CN204979240U - Carry lifesaving articles for use unmanned aerial vehicle - Google Patents
Carry lifesaving articles for use unmanned aerial vehicle Download PDFInfo
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- CN204979240U CN204979240U CN201520740933.4U CN201520740933U CN204979240U CN 204979240 U CN204979240 U CN 204979240U CN 201520740933 U CN201520740933 U CN 201520740933U CN 204979240 U CN204979240 U CN 204979240U
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Abstract
The utility model discloses a carry lifesaving articles for use unmanned aerial vehicle, the unmanned aerial vehicle main part is semi -circular structure, the outer lane of unmanned aerial vehicle main part is equipped with the screw that annular matrix distributes, the top of unmanned aerial vehicle main part is equipped with infrared camera, the left and right sides is equipped with in the lower part of unmanned aerial vehicle main part the megaphone, the megaphone symmetric distribution, the lower partial front and back end of unmanned aerial vehicle main part is equipped with the high power microphone, high power microphone symmetric distribution, the lower extreme of unmanned aerial vehicle main part is equipped with two rows and falls to the ground the foot, two rows fall to the ground be equipped with between the foot with the foot that falls to the ground two rows of parallel robotic arm, its advantage lies in: the utility model has the advantages of being simple in structure and convenient in operation, can realize visual, can talk with, can carry the lifesaving articles for use and can accurately put in, can be in some in a particular case perform tasks, guarantee people property safety.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, especially relates to a kind of conveying life-saving unmanned plane.
Background technology
Along with the development of world economy, city is high-rise, high-rise building is increasing, and tens meters even high building of up to a hundred meters, once presence of fire, can face the difficult problem in fire-fighting.The effective operating altitude of common fire fighting turnable ladder is 30 ~ 50m, highly again reach 60 ~ 70m, fire fighting turnable ladder the highest is in the world speedily carried out rescue work fire control platform aerial ladder truck in the sky of holding up that the rich wave aerial ladder truck Co., Ltd of Finland manufactures, the maximum effective operating altitude of this aerial ladder truck is 101m, just there is introduction in the big city only having minority economically developed in China, expensive, maintenance difficulty.And by the restriction such as area, the unimpeded degree in street, responding speed, motor fire engine can not arrive in the scene of catching fire under many circumstances the very first time.And use fire extinguishing tanker fire fighting, mainly still rely on fire fighter, fire fighter is directly adjacent to the scene of a fire, has very high danger sometimes even can cause unnecessary injures and deaths.
Unmanned air vehicle technique is in the technology being now relative maturity, flexible operation, speed is fast, appointed place can not be arrived by the restriction of geographical environment, although also have practice behavior unmanned plane being used for fire scene rescue now, but be generally when forest and deserted mountain presence of fire, the scene that location fire is concrete.Directly throw extinguishing material with general unmanned plane, be also difficult to reach the requirement of accurately throwing, and unmanned plane carrying capacity is little, the extinguishing material limited amount carried, if use multiple UAVs, then needs many people to operate, at substantial manpower and time for positioning.
Summary of the invention
The purpose of this utility model be to provide a kind of visual, can talk with, can life-saving be carried and the conveying life-saving unmanned plane that can precisely throw in.
The technical solution adopted in the utility model is:
A kind of conveying life-saving unmanned plane, main body is unmanned plane, its innovative point is: described unmanned plane comprises unmanned plane main body, screw propeller, infrared camera, loudspeaker, high power microphone, landing leg, mechanical arm and be arranged on described unmanned plane body interior unmanned aerial vehicle (UAV) control device form, described unmanned plane main body is semicircular structure, the outer ring of described unmanned plane main body is provided with the screw propeller of ring quasi array distribution, the upper part of described unmanned plane main body is provided with infrared camera, in the lower part of described unmanned plane main body, the left and right sides is provided with described loudspeaker, described loudspeaker is symmetrical, the lower part front and back end of described unmanned plane main body is provided with described high power microphone, described high power microphone is symmetrical, the lower end of described unmanned plane main body is provided with two row's landing legs, be provided with parallel with described landing leg two between described two row's landing legs and arrange mechanical arm.
As preferably, described unmanned plane main body is many rotor wing unmanned aerial vehicles or depopulated helicopter.
As preferably, described infrared camera is 360 ° of rotational structures.
As preferably, described mechanical arm is can left and right adjusting, up and down stretching structure.
As preferably, described unmanned aerial vehicle (UAV) control device comprises GPS registration device, wireless signal transceiver, infrared rays communication module.
The beneficial effects of the utility model are:
(1) the utility model structure is simple, easy to operate, can realize visual, can talk with, can life-saving be carried and can precisely throw in, in particular cases can execute the task at some, ensure people's property safety.
(2) infrared camera of the present utility model has night vision function, can when night or sleety weather safety send to life-saving, and can 360 ° of rotations, each orientation can be observed.
(3) mechanical arm of the present utility model, can regulate freely and stretch, meet the transport of life-saving to greatest extent.
(4) loudspeaker of the present utility model and high power microphone, when environment is more severe, can meets dialogue and links up, help trapped personnel to depart from dangerous situation as early as possible.
(5) unmanned plane main body is built with GPS registration device, the location information of unmanned plane can be sent to ground station, after ground station is received by antenna, the position of unmanned plane can be shown in map display screen, and other multiple unmanned planes can be given by position information share, multiple like this unmanned plane can participate in rescue attempt together.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
Fig. 2 is the utility model birds-eye view.
Detailed description of the invention
For making utility model object of the present utility model, technical scheme and advantage clearly, below in conjunction with accompanying drawing, embodiment of the present utility model is described in further detail.
As shown in Figure 1, a kind of conveying life-saving unmanned plane, main body is unmanned plane, described unmanned plane comprises unmanned plane main body 1, screw propeller 2, infrared camera 3, loudspeaker 4, high power microphone 5, landing leg 6, mechanical arm 7 and be arranged on described unmanned plane body interior unmanned aerial vehicle (UAV) control device form, described unmanned plane main body 1 is semicircular structure, the outer ring of described unmanned plane main body 1 is provided with the screw propeller 2 of ring quasi array distribution, the upper part of described unmanned plane main body 1 is provided with infrared camera 3, in the lower part of described unmanned plane main body 1, the left and right sides is provided with described loudspeaker 4, described loudspeaker 4 is symmetrical, the lower part front and back end of described unmanned plane main body 1 is provided with described high power microphone 5, described high power microphone 5 is symmetrical, the lower end of described unmanned plane main body 1 is provided with two row's landing legs 6, be provided with parallel with described landing leg 6 two between described two row's landing legs 6 and arrange mechanical arm 7.
Above-described embodiment is preferred embodiment of the present utility model; it is not the restriction to technical solutions of the utility model; as long as without the technical scheme that creative work can realize on the basis of above-described embodiment, all should be considered as falling within the scope of the rights protection of the utility model patent.
Claims (5)
1. a conveying life-saving unmanned plane, main body is unmanned plane, it is characterized in that: described unmanned plane comprises unmanned plane main body (1), screw propeller (2), infrared camera (3), loudspeaker (4), high power microphone (5), landing leg (6), mechanical arm (7) and be arranged on the inner unmanned aerial vehicle (UAV) control device of described unmanned plane main body (1) and form, described unmanned plane main body (1) is semicircular structure, the outer ring of described unmanned plane main body (1) is provided with the screw propeller (2) of ring quasi array distribution, the upper part of described unmanned plane main body (1) is provided with infrared camera (3), in the lower part of described unmanned plane main body (1), the left and right sides is provided with described loudspeaker (4), described loudspeaker (4) is symmetrical, the lower part front and back end of described unmanned plane main body (1) is provided with described high power microphone (5), described high power microphone (5) is symmetrical, the lower end of described unmanned plane main body (1) is provided with two row's landing legs (6), be provided with parallel with described landing leg (6) two between described two rows landing leg (6) and arrange mechanical arm (7).
2. one conveying life-saving unmanned plane according to claim 1, is characterized in that: described unmanned plane main body (1) is many rotor wing unmanned aerial vehicles or depopulated helicopter.
3. one conveying life-saving unmanned plane according to claim 1, is characterized in that: described infrared camera (3) is 360 ° of rotational structures.
4. one conveying life-saving unmanned plane according to claim 1, is characterized in that: described mechanical arm (7) is can left and right adjusting, up and down stretching structure.
5. one conveying life-saving unmanned plane according to claim 1, is characterized in that: described unmanned aerial vehicle (UAV) control device comprises GPS registration device, wireless signal transceiver, infrared rays communication module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520740933.4U CN204979240U (en) | 2015-09-23 | 2015-09-23 | Carry lifesaving articles for use unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520740933.4U CN204979240U (en) | 2015-09-23 | 2015-09-23 | Carry lifesaving articles for use unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204979240U true CN204979240U (en) | 2016-01-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520740933.4U Expired - Fee Related CN204979240U (en) | 2015-09-23 | 2015-09-23 | Carry lifesaving articles for use unmanned aerial vehicle |
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| CN (1) | CN204979240U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105799923A (en) * | 2016-04-28 | 2016-07-27 | 南京信息工程大学 | Four-rotor aircraft-based carrying manipulator |
| CN106628137A (en) * | 2016-11-11 | 2017-05-10 | 苏州曾智沃德智能科技有限公司 | Unmanned aerial vehicle for earthquake relief work |
| CN108492525A (en) * | 2018-05-10 | 2018-09-04 | 湖北师范大学 | A kind of the indoor human body tumble position monitor rescue skills and system of Multi-information acquisition |
| WO2019007427A1 (en) * | 2017-07-07 | 2019-01-10 | 苏州工业园区凯艺精密科技有限公司 | Mechanical hand structure with viewing function |
| CN109541625A (en) * | 2018-11-27 | 2019-03-29 | 中国农业大学 | Plant protection drone flight parameter measurement method and system |
| CN109922309A (en) * | 2019-01-04 | 2019-06-21 | 浙江海洋大学 | A kind of engineering explosion operation field emergency management and rescue resource information management system |
-
2015
- 2015-09-23 CN CN201520740933.4U patent/CN204979240U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105799923A (en) * | 2016-04-28 | 2016-07-27 | 南京信息工程大学 | Four-rotor aircraft-based carrying manipulator |
| CN106628137A (en) * | 2016-11-11 | 2017-05-10 | 苏州曾智沃德智能科技有限公司 | Unmanned aerial vehicle for earthquake relief work |
| WO2019007427A1 (en) * | 2017-07-07 | 2019-01-10 | 苏州工业园区凯艺精密科技有限公司 | Mechanical hand structure with viewing function |
| CN108492525A (en) * | 2018-05-10 | 2018-09-04 | 湖北师范大学 | A kind of the indoor human body tumble position monitor rescue skills and system of Multi-information acquisition |
| CN109541625A (en) * | 2018-11-27 | 2019-03-29 | 中国农业大学 | Plant protection drone flight parameter measurement method and system |
| CN109541625B (en) * | 2018-11-27 | 2020-10-09 | 中国农业大学 | Method and system for measuring flight parameters of plant protection unmanned aerial vehicle |
| CN109922309A (en) * | 2019-01-04 | 2019-06-21 | 浙江海洋大学 | A kind of engineering explosion operation field emergency management and rescue resource information management system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160530 Address after: 056000 northeast corner of Zhu Ming Street and Xincheng Road intersection, Xincheng Industrial Park, Linzhang County, Hebei, Handan Patentee after: Hebei Mitutoyo Air Technology Development Co.,Ltd. Address before: Shijiazhuang City, Hebei province 050000 Bridge West Liu Ying Xiang Xi Jian Liang Cun build Hutong No. 12 Patentee before: Wang Zhihong |
|
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 056000 Northeast corner of the intersection of Zhuming Street and Beimen Road, Linzhang New Town Industrial Park, Handan City, Hebei Province Patentee after: Hebei Sanfeng Aviation Technology Co.,Ltd. Address before: 056000 Northeast corner of the intersection of Zhuming Street and Beimen Road, Linzhang New Town Industrial Park, Handan City, Hebei Province Patentee before: Hebei Mitutoyo Air Technology Development Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160120 Termination date: 20210923 |