A window breaking drone

Abstract

The utility model relates to a kind of broken window unmanned aerial vehicle, including fuselage, the first landing gear and the second landing gear of interval arrangement. The first landing gear has first vertical support pole, its upper end is connected with fuselage, lower end is connected with first horizontal support pole, first horizontal support pole middle is equipped with first mounting block and installs first broken window bomb launcher, end portion has first broken window hammer head;The second landing gear has second vertical support pole, upper end is connected with fuselage, lower end is connected with second horizontal support pole, second horizontal support pole middle is equipped with second mounting block and installs second broken window bomb launcher, end portion has second broken window hammer head. First, second horizontal support pole has support leg, and first, second fire water gun is respectively arranged in one end, and fire water pipe is connected between the two and is equipped with water pipe joint. The unmanned aerial vehicle can use broken window bomb to break window initially, also can use broken window hammer head to expand broken window area, reduce broken window bomb consumption, can also extinguish fire immediately after breaking window, realize broken window and continuous operation of fire extinguishing, improve rescue efficiency.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a window-breaking UAV. Background Technology

[0002] Fire safety in high-rise buildings faces severe challenges and has become a major issue that cannot be ignored. When a fire breaks out in a high-rise building, and the situation is critical and personnel cannot safely enter the burning floor to carry out firefighting operations, drones are needed to break windows for firefighting. Currently, most drone window breaking operations use window-breaking grenades, which have problems such as long aiming time and low accuracy. They also require the use of special window-breaking grenades, and it is difficult to find alternatives in emergencies. Furthermore, after using window-breaking grenades, some windows only have small holes, and to expand the broken area, multiple window-breaking grenades need to be fired, resulting in a large consumption of window-breaking grenades and prolonging the rescue time. Utility Model Content

[0003] The purpose of this invention is to provide a window-breaking drone that solves the aforementioned problems of current window-breaking drones.

[0004] To achieve the above objectives, the present invention adopts the following technical solution:

[0005] A window-breaking unmanned aerial vehicle (UAV) includes a fuselage, a first landing gear, and a second landing gear. The first landing gear includes a first vertical support rod and a first horizontal support rod. The upper end of the first vertical support rod is connected to the fuselage, and the lower end of the first horizontal support rod is connected to the lower end of the first vertical support rod. A first window-breaking projectile launcher is mounted on the first horizontal support rod, and a first window-breaking hammer is mounted at the end of the first horizontal support rod. The first horizontal support rod is configured to support the fuselage when it lands, and to drive the first window-breaking hammer to break windows when the fuselage takes off. Operation; the second landing gear and the first landing gear are spaced apart. The second landing gear includes a second vertical support rod and a second horizontal support rod. The upper end of the second vertical support rod is connected to the fuselage, and the second horizontal support rod is connected to the lower end of the second vertical support rod. A second window-breaking missile launcher is provided on the second horizontal support rod, and a second window-breaking hammer is provided at the end of the second horizontal support rod. The second horizontal support rod is configured to support the fuselage when the fuselage is landing, and to drive the second window-breaking hammer to perform window-breaking operations when the fuselage is taking off.

[0006] Furthermore, the first vertical support rod is connected to the middle position of the first horizontal support rod, and the launching end of the first window-breaking bullet launcher is positioned opposite to the working end of the first window-breaking hammer head; the second vertical support rod is connected to the middle position of the second horizontal support rod, and the launching end of the second window-breaking bullet launcher is positioned opposite to the working end of the second window-breaking hammer head.

[0007] Furthermore, a first mounting block is provided on the first transverse support rod, and the first window-breaking bullet launcher is mounted on the first transverse support rod through the first mounting block. A second mounting block is provided on the second transverse support rod, and the second window-breaking bullet launcher is mounted on the second transverse support rod through the second mounting block.

[0008] Furthermore, both the first and second transverse support rods are equipped with feet.

[0009] Furthermore, a first fire hose is provided on the first transverse support rod at the end away from the first window-breaking hammer head, and a second fire hose is provided on the second transverse support rod at the end away from the second window-breaking hammer head.

[0010] Furthermore, a fire hose is connected between the first transverse support rod and the second transverse support rod. One end of the fire hose is connected to the first fire hose nozzle, and the other end is connected to the second fire hose nozzle. A hose connector is provided on the fire hose.

[0011] The beneficial effects of this utility model are:

[0012] This utility model of a window-breaking drone features a first window-breaking hammer at the end of a first transverse support rod and a second window-breaking hammer at the end of a second transverse support rod. Upon takeoff, the drone can drive the hammers to break windows. After initially breaking the window with a window-breaking projectile, the hammers can be used to further expand the broken area, eliminating the need for multiple projectiles and reducing their consumption. This significantly shortens rescue time and effectively improves window-breaking efficiency. In addition to launching window-breaking projectiles, it can also directly use the hammers to break windows. When facing relatively thin windows or situations where high precision is not required, the drone can be directly controlled to take off, allowing the hammers to strike the window and break it, providing more options for window-breaking operations and enhancing flexibility and adaptability. The first and second landing gears cleverly integrate the window-breaking projectile launcher and the hammers while supporting the drone's landing. The first vertical support rod and the second vertical support rod connect the first horizontal support rod and the second horizontal support rod to the fuselage, respectively. The feet on the first horizontal support rod and the second horizontal support rod ensure the stability of the fuselage during landing. This structural design not only meets the requirements for normal take-off and landing of the UAV, but also makes full use of the structural space of the landing gear, and realizes the effective integration of the window-breaking function, enabling the UAV to have a variety of practical functions in a limited space.

[0013] Furthermore, this window-breaking drone is equipped with a first fire hose and a second fire hose on the first and second horizontal support rods, respectively, and connected to each other via a fire hose. The fire hose is also equipped with a hose connector for easy connection to external fire hydrant equipment. After breaking the window, the fire hose can be immediately activated to spray and extinguish the fire, achieving continuous operation of breaking the window and extinguishing the fire, improving rescue efficiency, and providing a more comprehensive solution for high-rise building fire rescue. Attached Figure Description

[0014] Figure 1 This is a structural schematic diagram of the window-breaking drone of this utility model;

[0015] Figure 2 yes Figure 1 A structural diagram from another angle;

[0016] Figure 3 This is a schematic diagram of the structure of the first window-breaking projectile launcher in the window-breaking drone of this utility model.

[0017] The names corresponding to each mark in the diagram:

[0018] 1. Fuselage; 2. First vertical support rod; 3. First horizontal support rod; 4. First mounting block; 5. First window-breaking bullet launcher; 6. First window-breaking hammer; 7. First fire hose nozzle; 8. Support leg; 9. Second vertical support rod; 10. Second horizontal support rod; 11. Second mounting block; 12. Second window-breaking bullet launcher; 13. Second window-breaking hammer; 14. Second fire hose nozzle; 15. Fire hose; 16. Pipe connector. Detailed Implementation

[0019] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention.

[0020] like Figures 1-3 As shown, this window-breaking drone mainly includes the fuselage 1, the first landing gear, and the second landing gear.

[0021] Figure 1 and Figure 2 As shown, the first landing gear consists of a first vertical support rod 2 and a first horizontal support rod 3. The upper end of the first vertical support rod 2 is fixedly connected to the fuselage 1, and the first vertical support rod 2 is connected to the middle position of the first horizontal support rod 3. A first mounting block 4 is provided on the first horizontal support rod 3, and the first window-breaking bullet launcher 5 is mounted on the first horizontal support rod 3 through the first mounting block 4. A first window-breaking hammer head 6 is provided at the end of the first horizontal support rod 3, and the launching end of the first window-breaking bullet launcher 5 is opposite to the working end of the first window-breaking hammer head 6. A first fire hose 7 is provided on the first horizontal support rod 3 at the end away from the first window-breaking hammer head 6, and a support leg 8 is also provided on the first horizontal support rod 3 for stable support during the landing of the fuselage 1.

[0022] The second landing gear is spaced apart from the first landing gear. The second landing gear includes a second vertical support rod 9 and a second lateral support rod 10. The upper end of the second vertical support rod 9 is fixedly connected to the fuselage 1, and the second vertical support rod 9 is connected to the middle position of the second lateral support rod 10. A second mounting block 11 is provided on the second lateral support rod 10, and a second window-breaking bullet launcher 12 is mounted on the second lateral support rod 10 through the second mounting block 11. A second window-breaking hammer head 13 is provided at the end of the second lateral support rod 10, and the launching end of the second window-breaking bullet launcher 12 is positioned opposite to the working end of the second window-breaking hammer head 13. A second fire hose 14 is provided on the second lateral support rod 10 at the end away from the second window-breaking hammer head 13, and a support leg 8 is also provided on the second lateral support rod 10 for stable support during the landing of the fuselage 1.

[0023] A fire water pipe 15 is connected between the first horizontal support rod 3 and the second horizontal support rod 10. One end of the fire water pipe 15 is connected to the first fire nozzle 7, and the other end is connected to the second fire nozzle 14. A pipe joint 16 is provided on the fire water pipe 15 to facilitate connection with other fire water source equipment.

[0024] Working principle:

[0025] When a fire breaks out in a high-rise building and the situation is critical and it is difficult for personnel to safely enter the burning floor to carry out work, a window-breaking drone can be operated to fly to the vicinity of the window of the burning floor.

[0026] When conducting window breaking operations, there are two methods to choose from. One method is to use window-breaking projectiles. By controlling the first window-breaking projectile launcher 5 or the second window-breaking projectile launcher 12 to fire window-breaking projectiles, the window is initially broken. Since the firing end of the first window-breaking projectile launcher 5 is positioned opposite the working end of the first window-breaking hammer 6, and the firing end of the second window-breaking projectile launcher 12 is positioned opposite the working end of the second window-breaking hammer 13, after firing the window-breaking projectiles, if only a small hole appears in the window, the fuselage 1 can be controlled to take off. The fuselage 1 drives the first and second landing gears to move, thereby causing the first window-breaking hammer 6 or the second window-breaking hammer 13 to strike the window. The impact force of the window-breaking hammers is used to expand the broken area. Compared with simply firing multiple window-breaking projectiles, this method reduces the consumption of window-breaking projectiles and shortens the rescue time.

[0027] Another method of breaking windows is to directly control the fuselage 1 to take off, so that the first window-breaking hammer 6 or the second window-breaking hammer 13 can hit the window to break it. This method is suitable for situations where the window glass is relatively thin or where the window-breaking precision requirement is not high.

[0028] After breaking the window, if fire extinguishing is required, the fire hose 15 can be connected to the external fire water source equipment through the hose connector 16, and the first fire hose 7 and the second fire hose 14 can be turned on to spray and extinguish the fire, so as to realize the continuous operation of breaking the window and extinguishing the fire and improve the rescue efficiency.

[0029] Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of this utility model are within the protection scope of this utility model.

Claims

1. A window-breaking drone, characterized in that: The aircraft includes a fuselage, a first landing gear, and a second landing gear. The first landing gear includes a first vertical support rod and a first horizontal support rod. The upper end of the first vertical support rod is connected to the fuselage, and the lower end of the first horizontal support rod is connected to the lower end of the first vertical support rod. A first window-breaking missile launcher is mounted on the first horizontal support rod, and a first window-breaking hammer is mounted at the end of the first horizontal support rod. The first horizontal support rod is configured to support the fuselage during landing and to drive the first window-breaking hammer to perform window-breaking operations during takeoff. The second landing gear and the first landing gear are spaced apart. The second landing gear includes a second vertical support rod and a second lateral support rod. The upper end of the second vertical support rod is connected to the fuselage, and the second lateral support rod is connected to the lower end of the second vertical support rod. A second window-breaking missile launcher is provided on the second lateral support rod, and a second window-breaking hammer is provided at the end of the second lateral support rod. The second lateral support rod is configured to support the fuselage when the fuselage is landing, and to drive the second window-breaking hammer to perform window-breaking operations when the fuselage is taking off.

2. The window-breaking drone according to claim 1, characterized in that: The first vertical support rod is connected to the middle position of the first horizontal support rod, and the firing end of the first window-breaking bullet launcher is opposite to the working end of the first window-breaking hammer head; the second vertical support rod is connected to the middle position of the second horizontal support rod, and the firing end of the second window-breaking bullet launcher is opposite to the working end of the second window-breaking hammer head.

3. The window-breaking drone according to claim 2, characterized in that: A first mounting block is provided on the first transverse support rod, and the first window-breaking bullet launcher is mounted on the first transverse support rod through the first mounting block. A second mounting block is provided on the second transverse support rod, and the second window-breaking bullet launcher is mounted on the second transverse support rod through the second mounting block.

4. The window-breaking drone according to claim 3, characterized in that: Both the first and second transverse support rods are equipped with feet.

5. The window-breaking drone according to claim 4, characterized in that: A first fire hose is installed on the first transverse support rod at the end away from the first window-breaking hammer, and a second fire hose is installed on the second transverse support rod at the end away from the second window-breaking hammer.

6. The window-breaking drone according to claim 5, characterized in that: A fire hose is connected between the first horizontal support rod and the second horizontal support rod. One end of the fire hose is connected to the first fire hose nozzle, and the other end is connected to the second fire hose nozzle. A hose connector is provided on the fire hose.

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