Unmanned aerial vehicle carrier loader for low-altitude emergency fire fighting

Abstract

The utility model relates to an unmanned aerial vehicle carrier loader for low-altitude emergency fire fighting, belongs to the technical field of fire extinguishing, and solves the technical problems that a water hose needs to be connected to an unmanned aerial vehicle on site in the prior art, time is consumed, and the fire extinguishing opportunity is delayed. The unmanned aerial vehicle comprises an unmanned aerial vehicle storage cabin, a water tank and a water hose assembly. The unmanned aerial vehicle storage cabin comprises a cabin body and a parking apron, and an unmanned aerial vehicle is parked on the parking apron; the water hose assembly comprises a water hose, one end of the water hose is connected to the unmanned aerial vehicle, and the other end of the water hose is connected to the water tank; when the parking apron does not ascend, the parking apron locks the water hose; after the parking apron ascends, the locking state of the water hose is released, and the water hose can be unfolded along with flying of the unmanned aerial vehicle. The water hose is connected with the unmanned aerial vehicle and the water tank, when the unmanned aerial vehicle flies out of the unmanned aerial vehicle carrier loader, the water hose is unfolded, the unmanned aerial vehicle directly enters a fire scene for fire rescue, the water hose connecting time is saved, and the fire behavior is controlled in time.

Description

A drone transport vehicle for low-altitude emergency firefighting Technical Field

[0001] This utility model relates to the field of fire extinguishing technology, and in particular to a drone transport vehicle for low-altitude emergency fire fighting. Background Technology

[0002] With the development of unmanned technology in modern urban construction, drone-based firefighting systems are being applied to high-altitude fire rescue.

[0003] In existing technologies, the fire hose and the drone are not connected. Before extinguishing a fire, the fire hose needs to be manually unlocked, deployed, and then connected to the water tank and the drone. In a fire scene where every second counts, this connection process takes a lot of time, delaying the opportunity to extinguish the fire.

[0004] Therefore, how to provide a drone transport vehicle for low-altitude emergency firefighting that can transport drones to the fire scene without requiring manual deployment and connection of fire hoses, and can directly deploy fire hoses as the drones fly out of the drone transport vehicle to quickly extinguish the fire, is a technical problem that urgently needs to be solved by those skilled in the art. Summary of the Invention

[0005] Based on the above analysis, the present invention aims to provide a drone transport vehicle for low-altitude emergency firefighting, in order to solve the technical problem that existing drones need to be connected to water hoses on-site, which delays the timing of firefighting.

[0006] The objective of this utility model is mainly achieved through the following technical solutions:

[0007] A drone transport vehicle for low-altitude emergency firefighting includes a drone storage compartment, a water tank, and a water hose assembly.

[0008] The drone storage compartment includes a compartment body and a landing pad, the landing pad being located inside the compartment body, and the drone being parked on the landing pad;

[0009] The water hose assembly includes a water hose, one end of which is connected to the drone, and the other end of which is connected to the water tank;

[0010] When the helipad is not raised, the water hose is locked in place; after the helipad is raised, the water hose is released from its locked state and can be deployed as the drone flies.

[0011] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the landing pad includes a brake pin, which is disposed on the lower end face of the landing pad.

[0012] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the water hose assembly includes a rotating shaft, and the water hose is wound around the rotating shaft; a groove is provided on the rotating shaft, and the groove is disposed opposite to the brake pin;

[0013] When the helipad is not raised, the brake pin is inserted into the groove, and the water hose is in a locked state; after the helipad is raised, the brake pin is pulled out from the groove, and the water hose is released from its unlocked state.

[0014] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the cabin includes a door, the door includes a hinged end and a free end, and the hinged end is hinged to the upper surface of the cabin.

[0015] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the drone storage compartment also includes a telescopic boom, which is vertically installed on the helipad.

[0016] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the telescopic rod is positioned opposite to the free end.

[0017] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the upper end of the telescopic rod is located on the lower end face of the hatch, and the lower end of the telescopic rod is located on the landing pad.

[0018] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the telescopic rod includes an inner cylinder and an outer cylinder, the outer cylinder includes a hollow cavity with one end open, and the inner cylinder is telescopically disposed in the hollow cavity.

[0019] Furthermore, in the aforementioned drone transport vehicle for low-altitude emergency firefighting, the drone storage compartment also includes a drive unit, and the landing pad is located at the output end of the drive unit, which is used to drive the landing pad to rise and fall.

[0020] Furthermore, the drone transport vehicle for low-altitude emergency firefighting also includes a high-pressure water pump, the two ends of which are connected to the water tank and the water hose.

[0021] Compared with the prior art, the present invention can achieve at least one of the following beneficial effects:

[0022] (1) The UAV transport vehicle for low-altitude emergency fire fighting of this utility model includes a UAV storage compartment, a water tank and a water hose assembly; the water hose assembly includes a water hose, with the water tank and the UAV connected at both ends; when the landing pad is not raised, the landing pad locks the water hose, and the water hose is in a locked state; when UAV rescue is needed, after the landing pad is raised, the locked state of the water hose is released, and the water hose can be deployed as the UAV flies. When the UAV transport vehicle arrives at the fire scene, the UAV can directly enter the fire scene to carry out fire rescue, saving water hose connection time, thereby controlling the fire more promptly, saving lives and reducing property losses.

[0023] (2) In the drone transport vehicle for low-altitude emergency firefighting of this utility model, during the ascent of the landing pad, the telescopic rod on the landing pad pushes the free end of the hatch to open the hatch. During the ascent of the landing pad, the hatch can be opened and the locking state of the fire hose can be released, allowing the drone to quickly fly out of the cabin, deploy the fire hose, draw water from the water tank, quickly control the fire, and improve the fire extinguishing efficiency.

[0024] In this invention, the above-described technical solutions can be combined with each other to achieve more preferred combinations. Other features and advantages of this invention will be set forth in the following description, and some advantages will become apparent from the description or be learned by practicing this invention. The objectives and other advantages of this invention can be realized and obtained from the details specifically pointed out in the text and accompanying drawings. Attached Figure Description

[0025] The accompanying drawings are for illustrative purposes only and are not intended to limit the scope of the invention. Throughout the drawings, the same reference numerals denote the same parts.

[0026] Figure 1 is one of the structural schematic diagrams of the UAV transport vehicle for low-altitude emergency firefighting described in Example 1;

[0027] Figure 2 is a structural schematic diagram of the drone transport vehicle for low-altitude emergency firefighting described in Example 2 with the hatch closed.

[0028] Figure 3 is a structural schematic diagram of the unmanned aerial vehicle (UAV) transport vehicle for low-altitude emergency firefighting described in Example 2 with the hatch open.

[0029] Figure 4 is a schematic diagram of the telescopic rod described in Example 2.

[0030] Figure label:

[0031] 1-Unmanned Aerial Vehicle (UAV) Transport Vehicle;

[0032] 2-UAV storage compartment, 21-Compartment, 211-Compartment door, 22-Landing pad, 221-Brake pin; 23-Telescopic rod, 231-Inner cylinder, 232-Outer cylinder;

[0033] 3-Water tank;

[0034] 4-Water hose assembly, 41-Water hose, 42-Shaft, 421-Groove, 43-Windlass, 44-Windlass support frame;

[0035] 5-Drive unit;

[0036] 6-High-pressure water pump. Detailed Implementation

[0037] The preferred embodiments of the present invention will now be described in detail with reference to the accompanying drawings, which constitute a part of the present invention and are used together with the embodiments of the present invention to illustrate the principles of the present invention, but are not intended to limit the scope of the present invention.

[0038] Example 1

[0039] This embodiment provides a drone transport vehicle for low-altitude emergency firefighting, as shown in Figure 1, including a drone storage compartment 2, a water tank 3, and a water hose assembly 4;

[0040] The drone storage compartment 2 is used to store drones; the drone storage compartment 2 includes a compartment body 21 and a landing pad 22, the landing pad 22 is set inside the compartment body 21, and the drone is parked on the landing pad 22;

[0041] Water hose assembly 4 includes water hose 41, one end of which is connected to the drone and the other end of which is connected to the water tank 3;

[0042] When the helipad 22 is not raised, the water hose 41 is locked in place. After the helipad 22 is raised, the water hose 41 is released from its locked state and can be deployed as the drone flies.

[0043] This utility model discloses a drone transport vehicle for low-altitude emergency firefighting. When the drone transport vehicle 1 transports the drone to the fire scene, the landing pad 22 where the drone is parked rises, releasing the locking state of the landing pad 22 to the water hose 41. When the drone takes off from the landing pad 22 to carry out fire rescue, the water hose 41 unfolds under the pull of the drone, saving the connection time of the water hose 41, thereby controlling the fire more promptly, saving lives and reducing property damage.

[0044] Furthermore, the helipad 22 includes a brake pin 221, which is disposed on the lower end face of the helipad 22 and is disposed opposite to the water hose assembly 4.

[0045] The water hose assembly 4 includes a rotating shaft 42, a winch 43, and a winch support frame 44. The winch 43 is mounted on the winch support frame 44, and the rotating shaft 42 is rotatably mounted on the winch 43. The water hose 41 is wound around the rotating shaft 42, and a groove 421 is provided on the rotating shaft 42. The groove 421 is positioned opposite to the brake pin 221. When the helipad 22 is not raised, the brake pin 221 is inserted into the groove 421, and the water hose 41 is in a locked state. After the helipad 22 is raised, the brake pin 221 is pulled out from the groove 421, and the water hose 41 is released from its unlocked state.

[0046] Furthermore, the water hose assembly 4 also includes a drive motor (not shown in the figure), with the rotating shaft 42 mounted on the drive motor. When the drone completes the fire rescue work, during the process of the drone being recovered to the landing pad 22, the drive motor controls the rotating shaft 42 to rotate in the opposite direction to recover the water hose 41. The recovery speed of the water hose 41 by the drive motor is matched with the descent speed of the drone.

[0047] Furthermore, in order to ensure sufficient water supply during drone firefighting, this embodiment also includes a high-pressure water pump 6, with the two ends of the high-pressure water pump 6 connected to a water tank 3 and a water hose 41.

[0048] Example 2

[0049] The drone transport vehicle for low-altitude emergency firefighting shown in this embodiment is illustrated in Figures 2 and 3. Based on embodiment 1, the upper surface of the cabin 21 on which the drone is placed is provided with a door 211. The door 211 includes a hinged end and a free end, with the hinged end hinged to the upper surface of the cabin 21.

[0050] In order to enable the automatic opening of the hatch 211, this embodiment also includes a telescopic rod 23, which is vertically installed on the apron 22 and is positioned opposite to the free end.

[0051] In this embodiment, the drone transport vehicle for low-altitude emergency firefighting transports the drone to the fire scene. The landing pad 22 rises under the push of the drive device 5. As the landing pad 22 rises, the telescopic boom 23 pushes the free end of the hatch 211, opening it. Simultaneously, after the landing pad 22 rises, the locking state of the water hose 41 is released, and the drone flies out of the drone storage compartment 2 with the hatch 211 open, deploying the water hose 41.

[0052] During the ascent of the helipad 22, the telescopic boom 23 pushes the free end of the hatch 211, opening the hatch 211 and releasing the helipad 22 from the locking state of the water hose 41. This saves time in opening the hatch 211 and connecting the water hose 41, allowing direct access to the fire scene for fire rescue, thereby controlling the fire more promptly, saving lives and reducing property damage.

[0053] The upper end of the telescopic boom 23 is located on the lower end face of the hatch 211, and the lower end of the telescopic boom 23 is located on the apron 22. As shown in Figure 4, the telescopic boom 23 includes an inner cylinder 231 and an outer cylinder 232. The outer cylinder 232 includes a hollow cavity with one end open, and the inner cylinder 231 is telescopically disposed in the hollow cavity. A sliding groove is provided on the inner wall of the hollow cavity, and a slider matching the sliding groove is provided on the outer wall of the inner cylinder 231, allowing the inner cylinder 231 to slide up and down within the sliding groove of the hollow cavity of the outer cylinder 232.

[0054] The upper end of the inner cylinder 231 is hinged to the free end of the hatch 211, and the lower end of the outer cylinder 232 is hinged to the apron 22. After the telescopic rod 23 pushes the hatch 211 to open, the inner cylinder 231 extends out of the outer cylinder 232 as the hatch 211 opens, so that the hatch 211 can be opened smoothly.

[0055] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in the present utility model should be included within the protection scope of the present utility model.

Claims

1. A drone transport vehicle for low-altitude emergency firefighting, characterized in that, The system includes a drone storage compartment (2), a water tank (3), and a water hose assembly (4). The drone storage compartment (2) is used to store drones. The drone storage compartment (2) includes a cabin body (21) and a landing pad (22). The landing pad (22) is located inside the cabin body (21), and the drone is parked on the landing pad (22). The water hose assembly (4) includes a water hose (41). One end of the water hose (41) is connected to the drone, and the other end of the water hose (41) is connected to the water tank (3). When the landing pad (22) is not raised, the landing pad (22) locks the water hose (41). After the landing pad (22) is raised, the locking state of the water hose (41) is released, and the water hose (41) can be deployed as the drone flies.

2. The UAV transport vehicle for low-altitude emergency firefighting according to claim 1, characterized in that, The helipad (22) includes a brake pin (221), which is disposed on the lower end face of the helipad (22).

3. The UAV transport vehicle for low-altitude emergency firefighting according to claim 2, characterized in that, The water hose assembly (4) also includes a rotating shaft (42), and the water hose (41) is wound around the rotating shaft (42). The rotating shaft (42) has a groove (421) which is opposite to the brake pin (221). When the helipad (22) is not raised, the brake pin (221) is inserted into the groove (421) and the water hose (41) is in a locked state. After the helipad (22) is raised, the brake pin (221) is pulled out from the groove (421) and the unlocked state of the water hose (41) is released.

4. The UAV transport vehicle for low-altitude emergency firefighting according to claim 3, characterized in that, The cabin (21) includes a hatch (211), which has a hinged end and a free end, the hinged end being hinged to the upper surface of the cabin (21).

5. The UAV transport vehicle for low-altitude emergency firefighting according to claim 4, characterized in that, The drone storage compartment (2) also includes a telescopic pole (23), which is vertically installed on the landing pad (22).

6. The UAV transport vehicle for low-altitude emergency firefighting according to claim 5, characterized in that, The telescopic rod (23) is positioned opposite to the free end. When the landing pad (22) rises, the telescopic rod (23) pushes the free end of the hatch (211) to open the hatch (211).

7. The UAV transport vehicle for low-altitude emergency firefighting according to claim 6, characterized in that, The upper end of the telescopic rod (23) is located on the lower end face of the cabin door (211), and the lower end of the telescopic rod (23) is located on the apron (22).

8. The UAV transport vehicle for low-altitude emergency firefighting according to claim 6, characterized in that, The telescopic rod (23) includes an inner cylinder (231) and an outer cylinder (232). The outer cylinder (232) includes a hollow cavity with one end open. The inner cylinder (231) is telescopically disposed in the hollow cavity.

9. The unmanned aerial vehicle (UAV) transport vehicle for low-altitude emergency firefighting according to claim 8, characterized in that, The drone storage compartment (2) also includes a drive unit (5), and the landing pad (22) is located at the output end of the drive unit (5). The drive unit (5) is used to drive the landing pad (22) to rise and fall.

10. The UAV transport vehicle for low-altitude emergency firefighting according to claim 9, characterized in that, It also includes a high-pressure water pump (6), the two ends of which are connected to the water tank (3) and the water hose (41).

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