CN216636823U - Rescue unmanned aerial vehicle and rescue system - Google Patents

Abstract

The utility model discloses a rescue drone and a rescue system. The rescue drone comprises a drone main body, a camera device and a storage device. The camera device is fixed on the bottom of the drone main body; the storage device includes a storage component, a throwing component and a storage device. The drive assembly, the storage assembly includes a storage box and a bottom plate that is covered and sealed at the bottom of the storage box, the bottom plate is rotatably connected to the storage box, the storage box is fixed on the bottom of the main body of the drone, and a storage cavity for accommodating the throwing component is formed inside the storage box The delivery assembly includes a telescopic piece and a delivery box for storing rescue materials, and the two ends of the telescopic piece are respectively connected with the storage box and the delivery box; the driving component includes a first driving piece and a second driving piece, the first driving piece and the bottom plate The rotating shaft is connected to drive the bottom plate to rotate, and the second driving part is connected to the telescopic part to drive the expansion and contraction of the telescopic part, which can realize remote rescue on the battlefield, and the rescue drone is fast and flexible, which improves the rescue efficiency.

Description

Rescue drones and rescue systems

technical field

The utility model relates to the technical field of battlefield rescue, in particular to a rescue drone and a rescue system.

Background technique

Unmanned aircraft, referred to as "UAV", is an unmanned aircraft operated by radio remote control equipment and self-provided program control devices. There is no cockpit on the plane, but it is equipped with autopilot, program control devices and other equipment. Personnel on the ground, on the submarine or at the remote control station of the mother machine use radar and other equipment to track, locate, telemetry and digitally transmit it. It can take off like an ordinary plane under radio remote control or launch it with a booster rocket, or it can be brought into the air by the mother plane for flight. When it is recovered, it can be automatically landed in the same way as the ordinary aircraft landing process, or it can be recovered by remote control with a parachute or block.

However, the existing UAV rescue technology is not timely and inefficient.

Utility model content

The main purpose of the utility model is to provide a rescue drone and a rescue system, which aims to solve the technical problem of low rescue efficiency in the existing battlefield.

In order to achieve the above purpose, the utility model provides a rescue drone, comprising:

The main body of the drone;

a camera device, the camera device is fixed on the bottom of the drone body;

A storage device, the storage device includes a storage assembly, a throwing assembly and a drive assembly, the storage assembly includes a storage box and a bottom plate that is covered and sealed at the bottom of the storage box, the bottom plate is rotatably connected to the storage box, so The storage box is fixed on the bottom of the main body of the drone, and a storage cavity for accommodating the delivery component is formed inside the storage box; the delivery component includes a telescopic piece and a delivery box for storing rescue materials, Two ends of the telescopic element are respectively connected with the storage box and the release box; the drive assembly includes a first drive part and a second drive part, the first drive part is connected with the rotating shaft of the bottom plate to drive the The bottom plate rotates, and the second driving element is connected with the telescopic element to drive the telescopic element to extend and retract.

Optionally, the number of the bottom plates is two, and the two bottom plates are respectively rotatably connected to opposite sides of the storage box.

Optionally, the storage box includes a storage body and a reinforcing rib disposed outside the box body.

Optionally, the delivery box includes a delivery main body for storing rescue materials and a connecting piece disposed on the delivery main body and connected with the telescopic piece, the connecting piece comprising a connecting portion connected with the telescopic piece. and a first support portion and a second support portion respectively connected to both ends of the connecting portion and arranged at intervals, and both ends of the first support portion and both ends of the second support portion are connected to the throwing body.

Optionally, the drone body includes a fuselage, a left wing and a right wing arranged on both sides of the fuselage, and a first power assembly connected with the left wing, and the right wing. A wing-connected second power assembly.

Optionally, the first power assembly includes a left longitudinal rod disposed on the left wing and a first left rotor disposed on the left longitudinal rod, and the second power assembly includes a left longitudinal rod disposed on the right The right longitudinal rod on the wing and the first right rotor arranged on the right longitudinal rod, the left longitudinal rod and the right longitudinal rod are respectively parallel to the fuselage.

Optionally, the first power assembly further includes a second left rotor, the first left rotor and the second left rotor are respectively arranged at both ends of the left longitudinal rod, and the second power assembly further includes The second right rotor, the first right rotor and the second right rotor are respectively arranged on both ends of the right longitudinal rod.

Optionally, the drone body further includes a left crossbar and a right crossbar, two ends of the left crossbar are respectively connected with the tail of the fuselage and the left vertical bar, and the right crossbar is Both ends are respectively connected with the tail of the fuselage and the right longitudinal rod.

Optionally, the top of the drone body is provided with a solar panel.

In addition, the present invention also provides a rescue system, which includes a command terminal and the above-mentioned rescue drone, and the command terminal is in communication connection with the rescue drone.

In the technical solution of the present utility model, the rescue drone includes a drone body, a camera device and a storage device. The drone body is fixed at the bottom of the drone body and is used for shooting battlefield rescue video images and transmitting them to the commander. The terminal is for the commander to view. The storage device includes a storage component, a release component and a drive component. The storage component includes a storage box and a bottom plate that is covered and sealed at the bottom of the storage box. The bottom plate is rotatably connected to the storage box, and the storage box is fixed on the UAV. At the bottom of the main body, a storage cavity for accommodating the delivery component is formed inside the storage box. The delivery component includes a retractable part and a delivery box for storing rescue materials. When the rescue drone reaches the top of the rescue site, it hovers in the air, and the first A driving member drives the bottom plate to rotate, opening the bottom of the storage box, and the second driving member drives the telescopic member to extend, so that the release box is lowered to the position of the rescue site, so that the rescuers need to open the release box and obtain the rescue materials, and then the second drive The first driving element drives the bottom plate to rotate and closes the storage box, which can realize remote rescue on the battlefield, and the rescue drone is fast and flexible, which improves the rescue efficiency.

Description of drawings

In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description These are just some embodiments of the present invention, and for those of ordinary skill in the art, other drawings can also be obtained based on the structures shown in these drawings without any creative effort.

1 is a schematic structural diagram of a rescue drone according to an embodiment of the present invention;

FIG. 2 is a schematic structural diagram of another angle of the rescue drone shown in FIG. 1;

Fig. 3 is a partial structural schematic diagram of the rescue drone shown in Fig. 1;

FIG. 4 is a schematic structural diagram of another part of the rescue drone shown in FIG. 1 .

The realization, functional characteristics and advantages of the purpose of the present utility model will be further described with reference to the accompanying drawings in conjunction with the embodiments.

Detailed ways

The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, not all of them. Example. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work fall within the protection scope of the present invention.

It should be noted that all directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the difference between the various components under a certain posture (as shown in the accompanying drawings). If the specific posture changes, the directional indication also changes accordingly.

In addition, the descriptions involving "first", "second", etc. in the present invention are only for description purposes, and should not be understood as indicating or implying their relative importance or implicitly indicating the number of indicated technical features. Thus, a feature delimited with "first", "second" may expressly or implicitly include at least one of that feature. In addition, the technical solutions between the various embodiments can be combined with each other, but must be based on the realization by those of ordinary skill in the art. When the combination of technical solutions is contradictory or cannot be realized, it should be considered that the combination of such technical solutions does not exist. , is not within the scope of protection required by the present utility model.

As shown in FIG. 1 and FIG. 3 , the present invention proposes a rescue drone, including a drone body 100, a camera device 200 and a storage device 300; the camera device 200 is fixed on the bottom of the drone body 100; the storage device 300 includes a storage assembly 310, a throwing assembly 320 and a driving assembly (not shown in the figure). The storage assembly 310 includes a storage box 311 and a bottom plate 312 that is covered and sealed at the bottom of the storage box 311. The bottom plate 312 is rotatably connected to the storage box 311 for storing The box 311 is fixed on the bottom of the drone body 100, and a storage cavity 313 is formed inside the storage box 311 to accommodate the delivery assembly 320; The two ends are respectively connected with the storage box 311 and the release box 323; the driving assembly includes a first driving member and a second driving member, the first driving member is connected with the rotating shaft of the bottom plate 312 to drive the bottom plate 312 to rotate, and the second driving member is connected with the telescopic member 321 is connected to drive the telescopic element 321 to expand and contract.

The rescue drone is connected to the command terminal through the communication module, and the video images captured by the camera device 200 can be transmitted to the command terminal through the communication module for the commander to view. The camera device 200 may include a set on the command terminal to remotely control the rescue drone The flight, hovering, and the start and stop of the first driving part and the second driving part, the first driving part and the second driving part can be motors, air cylinders or hydraulic cylinders, when the rescue drone arrives over the rescue site, Hovering in the air, the first driving member drives the rotation shaft of the bottom plate 312 to rotate, the bottom of the storage box 311 is opened, and the second driving member drives the telescopic member 321 to extend until the release box 323 reaches the rescue location, and the individual soldier can be opened and released. The box 323 takes the rescue materials, and then the second driving member drives the retractable member 321 to shorten until the delivery box 323 is located in the storage cavity 313 of the storage box 311, and the first driving member drives the bottom plate 312 to rotate, closing the bottom of the storage box 311. The rescue drone of the utility model can realize remote rescue, reduce the difficulty of rescue, and improve the rescue efficiency.

Specifically, the number of the bottom plates 312 is two, and the two bottom plates 312 are rotatably connected to opposite sides of the storage box 311 respectively. They are arranged in a one-to-one correspondence to respectively drive the rotation shafts of the two base plates 312 to rotate. When the rescue drone arrives above the rescue site, the two bottom plates 312 are rotated in opposite directions away from each other to open the bottom of the storage box 311. When the rescue is completed, the two bottom plates 312 are rotated toward each other to close Bottom of storage box 311. In another embodiment, the number of the bottom plate 312 may also be one, one side of the bottom plate 312 is hinged with the storage box 311 , and the entire bottom plate 312 is covered with the bottom of the storage box 311 .

More specifically, as shown in FIG. 3 , the storage box 311 includes a storage body 314 and a reinforcing rib 315 disposed outside the box body. The number of the reinforcing ribs 315 can be two, and the two reinforcing ribs 315 are respectively located on the main body 100 of the drone. On both sides of the fuselage 110, the reinforcing ribs 315 include a first vertical rib, a transverse rib and a second vertical rib which are connected in sequence. On the side, transverse ribs are provided on the top of the storage box 311 . Of course, in other embodiments, the reinforcing ribs 315 can also be arranged around the circumference of the storage box 311, and the number can also be set according to specific requirements, and the shape and number thereof are not specifically limited herein.

As shown in FIG. 3 and FIG. 4 , the delivery box 323 includes a delivery body 324 for storing relief materials, and a connector 325 disposed on the delivery body 324 and connected to the retractable member 321 . The connector 325 includes a connector connected to the retractable member 321 . The connecting portion 326 and the first supporting portion 327 and the second supporting portion 328 are respectively connected to both ends of the connecting portion 326 and are arranged at intervals. 324 is connected, the middle parts of the first support part 327 and the second support part 328 are both arched in the direction away from the throwing body 324, the two ends of the connection part 326 are respectively connected with the middle part of the first support part 327 and the second support part 328 The above structure makes the structure of the drop box 323 more stable, and can smoothly move up and down with the telescopic member 321 .

Please refer to FIG. 2 , the drone body 100 includes a fuselage 110 , a left wing 120 and a right wing 130 disposed on both sides of the fuselage 110 , a first power assembly 140 connected to the left wing 120 , and a right wing 140 . The second power assembly 150, the first power assembly 140 and the second power assembly 150 connected to the wing 130 can realize the vertical take-off, landing and hovering of the rescue drone. The first power assembly 140 includes a left longitudinal rod 141 disposed on the left wing 120 and a first left rotor 142 disposed on the left longitudinal rod 141 , and the second power assembly 150 includes a right longitudinal rod disposed on the right wing 130 151 and the first right rotor 152 arranged on the right longitudinal rod 151, the left longitudinal rod 141 and the right longitudinal rod 151 are respectively parallel to the fuselage 110, which can not only enhance the stability of the rescue drone, but also reduce the flight resistance. The rotating shaft of the first left rotor 142 and the rotating shaft of the first right rotor 152 are both streamlined to reduce flight resistance and power loss. The first left rotor 142 and the first right rotor 152 are both propeller structures, and the rotor of the propeller structure has a simple structure, Powerful advantage.

In one embodiment, the first power assembly 140 further includes a second left rotor 143, the first left rotor 142 and the second left rotor 143 are respectively disposed on both ends of the left longitudinal rod 141, and the second power assembly 150 further includes a second left rotor 143. The right rotor 153 , the first right rotor 152 and the second right rotor 153 are respectively arranged at both ends of the right longitudinal rod 151 , which further increases the power of the rescue drone. Similarly, the second left rotor 143 and the second right rotor 153 are also propeller structures. Among them, the first left rotor 142 and the first right rotor 152 are arranged near the head of the fuselage 110, and the second left rotor 143 and the second right rotor 153 are arranged near the tail of the fuselage 110, which improves the balance stability of the drone . The drone body 100 further includes a left crossbar and a right crossbar. The two ends of the left crossbar are respectively connected with the tail of the fuselage 110 and the left vertical rod 141, and the two ends of the right crossbar are respectively connected with the tail and the right crossbar of the fuselage 110. The longitudinal rods 151 are connected to further strengthen the stability of the drone body 100 .

Optionally, as shown in FIG. 2 , a solar panel 160 is arranged on the top of the drone body 100 , a battery is arranged inside the drone body 100 , and the output end of the solar panel is connected with the charging circuit inside the drone body 100 . Battery connection. In another embodiment, the drone body 100 is composed of photoelectric conversion materials, which can collect energy anytime and anywhere, and transmit the electric energy obtained by photoelectric conversion to the battery for storage through the charging circuit.

In addition, the present invention also provides a rescue system, which includes a command terminal and the above-mentioned rescue drone, and the command terminal is in communication connection with the rescue drone. Since the rescue system adopts all the technical solutions of the above-mentioned embodiments, it has at least all the beneficial effects brought by the technical solutions of the above-mentioned embodiments, which will not be repeated here.

The above are only the preferred embodiments of the present utility model, and are not intended to limit the scope of the present utility model's patent. Any equivalent structure transformation made by using the contents of the present invention's description and accompanying drawings under the concept of the present utility model, or directly / Indirect applications in other related technical fields are included in the scope of patent protection of the present utility model.

Claims (10)

1. a rescue drone, is characterized in that, comprises: The main body of the drone; a camera device, the camera device is fixed on the bottom of the drone body; A storage device, the storage device includes a storage assembly, a throwing assembly and a drive assembly, the storage assembly includes a storage box and a bottom plate that is covered and sealed at the bottom of the storage box, the bottom plate is rotatably connected to the storage box, so The storage box is fixed on the bottom of the main body of the drone, and a storage cavity for accommodating the delivery component is formed inside the storage box; the delivery component includes a telescopic piece and a delivery box for storing rescue materials, Two ends of the telescopic element are respectively connected with the storage box and the release box; the drive assembly includes a first drive part and a second drive part, the first drive part is connected with the rotating shaft of the bottom plate to drive the The bottom plate rotates, and the second driving element is connected with the telescopic element to drive the telescopic element to extend and retract. 2 . The rescue drone according to claim 1 , wherein the number of the bottom plates is two, and the two bottom plates are respectively rotatably connected to opposite sides of the storage box. 3 . 3 . The rescue drone of claim 1 , wherein the storage box comprises a storage body and a reinforcing rib disposed outside the box body. 4 . 4 . The rescue drone according to claim 1 , wherein the delivery box comprises a delivery body for storing rescue materials and a connecting piece arranged on the delivery body and connected to the telescopic piece, 4 . The connecting piece includes a connecting portion connected to the telescopic piece, and a first supporting portion and a second supporting portion that are respectively connected to both ends of the connecting portion and are spaced apart. Both ends of the two support parts are connected with the throwing body. 5. The rescue drone of claim 1, wherein the drone body comprises a fuselage, left and right wings disposed on both sides of the fuselage, and a A first power assembly connected to the wing, and a second power assembly connected to the right wing. 6 . The rescue drone of claim 5 , wherein the first power assembly comprises a left longitudinal rod disposed on the left wing and a first left-handed rotation rod disposed on the left longitudinal rod. 7 . wing, the second power assembly includes a right longitudinal rod disposed on the right wing and a first right rotor disposed on the right longitudinal rod, the left longitudinal rod and the right longitudinal rod are respectively connected with the aircraft body parallel. 7 . The rescue drone according to claim 6 , wherein the first power assembly further comprises a second left rotor, and the first left rotor and the second left rotor are respectively arranged on the left At both ends of the vertical rod, the second power assembly further includes a second right rotor, and the first right rotor and the second right rotor are respectively arranged at both ends of the right vertical rod. 8 . The rescue drone according to claim 6 , wherein the main body of the drone further comprises a left crossbar and a right crossbar, and two ends of the left crossbar are respectively connected to the tail of the fuselage. 9 . is connected with the left longitudinal rod, and the two ends of the right transverse rod are respectively connected with the tail of the fuselage and the right longitudinal rod. 9 . The rescue drone according to claim 1 , wherein a solar panel is provided on the top of the main body of the drone. 10 . 10. A rescue system, comprising a command terminal and the rescue drone according to any one of claims 1 to 9, wherein the command terminal is in communication connection with the rescue drone.

Images