CN214824096U

CN214824096U - Fireproof unmanned aerial vehicle

Info

Publication number: CN214824096U
Application number: CN202121276699.6U
Authority: CN
Inventors: 王恪淳
Original assignee: Harbin Dongfang Huarui Technology Development Co ltd
Current assignee: Harbin Dongfang Huarui Technology Development Co ltd
Priority date: 2021-06-08
Filing date: 2021-06-08
Publication date: 2021-11-23
Anticipated expiration: 2031-06-08

Abstract

The utility model discloses a fire prevention unmanned aerial vehicle, including the equipment principal, one side of equipment principal is provided with the horn, one side top of horn is provided with the screw, the positive top of equipment principal is provided with the camera, the bottom of equipment principal is provided with the fuselage and stores the storehouse, one side that the storehouse was stored to the fuselage is provided with flexible spray lance, the bottom that the storehouse was stored to the fuselage is provided with the transmission case, the bottom of transmission case is provided with the couple, one side bottom that the storehouse was stored to the fuselage is provided with the support, the inside of transmission case is provided with connects the storehouse, one side of connecting the storehouse is provided with the motor, the bottom of connecting the storehouse is provided with the rope, the front of equipment principal is provided with sealing door, the opposite side that the storehouse was stored to the fuselage is provided with sealed feed inlet, the inside of equipment principal is provided with porous basalt fiber felt.

Description

Fireproof unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a fire prevention unmanned aerial vehicle.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Compared with piloted planes, unmanned planes are often more suitable for tasks too easy, dirty or dangerous, and can be divided into military and civil aspects according to application fields, wherein the unmanned planes are divided into reconnaissance planes and target planes, and the civil aspect is that the unmanned planes plus the industry are really just needed; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

The prior art has the following defects or problems:

1. in the prior art, when the unmanned aerial vehicle conveys materials and approaches a dangerous area, safe long-line transportation at a distance cannot be maintained, and meanwhile, the unmanned aerial vehicle is inconvenient to maintain inside;

2. unmanned aerial vehicle among the prior art is when the fire rescue, and the easy high temperature of flame burns to damage inside electronic component.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to prior art's weak point, provide a fire prevention unmanned aerial vehicle to solve the problem that provides in the background art.

In order to achieve the above object, the utility model provides a following technical scheme: including the equipment main part, one side of equipment main part is provided with the horn, one side top of horn is provided with the screw, the positive top of equipment main part is provided with the camera, the bottom of equipment main part is provided with the fuselage and stores the storehouse, one side that the storehouse was stored to the fuselage is provided with flexible spray lance, the bottom that the storehouse was stored to the fuselage is provided with the transmission case, the bottom of transmission case is provided with the couple, one side bottom that the storehouse was stored to the fuselage is provided with the support, the inside of transmission case is provided with connects the storehouse, one side of connecting the storehouse is provided with the motor, the bottom of connecting the storehouse is provided with the rope, the front of equipment main part is provided with sealing door, the opposite side that the storehouse was stored to the fuselage is provided with sealed feed inlet, the inside of equipment main part is provided with porous basalt fiber felt.

Optionally, the horn is fixedly connected with the equipment main body, the screw propeller is fixedly connected with the horn, and the horn and the screw propeller are respectively provided with six groups.

Optionally, camera and equipment main part fixed connection, storehouse and equipment main part fixed connection are stored to the fuselage, storehouse fixed connection is stored with the fuselage to flexible spray lance.

Optionally, storehouse fixed connection is stored with the fuselage to the transmission case, couple and transmission case swing joint, storehouse fixed connection is stored with the fuselage to the support, the support is provided with two sets ofly.

Optionally, the connection bin is fixedly connected with the transmission case, the motor is fixedly connected with the connection bin, and the rope is fixedly connected with the connection bin.

Optionally, the sealing door is movably connected with the equipment main body, the sealing feed inlet is fixedly connected with the machine body storage bin, and the porous basalt fiber felt is fixedly connected with the equipment main body.

Optionally, a carbon fiber layer is arranged inside the porous basalt fiber felt, a rubber layer is arranged inside the carbon fiber layer, a heat insulation layer is arranged inside the rubber layer, the carbon fiber layer is fixedly connected with the porous basalt fiber felt, the rubber layer is fixedly connected with the carbon fiber layer, and the heat insulation layer is fixedly connected with the rubber layer.

Compared with the prior art, the utility model provides a fire prevention unmanned aerial vehicle possesses following beneficial effect:

1. the utility model discloses a flexible spray lance and sealed feed inlet that set up can be convenient for unmanned aerial vehicle long-range action of putting out a fire when carrying out fire rescue so that the unmanned aerial vehicle that can not be closely be close to the scene of fire, can be convenient for unmanned aerial vehicle accurately to put in goods and materials and give stranded personnel in the fire control conflagration through motor and the rope that sets up;

2. the utility model discloses a porous basalt fiber felt and the fibrous layer that sets up can be so that unmanned aerial vehicle's body is not ignited by flame when being close to flame to avoided the effect of equipment principal burning loss, can be when the whereabouts at the equipment principal through the rubber layer that sets up, guaranteed that the equipment principal can not receive the damage, the inside electronic components of equipment principal that can make through the temperature-insulating heat preservation that sets up is not melted by high temperature.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the internal structure of the present invention;

FIG. 3 is a schematic structural view of the sealing door of the present invention;

fig. 4 is the structural schematic diagram of the porous basalt fiber felt of the present invention.

In the figure: 1. an apparatus main body; 2. a horn; 3. a propeller; 4. a camera; 5. a machine body storage bin; 6. A telescopic spray rod; 7. a transmission case; 8. hooking; 9. a support; 10. a connecting bin; 11. a motor; 12. a rope; 13. a sealing door; 14. sealing the feed inlet; 15. porous basalt fiber felt; 16. a carbon fiber layer; 17. a rubber layer; 18. a heat insulation layer.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.

In the description of the present invention, it should be further noted that, unless explicitly stated or limited otherwise, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected, mechanically connected, electrically connected, directly connected, connected through an intermediate medium, or connected to the inside of two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

Referring to fig. 1-4, in this embodiment: the utility model provides a fire prevention unmanned aerial vehicle, including equipment main part 1, one side of equipment main part 1 is provided with horn 2, one side top of horn 2 is provided with screw 3, the positive top of equipment main part 1 is provided with camera 4, the bottom of equipment main part 1 is provided with the fuselage and stores storehouse 5, one side that the storehouse 5 was stored to the fuselage is provided with flexible spray lance 6, the bottom that storehouse 5 was stored to the fuselage is provided with transmission case 7, the bottom of transmission case 7 is provided with couple 8, one side bottom that storehouse 5 was stored to the fuselage is provided with support 9, the inside of transmission case 7 is provided with connects storehouse 10, one side of connecting storehouse 10 is provided with motor 11, the model is Y132S1, the bottom of connecting storehouse 10 is provided with rope 12, the front of equipment main part 1 is provided with sealing door 13, the opposite side that storehouse 5 was stored to the fuselage is provided with sealed feed inlet 14, the inside of equipment main part 1 is provided with porous basalt fiber felt 15.

Further, the machine arm 2 is fixedly connected with the equipment main body 1, the propeller 3 is fixedly connected with the machine arm 2, six groups of the machine arm 2 and six groups of the propeller 3 are respectively arranged, the machine arm 2 is used for connecting the equipment main body 1, and the propeller 3 is used for rotating so as to drive the equipment main body 1 to rise.

Further, camera 4 and 1 fixed connection of equipment main part,

storehouse

5 and 1 fixed connection of equipment main part are stored to the fuselage, and storehouse 5 fixed connection is stored to flexible spray lance 6 and fuselage, and camera 4 is used for shooing the scene picture, and storehouse 5 is stored to the fuselage is used for storing the raw materials of putting out a fire, and flexible spray lance 6 is used for spraying the raw materials of putting out a fire.

Further, storehouse 5 fixed connection is stored with the fuselage to transmission case 7, and couple 8 and transmission case 7 swing joint, and storehouse 5 fixed connection is stored with the fuselage to support 9, and support 9 is provided with two sets ofly, and transmission case 7 is used for depositing motor 11, and couple 8 is used for hanging and gets the goods and materials, and support 9 is used for the stability of supporting equipment main part 1 on ground.

Further, the connecting bin 10 is fixedly connected with the transmission case 7, the motor 11 is fixedly connected with the connecting bin 10, the rope 12 is fixedly connected with the connecting bin 10, the connecting bin 10 is used for storing the rope 12, and the motor 11 is used for driving the rope 12 to be wound and unwound.

Further, a sealing door 13 is movably connected with the equipment main body 1, a sealing feed port 14 is fixedly connected with the machine body storage bin 5, a porous basalt fiber felt 15 is fixedly connected with the equipment main body 1, the sealing door 13 is used for facilitating internal maintenance work of the equipment main body 1, and the sealing feed port 14 is used for facilitating entering of raw materials.

Further, a carbon fiber layer 16 is arranged inside the porous basalt fiber felt 15, a rubber layer 17 is arranged inside the carbon fiber layer 16, a heat insulation layer 18 is arranged inside the rubber layer 17, the carbon fiber layer 16 is fixedly connected with the porous basalt fiber felt 15, the rubber layer 17 is fixedly connected with the carbon fiber layer 16, the heat insulation layer 18 is fixedly connected with the rubber layer 17, the porous basalt fiber felt 15 and the carbon fiber layer 16 are used for preventing fire, the rubber layer 17 is used for absorbing shock, and the heat insulation layer 18 is used for isolating the external temperature.

The utility model discloses a theory of operation and use flow: during the use, the user pours the raw materials of putting out a fire into fuselage through sealed feed inlet 14 and stores 5 insidely, through rising equipment subject 1 of control screw 3, control motor 11 and rope 12 put down couple 8, catch on required goods and materials, look for conflagration stranded personnel through camera 4, put down couple 8 through control motor 11, deliver to stranded personnel after with the goods, will put out a fire the raw materials and spray to the place of starting a fire through flexible spray lance 6 until will fire out can.

The above only is the preferred embodiment of the present invention, not so limiting the patent scope of the present invention, all under the concept of the present invention, the equivalent structure transformation made by the contents of the specification and the drawings is utilized, or the direct/indirect application is included in other related technical fields in the patent protection scope of the present invention.

Claims

1. The utility model provides a fire prevention unmanned aerial vehicle which characterized in that: comprises an equipment main body (1), wherein a machine arm (2) is arranged on one side of the equipment main body (1), a propeller (3) is arranged at the top end of one side of the machine arm (2), a camera (4) is arranged at the top of the front of the equipment main body (1), a machine body storage bin (5) is arranged at the bottom of the equipment main body (1), a telescopic spray rod (6) is arranged on one side of the machine body storage bin (5), a transmission case (7) is arranged at the bottom of the machine body storage bin (5), a hook (8) is arranged at the bottom of the transmission case (7), a support (9) is arranged at the bottom of one side of the machine body storage bin (5), a connection bin (10) is arranged inside the transmission case (7), a motor (11) is arranged on one side of the connection bin (10), a rope (12) is arranged at the bottom of the connection bin (10), a sealing door (13) is arranged on the front of the equipment main body (1), the other side of the machine body storage bin (5) is provided with a sealed feeding hole (14), and a porous basalt fiber felt (15) is arranged inside the equipment main body (1).

2. The fire-resistant unmanned aerial vehicle of claim 1, wherein: the mechanical arm (2) is fixedly connected with the equipment main body (1), the propeller (3) is fixedly connected with the mechanical arm (2), and six groups are respectively arranged on the mechanical arm (2) and the propeller (3).

3. The fire-resistant unmanned aerial vehicle of claim 1, wherein: camera (4) and equipment main part (1) fixed connection, storehouse (5) and equipment main part (1) fixed connection are stored to the fuselage, storehouse (5) fixed connection is stored with the fuselage to flexible spray lance (6).

4. The fire-resistant unmanned aerial vehicle of claim 1, wherein: storehouse (5) fixed connection is stored with the fuselage to transmission case (7), couple (8) and transmission case (7) swing joint, storehouse (5) fixed connection is stored with the fuselage to support (9), support (9) are provided with two sets ofly.

5. The fire-resistant unmanned aerial vehicle of claim 1, wherein: connect storehouse (10) and transmission case (7) fixed connection, motor (11) with connect storehouse (10) fixed connection, rope (12) with connect storehouse (10) fixed connection.

6. The fire-resistant unmanned aerial vehicle of claim 1, wherein: the device is characterized in that the sealing door (13) is movably connected with the device main body (1), the sealing feed inlet (14) is fixedly connected with the machine body storage bin (5), and the porous basalt fiber felt (15) is fixedly connected with the device main body (1).

7. The fire-resistant unmanned aerial vehicle of claim 1, wherein: the heat insulation and protection device is characterized in that a carbon fiber layer (16) is arranged inside the porous basalt fiber felt (15), a rubber layer (17) is arranged inside the carbon fiber layer (16), a heat insulation layer (18) is arranged inside the rubber layer (17), the carbon fiber layer (16) is fixedly connected with the porous basalt fiber felt (15), the rubber layer (17) is fixedly connected with the carbon fiber layer (16), and the heat insulation layer (18) is fixedly connected with the rubber layer (17).