Universal wounded transportation platform and rescue system based on unmanned aerial vehicle

Abstract

The utility model provides a general wounded transportation platform and rescue system based on an unmanned aerial vehicle. The general wounded transportation platform comprises the unmanned aerial vehicle; the connecting mechanism comprises a supporting beam and an assembly part, the supporting beam comprises a beam body and a sliding groove, the sliding groove is formed in the beam body, and the assembly part is arranged on the beam body and detachably connected with the aircraft; the rescue cabin comprises a body and a moving assembly, the moving assembly comprises a connecting rod and a pulley, the connecting rod is arranged at the bottom of the body, the pulley is arranged at the end of the connecting rod, and the pulley can move along the interior of the sliding groove. The purposes of overcoming site limitation and improving rescue efficiency are achieved through the aircraft, meanwhile, transportation manpower and time are greatly reduced, and the efficiency and safety of emergency rescue and battlefield first aid are remarkably improved. Compared with conventional rescue equipment at the present stage, the emergency rescue equipment has the remarkable advantages of being convenient to operate, wide in application range, high in safety, capable of improving the rescue efficiency and the like, and a new thought is provided for use and development of the emergency equipment.

Description

Technical Field

[0001] The utility model relates to the technical field of rescue equipment, and in particular to a universal wounded transport platform and rescue system based on an unmanned aerial vehicle. Background Art

[0002] In today's emergency rescue and battlefield first aid practices, the transportation of the wounded primarily relies on the manual handling of emergency vehicles and stretcher bearers. While emergency vehicles can quickly reach the scene and perform efficient rescue missions in open terrain with clear roads, their mobility is severely limited when encountering complex terrain, such as rugged mountains, dense urban areas, dense forests, or battlefield ruins. In these situations, rescuers are often forced to rely on stretcher bearers to traverse obstacles on foot and transport the wounded from dangerous environments. However, this traditional rescue model has exposed numerous shortcomings in actual combat.

[0003] First, stretcher bearers are inefficient at carrying the wounded, especially when they have to travel long distances or cross multiple obstacles. This not only consumes a significant amount of time and energy, but can also worsen the patient's condition due to delayed treatment. Second, faced with large obstacles such as rivers, walls, and deep trenches, stretcher bearers are often helpless and can only choose to detour or take other time-consuming and uncertain measures. This not only further prolongs rescue time but can also put the wounded in even greater danger. More seriously, in battlefield environments, stretcher bearers, due to their slow movement speed and obvious targeting, are easily targeted by enemy fire while carrying the wounded. This not only poses a threat to the safety of the wounded but also greatly increases the safety risks for the rescuers themselves.

[0004] Furthermore, the manual handling of stretchers consumes considerable human resources, which can affect other rescue missions in emergencies, leading to a decrease in overall rescue efficiency. Therefore, to overcome these limitations and improve the efficiency and safety of emergency rescue and battlefield first aid, it is urgent to develop a new type of casualty transport technology. Summary of the Invention

[0005] To this end, the technical problem to be solved by the present invention is to overcome the problems in the existing technology that the use scenarios of rescue equipment are limited and the rescue efficiency needs to be improved, and to provide a universal wounded transportation platform and rescue system based on unmanned aerial vehicles.

[0006] In order to solve the above technical problems, the utility model provides a universal wounded transport platform based on an unmanned aerial vehicle, which includes: an aircraft; a connecting mechanism, the connecting mechanism includes a support beam and at least one assembly part, the support beam includes a beam body and a slide groove, the slide groove is arranged inside the beam body, and at least one assembly part is arranged on the beam body and is detachably connected to the aircraft; a rescue cabin, the rescue cabin includes a main body and a moving component, the person to be rescued is located inside the main body, and the moving component includes a connecting rod and a pulley, wherein the connecting rod is arranged at the bottom of the main body, the pulley is arranged at the end of the connecting rod, and the pulley can move along the inside of the slide groove to drive the main body to connect / disconnect from the connecting mechanism.

[0007] In one embodiment of the present invention, the connecting mechanism further comprises a reinforcing rod, wherein the reinforcing rod and the beam body are arranged perpendicular to each other in the same horizontal plane, and the assembly part is arranged at the end of the reinforcing rod and is detachably connected to the telescopic frame of the aircraft.

[0008] In one embodiment of the present invention, the beam body includes a docking portion and a guide portion, the guide portion extends in the length direction of the beam body, the docking portion is arranged at one end of the guide portion, and the rescue capsule passes through the docking portion and the guide portion in sequence along a first direction and is connected to the support beam, wherein the docking portion is gradually inclined toward the ground in a direction away from the guide portion.

[0009] In one embodiment of the present invention, the connection mechanism further includes at least one limiting member, which is connected to the support beam and extends along the height direction of the body to abut against the side wall of the body.

[0010] In one embodiment of the present invention, the main body includes a bottom plate, side plates and a door body, the bottom plate support is connected to the support beam, the side plates and the door body are arranged around the edge of the bottom plate, wherein the side plates extend along the height direction of the main body, and the door body is rotatably connected to the main body.

[0011] In one embodiment of the present invention, the rescue cabin further comprises a top cover and at least one locking member, wherein the top cover can be buckled onto the side panels and detachably connected to the main body via the locking member.

[0012] In one embodiment of the present invention, a first observation window is provided on the main body, and a second observation window is provided on the top cover, wherein the first observation window is installed on the side panel.

[0013] In one embodiment of the present invention, it further includes an auxiliary rescue mechanism, which is arranged in the main body and includes a ventilator, an air conditioner and a monitor.

[0014] In one embodiment of the present invention, the auxiliary rescue mechanism further includes a control system, the control system is connected to a ground station, and the ventilator, the air conditioner and the monitor are respectively connected to the control system signals.

[0015] The utility model also provides a rescue system, which includes the universal wounded transport platform.

[0016] The above technical solution of the utility model has the following advantages compared with the prior art:

[0017] The utility model discloses a universal wounded transport platform and rescue system based on an unmanned aerial vehicle. The rescue cabin is mounted on the aircraft through a connecting mechanism, thereby driving the rescue cabin to move through the aircraft, thereby overcoming site limitations and improving rescue efficiency. The sliding connection structure between the rescue cabin and the connecting mechanism can also achieve smooth transportation of rescue personnel, thereby significantly reducing transportation manpower and time, and significantly improving the efficiency and safety of emergency rescue and battlefield first aid. Compared with conventional rescue equipment at this stage, this application has significant advantages such as easy operation, wide application range, high safety, and improved rescue efficiency, providing new ideas for the use and development of first aid equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to make the content of the present invention more clearly understood, the present invention is further described in detail below based on specific embodiments of the present invention in conjunction with the accompanying drawings.

[0019] Figure 1 This is a schematic diagram of the three-dimensional structure of the universal wounded transport platform based on an unmanned aerial vehicle in a preferred embodiment of the utility model during use;

[0020] Figure 2 yes Figure 1 A schematic diagram of the three-dimensional structure of the rescue cabin in the universal casualty transport platform based on an unmanned aerial vehicle during movement is shown;

[0021] Figure 3 yes Figure 1 The figure shows a schematic diagram of the three-dimensional structure of the connection mechanism and the rescue cabin in the universal casualty transport platform based on the unmanned aerial vehicle;

[0022] Figure 4 yes Figure 1 A schematic diagram of the three-dimensional structure of the connecting mechanism in the universal wounded transport platform based on the unmanned aerial vehicle is shown;

[0023] Figure 5 yes Figure 1 The diagram shows the explosion structure of the rescue cabin in the universal casualty transport platform based on the unmanned aerial vehicle;

[0024] Figure 6 yes Figure 1 The figure shows a schematic diagram of the three-dimensional structure of the main body and auxiliary rescue mechanism of the universal casualty transport platform based on unmanned aerial vehicles;

[0025] Figure 7 yes Figure 1 The figure shows a schematic diagram of signal transmission for auxiliary rescue agencies in a universal casualty transport platform based on an unmanned aerial vehicle.

[0026] Explanation of the reference numerals in the specification: 100, aircraft; 110, telescopic frame; 200, connecting mechanism; 210, assembly part; 220, support beam; 221, beam body; 2211, docking part; 2212, guide part; 222, slide groove; 223, limit member; 230, reinforcement rod; 300, rescue cabin; 310, main body; 311, bottom plate; 312, door body; 313, side panel; 314, first observation window; 320, top cover; 321, second observation window; 330, moving assembly; 331, connecting rod; 332, pulley; 340, locking member; 400, auxiliary rescue mechanism; 410, ventilator; 420, air conditioner; 430, patient monitor; X, first direction; Y, second direction; Z, third direction. DETAILED DESCRIPTION

[0027] The present invention will be further described below with reference to the accompanying drawings and specific embodiments so that those skilled in the art can better understand the present invention and implement it. However, the embodiments are not intended to limit the present invention. Example 1

[0028] See also Figure 1 and Figure 2 As shown, this embodiment provides a universal casualty transport platform based on an unmanned aerial vehicle, which includes: an aircraft 100; a connecting mechanism 200, wherein the connecting mechanism 200 includes a support beam 220 and at least one assembly part 210, wherein the support beam 220 includes a beam body 221 and a slide groove 222, wherein the slide groove 222 is disposed inside the beam body 221, and at least one assembly part 210 is disposed on the beam body 221 and is detachably connected to the aircraft 100; a rescue capsule 300, wherein the rescue capsule 300 includes a body 310 and a moving assembly 330, wherein a person to be rescued is located inside the body 310, and the moving assembly 330 includes a connecting rod 331 and a pulley 332, wherein the connecting rod 331 is disposed at the bottom of the body 310, and the pulley 332 is disposed at the end of the connecting rod 331, and the pulley 332 is movable along the slide groove 222 to drive the body 310 to connect to / disconnect from the connecting mechanism 200.

[0029] The universal casualty transport platform based on an unmanned aerial vehicle described in this embodiment assembles the rescue cabin 300 on the aircraft 100 via a connecting mechanism 200, thereby driving the rescue cabin 300 to move via the aircraft 100, thereby overcoming site limitations and improving rescue efficiency. The sliding connection structure between the rescue cabin 300 and the connecting mechanism 200 also enables smooth transportation of rescue personnel, thereby significantly reducing transportation manpower and time, and significantly improving the efficiency and safety of emergency rescue and battlefield first aid. Compared to conventional rescue equipment at this stage, this application has significant advantages such as ease of operation, wide application range, high safety, and improved rescue efficiency, providing new ideas for the use and development of first aid equipment.

[0030] It should be noted that, for ease of expression, this embodiment defines the length direction of the universal wounded transport platform based on an unmanned aerial vehicle as a first direction X, the width direction of the universal wounded transport platform based on an unmanned aerial vehicle as a second direction Y, and the height direction of the universal wounded transport platform based on an unmanned aerial vehicle as a third direction Z. The first direction X, the second direction Y, and the third direction Z are arranged perpendicular to each other in pairs, and the first direction X and the second direction Y are located in the same plane.

[0031] See also Figure 1 and Figure 2 As shown, in the universal wounded transport platform based on an unmanned aerial vehicle in this embodiment, the aircraft 100 is used to drive the rescue cabin 300 to fly and move, which includes an aircraft body and a telescopic frame 110 arranged at the bottom thereof. One end of the telescopic frame 110 is fixedly connected to the aircraft body, and the other end is used to connect to the connecting mechanism 200; the connecting mechanism 200 is used to provide an installation platform for the rescue cabin 300, and the rescue cabin 300 is used to accommodate people to be rescued.

[0032] Further, see Figure 3 and Figure 4 As shown, the rescue capsule 300 in this embodiment is supported on the support beam 220 of the connection mechanism 200. Specifically, this embodiment includes two parallel support beams 220, both extending along the first direction X and spaced apart along the second direction Y. The two support beams 220 are symmetrically arranged, with a connecting space between them. A slide groove 222 is provided within the beam body 221 of each support beam 220. The slide groove 222 is connected to the external environment through the side of the corresponding support beam 220 that is connected to the installation space, so as to facilitate the guided assembly of the rescue capsule 300 and form a stop limit for the rescue capsule 300 in the first direction X after assembly.

[0033] Further, the beam body 221 comprises a docking portion 2211 and a guiding portion 2212, the guiding portion 2212 extends along the length direction of the beam body 221, the docking portion 2211 is arranged at one end of the guiding portion 2212, the rescue cabin 300 is connected to the support beam 220 in sequence through the docking portion 2211 and the guiding portion 2212 along the first direction X, wherein the docking portion 2211 is arranged to be gradually inclined to the ground in the direction away from the guiding portion 2212, thereby facilitating the auxiliary guiding of the rescue cabin 300 during installation.

[0034] In the embodiment, the connecting mechanism 200 further comprises a reinforcing rod 230, the reinforcing rod 230 is arranged to be perpendicular to the beam body 221 in the same horizontal plane, the assembly part 210 is arranged at the end of the reinforcing rod 230 and is detachably connected with the telescopic frame 110 of the aircraft 100, thereby strengthening the overall strength of the connecting mechanism 200 and realizing the installation and connection platform of the support beam 220 and the assembly part 210. For different aircrafts 100, the connecting mechanism 200 is correspondingly provided with different assembly parts 210, which only need to realize the connection function with the telescopic frame 110, and the utility model does not make specific limitation on this.

[0035] Further, in order to improve the stability of the rescue cabin 300 during flight transportation, the connecting mechanism 200 in the embodiment further comprises at least one limiting part 223, the limiting part 223 is connected to the support beam 220 and extends along the height direction of the body 310 to abut against the side wall of the body 310, which can realize the limiting and fixing purpose of the rescue cabin 300 through the mutual abutment of the side wall of the rescue cabin 300. Specifically, it can be a stop pin connected through an elastic part or a stop block with a guiding inclined surface, and the utility model does not make specific limitation on this.

[0036] Referring to Figure 5 and Figure 6 , the body 310 in the embodiment comprises a bottom plate 311, a side plate 313 and a door body 312, the bottom plate 311 is supported and connected to the support beam 220, the side plate 313 and the door body 312 are arranged around the edge of the bottom plate 311, wherein the side plate 313 extends along the height direction of the body 310, and the door body 312 is rotationally connected to the body 310. In the embodiment, the body 310 can accommodate one lying injured person or two sitting injured persons. The bottom part is provided with two moving assemblies 330, any moving assembly 330 extends along the second direction Y, and both ends of any moving assembly 330 are respectively connected with pulleys 332, during the assembly process, the pulleys 332 can move along the sliding groove 222 until the rescue cabin 300 is stably supported on the connecting mechanism 200.

[0037] Furthermore, the rescue chamber 300 also includes a top cover 320 and at least one locking member 340. The top cover 320 can be snapped onto the side panels 313 and detachably connected to the body 310 via the locking member 340. Furthermore, a first observation window 314 is provided on the body 310, and a second observation window 321 is provided on the top cover 320, wherein the first observation window 314 is mounted on the side panels 313.

[0038] See also Figure 6 and Figure 7 As shown, this embodiment also includes an auxiliary rescue mechanism 400, which is arranged in the main body 310 and includes a ventilator 410, an air conditioner 420, and a monitor 430. Furthermore, the auxiliary rescue mechanism also includes a control system, which is connected to a ground station, and the ventilator 410, the air conditioner 420, and the monitor 430 are respectively connected to the control system by signal. Specifically, the auxiliary rescue mechanism 400 in this embodiment is configured with a communication network link, and the monitor 430, the ventilator 410, and the air conditioner 420 can be connected to a bridge via a router, and the bridge is connected to the ground station, thereby enabling the above-mentioned devices to be remotely monitored and controlled via the network link. Example 2

[0039] This embodiment provides a rescue system, which includes the above-mentioned universal wounded transport platform.

[0040] In summary, the universal wounded transport platform and rescue system based on an unmanned aerial vehicle described in the present invention assembles the rescue cabin 300 on the aircraft 100 via the connecting mechanism 200, thereby driving the rescue cabin 300 to move via the aircraft 100, thereby achieving the purpose of overcoming site limitations and improving rescue efficiency. The sliding connection structure between the rescue cabin 300 and the connecting mechanism 200 can also achieve smooth transportation of rescue personnel, thereby significantly reducing transportation manpower and time, and significantly improving the efficiency and safety of emergency rescue and battlefield first aid. Compared to conventional rescue equipment at this stage, this application has significant advantages such as ease of operation, wide range of applications, high safety, and improved rescue efficiency, providing new ideas for the use and development of first aid equipment.

[0041] Obviously, the above embodiments are merely examples for clarity of explanation and are not intended to limit the implementation methods. Those skilled in the art will readily appreciate that other variations or modifications based on the above descriptions are possible. It is not necessary and impossible to enumerate all implementation methods here. Obvious variations or modifications arising therefrom remain within the scope of protection of the present invention.

Claims

1. A universal casualty transport platform based on an unmanned aerial vehicle, characterized by: include: aircraft; a connecting mechanism, the connecting mechanism comprising a support beam and at least one assembly member, the support beam comprising a beam body and a slide groove, the slide groove being disposed inside the beam body, and at least one assembly member being disposed on the beam body and detachably connected to the aircraft; The rescue cabin includes a main body and a moving component, the person to be rescued is located inside the main body, and the moving component includes a connecting rod and a pulley, wherein the connecting rod is arranged at the bottom of the main body, and the pulley is arranged at the end of the connecting rod, and the pulley can move along the inside of the slide groove to drive the main body to connect / disconnect with the connecting mechanism.

2. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 1, characterized in that: The connecting mechanism further comprises a reinforcing rod, which is arranged perpendicularly to the beam body in the same horizontal plane. The assembly part is arranged at the end of the reinforcing rod and is detachably connected to the telescopic frame of the aircraft.

3. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 1, characterized in that: The beam body includes a docking portion and a guide portion, the guide portion extends in the length direction of the beam body, the docking portion is arranged at one end of the guide portion, and the rescue capsule passes through the docking portion and the guide portion in sequence along a first direction and is connected to the support beam, wherein the docking portion is gradually inclined toward the ground in a direction away from the guide portion.

4. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 1, characterized in that: The connection mechanism further includes at least one limiting member, which is connected to the support beam and extends along the height direction of the body to abut against the side wall of the body.

5. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 1 is characterized in that: The main body includes a bottom plate, side plates and a door body, the bottom plate is supported and connected to the support beam, the side plates and the door body are arranged around the edge of the bottom plate, wherein the side plates extend along the height direction of the main body, and the door body is rotatably connected to the main body.

6. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 5, characterized in that: The rescue cabin further includes a top cover and at least one locking member. The top cover can be buckled onto the side panels and detachably connected to the body via the locking member.

7. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 6, characterized in that: The main body is provided with a first observation window, and the top cover is provided with a second observation window, wherein the first observation window is installed on the side panel.

8. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 1, characterized in that: It also includes an auxiliary rescue mechanism, which is arranged in the main body and includes a ventilator, an air conditioner and a monitor.

9. The universal wounded transport platform based on an unmanned aerial vehicle according to claim 8, characterized in that: The auxiliary rescue mechanism also includes a control system, which is connected to a ground station. The ventilator, the air conditioner and the monitor are respectively connected to the control system signal.

10. A rescue system, characterized in that: A universal wounded transport platform comprising the universal wounded transport platform as described in any one of claims 1 to 9.

Images