Multifunctional search and rescue shelter and vehicle
By designing a multi-functional search and rescue cabin, using the roof door, side door and partition separation, combined with lifting components and centralized components, the time-consuming deployment of traditional search and rescue cabin equipment is solved, and fast response and efficient rescue operations are achieved.
Patent Information
- Application Number
- CN202421693850.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-17
- Publication Date
- 2025-06-03
- Estimated Expiration
- 2034-07-17
AI Technical Summary
The traditional search and rescue cabin cannot effectively store and deploy a variety of search and rescue equipment, which makes it time-consuming to remove, assemble and debug the equipment during the search and rescue process, and the rescue operation cannot be launched quickly.
A multi-functional search and rescue cabin is designed. By setting up a roof door, side door and partition separation on the cabin, it realizes partition management and rapid entry and exit of sky search and rescue equipment and ground search and rescue equipment, and combines lifting components and down-to-earth components to realize the automatic operation of the equipment.
It improves the utilization rate of space in the search and rescue cabin, simplifies the deployment and debugging process of equipment, reduces manual preparation time, and can quickly respond and launch rescue operations.
Smart Images

Figure CN222933804U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of rescue equipment, in particular to a multi-functional search and rescue cabin and vehicle. Background Art
[0002] After natural disasters, accidents and other emergencies, it is of great significance to quickly carry out search and rescue operations to reduce casualties, minimize economic losses and restore social order. In this process, modern intelligent search and rescue equipment has played a crucial role.
[0003] These intelligent search and rescue equipment are generally transported by vehicle-mounted cabins. However, traditional cabins can only achieve a single transportation function. After arriving at the search and rescue area, it is necessary to manually take out, assemble and debug equipment such as drones and search and rescue robots. The deployment process takes a long time, and rescue operations cannot be quickly launched, delaying precious search and rescue time. Summary of the Utility Model
[0004] Based on this, in view of the above problems, it is necessary to provide a multi-functional search and rescue cabin and vehicle that can comprehensively store a variety of search and rescue equipment and enable the search and rescue equipment to freely enter and exit.
[0005] A multi-functional search and rescue cabin includes a cabin body. A top cabin door is arranged at the top of the cabin body, and a side cabin door is arranged on the side. After the side cabin door is opened, an intermediate platform connecting the cabin body and the ground is formed.
[0006] The inner cavity of the cabin body is partitioned. Among them, the sky search and rescue equipment partition and the communication component partition are arranged facing the top cabin door, and the ground search and rescue equipment partition is arranged facing the side cabin door.
[0007] In one embodiment, the top cabin door is slidably engaged with the cabin body.
[0008] In one embodiment, the top cabin door includes a left cabin door and a right cabin door. When opened, the left cabin door slides to the left, and the right cabin door slides to the right.
[0009] In one embodiment, the lower end of the side cabin door is hinged to the lower end of the cabin body, and the upper end is a free end;
[0010] The free end rotates around the hinge end and abuts against the ground after being fully opened, forming an intermediate platform connecting the cabin body and the ground.
[0011] In one embodiment, on the inner side surface of the side cabin door, a fixing member is arranged from the free end to the middle section position, and a sliding die assembly is arranged inside the cabin body;
[0012] A pulley assembly opposite to the position of the fixing member is arranged at the upper end of the cabin body and on the sliding die assembly;
[0013] Fix one end of the sling to the fixing part, pass the other end through the pulley assembly and then fix it to the inner side wall of the cabin. Then, drive the sling to slide on the pulley assembly through the movement of the slip form assembly, apply a force to the sling to control the opening and closing of the side cabin door.
[0014] In one embodiment, a pull rod is provided to control the opening and closing of the side cabin door;
[0015] One end of the pull rod is connected to the inner side of the side cabin door; the other end is connected to the inside of the cabin; and / or
[0016] A support member is provided inside the cabin, one end of the pull rod is connected to the inner side of the side cabin door; the other end is fixed to the support member.
[0017] In one embodiment, a lifting assembly is further provided in the sky search and rescue equipment partition, and a landing platform is provided on the lifting assembly; the landing platform is driven to rise or fall by the lifting assembly.
[0018] In one embodiment, a centering assembly is further provided on the landing platform; the centering assembly centers and / or fixes the sky search and rescue equipment parked on the landing platform.
[0019] In one embodiment, a maintenance door is further provided on the cabin; the maintenance door is provided on any side other than the side cabin door.
[0020] A vehicle includes the multi-functional search and rescue cabin as described in any one of the above.
[0021] Compared with the prior art, the multi-functional search and rescue cabin and vehicle provided by the present utility model have the following effects:
[0022] 1. Reasonably partition the functions of the cabin, with clear function management, which can effectively improve the utilization rate of the space inside the cabin.
[0023] 2. A top cabin door is provided, and the sky search and rescue equipment partition and the communication component partition are arranged facing the top cabin door, which is convenient for the release and landing of the sky search and rescue equipment; and the communication component is placed at a relatively high position for communication to maintain the stability of communication and data transmission.
[0024] 3. A side cabin door is provided on one side of the cabin. When the cabin door is opened, the side cabin door forms an intermediate platform connecting the cabin and the ground, which is convenient for ground search and rescue equipment to freely enter and exit the cabin based on this intermediate platform, improving the mobility of each equipment. Description of the Drawings
[0025] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the following will briefly introduce the accompanying drawings required for the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on the structures shown in these drawings.
[0026] Figure 1 It is a three-dimensional structure diagram of the multifunctional search and rescue shelter provided in Embodiment 1 of the present utility model;
[0027] Figure 2 In Embodiment 1 of the present utility model Figure 1 Enlarged schematic diagram of B;
[0028] Figure 3 It is a top view of the multifunctional search and rescue shelter provided in Embodiment 1 of the present utility model;
[0029] Figure 4 In Embodiment 1 of the present utility model Figure 3 Sectional view A-A;
[0030] Figure 5 It is a schematic diagram of the layout of search and rescue equipment provided in Embodiment 1 of the present utility model;
[0031] Figure 6 It is a three-dimensional structure diagram of the multifunctional search and rescue shelter provided in Embodiment 2 of the present utility model.
[0032] Explanation of reference numerals:
[0033] Cabin body 1, top cabin door 11, left cabin door 111, right cabin door 112, partition board 113, maintenance door 12, side cabin door 13, sling 131, fixing member 132, fixed pulley 133, movable pulley 134, slip form assembly 135;
[0034] Sky search and rescue equipment area 21, lifting assembly 211, landing platform 212, centering assembly 213; Communication component area 22, installation platform 221, antenna 222; Ground search and rescue equipment area 23;
[0035] UAV 31, antenna 32, visual monitoring device 33, search robot 34, rescue machine 35;
[0036] Pull rod 41, support member 42.
[0037] The realization, functional characteristics and advantages of the object of the present invention will be further described in conjunction with the embodiments with reference to the accompanying drawings. Detailed implementation manners
[0038] In order to make the above objects, features, and advantages of the present utility model more obvious and understandable, the following will describe in detail the specific embodiments of the present utility model with reference to the accompanying drawings. Many specific details are set forth in the following description to facilitate a full understanding of the present utility model. However, the present utility model can be implemented in many other ways different from those described herein, and those skilled in the art can make similar improvements without departing from the connotation of the present utility model. Therefore, the present utility model is not limited by the specific embodiments disclosed below.
[0039] The terms "first" and "second" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include at least one of such features. In the description of the present utility model, the meaning of "a plurality of" is at least two, such as two, three, etc., unless otherwise specifically defined.
[0040] In the present utility model, unless otherwise clearly defined and limited, the terms "installed", "connected", "connected to", "fixed", etc. shall be understood in a broad sense. For example, it may be a fixed connection, a detachable connection, or integrated; it may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium, and it may be the internal communication of two components or the interaction relationship between two components, unless otherwise clearly limited. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.
[0041] The following will describe in detail the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present utility model.
[0042] Embodiment 1
[0043] Refer to Figures 1 to 5 , which is the first multi-functional search and rescue shelter structure provided in this embodiment, including a cabin body 1. A top cabin door 11 is provided at the top of the cabin body 1, and a side cabin door 13 is provided on the side. After the side cabin door 13 is opened, an intermediate platform connecting the cabin body 1 and the ground is formed. The inner cavity of the cabin body 1 is partitioned. Among them, the sky search and rescue equipment partition 21 and the communication component partition 22 are arranged facing the top cabin door 11, and the ground search and rescue equipment partition 23 is arranged facing the side cabin door 13.
[0044] Through such partition settings, the layout functions inside the cabin can be made clear, facilitating management. At the same time, the utilization rate of the space inside the mobile cabin can also be improved. In addition, a top cabin door 11 is provided at the top of the cabin 1, and then the sky search and rescue equipment partition 21 and the communication component partition 22 are arranged facing the top cabin door 11, facilitating the launch and landing of the sky search and rescue equipment; and, the communication components are placed at a relatively high position for communication to maintain the stability of communication and data transmission. A side cabin door 13 is provided on the side of the cabin 1. When the side cabin door 13 is opened, an intermediate platform connecting the cabin 1 and the ground is formed, facilitating the ground search and rescue equipment to freely enter and exit the mobile cabin based on this intermediate platform. When rescue is needed, the equipment can be assembled and debugged in advance. When arriving at the search and rescue area, manual handling is not required, and each piece of equipment can independently and quickly start rescue operations according to instructions, reducing the manual preparation time at the rescue site, thus saving precious search and rescue time.
[0045] Specifically, the cabin 1 is a cavity structure enclosed by multiple plate-like structures, with a top cabin door 11 provided at its top and a maintenance door 12 and a side cabin door 13 provided on its side. The interior of the cavity structure is divided into a sky search and rescue equipment partition 21, a communication component partition 22, and a ground search and rescue equipment partition 23 by a partition plate 113. The openings of the sky search and rescue equipment partition 21 and the communication component partition 22 face the top cabin door 11, and the opening of the ground search and rescue equipment partition 23 faces the side cabin door 13. Each piece of equipment enters and exits for work through different exits, with clear functions and reasonable space utilization, reducing the congestion problem caused by different equipment entering and exiting the same area simultaneously; the sky search and rescue equipment and the ground search and rescue equipment are managed separately, which can improve the response speed of each piece of equipment.
[0046] During transportation, the top cabin door 11, the maintenance door 12, and the side cabin door 13 together with other plate-like structures form a sealed cavity structure to protect various equipment components inside the cabin 1. When arriving at the destination, the top cabin door 11 and the side cabin door 13 are opened according to instructions to facilitate the start of work of each search and rescue equipment.
[0047] Among them, the top cabin door 11 is in sliding fit with the cabin. The sliding fit methods include but are not limited to: the way of gear driving and rack meshing, plus the guidance of a linear guide rail; or the way of sprocket and chain driving, plus the guidance of a linear guide rail; or the way of a lead screw module driving a wire pulley, plus the guidance of a linear guide rail, or the way of a scissor-type crank connecting mechanism driving, plus the guidance of a linear guide rail, etc.
[0048] For example, when using the method of gear driving rack meshing and guiding with linear guides, on the top of the cabin body 1, linear guides are respectively arranged on both sides along the movement direction, and gears are arranged inside the guides; on the bottom of the top cabin door 11, sliders matching with the linear guides and racks matching with the gears are arranged; the guiding is achieved through the cooperation of the sliders and the linear guides, and the opening and closing of the top cabin door 11 are realized through the meshing of the rack and the gear. Other sliding cooperation methods are similar and will not be elaborated here.
[0049] It should be noted that when using the above sliding cooperation method, the opening and closing degree of the top cabin door 11 can be controlled by electric drive to meet the requirements in different scenarios. Moreover, in the method of linear guide and slider cooperation, the linear guide is composed of a high-precision ball screw or slide rail, so as to be able to bear a large load and provide precise control. The electric sliding method uses a motor and a transmission device (such as a screw, rack and gear) to push the top cabin door 11 to slide, and the precise control of the cabin door is realized by controlling the rotation speed and direction of the motor.
[0050] Furthermore, the top cabin door 11 includes a left cabin door 111 and a right cabin door 112. During operation, the left cabin door 111 slides to the left, and the right cabin door 112 slides to the right. When the left cabin door 111 and the right cabin door 112 slide to both sides respectively, the length of their sliding paths should be such that the sky search and rescue equipment area 21 and the communication component area 22 can be completely exposed, so as to ensure that the work of the sky search and rescue equipment and the communication components is not interfered.
[0051] A door frame is provided on the side of the cabin body 1, and a side cabin door 13 is installed. The lower end of the door frame is hinged to the lower end of the side cabin door 13, and the upper end is a free end; the free end rotates around the hinge end to open until it abuts against the ground, forming an intermediate platform connecting the cabin body 1 and the ground.
[0052] When controlling the opening and closing of the side cabin door 13, it is completed through the cooperation of the sliding mode component 135 and the pulley component. Specifically, on the left and right sides of the side cabin door 13, fixing parts 132 are respectively arranged from the free end to the middle section position; on the left and right sides inside the cabin body 1, sliding mode components 135 are respectively arranged along the width direction; on the upper end of the cabin body, that is, on the upper part of the door frame and the sliding mode component 135, pulley components opposite to the positions of the fixing parts 132 are arranged. Based on the principle of the movable pulley, the moving distance of the object is half of the pulling distance of the rope. Therefore, the number of pulley components needs to be set according to the situation to meet the requirement of being able to completely open or close the side cabin door 13. In this embodiment, refer to Figure 2, there are two sets of pulley assemblies. Each set of pulley assemblies includes a fixed pulley 133 and a movable pulley 134. Among them, the fixed pulley 133 is arranged on the door frame, and the movable pulley 134 is arranged on the slip form assembly 135. One end of the sling 131 is fixed to the fixing member 132, and the other end passes through the fixed pulley 133 and the movable pulley 134 in the pulley assembly in sequence and then is fixed to the inner side wall of the cabin body 1. Then, through the movement of the slip form assembly 135, a force is applied to the sling 131 to drive the sling 131 to slide on the pulley assembly to control the opening and closing of the side cabin door. It should be noted that the slip form assembly 135 is a conventional matching mode of a chute and a slider, which will not be elaborated here.
[0053] A maintenance door 12 is also arranged on the cabin body 1. The maintenance door 12 is arranged on any side other than the side cabin door 13. It can be a swing door as shown in the figure, or can be set as a sliding door, a folding door, etc., which is specifically set according to the structure of the cabin body. When a fault occurs in the internal structure of the cabin body 1 or a rescue device fails, enter the cabin body 1 through the maintenance door 12 for inspection and maintenance.
[0054] Inside the cabin body 1, the sky search and rescue equipment area 21 and the communication component area 22 are arranged above the cavity structure, and the ground search and rescue equipment area 23 is arranged below the cavity structure. The spaces of each area are separated by a partition board 113.
[0055] In this embodiment, no partition board 113 is arranged between the sky search and rescue equipment area 21 and the communication component area 22 above the cavity structure. Instead, the left side is set as the sky search and rescue equipment area 21 and the right side is set as the communication component area 22 in terms of space. However, a partition board 113 can also be arranged between the two areas according to the situation.
[0056] A lifting component 221 is arranged in the sky search and rescue equipment area 21, and a landing platform 212 is arranged on the lifting component 221; the lifting component 211 can rise or fall through mechanical movement, thereby driving the landing platform 212 to rise or fall. During operation, the top cabin door 11 is opened, and the landing platform 212 rises to a height flush with the top cabin door 11 or slightly higher than the top cabin door 11 under the drive of the lifting component 211 to facilitate the landing or takeoff of the sky search and rescue equipment. Further, a centering component 213 is arranged on the landing platform to center and / or fix the sky search and rescue equipment parked on the landing platform 211. The lifting component 211 and the centering component 213 are of conventional structural settings, which will not be elaborated here.
[0057] An installation platform 221 is arranged in the communication component area 22, and the communication components are fixed through the installation platform.
[0058] Refer to Figure 5, which is a schematic diagram of the layout of the search and rescue equipment provided in this embodiment. Among them, the aerial search and rescue equipment is the unmanned aerial vehicle 31; the communication component includes the antenna 32 and the visual monitoring device 33; the ground search and rescue equipment area 23 includes the search robot 34 and the rescue robot 35. During operation, the left hatch 111 and the right hatch 112 slide open to both sides. After the lifting component 211 drives the landing platform 212 to rise to the designated height, the unmanned aerial vehicle 31 is ready to take off. After the side hatch 13 rotates and opens and abuts against the ground to form an intermediate platform, after receiving the command, the search robot 34 reaches the ground from the ground search and rescue equipment area 23 through this intermediate platform and starts the search work. When the target is found, the rescue robot 35 is dispatched, reaches the ground from the ground search and rescue equipment area 23 through this intermediate platform, and goes to the destination to complete the rescue work. After the search and rescue is completed, the unmanned aerial vehicle 31 lands on the landing platform 212 and is centered and fixed by the centering component 213. The lifting component 211 drives the landing platform 212 to descend, the antenna 32 automatically retracts, and the top hatch 11 closes. The search robot 34 and the rescue robot 35 return to their corresponding positions in the ground search and rescue equipment area 23 from the ground through the intermediate platform, and the side hatch 13 closes, completing the automatic retraction of each search and rescue equipment.
[0059] Embodiment 2
[0060] Refer to Figure 6 , which is the second multi-functional search and rescue shelter structure provided in this embodiment. Its basic structure is the same as that of Embodiment 1, and the main difference lies in the opening and closing method of the side hatch 13. In this embodiment, the opening and closing of the side hatch 13 are mainly controlled by a pull rod. One end of the pull rod 41 is connected to the inner side surface of the side hatch 13, and the other end is connected to the inside of the cabin body 1 and fixed on the inner side wall of the cabin body 1.
[0061] As shown in the figure, the pull rod 41 can be an electric pull rod, and the side hatch 13 is pulled or pushed through the telescopic movement of the pull rod. It should be noted that it can also be controlled by a mechanical pull rod, that is, the rotation of a long rod or a short rod to open and close the side hatch 13; or controlled by a pneumatic pull rod, that is, the telescopic movement of a cylinder is used to control the pull rod 41, so as to realize the opening and closing of the side hatch 13; or controlled by a spring-assisted pull rod, that is, a spring is added to the pull rod structure, and the elastic force of the spring is used to assist the movement of the pull rod 41 to make the opening and closing of the side hatch 13 more stable and labor-saving; it is specifically set according to the situation.
[0062] Furthermore, a support member 42 can be added, or the other end of the pull rod 41 is not fixed on the inner side wall of the cabin body 1, but only the support member 42 is set to support the pull rod 41 to ensure the stability of the pull rod 41. The support member 42 can be a vertical support as shown in the figure, or form an angle with the pull rod 41 to provide a reverse support.
[0063] In one of the embodiments, a vehicle is provided, which comprises the multifunctional search and rescue cabin described in any one of the above-mentioned Embodiment 1 or Embodiment 2.
[0064] The technical features of the above-described embodiments may be arbitrarily combined. To make the description concise, not all possible combinations of the technical features in the above-described embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.
[0065] The above-mentioned embodiments only express several implementation methods of the utility model, and the description is relatively specific and detailed, but it cannot be understood as limiting the scope of the utility model. It should be pointed out that for ordinary technicians in this field, several modifications and improvements can be made without departing from the concept of the utility model, which all belong to the protection scope of the utility model. Therefore, the protection scope of the utility model shall be based on the attached claims.
Claims
1. A multifunctional search and rescue shelter, comprising a shelter, characterized in that: The cabin body is provided with a top hatch on the top and a side hatch on the side, and the side hatch is opened to form an intermediate platform connecting the cabin body and the ground; The inner cavity of the cabin is partitioned, wherein the sky search and rescue equipment partition and the communication component partition are arranged toward the top cabin door, and the ground search and rescue equipment partition is arranged toward the side cabin door.
2. The multifunctional search and rescue shelter according to claim 1, characterized in that: The top hatch is slidably matched with the cabin body.
3. The multifunctional search and rescue shelter according to claim 2, characterized in that: The top door comprises a left door and a right door. When opened, the left door slides to the left and the right door slides to the right.
4. The multifunctional search and rescue shelter according to claim 1, characterized in that: The lower end of the side door is hinged to the lower end of the cabin body, and the upper end is a free end; The free end rotates around the hinged end and abuts against the ground after being fully opened, forming an intermediate platform connecting the cabin body and the ground.
5. The multifunctional search and rescue shelter according to claim 4, characterized in that: A fixing piece is provided on the inner side of the side door from the free end to the middle section, and a sliding mold assembly is provided in the cabin body; A pulley assembly is provided at the upper end of the cabin and on the sliding mold assembly, the pulley assembly being opposite to the position of the fixing member; One end of the sling is fixed on the fixing part, and the other end is fixed on the inner wall of the cabin body after passing through the pulley assembly. Then, the sling is driven to slide on the pulley assembly through the movement of the sliding mold assembly, and the opening and closing of the side door is controlled by applying force to the sling.
6. The multifunctional search and rescue shelter according to claim 4, characterized in that: A pull rod is provided to control the opening and closing of the side door; One end of the pull rod is connected to the inner side of the side door; the other end is connected to the cabin body; and / or A support member is arranged in the cabin body, one end of the pull rod is connected to the inner side surface of the side cabin door, and the other end is fixed on the support member.
7. The multifunctional search and rescue shelter according to any one of claims 1 to 6, characterized in that: The sky search and rescue equipment partition is also provided with a lifting assembly, and a landing platform is provided on the lifting assembly; The landing platform is driven to rise or fall by the lifting assembly.
8. The multifunctional search and rescue shelter according to claim 7, characterized in that: The landing platform is also provided with a centering component; The centering component centers and / or fixes the air search and rescue equipment parked on the landing platform.
9. The multifunctional search and rescue shelter according to any one of claims 1 to 6, characterized in that: A maintenance door is also provided on the cabin; The maintenance door is arranged on any side except the side door.
10. A vehicle, characterized in that: The multifunctional search and rescue shelter comprises any one of claims 1 to 9.