CN210882619U - Fire control unmanned aerial vehicle - Google Patents
Fire control unmanned aerial vehicle Download PDFInfo
- Publication number
- CN210882619U CN210882619U CN201820851748.6U CN201820851748U CN210882619U CN 210882619 U CN210882619 U CN 210882619U CN 201820851748 U CN201820851748 U CN 201820851748U CN 210882619 U CN210882619 U CN 210882619U
- Authority
- CN
- China
- Prior art keywords
- fire
- machine body
- unmanned aerial
- aerial vehicle
- cloud platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Manipulator (AREA)
Abstract
The utility model discloses a fire control unmanned aerial vehicle, including organism, rotor and undercarriage, be provided with the cloud platform nacelle in the organism, install the magazine of putting out a fire on the cloud platform nacelle, but the top of cloud platform nacelle is through the setting on the organism of the first pivot horizontal hunting that sets up along the organism fore-and-aft direction. The utility model discloses at the in-process of work, because the hot gas flow perhaps turns to the factor, the skew of angle can take place for fire control unmanned aerial vehicle on the whole, but because the cloud platform nacelle is connected through first pivot and organism, under the effect of gravity, the cloud platform nacelle is in the state of ajusting with the magazine of putting out a fire all the time, is convenient for put out a fire the accurate transmission of bullet.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a fire control unmanned aerial vehicle.
Background
The fire disaster is a disaster with the highest occurrence frequency in multiple disasters in the world, about ten thousand fires occur in China every year, huge loss is caused to lives and properties of the country and people, particularly, the fire disaster extinguishing for some high-rise buildings and forests is difficult to extinguish, the existing fire extinguishing equipment and fire fighting facilities are difficult to reach the height of the high-rise buildings, the existing fire extinguishing equipment and fire fighting facilities for the forests are difficult to move to forest fire disaster points due to the limitation of road conditions, and in recent years, some unmanned aerial vehicles for fire fighting are also developed along with the rapid development of unmanned aerial vehicle technology.
The unmanned aerial vehicle that is used for fire control that has now generally has two kinds of forms, one kind is the bullet formula of throwing, the bullet formula of throwing limitation is great, just can put in directly over flying to the fire disaster, damage unmanned aerial vehicle easily, and be not convenient for control, another kind is the emission formula, unmanned aerial vehicle is in the fire disaster periphery promptly, the mode through the transmission launches the fire disaster, put out a fire, the advantage of this kind of mode lies in the safety of the unmanned aerial vehicle of having ensured of the maximum possibility, the field of vision is the preferred simultaneously, but because the design reason, it has a lot of unstable factors in actual work, for example, unmanned aerial vehicle is turning to, or when meetting the hot gas flow, the organism can take place the deflection, and then drive the bullet of putting out a fire and launch a section of thick bamboo and the skew of putting out a.
SUMMERY OF THE UTILITY MODEL
The utility model aims to avoid prior art's weak point, provide fire control unmanned aerial vehicle to effectively solve the weak point that exists among the prior art.
In order to achieve the above purpose, the utility model adopts the following technical scheme: fire control unmanned aerial vehicle, including organism, rotor and undercarriage, be provided with the cloud platform nacelle in the organism, install the magazine of putting out a fire on the cloud platform nacelle, but the top of cloud platform nacelle is through setting up on the organism along the first pivot horizontal hunting that the organism fore-and-aft direction set up.
Further, the machine body is door-shaped, a reinforcing structure is arranged at the bottom of the machine body, and the cradle head pod is arranged in a space enclosed by the machine body and the reinforcing structure.
Furthermore, two sides of the fire extinguishing bomb bin can be arranged on the cradle head pod in a front-back swinging mode through a second rotating shaft arranged along the left-right direction of the machine body.
Furthermore, a servo motor is installed on the cradle head pod, and an output shaft of the servo motor is fixedly connected with the second rotating shaft.
Further, a camera device is mounted on the cradle head pod.
Further, the imaging device is an infrared imaging device.
Further, a battery bin and a control bin are arranged on the machine body.
Further, the height of rotor is highly unanimous with the holistic focus height of fire control unmanned aerial vehicle.
The above technical scheme of the utility model following beneficial effect has: the utility model discloses at the in-process of work, because the hot gas flow perhaps turns to the factor, the skew of angle can take place for fire control unmanned aerial vehicle on the whole, but because the cloud platform nacelle is connected through first pivot and organism, under the effect of gravity, the cloud platform nacelle is in the state of ajusting with the magazine of putting out a fire all the time, is convenient for put out a fire the accurate transmission of bullet.
Drawings
Fig. 1 is a schematic structural diagram of an embodiment of the present invention;
fig. 2 is a top view of fig. 1.
Detailed Description
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
As shown in fig. 1-2, the fire-fighting unmanned aerial vehicle according to the embodiment includes a machine body 1, a rotor 2 and an undercarriage 3, a pan-tilt pod 4 is provided in the machine body 1, a fire-fighting cartridge 5 is installed on the pan-tilt pod 4, a plurality of fire-fighting cartridge launching cylinders 5a are provided on the fire-fighting cartridge 5 in parallel, the fire-fighting cartridge launching cylinders 5a are structures commonly used by fire-fighting unmanned aerial vehicles in the prior art, and the top of the pan-tilt pod 4 is provided on the machine body 1 through a first rotating shaft 6 arranged along the front-back direction of the machine body 1 in a left-right swinging manner.
In the in-process of work, because the hot gas flow or the factor that turns to, the skew of angle can take place for fire control unmanned aerial vehicle on the whole, but because cloud platform nacelle 4 is connected with organism 1 through first pivot 6, under the effect of gravity, cloud platform nacelle 4 is in the state of ajusting all the time with the magazine 5 of putting out a fire, is convenient for put out a fire the accurate transmission of bullet.
The machine body 1 is door-shaped, the bottom of the machine body 1 is provided with a reinforcing structure 7, the reinforcing structure 7 is a reinforcing plate, an X-shaped bracket and the like, and the cradle head pod 4 is arranged in a space enclosed by the machine body 1 and the reinforcing structure 7.
Two sides of the fire extinguishing bomb bin 5 can be arranged on the cloud platform nacelle 4 in a front-back swinging mode through a second rotating shaft 8 arranged along the left-right direction of the machine body 1.
Preferably, the pan-tilt-cabin 4 is in the shape of an inverted Y, and the fire-extinguishing cartridge 5 is mounted in the accommodating space of the Y.
The cloud platform nacelle 4 is provided with the servo motor 9, an output shaft of the servo motor 9 is fixedly connected with the second rotating shaft 8, the servo motor 9 is connected with the control device, the control device is connected with the wireless signal receiver, the angle of the fire extinguishing bomb bin 5 can be controlled through the servo motor 9, and then the upper and lower emission angles of the fire extinguishing bomb are controlled.
The cradle head pod 4 is provided with an image pickup device 11, the image pickup device 11 is an infrared image pickup device which has a night vision function and can meet the use requirements of day and night, and the cradle head pod 4 is also provided with an auxiliary system such as a sighting device 12 and a distance measuring device 10.
Of course, aiming scales can also be directly added on the screen of the camera device 11 and integrated into an infrared camera aiming device to realize the aiming function.
The aircraft is characterized in that a battery bin and a control bin are arranged on the aircraft body 1, a high-energy battery pack is arranged in the power supply bin, the battery bins are arranged on two sides of the aircraft body 1, a GPS navigation device and a flight control system are arranged in the control bin, and the control bin is arranged on the top of the aircraft body 1
The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (8)
1. Fire control unmanned aerial vehicle, including organism, rotor and undercarriage, its characterized in that: the fire extinguishing device is characterized in that a cradle head pod is arranged in the machine body, a fire extinguishing cartridge magazine is mounted on the cradle head pod, and the top of the cradle head pod can swing left and right on the machine body through a first rotating shaft arranged in the front-back direction of the machine body.
2. A fire fighting drone according to claim 1, characterized in that: the machine body is door-shaped, a reinforcing structure is arranged at the bottom of the machine body, and the cradle head pod is arranged in a space enclosed by the machine body and the reinforcing structure.
3. A fire fighting drone according to claim 1, characterized in that: two sides of the fire extinguishing cartridge magazine are arranged on the cradle head pod in a way that the fire extinguishing cartridge magazine can swing back and forth through a second rotating shaft arranged along the left and right directions of the machine body.
4. A fire fighting drone according to claim 3, characterized in that: and a servo motor is installed on the cradle head pod, and an output shaft of the servo motor is fixedly connected with the second rotating shaft.
5. A fire fighting drone according to claim 1, characterized in that: and the cloud platform pod is provided with a camera device.
6. A fire fighting drone according to claim 5, characterized in that: the camera device is an infrared camera device.
7. A fire fighting drone according to claim 1, characterized in that: the machine body is provided with a battery bin and a control bin.
8. A fire fighting drone according to claim 1, characterized in that: the height of rotor is highly unanimous with the holistic focus height of fire control unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820851748.6U CN210882619U (en) | 2018-06-04 | 2018-06-04 | Fire control unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820851748.6U CN210882619U (en) | 2018-06-04 | 2018-06-04 | Fire control unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210882619U true CN210882619U (en) | 2020-06-30 |
Family
ID=71329169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820851748.6U Expired - Fee Related CN210882619U (en) | 2018-06-04 | 2018-06-04 | Fire control unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210882619U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115779299A (en) * | 2022-11-15 | 2023-03-14 | 亿航智能设备（广州）有限公司 | Automatic fire extinguishing system and method for unmanned aerial vehicle |
-
2018
- 2018-06-04 CN CN201820851748.6U patent/CN210882619U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115779299A (en) * | 2022-11-15 | 2023-03-14 | 亿航智能设备（广州）有限公司 | Automatic fire extinguishing system and method for unmanned aerial vehicle |
| CN115779299B (en) * | 2022-11-15 | 2024-05-03 | 亿航智能设备（广州）有限公司 | Unmanned aerial vehicle automatic fire extinguishing system and method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102785778B (en) | A kind of tubular type launches fire extinguishing unmanned plane and fire extinguishing control method | |
| CN104527979B (en) | Space base teargas bullet automatic feeder | |
| KR20180042403A (en) | Multifunctional Unmanned Aircraft for Police | |
| CN108771803B (en) | Control system for high-rise building rotor unmanned aerial vehicle fire extinguishment and fire extinguishing system | |
| CN109248390A (en) | A kind of fire-fighting and rescue integrated system and method based on unmanned aerial vehicle platform | |
| CN204415724U (en) | Unmanned vehicle system is scouted in a kind of patrol | |
| CN109383806B (en) | Triggering method for launching fire monitor of fire-fighting unmanned aerial vehicle | |
| CN105963882A (en) | Air-to-surface rocket fire extinguisher and method | |
| WO2023070787A1 (en) | Airdrop forest fire extinguishing bomb | |
| WO2020052103A1 (en) | Firefighting method using firefighting unmanned aerial vehicle | |
| CN109305364B (en) | Aiming method of fire-fighting unmanned aerial vehicle | |
| WO2020052105A1 (en) | Fully electric driven fire-fighting unmanned aerial vehicle | |
| CN210437388U (en) | Forest fire-fighting fixed wing unmanned aerial vehicle | |
| CN108619641B (en) | Fire extinguishing system and method for vertical emission guidance fire extinguishing body | |
| CN205854503U (en) | A kind of suspension unmanned plane fire extinguishing system | |
| CN111268128A (en) | Mooring type fire rescue unmanned aerial vehicle system | |
| CN210882619U (en) | Fire control unmanned aerial vehicle | |
| CN111380422A (en) | Satellite guidance fire extinguishing shrapnel | |
| Tian et al. | Research on structure and fire control system of fire fighting UAV based on polymer gel fire bomb | |
| CN104503458A (en) | Micro individual combat unmanned plane system | |
| CN112618992B (en) | Low-cost suicide networking fire extinguishing method and unmanned aerial vehicle system | |
| CN212006942U (en) | Satellite guidance fire extinguishing shrapnel | |
| CN211996145U (en) | Reconnaissance and fire fighting integrated forest fire-fighting fixed wing unmanned aerial vehicle with accurate fire extinguishing function | |
| CN108128456A (en) | Unmanned helicopter-mounted fire-fighting fire extinguishing gondola | |
| CN207860455U (en) | Unmanned helicopter-mounted fire-fighting fire extinguishing gondola |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200630 Termination date: 20210604 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |