged on a bottom plate of the box body and used for being detachably connected with a fuselage and arms of the unmanned aerial vehicle. The emergency command vehicle solves the problems that an emergency command vehicle in the prior art is high in emergency rescue cost and poor in emergency response speed and emergency command efficiency.

Description

Technical Field

[0001] The utility model relates to the technical field of emergency rescue equipment, in particular to an emergency command vehicle. Background Art

[0002] In dealing with emergencies and natural disasters, rapid and effective emergency command and coordination are crucial. Traditional emergency command methods often rely on fixed command centers, which have problems such as untimely response and limited access to on-site information. To solve the above problems existing in fixed command centers, in related technologies, drones and emergency command vehicles are used, and the emergency command vehicle is used to command the drone to collect information on the incident site.

[0003] Currently, either the existing emergency command vehicle does not have the function of transporting drones. In this case, a dedicated transport vehicle needs to be additionally equipped to transport large drones, increasing the cost of emergency rescue and reducing the emergency response speed. Or it can only carry small quadrotor drones and cannot carry and transport medium and large compound-wing drones. The attitude perception range of small quadrotor drones is small and the functions are single, which limits the exertion of emergency command effectiveness.

[0004] Therefore, how to reduce the cost of emergency rescue, improve the emergency response speed and emergency command effectiveness is an urgent problem to be solved in the industry. Summary of the Utility Model

[0005] The utility model provides an emergency command vehicle to solve the problems of high cost of emergency rescue, poor emergency response speed and emergency command effectiveness existing in the existing emergency command vehicle.

[0006] The utility model provides an emergency command vehicle, comprising:

[0007] A box body having an opening for a medium compound-wing drone to enter and exit the box body;

[0008] A first connection component and a second connection component; one of the first connection component and the second connection component is arranged on the left inner wall of the box body, and the other is arranged on the right inner wall of the box body; the first connection component is used for detachably connecting with the left wing and the right wing of the medium compound-wing drone; the second connection component is used for detachably connecting with the tail wing and the wing tip of the medium compound-wing drone;

[0009] A third connection component arranged on the bottom plate of the box body for detachably connecting with the fuselage and the arm of the drone.

[0010] According to the emergency command vehicle provided by the utility model, the first connection component includes:

[0011] The first connection structure includes a plurality of first connecting members; the plurality of first connecting members are arranged at intervals in the front-rear direction and are used for detachably connecting to one of the left wing or the right wing;

[0012] The second connection structure includes a plurality of second connecting members; the plurality of second connecting members are arranged at intervals in the front-rear direction and are located below the first connection structure; the second connecting members are used for detachably connecting to the other of the left wing or the right wing.

[0013] According to the emergency command vehicle provided by the present utility model, the second connection assembly includes:

[0014] The third connection structure is used for detachably connecting to one of the tail wing or the wing tip;

[0015] The fourth connection structure is located in front of or behind the third connection structure; the fourth connection structure is used for detachably connecting to the other of the tail wing or the wing tip.

[0016] According to the emergency command vehicle provided by the present utility model, the third connection assembly includes:

[0017] The landing gear includes a plurality of support frames; the plurality of support frames are arranged at intervals in the front-rear direction on the bottom plate and are used for detachably connecting to the fuselage;

[0018] The fifth connection structure includes a plurality of fifth connecting members; the plurality of fifth connecting members are arranged at intervals in the front-rear direction on the bottom plate and are located on the left side or the right side of the landing gear and are used for detachably connecting to the machine arm.

[0019] According to the emergency command vehicle provided by the present utility model, the emergency command vehicle further includes a communication command module, and the communication command module includes:

[0020] The communication command seat is arranged at the front end inside the box body and is used for communicating and connecting with the medium-sized compound-wing unmanned aerial vehicle and the upper computer;

[0021] The lifting platform is arranged inside the box body; the lifting platform is connected to the communication antenna of the communication command seat and is used for driving the communication antenna to enter and exit the box body in the up-down direction.

[0022] According to the emergency command vehicle provided by the present utility model, the emergency command vehicle further includes a power supply module, and the power supply module includes at least two of a solar battery, a battery pack or a generator.

[0023] According to the emergency command vehicle provided by the present utility model, the length of the box body is not greater than.m.

[0024] According to the emergency command vehicle provided by the present utility model, the carriage further includes:

[0025] The first door body assembly, one end of which is hinged to the box body, is used to close or open the opening; when the first door body assembly is opened, the first door body assembly is used to load the medium-sized compound-wing unmanned aerial vehicle.

[0026] The first driving assembly is installed on the box body and is used to drive the first door body assembly to move up and down, so that the first door body assembly can load and unload the medium-sized compound-wing unmanned aerial vehicle.

[0027] According to the emergency command vehicle provided by the present invention, the carriage further includes:

[0028] The second door body assembly is located above the first door body assembly, and the upper end of the second door body assembly is hinged to the box body.

[0029] The second driving assembly is installed on the box body, and the second driving assembly is used to drive the second door body assembly to flip, so as to cooperate with the first door body assembly to close or open the opening.

[0030] According to the emergency command vehicle provided by the present invention, the carriage further includes:

[0031] The locking assembly is used to lock the first door body assembly to the box body, so that the first door body assembly can close the opening.

[0032] For the emergency command vehicle provided by the present invention, by providing the first connection assembly on one of the left inner wall and the right inner wall of the box body, and the second connection assembly on the other, and by providing the third connection assembly on the bottom plate of the box body, the various parts of the medium-sized compound-wing unmanned aerial vehicle can be reasonably arranged and installed at different positions of the box body, ensuring that the box body can carry the medium-sized compound-wing unmanned aerial vehicle. In this way, on the one hand, it avoids using a dedicated transportation tool to transport the medium-sized compound-wing unmanned aerial vehicle, reduces the emergency command cost, and improves the emergency response speed. On the other hand, compared with the small four-rotor unmanned aerial vehicle, the medium-sized compound-wing unmanned aerial vehicle has a wider attitude perception range and richer functions, so it is beneficial to the exertion of emergency command effectiveness. Therefore, this embodiment solves the problems of high emergency rescue cost, poor emergency response speed and poor emergency command effectiveness existing in the emergency command vehicle of the prior art. Description of the Drawings

[0033] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings without creative efforts.

[0034] Figure 1It is one of the schematic structural diagrams of the carriage in the open state provided by the present utility model.

[0035] Figure 2 It is Figure 1 the enlarged structural schematic diagram of part A in

[0036] Figure 3 It is Figure 1 the enlarged structural schematic diagram of part B in

[0037] Figure 4 It is Figure 1 the enlarged structural schematic diagram of part C in

[0038] Figure 5 It is one of the schematic structural diagrams of the carriage in the closed state provided by the present utility model.

[0039] Figure 6 It is one of the schematic structural diagrams of the emergency command vehicle provided by the present utility model.

[0040] Figure 7 It is the second schematic structural diagram of the emergency command vehicle provided by the present utility model.

[0041] Reference numerals:

[0042] 100, carriage; 110, box body; 120, first door body assembly; 121, first door body part; 122, extension part; 130, first driving assembly; 140, second door body assembly; 141, second door body part; 142, protruding limiting part; 151, clamping groove; 152, clamping part; 153, locking part; 160, first connection assembly; 161, first connection structure; 162, second connection structure; 163, first connecting part; 164, second connecting part; 170, second connection assembly; 171, third connection structure; 172, fourth connection structure; 173, third connecting part; 174, fourth connecting part; 180, third connection assembly; 181, landing gear; 182, fifth connection structure; 183, support frame; 184, fifth connecting part;

[0043] 200, power supply module;

[0044] 300, environmental detection module; 310, camera; 320, anemometer; 330, positioning module;

[0045] 400, communication command module; 410, communication command seat; 420, lifting platform. Detailed implementation manners

[0046] To make the objectives, technical solutions and advantages of the present utility model more clear, the following will clearly and completely describe the technical solutions in the present utility model in conjunction with the accompanying drawings in the present utility model. Apparently, the described embodiments are some, but not all, of the embodiments of the present utility model. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present utility model without making creative efforts fall within the protection scope of the present utility model.

[0047] In the description of the embodiments of the present utility model, it should be noted that the orientation or positional relationships indicated by the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. are based on the orientation or positional relationships shown in the accompanying drawings. They are only for the convenience of describing the embodiments of 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 thus should not be construed as a limitation to the embodiments of the present utility model. In addition, the terms "first", "second", "third" are only used for descriptive purposes and should not be construed as indicating or implying relative importance.

[0048] In the description of the present utility model, it should be noted that unless otherwise clearly specified and defined, the terms "connected" and "coupled" 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 directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the embodiments of the present utility model can be understood according to specific situations.

[0049] In the embodiments of the present utility model, unless otherwise clearly specified and defined, the first feature being "on" or "under" the second feature can be that the first and second features are in direct contact, or the first and second features are indirectly in contact through an intermediate medium. Moreover, the first feature being "above", "over" and "on top of" the second feature can be that the first feature is directly above or obliquely above the second feature, or merely indicates that the first feature has a higher horizontal height than the second feature. The first feature being "under", "beneath" and "underneath" the second feature can be that the first feature is directly below or obliquely below the second feature, or merely indicates that the first feature has a lower horizontal height than the second feature.

[0050] In the description of this specification, the descriptions referring to terms such as "one embodiment", "some embodiments", "example", "specific example", or "some examples" mean that the specific features, structures, materials, or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the embodiments of the present utility model. In this specification, the schematic expressions of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in a suitable manner in any one or more embodiments or examples. In addition, without contradiction, those skilled in the art can combine and combine the different embodiments or examples described in this specification and the features of different embodiments or examples.

[0051] The following will Figures 1 to 7 give a detailed description of the emergency command vehicle provided by the present utility model.

[0052] As Figures 1 to 7 shown, the present utility model provides an emergency command vehicle, and the emergency command vehicle includes a carriage 100. The carriage 100 includes a box body 110, a first connection component 160, a second connection component 170, and a third connection component 180. The box body 110 has an opening for a medium-sized compound-wing unmanned aerial vehicle to enter and exit the box body 110. One of the first connection component 160 and the second connection component 170 is arranged on the left inner wall of the box body 110, and the other is arranged on the right inner wall of the box body 110; the first connection component 160 is used for detachably connecting with the left wing and the right wing of the medium-sized compound-wing unmanned aerial vehicle; the second connection component 170 is used for detachably connecting with the tail wing and the wing tip of the medium-sized compound-wing unmanned aerial vehicle. The third connection component 180 is arranged on the bottom plate of the box body 110 and is used for detachably connecting with the fuselage and the arms of the unmanned aerial vehicle.

[0053] In this embodiment, by arranging the first connection component 160 on one of the left inner wall and the right inner wall of the box body 110, arranging the second connection component 170 on the other, and arranging the third connection component 180 on the bottom plate of the box body 110, the various components of the medium-sized compound-wing unmanned aerial vehicle can be reasonably arranged and installed at different positions of the box body 110, ensuring that the box body 110 can carry the medium-sized compound-wing unmanned aerial vehicle. In this way, on the one hand, it avoids using a dedicated transportation tool to transport the medium-sized compound-wing unmanned aerial vehicle, reduces the emergency command cost, and improves the emergency response speed. On the other hand, compared with a small four-rotor unmanned aerial vehicle, the medium-sized compound-wing unmanned aerial vehicle has a wider attitude perception range and richer functions, so it is beneficial to the exertion of emergency command efficiency. Therefore, this embodiment solves the problems of high emergency rescue cost, poor emergency response speed, and poor emergency command efficiency existing in the emergency command vehicle in the prior art.

[0054] It should be noted that in this embodiment, the direction of the front of the emergency command vehicle is the front end.

[0055] As Figure 7 shown, in some embodiments, the first connection assembly 160 includes a first connection structure 161 and a second connection structure 162. The first connection structure 161 includes a plurality of first connection members 163; the plurality of first connection members 163 are spaced apart in the front-rear direction and are used for detachably connecting to one of the left wing or the right wing. The second connection structure 162 includes a plurality of second connection members 164; the plurality of second connection members 164 are spaced apart in the front-rear direction and are located below the first connection structure 161; the second connection members 164 are used for detachably connecting to the other of the left wing or the right wing. Specifically, the plurality of first connection members 163 are spaced apart in the front-rear direction on the left inner wall, and the plurality of second connection members 164 are spaced apart in the front-rear direction on the left inner wall and are located below the first connection structure 161. That is, along the length direction of the left wing and the rear wing, the left wing and the rear wing are mounted on the left inner wall. And the left wing and the rear wing are arranged in the up-down direction. It can further improve the space utilization rate of the box body 110 and is beneficial to the miniaturized design of the whole vehicle.

[0056] Exemplarily, the first connection member 163 is provided with a mounting groove in the front-rear direction, and the left wing is clamped in the mounting groove. In order to further improve the mounting stability, the left wing is mounted in the mounting groove by a strap.

[0057] Exemplarily, the structure of the second connection member 164 and the first connection member 163 may be the same.

[0058] As Figure 6 shown, in some embodiments, the second connection assembly 170 includes a third connection structure 171 and a fourth connection structure 172. The third connection structure 171 is used for detachably connecting to one of the tail wing or the wing tip. The fourth connection structure 172 is located in front of or behind the third connection structure 171; the fourth connection structure 172 is used for detachably connecting to the other of the tail wing or the wing tip. Specifically, the third connection structure 171 includes a plurality of third connection members 173; the plurality of third connection members 173 are spaced apart in the up-down direction on the right inner wall, and the third connection members 173 are used for detachably connecting to the tail wing. The fourth connection structure 172 includes a plurality of fourth connection members 174; the plurality of fourth connection members 174 are spaced apart in the up-down direction on the right inner wall, and the fourth connection members 174 are used for detachably connecting to the wing tip. That is, the tail wing or the wing tip is detachably arranged on the right inner wall, which can further improve the space utilization rate of the box body 110 and is beneficial to the miniaturized design of the whole vehicle.

[0059] Exemplarily, the second connection assembly 170 includes two fourth connection structures 172; both of the two fourth connection structures 172 are located behind the third connection structure 171, and the two fourth connection structures 172 are respectively used for detachably connecting to the left outer wing and the right outer wing of the wing tip.

[0060] Exemplarily, the third connecting member 173 is provided with an installation groove in the up-down direction, and the tail wing is clamped in the installation groove. In order to further improve the installation stability, the tail wing is installed in the installation groove by a strap.

[0061] Exemplarily, the structure of the fourth connecting member 174 may be the same as that of the third connecting member 173.

[0062] As Figure 6 and Figure 7 shown, in some embodiments, the third connection assembly 180 includes a landing gear 181 and a fifth connection structure 182. The landing gear 181 includes a plurality of support frames 183; the plurality of support frames 183 are arranged at intervals in the front-rear direction on the bottom plate and are used for detachably connecting with the fuselage. The fifth connection structure 182 includes a plurality of fifth connecting members 184; the plurality of fifth connecting members 184 are arranged at intervals in the front-rear direction on the bottom plate and are located on the left or right side of the landing gear 181 and are used for detachably connecting with the arm. That is to say, the fuselage and the arm are arranged in parallel on the bottom plate in the left-right direction. The fuselage and the arm extend in the front-rear direction. It can further improve the space utilization rate of the box body 110 and is beneficial to the miniaturized design of the whole vehicle.

[0063] Exemplarily, the fifth connecting member 184 is provided with an installation groove in the up-down direction, and the arm is clamped in the installation groove. In order to further improve the installation stability, the arm is installed in the installation groove by a strap.

[0064] Preferably, the first connecting member 163, the second connecting member 164, the third connecting member 173, the fourth connecting member 174 and the fifth connecting member 184 are made of foam material, and the installation surfaces are milled according to the shapes of the respective parts of the drone, and are bonded to the inner side surface of the box body 110 by high-strength structural adhesive.

[0065] Preferably, the strap is a nylon strap with a buckle. One end is sewn on the corresponding connecting member, and the other end passes through the buckle and is tightened and then bonded to the body buckle of the strap to achieve the locking function.

[0066] In some embodiments, the length of the box body 110 is not greater than 4.2 m. That is to say, the dimension of the box body 110 in the front-rear direction is not greater than 4.2 m. It can not only load medium and large composite wing drones, but also reduce the requirements for the driver and ensure the passability of the emergency command vehicle at the front line.

[0067] Specifically, the length of the emergency command vehicle equipped with the box body 110 is not greater than 6 m.

[0068] Exemplarily, the length of the emergency command vehicle equipped with the box body 110 is 5.9 m, the width is 1.8 m, and the height is 1.4 m.

[0069] In the related art, whether it is transporting small quadrotor drones or using special transport vehicles to transport medium and large compound-wing drones, either the individual components of the drone are carried onto or off the vehicle compartment one by one, or the individual components are first packed in packaging boxes and then the packaging boxes are carried onto or off the vehicle compartment. The above two ways of loading and unloading both have the problem of slow state conversion speed of the drone, thus affecting the emergency response speed of the emergency rescue vehicle and the on-site command efficiency. Therefore, how to improve the state conversion speed of the drone is also an urgent problem to be solved in the industry.

[0070] To solve the above problems, as Figures 1 to 5 shown, in some embodiments, the vehicle compartment 100 further includes a first door assembly 120 and a first drive assembly 130. The first door assembly 120 is hinged to the box body 110 and is used to close or open the opening; when the first door assembly 120 is opened, the first door assembly 120 is used to load medium compound-wing drones. The first drive assembly 130 is installed on the box body 110 and is used to drive the first door assembly 120 to lift and lower, so that the first door assembly 120 can load and unload medium compound-wing drones.

[0071] In this embodiment, by providing the first door assembly 120 that can load medium compound-wing drones in the open state, and by providing the first drive assembly 130 that can drive the first door assembly 120 to lift and lower, when it is necessary to load and unload medium compound-wing drones, the various parts of the medium compound-wing drone can be first loaded on the first door assembly 120, and then the first drive assembly 130 is used to drive the first door assembly 120 to lift and lower, so as to achieve the purpose of loading and unloading multiple parts of the medium compound-wing drone at one time, improve the loading and unloading speed, thereby improving the state conversion speed of the medium compound-wing drone, and improving the emergency response speed and on-site command efficiency.

[0072] In some embodiments, the first drive assembly 130 includes a cylinder. The cylinder is installed on the box body 110, and the driving end of the cylinder is connected to the first door assembly 120 and is used to drive the first door assembly 120 to lift and lower.

[0073] Further, when the first door assembly 120 is in a closed state, the first door assembly 120 is in a vertical state. When the first door assembly 120 is in an open state, the first door assembly 120 is in a horizontal state.

[0074] As Figure 1 and Figure 4 shown, specifically, the first drive assembly 130 includes a linear motor. The mounting end of the linear motor is installed on the box body 110, and the driving end of the linear motor is hinged to the lower end of the first door assembly 120. As Figure 4 shown, the linear motor drives the open first door assembly 120 to lift and lower.

[0075] Exemplarily, the first driving assembly 130 includes two linear motors; the two linear motors are respectively installed at the rear ends of the left side wall and the right side wall of the box body 110, and the driving ends of the two linear motors are respectively hinged to the lower ends of the left side surface and the right side surface of the first door assembly 120. This improves the stability of the lifting of the first door assembly 120.

[0076] As Figure 1 shown, in some embodiments, the first door assembly 120 includes a first door member 121 and an extension member 122; the lower ends of the left side surface and the right side surface of the first door member 121 are respectively and correspondingly hinged to the driving ends of the linear motors. The extension member 122 is formed at the upper end of the first door member 121, and the inner side surface of the extension member 122 is an inclined plane, with the front end of the extension member 122 being higher than the rear end. In other words, the end of the extension member 122 close to the first door member 121 is higher than the end away from the first door member 121. By providing the extension member 122 with an inclined inner side surface, it is convenient for the unmanned aerial vehicle to get on and off the first door assembly 120.

[0077] As Figures 1 to 3 shown, in some embodiments, the carriage 100 further includes a locking assembly; the locking assembly is used to lock the first door assembly 120 to the box body 110 so that the first door assembly 120 closes the opening. By providing the locking assembly, it can be avoided that the first door assembly 120 opens during transportation.

[0078] As Figure 1 、 Figure 2 and Figure 3 shown, further, the locking assembly includes a slot 151 and a clamping member 152 that is in clamping engagement with the slot 151; the slot 151 is formed in the box body 110, and the clamping member 152 is hinged to the first door assembly 120; alternatively, the slot 151 is formed in the first door assembly 120, and the clamping member 152 is hinged to the box body 110. The structures of the slot 151 and the clamping member 152 are simple and convenient to operate.

[0079] Specifically, the locking assembly includes two locking members 153, and the two locking members 153 are respectively and correspondingly installed on the rear side surfaces of the left side wall and the right side wall of the box body 110. Along the left - right direction, the locking member 153 is provided with a slot 151, and the clamping member 152 is in limit clamping engagement with the slot 151 to lock the first door assembly 120 to the box body 110. By providing the locking member 153, it is avoided to open slots on the box body 110. Additionally, according to actual needs, the locking member 153 can be installed at different height positions.

[0080] Specifically, the upper end of the slot 151 is bent downward and inward to form a limiting portion, and the end of the clamping member 152 away from the hinge point abuts against the limiting portion to prevent the clamping member 152 from leaving the slot 151 during transportation.

[0081] As Figure 1 shown, in some embodiments, the carriage 100 further includes a second door assembly 140 and a second driving assembly; the second door assembly 140 is located above the first door assembly 120, and the upper end of the second door assembly 140 is hinged to the box body 110. The second driving assembly is installed on the box body 110, and the second driving assembly is used to drive the second door assembly 140 to flip, so as to cooperate with the first door assembly 120 to close or open the opening. Specifically, the first door assembly 120 realizes the closing of the lower opening, and the second door assembly 140 realizes the closing of the upper opening. When both the first door assembly 120 and the second door assembly 140 are in the vertical state, the opening is completely closed.

[0082] In this embodiment, by setting the second door assembly 140 and the second driving assembly, the weight of the first door assembly 120 can be reduced, the power of the linear motor can be decreased, the workload of personnel can be alleviated, and the force on the locking assembly can be reduced. In addition, once the first door assembly 120 is damaged, on the basis of the second door assembly 140, by adding some baffles, a temporary door can be quickly formed, improving the reliability of task execution.

[0083] As Figure 1 and Figure 5 shown, further, the second door assembly 140 includes a second door member 141 and a protruding limiting member 142; the upper end of the second door member 141 is hinged to the box body 110. The protruding limiting member 142 is installed on the outer side surface of the second door member 141; the upper end of the protruding limiting member 142 protrudes from the outer side surface of the first door assembly 120. By providing the protruding limiting member 142 whose upper end protrudes from the outer side surface of the limiting member of the first door assembly 120, not only can the sealing performance of the opening be improved to prevent rainwater from entering the opening, but also it can play a role in shading and improve the equipment protection ability.

[0084] Further, the outer side surface of the protruding limiting member 142 contacts or separates from the upper end of the inner side surface of the first door assembly 120, so that the first door assembly 120 and the second door assembly 140 partially overlap, improving the sealing level.

[0085] Specifically, the outer side surface of the protruding limiting member 142 is an inclined surface. In other words, the thickness of the protruding limiting member 142, that is, the dimension of the protruding limiting member 142 in the front-back direction, decreases sequentially from top to bottom. The inclined surface of the protruding limiting member 142 fits with the inclined surface of the extension member 122.

[0086] As Figure 1As shown, in some embodiments, the emergency command vehicle further includes a power supply module 200; the power supply module 200 includes at least two of a solar cell, a battery pack, or a generator; the solar cell is disposed on the outer top of the box body 110. By providing at least two power supply modules 200, when one of the power supply modules 200 fails, the other can serve as a backup power source, which can expand the application scope of the emergency command vehicle, ensure the continuous operation ability of the emergency command vehicle under extreme conditions, and improve the reliability and independence of task execution.

[0087] Specifically, the power supply module 200 includes a solar cell, a battery pack, and a diesel generator. Ensure that the vehicle can independently operate all on-vehicle devices for a long time without external power supply. The power supply module 200 is designed with an energy management system to intelligently distribute power according to the power consumption requirements of the devices to ensure efficient use of power.

[0088] Specifically, the solar cell is preferably a solar photovoltaic panel, which is installed on the top of the carriage 100.

[0089] Exemplarily, the area of the solar photovoltaic panel in the unfolded state is 6 m 2 , with a power generation power of 1200 W. The diesel generator has a rated power generation power of 8 kw. The battery pack is installed under the cabinet, with a weight of 250 kg and an energy storage of 45000 Wh. After the external power supply fails, the generator supplies power first, and the battery pack and the photovoltaic panel are used as backup power supplies.

[0090] As Figure 6 and Figure 7 shown, in some embodiments, the emergency command vehicle further includes a communication command module 400; the communication command module includes a communication command seat 410 and a lifting platform 420. The communication command seat 410 is disposed at the front end inside the box body 110 for communication connection with a medium-sized compound-wing unmanned aerial vehicle and a host computer. The lifting platform 420 is disposed inside the box body 110; the lifting platform 420 is connected to the communication antenna of the communication command seat 410 for driving the communication antenna to enter and exit the box body 110 in the vertical direction. This can facilitate on-site command and dispatch and information release, and can improve the emergency response speed.

[0091] Furthermore, the communication command seat 410 is internally provided with a workstation and a communication module; the communication command seat 410 is used for the control of the unmanned aerial vehicle, emergency communication command, and interconnection with the command system. It is convenient for on-site command and dispatch and information release, supports remote video conferencing, and realizes mobile office.

[0092] Furthermore, the lifting platform 420 includes a lifting driving member and a support rod; the communication antenna is disposed on the support rod; the lifting driving member is located inside the box body 110 and is connected to the support rod for driving the communication antenna to enter and exit the box body 110 through the support rod.

[0093] Furthermore, the communication antenna includes a microwave data link directional antenna, an omnidirectional antenna, or a phased array satellite communication antenna. The lifting platform is used to carry the communication antenna up and down, enabling the communication antenna to extend out of the carriage 100. By providing multiple types of communication antennas, a stable and reliable command communication link can be established even in an environment without network or with weak signals. The intelligent management software automatically switches to the optimal communication link.

[0094] As Figure 1 shown, in some embodiments, the emergency command vehicle further includes an environment detection module 300; the environment detection module 300 is disposed outside the carriage 100, and the environment detection module 300 is communicatively connected to the communication command module for monitoring the surrounding environment to assist in decision-making.

[0095] Furthermore, the environment detection module 300 includes a camera 310, a temperature and humidity sensor, an anemometer 320, and / or a positioning module 330. By providing multiple types of environment detection modules, the surrounding environment can be detected more comprehensively, improving the accuracy of decision-making.

[0096] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that they can still modify the technical solutions described in the foregoing embodiments or perform equivalent replacements for some of the technical features; and these modifications or replacements do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. An emergency command vehicle, comprising a carriage (100), characterized in that, The carriage (100) includes: A box body (110) having an opening for a medium composite wing unmanned aerial vehicle to enter and exit the box body (110); A first connection component (160) and a second connection component (170); one of the first connection component (160) and the second connection component (170) is disposed on the left inner wall of the box body (110), and the other is disposed on the right inner wall of the box body (110); the first connection component (160) is used for detachably connecting to the left wing and the right wing of the medium composite wing unmanned aerial vehicle; the second connection component (170) is used for detachably connecting to the tail wing and the wing tip of the medium composite wing unmanned aerial vehicle; A third connection component (180) disposed on the bottom plate of the box body (110) for detachably connecting to the fuselage and the arm of the unmanned aerial vehicle.

2. The emergency command vehicle according to claim 1, wherein, The first connection component (160) includes: A first connection structure (161) including a plurality of first connection members (163); the plurality of first connection members (163) are spaced apart in the front-rear direction for detachably connecting to one of the left wing or the right wing; A second connection structure (162) including a plurality of second connection members (164); the plurality of second connection members (164) are spaced apart in the front-rear direction and are located below the first connection structure (161); the second connection members (164) are used for detachably connecting to the other of the left wing or the right wing.

3. The emergency command vehicle according to claim 1, wherein, The second connection component (170) includes: A third connection structure (171) for detachably connecting to one of the tail wing or the wing tip; A fourth connection structure (172) located in front of or behind the third connection structure (171); the fourth connection structure (172) is used for detachably connecting to the other of the tail wing or the wing tip.

4. The emergency command vehicle according to claim 1, characterized in that, The third connection component (180) includes: A landing gear (181) including a plurality of support frames (183); the plurality of support frames (183) are spaced apart in the front-rear direction on the bottom plate for detachably connecting to the fuselage; A fifth connection structure (182) including a plurality of fifth connection members (184); the plurality of fifth connection members (184) are spaced apart in the front-rear direction on the bottom plate and are located on the left or right side of the landing gear (181) for detachably connecting to the arm.

5. The emergency command vehicle according to claim 1, characterized in that, The emergency command vehicle further includes a communication command module (400), and the communication command module (400) includes: A communication command seat (410) disposed at the front end inside the box body (110) for communication connection with the medium composite wing unmanned aerial vehicle and the upper computer; A lift table (420) disposed inside the box body (110); the lift table (420) is connected to the communication antenna of the communication command seat (410) for driving the communication antenna to enter and exit the box body (110) in the up-down direction.

6. The emergency command vehicle according to claim 1, wherein The emergency command vehicle further includes a power supply module (200), and the power supply module (200) includes at least two of a solar cell, a battery pack or a generator.

7. The emergency command vehicle according to claim 1, characterized in that, The length of the box body (110) is not greater than 4.2 m.

8. The emergency command vehicle according to any one of claims 1 to 7, characterized in that, The carriage (100) further includes: A first door assembly (120), one end of which is hinged to the box body (110) and is used to close or open the opening; when the first door assembly (120) is opened, the first door assembly (120) is used to load the medium-sized compound-wing unmanned aerial vehicle; A first driving assembly (130), mounted on the box body (110), and is used to drive the first door assembly (120) to lift and lower, so that the first door assembly (120) can load and unload the medium-sized compound-wing unmanned aerial vehicle.

9. The emergency command vehicle according to claim 8, wherein, The carriage (100) further includes: A second door assembly (140), located above the first door assembly (120), and the upper end of the second door assembly (140) is hinged to the box body (110); A second driving assembly, mounted on the box body (110), and the second driving assembly is used to drive the second door assembly (140) to flip, so as to cooperate with the first door assembly (120) to close or open the opening.

10. The emergency command vehicle according to claim 8, characterized in that, The carriage (100) further includes: A locking assembly, and the locking assembly is used to lock the first door assembly (120) to the box body (110) so that the first door assembly (120) closes the opening.

Images