Marine public health emergency medical material putting and recycling integrated system

Abstract

The invention relates to the related technical field of medical treatment and public health, in particular to a marine public health emergency medical material putting and recycling integrated system which comprises a machine body, a connecting mechanism is arranged on the lower surface of the machine body, and a storage mechanism is arranged on the lower surface of the connecting mechanism. When the unmanned aerial vehicle carries the integrated system to work and fly, a rotating shaft drives a propeller to provide power to a target sea area, after the unmanned aerial vehicle arrives, a connecting mechanism air cylinder enables a connecting ring and a storage mechanism to be connected or separated, putting and recycling are completed, a camera can monitor surrounding conditions, and an illuminating lamp is arranged for assisting and a warning lamp is arranged for preventing collision; by means of the arrangement, the device has the capacity of dealing with medical material putting and recycling in ocean regions, the materials are put in time, then the working efficiency of offshore operation teams is improved, medical resources can be effectively recycled, waste of the medical resources is avoided, and the cost of public health emergency treatment is reduced.

Description

Technical Field

[0001] The present invention relates to the technical field of medical and health related fields, and in particular to an integrated system for delivering and recovering marine public health emergency medical supplies. Background Art

[0002] In the field of medical and health care, the guarantee of emergency medical supplies is crucial to responding to public health emergencies. The traditional land-based emergency medical supplies management system has accumulated certain experience and models in responding to epidemics or disasters in local areas of land, such as the establishment of material storage warehouses at different levels, relatively complete land transportation and allocation processes, and material management regulations within hospitals. However, the marine environment has its own particularity and complexity. Offshore drilling platforms and ocean-going fishing fleets are widely distributed in vast sea areas, making it difficult to build fixed and comprehensive and efficient material storage points. This makes it difficult to quickly and accurately deliver medical supplies in emergency situations. Moreover, in the post-use recovery link, due to the particularity of the marine area, the recovery work faces many difficulties and is difficult to carry out in an orderly and efficient manner like on land. Therefore, there is a special need for an integrated system for the delivery and recovery of marine public health emergency medical supplies.

[0003] However, the existing public health emergency medical supplies delivery and recovery equipment is often not capable of coping with the delivery and recovery of medical supplies in marine areas, resulting in untimely delivery of supplies, which in turn affects the health and work efficiency of the entire offshore operation team. Moreover, the inability to effectively recover will also cause a waste of medical resources and increase the cost of public health emergency response. Summary of the invention

[0004] The purpose of the present invention is to provide an integrated system for the delivery and recovery of marine public health emergency medical supplies, so as to solve the problem that the existing public health emergency medical supplies delivery and recovery devices proposed in the above background technology are often not capable of coping with the delivery and recovery of medical supplies in marine areas, resulting in untimely delivery of materials, which in turn affects the health and work efficiency of the entire marine operation team. Moreover, the inability to effectively recover will also cause a waste of medical resources and increase the cost of public health emergency treatment.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an integrated system for the delivery and recovery of marine public health emergency medical supplies, comprising a fuselage main body, a camera fixedly connected to one side surface of the fuselage main body, a lighting lamp fixedly connected to one side surface of the fuselage main body, a warning light bar fixedly connected to one side surface of the fuselage main body, a motor waterproof housing fixedly connected to one side surface of the motor waterproof housing, a propulsion motor fixedly connected to one side surface of the propulsion motor, a fan blade fixedly connected to one side surface of the propulsion motor, a rotating shaft fixedly connected to the upper surface of the fuselage main body, a rotating column fixedly connected to one side surface of the rotating shaft, a propeller fixedly connected to one side surface of the rotating column, a connecting mechanism provided on the lower surface of the fuselage main body, and a storage mechanism provided on the lower surface of the connecting mechanism;

[0006] The storage mechanism includes a storage cover, a waterproof pad, a waterproof ring, a telescopic shell, a spring, a telescopic block, a storage bucket, a limiting groove and a layered fixed baffle. The lower surface of the connecting mechanism is fixedly connected to the storage cover, the lower surface of the storage cover is fixedly connected to the waterproof pad, the lower surface of the waterproof pad is fixedly connected to the waterproof ring, the inner surface of the storage cover is fixedly connected to the telescopic shell, the inner surface of the telescopic shell is fixedly connected to the spring, the lower surface of the spring is fixedly connected to the telescopic block, the lower surface of the storage cover is slidably connected to the storage bucket, the inner surface of the storage bucket is provided with a limiting groove, and a side surface of the limiting groove is slidably connected to the layered fixed baffle.

[0007] Preferably, the lighting lamps are arranged in a group on each side of the camera, and the warning light bars are arranged in a group on each side surface of the fuselage body, and the warning light bars flash red and green lights when in use.

[0008] Preferably, the motor waterproof housing, propulsion motor and fan blades are arranged at the tail end of the fuselage body, so that when the drone falls into the water accidentally, it can be moved by driving the propulsion motor. The rotating column and propeller are symmetrically arranged in four groups about the central axis of the rotating shaft.

[0009] Preferably, the waterproof pad and the waterproof ring are arranged inside the storage cover, and when the storage bucket is rotated inward, liquid can be effectively prevented from penetrating into the interior of the storage bucket. A rotating thread is provided on the outer edge of one side of the storage bucket connected to the storage cover for rotational connection with the storage cover.

[0010] Preferably, two groups of springs are symmetrically arranged on the lower surface of the telescopic shell, and the inner size of the telescopic shell matches the outer size of the telescopic block.

[0011] Preferably, the limiting grooves are symmetrically arranged in four groups with respect to the perpendicular midline of the storage bucket, and the telescopic shells, springs and telescopic block structures are arranged in four groups at the same positions of the corresponding limiting grooves.

[0012] Preferably, there are four groups of support columns below the layered fixed baffle, which are installed corresponding to the positions of the limit grooves, and three groups of layered fixed baffles are placed in a stacked manner inside the storage barrel. The telescopic shell, spring and telescopic block play a role in pushing and fixing the top layered fixed baffle.

[0013] Preferably, the connecting mechanism includes a connecting column, a load-bearing plate, a cylinder, a push rod and a connecting ring, the lower part of the fuselage body is fixedly connected with a connecting column, the lower surface of the connecting column is fixedly connected with a load-bearing plate, one side surface of the load-bearing plate is fixedly connected with a cylinder, one side surface of the cylinder is slidably connected with a push rod, and one side surface of the push rod is movably connected with a connecting ring.

[0014] Preferably, the connecting columns and load-bearing plates are symmetrically arranged in two groups below the fuselage body, the cylinders are symmetrically arranged in two groups on the upper surfaces of the two groups of load-bearing plates, and two groups of push rods are arranged at one end of each group of cylinders.

[0015] Preferably, the cylinder is fixed to the connecting ring by placing the push rods relative to each other, and the fuselage body, the connecting column and the load-bearing plate are made of carbon fiber.

[0016] Compared with the prior art, the beneficial effects of the present invention are as follows: the integrated system works by using a drone as a carrier. During the flight, the rotating shaft above the fuselage body drives the rotating column and the propeller to rotate at high speed, providing lift and flight power for the drone, so that it can fly over the ocean to the offshore operation area of ​​the target sea area. When arriving at the designated location, the cylinder in the connecting mechanism works to push the push rod to move, so that the connecting ring can be connected or separated from the storage mechanism to achieve the delivery or recovery of the storage mechanism. For example, when delivering medical supplies, the cylinder moves to cause the connecting ring to loosen the storage mechanism and drop the storage barrel containing the medical supplies. When recovering, the opposite is true. The storage barrel is first connected and then lifted back under the fuselage body. The camera on one side of the fuselage body can be used to monitor the flight path and the target area in real time. The lighting provides lighting in a dark environment for better observation and operation. The flashing light of the warning light bar serves to warn surrounding ships and personnel to avoid collision accidents. If the drone is flying If the drone accidentally falls into the water during the process, the propulsion motor in the waterproof housing of the motor at the rear end of the fuselage body will start, driving the fan blades to rotate, thereby pushing the drone to move in the water, which is convenient for subsequent recovery or continuation of the mission. For the storage mechanism, the storage barrel is connected to the storage cover by a rotating thread to achieve sealing and fixation. Inside the storage barrel, the layered fixed baffles are installed and positioned through limit grooves, and under the action of the spring, telescopic housing and telescopic block, the top layered fixed baffles can be fixed, which can be used to store and fix different types or batches of medical supplies in layers to prevent confusion or damage caused by shaking during transportation. At the same time, the waterproof pad and waterproof ring can effectively prevent liquids such as seawater from penetrating into the storage barrel, ensuring the storage environment of medical supplies. This arrangement enables the device to have the ability to cope with the delivery and recovery of medical supplies in marine areas, and the materials are delivered in time, thereby improving the work efficiency of the offshore operation team. Moreover, they can be effectively recovered without wasting medical resources, reducing the cost of public health emergency treatment. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is a schematic diagram of the side appearance structure of the present invention;

[0018] Figure 2 It is a schematic diagram of the main structure of the fuselage of the present invention;

[0019] Figure 3 A schematic diagram of the cooperation between the camera and the lighting lamp of the present invention;

[0020] Figure 4 This is a schematic diagram of the structure of the cylinder and the push rod cooperating with each other in the present invention;

[0021] Figure 5 This is a schematic diagram of the structure of the push rod and the connecting ring cooperating with each other in the present invention;

[0022] Figure 6 It is a schematic diagram of the structure of the storage mechanism of the present invention;

[0023] Figure 7 This is a schematic diagram of the structure of the waterproof pad, the waterproof ring and the storage cover cooperating with each other in the present invention;

[0024] Figure 8 It is a schematic diagram of the structure in which the telescopic housing, the spring and the telescopic block cooperate with each other in the present invention.

[0025] In the figure: 1. body; 2. camera; 3. lighting; 4. warning light bar; 5. motor waterproof housing; 6. driving motor; 7. fan blades; 8. rotating shaft; 9. rotating column; 10. propeller; 11. connecting mechanism; 1101. connecting column; 1102. load-bearing plate; 1103. cylinder; 1104. push rod; 1105. connecting ring; 12. storage mechanism; 1201. storage cover; 1202. waterproof pad; 1203. waterproof ring; 1204. telescopic housing; 1205. spring; 1206. telescopic block; 1207. storage bucket; 1208. limit groove; 1209. layered fixed baffle. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0027] See also Figure 1-8 The present invention provides a technical solution: an integrated system for the delivery and recovery of marine public health emergency medical supplies, comprising a fuselage body 1, a camera 2 is fixedly connected to one side surface of the fuselage body 1, a lighting lamp 3 is fixedly connected to one side surface of the fuselage body 1, a warning light bar 4 is fixedly connected to one side surface of the fuselage body 1, a motor waterproof housing 5 is fixedly connected to one side surface of the fuselage body 1, a driving motor 6 is fixedly connected to one side surface of the motor waterproof housing 5, a fan blade 7 is fixedly connected to one side surface of the driving motor 6, a rotating shaft 8 is fixedly connected to the upper surface of the fuselage body 1, a rotating column 9 is fixedly connected to one side surface of the rotating shaft 8, a propeller 10 is fixedly connected to one side surface of the rotating column 9, a connecting mechanism 11 is arranged on the lower surface of the fuselage body 1, and a storage mechanism 12 is arranged on the lower surface of the connecting mechanism 11;

[0028] The storage mechanism 12 includes a storage cover 1201, a waterproof pad 1202, a waterproof ring 1203, a telescopic shell 1204, a spring 1205, a telescopic block 1206, a storage bucket 1207, a limit groove 1208 and a layered fixed baffle 1209. The lower surface of the connecting mechanism 11 is fixedly connected to the storage cover 1201, the lower surface of the storage cover 1201 is fixedly connected to the waterproof pad 1202, the lower surface of the waterproof pad 1202 is fixedly connected to the waterproof ring 1203, the inner surface of the storage cover 1201 is fixedly connected to the telescopic shell 1204, the inner surface of the telescopic shell 1204 is fixedly connected to the spring 1205, and the lower surface of the spring 1205 is fixedly connected to the telescopic block 120 6. The lower surface of the storage cover 1201 is slidably connected with a storage bucket 1207, and the inner surface of the storage bucket 1207 is provided with a limiting groove 1208. The side surface of the limiting groove 1208 is slidably connected with a layered fixed baffle 1209. Through the arrangement of the storage cover 1201, the waterproof pad 1202, the waterproof ring 1203, the telescopic shell 1204, the spring 1205, the telescopic block 1206, the storage bucket 1207, the limiting groove 1208 and the layered fixed baffle 1209, when in use, the rotating shaft 8 above the fuselage body 1 drives the rotating column 9 and the propeller 10 to rotate at high speed, providing lift and flight power for the UAV, so that it can fly over the ocean to the offshore operation area of ​​the target sea area. When arriving at the designated location, the cylinder 1103 in the connecting mechanism 11 works to push the push rod 1104 to move, so that the connecting ring 1105 can be connected or separated from the storage mechanism 12, and the storage mechanism 12 is put into or recovered. For example, when medical supplies are put in, the cylinder 1103 moves to make the connecting ring 1105 loosen the storage mechanism 12, and the storage bucket 1207 containing medical supplies is put down; when recovering, the opposite is true, first connect the storage bucket 1207, and then lift it back to the bottom of the fuselage body 1. The camera 2 on one side of the fuselage body 1 can be used to monitor the flight path and the target area in real time, the lighting 3 provides lighting in a dark environment for better observation and operation, and the flashing light of the warning light bar 4 serves to warn surrounding ships and personnel to avoid collision accidents. If the drone accidentally falls into the water during flight, the propulsion motor 6 in the motor waterproof housing 5 at the tail end of the fuselage body 1 is started, driving the fan blades 7 to rotate, thereby pushing the drone to move in the water, which is convenient for subsequent recovery or continuing to perform tasks. For the storage mechanism 12, the storage bucket 1207 is connected to the storage cover 1201 by a rotating thread to achieve sealing and fixation. Inside the storage barrel 1207, the layered fixed baffle 1209 is installed and positioned through the limit groove 1208, and under the action of the spring 1205, the telescopic shell 1204 and the telescopic block 1206, the top layered fixed baffle 1209 can be fixed, which can be used to store and fix different types or batches of medical supplies in layers to prevent confusion or damage caused by shaking during transportation.At the same time, the waterproof pad 1202 and the waterproof ring 1203 can effectively prevent liquids such as seawater from penetrating into the storage barrel 1207, ensuring the storage environment of medical supplies. This arrangement enables the device to cope with the delivery and recovery of medical supplies in marine areas, and the delivery of materials is timely, thereby improving the work efficiency of the offshore operation team. Moreover, it can be effectively recovered without wasting medical resources, reducing the cost of public health emergency treatment.

[0029] Furthermore, lighting lamps 3 are arranged in a group on each side of the camera 2, and warning light bars 4 are arranged in a group on each side surface of the fuselage main body 1, and the warning light bars 4 will flash red and green lights when in use. Through the arrangement of lighting lamps 3 and warning light bars 4, when in use, lighting lamps 3 are arranged in a group on each side of the camera 2. This layout can provide good auxiliary lighting for the camera 2, which helps the operator to more accurately control the UAV to complete the material delivery and recovery tasks. Warning light bars 4 are arranged in a group on each side surface of the fuselage main body 1 and flash red and green lights, which has a strong warning effect in the marine environment, ensuring that materials can be smoothly delivered and recovered, and no mission interruption or equipment damage will be caused by collision accidents.

[0030] Furthermore, the motor waterproof housing 5, the propulsion motor 6 and the fan blades 7 are arranged at the tail end of the fuselage body 1, so that when the UAV falls into the water accidentally, it can be moved by driving the propulsion motor 6. The rotating column 9 and the propeller 10 are symmetrically arranged in four groups around the central axis of the rotating shaft 8. Through the arrangement of the motor waterproof housing 5, the propulsion motor 6 and the fan blades 7, when in use, the motor waterproof housing 5, the propulsion motor 6 and the fan blades 7 are arranged at the tail end of the fuselage body 1. This design provides the UAV with the ability to move in the water. This underwater propulsion capability can allow the UAV to move toward a predetermined recovery point or a relatively safe area, which is convenient for subsequent salvage and maintenance work, and greatly reduces the risk of equipment loss.

[0031] Furthermore, the waterproof pad 1202 and the waterproof ring 1203 are arranged inside the storage cover 1201. When the storage bucket 1207 rotates inward, it can effectively prevent liquid from penetrating into the interior of the storage bucket 1207. A rotating thread is provided on the outer edge of one side of the storage bucket 1207 connected to the storage cover 1201, which is used for rotational connection with the storage cover 1201. Through the arrangement of the waterproof pad 1202 and the waterproof ring 1203, when in use, it is crucial to protect the quality of medical supplies, ensure that medicines, medical equipment, etc. will not be damaged or fail due to moisture, and ensure the storage safety of medical supplies in the marine environment.

[0032] Furthermore, two groups of springs 1205 are symmetrically arranged on the lower surface of the telescopic shell 1204, and the inner size of the telescopic shell 1204 is consistent with the outer size of the telescopic block 1206. Through the arrangement of the springs 1205, the telescopic shell 1204 and the telescopic block 1206, when in use, this symmetrical design can provide uniform and stable supporting force for the layered fixed baffle 1209, which remains in a suitable position to prevent it from shifting due to the shaking and bumping of the drone during transportation.

[0033] Furthermore, four groups of limiting grooves 1208 are symmetrically arranged about the mid-perpendicular line of the storage barrel 1207, and four groups of telescopic shell 1204, spring 1205 and telescopic block 1206 structures are arranged at the same position at the corresponding limiting grooves 1208. Through the setting of the limiting grooves 1208, when in use, this symmetrical layout provides precise positioning for the installation of the layered fixed baffle 1209, which can ensure that the baffle can be accurately placed at the predetermined position inside the storage barrel 1207, so that the layered fixed baffle 1209 remains stable in the horizontal direction without tilting or offset.

[0034] Furthermore, there are four groups of support columns below the layered fixed baffle 1209, which are installed corresponding to the position of the limit groove 1208, and three groups of layered fixed baffles 1209 are placed in a stacked manner inside the storage barrel 1207. The telescopic shell 1204, the spring 1205 and the telescopic block 1206 play a role in pushing and fixing the top layered fixed baffle 1209. Through the setting of the layered fixed baffle 1209, when in use, the internal space of the storage barrel 1207 can be effectively utilized, and different types of materials can be placed on different levels, which is convenient for the classification management and retrieval of medical materials, and improves the utilization efficiency of the storage space.

[0035] Furthermore, the connecting mechanism 11 includes a connecting column 1101, a load-bearing plate 1102, a cylinder 1103, a push rod 1104 and a connecting ring 1105. The lower part of the fuselage body 1 is fixedly connected with a connecting column 1101, the lower surface of the connecting column 1101 is fixedly connected with the load-bearing plate 1102, the one side surface of the load-bearing plate 1102 is fixedly connected with a cylinder 1103, the one side surface of the cylinder 1103 is slidably connected with a push rod 1104, and the one side surface of the push rod 1104 is movably connected with a connecting ring 1105. The setting of the connecting ring 1105, when in use, the sliding and movable connection between the cylinder 1103, the push rod 1104 and the connecting ring 1105 makes the delivery and recovery operations of the storage mechanism 12 more flexible. When medical supplies need to be delivered, the cylinder 1103 drives the push rod 1104 to move, so that the connecting ring 1105 releases the storage mechanism 12, thereby achieving fast and accurate delivery. During the recovery process, the opposite operation can make the connecting ring 1105 smoothly connected to the storage mechanism 12, and then the storage mechanism 12 is recovered by lifting the fuselage main body 1. This flexible connection and separation mechanism can adapt to different operating scenarios and task requirements.

[0036] Furthermore, two groups of connecting columns 1101 and load-bearing plates 1102 are symmetrically arranged below the fuselage body 1, and two groups of cylinders 1103 are symmetrically arranged on the upper surface of the two groups of load-bearing plates 1102, and two groups of push rods 1104 are arranged at one end of each group of cylinders 1103. Through the arrangement of the connecting columns 1101 and the load-bearing plates 1102, when in use, this symmetrical layout can evenly share the weight of the fuselage body 1, and can effectively prevent problems such as fuselage tilting and connection structure deformation caused by uneven force, thereby improving the stability of the entire system during flight.

[0037] Furthermore, the cylinder 1103 is placed relatively to connect the push rod 1104 to the connecting ring 1105 for fixation. The fuselage body 1, the connecting column 1101 and the load-bearing plate 1102 are made of carbon fiber. Through the arrangement of the fuselage body 1, the connecting column 1101 and the load-bearing plate 1102, when in use, the fuselage body 1, the connecting column 1101 and the load-bearing plate 1102 are made of carbon fiber material. This material has an excellent strength-to-weight ratio and can withstand the air resistance encountered by the fuselage body 1 during high-speed flight, the gravity and inertia force from the storage mechanism 12 borne by the connecting column 1101 and the load-bearing plate 1102, etc., to ensure the stability and safety of the entire structure.

[0038] Working principle: This is an integrated system for the delivery and recovery of marine public health emergency medical supplies. When in use, the rotating shaft 8 above the fuselage body 1 drives the rotating column 9 and the propeller 10 to rotate at high speed, providing lift and flight power for the drone, so that it can fly over the ocean to the offshore operation area of ​​the target sea area. When arriving at the designated location, the cylinder 1103 in the connecting mechanism 11 works to push the push rod 1104 to move, so that the connecting ring 1105 can be connected or separated from the storage mechanism 12 to achieve the delivery or recovery of the storage mechanism 12. For example, when delivering medical supplies, the air cylinder 1103 in the connecting mechanism 11 works to push the push rod 1104 to move, so that the connecting ring 1105 can be connected or separated from the storage mechanism 12 to achieve the delivery or recovery of the storage mechanism 12. The action of cylinder 1103 causes connecting ring 1105 to release storage mechanism 12, and storage barrel 1207 containing medical supplies is dropped down; when recovering, the opposite is true, first connect storage barrel 1207, and then lift it back to the bottom of fuselage body 1. Camera 2 on one side of fuselage body 1 can be used to monitor the flight path and target area in real time. Illuminating light 3 provides lighting in dark environment for better observation and operation. Flashing light of warning light bar 4 serves to warn surrounding ships and personnel to avoid collision. If the UAV accidentally falls into water during flight, the tail of fuselage body 1 The propulsion motor 6 in the waterproof housing 5 of the motor at the end is started, driving the fan blades 7 to rotate, thereby pushing the drone to move in the water, which is convenient for subsequent recovery or continuing to perform tasks. For the storage mechanism 12, the storage bucket 1207 is connected to the storage cover 1201 through a rotating thread to achieve sealing and fixation. Inside the storage bucket 1207, the layered fixed baffle 1209 is installed and positioned through the limiting groove 1208, and under the action of the spring 1205, the telescopic housing 1204 and the telescopic block 1206, the uppermost layered fixed baffle 1209 can be fixed, which can be used for different types or batches of The medical supplies are stored and fixed in layers to prevent confusion or damage caused by shaking during transportation. At the same time, the waterproof pad 1202 and the waterproof ring 1203 can effectively prevent seawater and other liquids from penetrating into the storage barrel 1207, ensuring the storage environment of medical supplies. This arrangement enables the device to cope with the delivery and recovery of medical supplies in marine areas, and the delivery of materials is timely, thereby improving the work efficiency of the offshore operation team. Moreover, it can be effectively recovered without causing waste of medical resources, reducing the cost of public health emergency treatment. The model of the driving motor 6 is YE2-132S-4.

[0039] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An integrated system for the delivery and recovery of marine public health emergency medical supplies, comprising a main body (1), characterized in that: A camera (2) is fixedly connected to one side surface of the fuselage main body (1), a lighting lamp (3) is fixedly connected to one side surface of the fuselage main body (1), a warning light bar (4) is fixedly connected to one side surface of the fuselage main body (1), a motor waterproof housing (5) is fixedly connected to one side surface of the motor waterproof housing (5), a driving motor (6) is fixedly connected to one side surface of the driving motor (6), a fan blade (7) is fixedly connected to one side surface of the driving motor (6), a rotating shaft (8) is fixedly connected to one side surface of the rotating shaft (8), a rotating column (9) is fixedly connected to one side surface of the rotating column (9), a propeller (10) is fixedly connected to one side surface of the rotating column (9), a connecting mechanism (11) is provided on the lower surface of the fuselage main body (1), and a storage mechanism (12) is provided on the lower surface of the connecting mechanism (11); The storage mechanism (12) comprises a storage cover (1201), a waterproof pad (1202), a waterproof ring (1203), a telescopic shell (1204), a spring (1205), a telescopic block (1206), a storage bucket (1207), a limiting groove (1208) and a layered fixed baffle (1209); the lower surface of the connecting mechanism (11) is fixedly connected to the storage cover (1201); the lower surface of the storage cover (1201) is fixedly connected to the waterproof pad (1202); the lower surface of the waterproof pad (1202) is fixedly connected to the waterproof ring (1203); 203), the inner surface of the storage cover (1201) is fixedly connected to a telescopic shell (1204), the inner surface of the telescopic shell (1204) is fixedly connected to a spring (1205), the lower surface of the spring (1205) is fixedly connected to a telescopic block (1206), the lower surface of the storage cover (1201) is slidably connected to a storage bucket (1207), the inner surface of the storage bucket (1207) is provided with a limiting groove (1208), and a side surface of the limiting groove (1208) is slidably connected to a layered fixed baffle (1209).

2. According to claim 1, a marine public health emergency medical material delivery and recovery integrated system is characterized by: The lighting lamps (3) are arranged in a group on each side of the camera (2), and the warning light bars (4) are arranged in a group on each side surface of the fuselage body (1), and the warning light bars (4) flash red and green lights when in use.

3. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: The motor waterproof housing (5), the propulsion motor (6) and the fan blades (7) are arranged at the rear end of the fuselage body (1), so that when the drone falls into the water unexpectedly, it can be moved by driving the propulsion motor (6). The rotating column (9) and the propeller (10) are symmetrically arranged in four groups around the central axis of the rotating shaft (8).

4. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: The waterproof pad (1202) and the waterproof ring (1203) are arranged inside the storage cover (1201), and can effectively prevent liquid from penetrating into the storage bucket (1207) when the storage bucket (1207) rotates inward. The outer edge of one side of the storage bucket (1207) connected to the storage cover (1201) is provided with a rotating thread for rotationally connecting with the storage cover (1201).

5. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: The springs (1205) are symmetrically arranged in two groups on the lower surface of the telescopic shell (1204), and the inner size of the telescopic shell (1204) is consistent with the outer size of the telescopic block (1206).

6. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: The limiting grooves (1208) are symmetrically arranged in four groups with respect to the perpendicular midline of the storage bucket (1207), and the telescopic shell (1204), spring (1205) and telescopic block (1206) structures are arranged in four groups at the same positions of the corresponding limiting grooves (1208).

7. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: There are four groups of support columns below the layered fixed baffle (1209), which are installed corresponding to the positions of the limit grooves (1208), and three groups of layered fixed baffles (1209) are placed in a stacked manner inside the storage bucket (1207). The telescopic shell (1204), the spring (1205) and the telescopic block (1206) play a role in pushing and fixing the top layered fixed baffle (1209).

8. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 1 is characterized by: The connection mechanism (11) comprises a connection column (1101), a load-bearing plate (1102), a cylinder (1103), a push rod (1104) and a connection ring (1105); the lower part of the fuselage main body (1) is fixedly connected to the connection column (1101); the lower surface of the connection column (1101) is fixedly connected to the load-bearing plate (1102); one side surface of the load-bearing plate (1102) is fixedly connected to the cylinder (1103); one side surface of the cylinder (1103) is slidably connected to the push rod (1104); and one side surface of the push rod (1104) is movably connected to the connection ring (1105).

9. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 8, characterized in that: The connecting columns (1101) and the load-bearing plates (1102) are arranged in two groups symmetrically on the left and right below the fuselage body (1), and the cylinders (1103) are arranged in two groups symmetrically on the upper surfaces of the two groups of load-bearing plates (1102), and two groups of push rods (1104) are arranged at one end of each group of cylinders (1103).

10. The integrated system for delivering and recovering marine public health emergency medical supplies according to claim 8, characterized in that: The cylinders (1103) are placed relatively to connect the push rods (1104) and fix the connecting ring (1105). The materials of the fuselage body (1), the connecting column (1101) and the load-bearing plate (1102) are carbon fibers.

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