CN206634203U - A kind of police unmanned plane of investigation type - Google Patents
A kind of police unmanned plane of investigation type Download PDFInfo
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- CN206634203U CN206634203U CN201720341773.5U CN201720341773U CN206634203U CN 206634203 U CN206634203 U CN 206634203U CN 201720341773 U CN201720341773 U CN 201720341773U CN 206634203 U CN206634203 U CN 206634203U
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- fuselage
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- unmanned plane
- investigation
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Abstract
A kind of police unmanned plane of investigation type is the utility model is related to, including the fuselage being vertically arranged and the upper end of close fuselage are in horizontal-extending multiple horns, are provided with foldable assembly in fuselage, each horn is connected with foldable assembly；The lower end of fuselage is fixed with multiple dampings；Damping includes support, universal wheel, elastic component；The lower end of fuselage is fixed with automatic traveling mechanism；Multiple investigation video cameras are disposed with fuselage.The beneficial effects of the utility model are：Unmanned plane can not only fly investigation in the air, but also it can be investigated in ground running, it can all be folded and withdrawn by horn by foldable assembly during ground running investigation, reduce the volume of unmanned plane, so as to facilitate unmanned plane to carry out walking investigation in some narrow and small regions, the addition of damping simultaneously can not only be solved the problems, such as because impulsive force of the unmanned plane in landing is larger after installation automatic traveling mechanism, and can also effectively strengthen stationarity when unmanned plane walking is investigated.
Description
Technical field
It the utility model is related to unmanned plane field, more particularly to a kind of police unmanned plane of investigation type.
Background technology
With the development of World Economics, the raising of the level of urbanization, city size and complexity lifting, public security is held
The difficulty of method management, fire rescue etc. proposes higher requirement.
Nearly 2 years unmanned planes are fast-developing in public security (police) field, are used to investigate including by unmanned plane, but mesh
The preceding unmanned plane pattern for investigation is single, can only carry out airflight investigation, can not carry out ground running investigation, meanwhile, it is existing
Some unmanned planes can not also carry out investigations in some narrow and small regions.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of police unmanned plane of investigation type, above-mentioned existing to overcome
Deficiency in technology.
The technical scheme that the utility model solves above-mentioned technical problem is as follows：A kind of police unmanned plane of investigation type, including it is perpendicular
The fuselage directly set and the upper end of close fuselage are in horizontal-extending multiple horns, and foldable assembly is provided with fuselage, each
Horn is connected with foldable assembly, and foldable assembly is used to control horn to be rotated, and its pivot center is horizontal direction and hung down
Directly in the length direction of horn；The lower end of fuselage is fixed with multiple dampings；Damping includes support, universal wheel, elasticity
Part；One end of support is fixedly connected with fuselage, and the other end of support is connected with elastic component, the one end of elastic component away from support with
Universal wheel is connected；The lower end of fuselage is fixed with automatic traveling mechanism；The whole height of damping in its natural state is more than
The height of automatic traveling mechanism；Multiple investigation video cameras are disposed with fuselage.
The beneficial effects of the utility model are：By installing automatic traveling mechanism on fuselage, so that unmanned plane is not
Can only fly investigation in the air, but also can be investigated in ground running, can pass through folding during ground running investigation
Stacked group part is all folded by horn and withdrawn, and the volume of unmanned plane is reduced, so as to facilitate unmanned plane to enter in some narrow and small regions
Every trade walk investigation, while additions of damping can not only solve because installation automatic traveling mechanism after unmanned plane land when
The problem of impulsive force is larger, and can also effectively strengthen stationarity when unmanned plane walking is investigated.
On the basis of above-mentioned technical proposal, the utility model can also do following improvement.
Further, support is in C fonts.
It is using above-mentioned further beneficial effect：Impulsive force of the unmanned plane in landing can be slowed down.
Further, elastic component includes the first sleeve, second sleeve, the first spring；One end of first sleeve is inserted into second
In sleeve, and the first sleeve can move axially in second sleeve, and the first spring is arranged on the first sleeve and second set
Cylinder between, the one end of the first sleeve away from second sleeve is fixedly connected with support, the one end of second sleeve away from the first sleeve and
Universal wheel is fixedly connected.
It is using above-mentioned further beneficial effect：Impulsive force of the unmanned plane in landing can further be slowed down.
Further, poisonous gas detection device is disposed with fuselage.
It is using above-mentioned further beneficial effect：Can understand in investigated environment has with the presence or absence of harmful
Poisonous gas, follow-up personnel are avoided to occur after entering in the environment dangerous.
Further, it is continuous vari-focus visible light camera, thermal imaging camera, the shooting of uncooled ir line to investigate video camera
At least one of machine.
Brief description of the drawings
Fig. 1 is the structural representation of the police unmanned plane of investigation type described in the utility model；
Fig. 2 is the enlarged drawing of partial structurtes in Fig. 1.
In accompanying drawing, the list of parts representated by each label is as follows：
1st, fuselage, 2, horn, 3, foldable assembly, 310, arc-shaped rack, 320, guide rod, 330, driving member, 340, indentation,
350th, motor, 4, damping, 410, support, 411, second spring, 420, universal wheel, 430, elastic component, 431, first
Sleeve, 432, second sleeve, the 433, first spring, 5, automatic traveling mechanism, 6, investigation video camera, 7, poisonous gas detection dress
Put.
Embodiment
Principle of the present utility model and feature are described below in conjunction with accompanying drawing, example is served only for explaining this practicality
It is new, it is not intended to limit the scope of the utility model.
As shown in Figure 1 and Figure 2, a kind of police unmanned plane of investigation type, including the fuselage 1 being vertically arranged and close fuselage 1
Upper end be in horizontal-extending multiple horns 2, each end of the horn 2 away from fuselage 1 is provided with paddle components, fuselage
Foldable assembly 3 is provided with 1, each horn 2 is connected with foldable assembly 3, and foldable assembly 3 is used to control horn 2 to be rotated,
Its pivot center is for horizontal direction and perpendicular to the length direction of horn 2.The quantity of horn 2 can be four, six, eight etc.
Other situations, in the present embodiment, the quantity of horn 2 is four, and the angle between adjacent horn 2 is 90 °.Fuselage 1 is provided with
The depressed part of horn 2 convenient for collecting.
Foldable assembly 3 includes the arc-shaped rack 310 that is arranged on horn 2, and (arc-shaped rack 310 can be around corresponding pivot center
Rotate), the guide rod 320 that is vertically provided in fuselage 1, be set on guide rod 320 and can the relative movement of guide rod 320 driving member
330th, it is vertically provided on driving member 330 and corresponds a plurality of indentation 340 engaged with arc-shaped rack 310, installs in fuselage 1
On motor 350, guide rod 320 be with motor 350 be connected screw mandrel, driving member 330 be and wire rod thread connect
The nut connect.Connected between arc-shaped rack 310 and fuselage 1 by axis of rotation.
Horn 2 folds and that deploys comprises the concrete steps that：
When unmanned plane needs to carry out flight, then motor 350 is controlled first to work, guide rod 320 starts around own axes
Rotation, and then driving member 330 can be driven to be moved straight down around guide rod 320, and under the engaged transmission of rack, each horn 2
Synchronously it is rotated up up to being in horizontality, otherwise when needing to collapse each horn 2, then by motor around corresponding rotating shaft
350 control guide rods 320 reversely rotate, driving member 330 rotates straight up along guide rod 320, each horn 2 synchronously rotate down until
It is posted by fuselage 1.
The lower end of fuselage 1 is fixed with automatic traveling mechanism 5, and remote control center can control automatic traveling mechanism 5 to carry out
Motion, so as to drive unmanned plane to walk.Automatic traveling mechanism 5 uses wheel type traveling mechanism of the prior art or crawler-type traveling
Mechanism.
The lower end of fuselage 1 is fixed with multiple dampings 4, and such unmanned plane will not be by excessive impact in landing
Power.The quantity of damping 4 can be two, three, four, six etc., and in the present embodiment, preferably four, four subtract
Mechanism 4 is shaken in arrangement, and the angle between adjacent damping 4 is 90 °.
In the present embodiment, the concrete structure of damping 4 is as follows：Damping 4 include support 410, universal wheel 420,
Elastic component 430.One end of support 410 is fixedly connected by screw with fuselage 1, and the other end of support 410 passes through screw and elasticity
Part 430 is connected, and the one end of elastic component 430 away from support 410 is connected by screw with universal wheel 420.In order to ensure damping
Mechanism 4 can play cushioning effect when unmanned plane lands, and the whole height of damping 4 in its natural state is more than automatic row
The height of mechanism 5 is walked, and after paddle components shut down, damping 4 is compressed under unmanned plane self gravitation, damping
The whole height of mechanism 4 now is equal to the height of automatic traveling mechanism 5, and such damping 4 can not only play the effect of damping
Fruit, but also play a part of guiding when unmanned plane starts walking mode, ensure stability during unmanned plane shape.
Support 410 includes first horizontal segment, segmental arc, the second horizontal segment, wherein, the both ends of segmental arc in succession first respectively
Horizontal segment and the second horizontal segment, are made between first horizontal segment and segmental arc of integral forming process, the second horizontal segment and arc
It is made between shape section of integral forming process, support 410 is made of carbon fibre material, and the global shape of support 410 is C words
Shape.In addition, support 410 also includes second spring 411, one end of wherein second spring 411 is connected with first horizontal segment, the second bullet
The other end of spring 411 is connected with the second horizontal segment, and second spring 411 can effectively ensure that the anti seismic efficiency of support 410, ensures branch
The service life of frame 410.
Investigation video camera 6 is fixed with by screw at the side of fuselage 1, top, investigation video camera 6 is that continuous vari-focus can
See at least one of light video camera, thermal imaging camera, uncooled ir line video camera.Continuous vari-focus visible light camera and
Uncooled ir line video camera can provide big field of view and scene for observer, and image quality is high.Thermal imaging camera
Image is gathered in the case of facilitating low visibility.
In the present embodiment, the concrete structure of elastic component 430 is as follows：
Elastic component 430 includes the first sleeve 431, second sleeve 432, the first spring 433.First sleeve 431 is provided with down
Open cavity is held, second sleeve 432 is provided with the open cavity in upper end, and one end of the first sleeve 431 is inserted into second sleeve
In 432, and the first sleeve 431 can move axially in second sleeve 432, and set cavity is interior in second sleeve 432
Footpath is equal to the external diameter that the first sleeve 431 is inserted into part, and one end of the first spring 433 extend into cavity set by the first sleeve 431
It is interior, and be fixedly connected with the first sleeve 431, the other end of the first spring 433 is extend into set by second sleeve 432 in cavity, and
It is fixedly connected with second sleeve 432, after the first sleeve 431 is connected with second sleeve 432 by the first spring 433, the first sleeve
431 to have part be in the second sleeve 432.First one end of sleeve 431 away from second sleeve 432 passes through screw and support
410 the second horizontal segment is fixedly connected, and the one end of second sleeve 432 away from the first sleeve 431 is solid by screw and universal wheel 420
Fixed connection.
Control system, two power supplys are also equipped with fuselage 1, two power supplys are used equally for as each electrical appliance in unmanned plane
Part provides electric energy, and control system is used to control the flight of unmanned plane and the transmission of data, motor 350 also with control system
Electrically connect, one of them in two power supplys is power supply, and another is stand-by power supply, and unmanned plane only utilizes in flight course
Power supply is powered, and when the power supply failure for power supply, the personnel of remote control center, can remotely be controlled
System, start stand-by power supply, when so can not only ensure the normal flight of unmanned plane, but also the continuation of the journey of unmanned plane can be improved
Between.
Poisonous gas detection device 7 is disposed with fuselage 1, poisonous gas detection device 7 is used to testing result passing through number
Control centre is transferred to according to transport module, the operating personnel of control centre can understand investigated environment so during investigation
In whether there is harmful toxic gas, avoid follow-up personnel from occurring after entering in the environment dangerous.
Although embodiment of the present utility model has been shown and described above, it is to be understood that above-described embodiment is
Exemplary, it is impossible to it is interpreted as to limitation of the present utility model, one of ordinary skill in the art is in the scope of the utility model
It is interior above-described embodiment to be changed, changed, replaced and modification.
Claims (5)
1. a kind of police unmanned plane of investigation type, including the fuselage (1) being vertically arranged and the upper end of close fuselage (1) are in water
Multiple horns (2) of flat extension, it is characterised in that foldable assembly (3) is provided with the fuselage (1), each horn (2) is equal
It is connected with foldable assembly (3), the foldable assembly (3) is used to control horn (2) to be rotated, and its pivot center is level side
To and perpendicular to the horn (2) length direction；The lower end of the fuselage (1) is fixed with multiple dampings (4)；Described
Any damping (4) includes support (410), universal wheel (420), elastic component (430)；One end of the support (410) and institute
State fuselage (1) to be fixedly connected, the other end of the support (410) is connected with the elastic component (430), the elastic component
(430) one end away from support (410) is connected with the universal wheel (420)；The lower end of the fuselage (1) is fixed with automatic row
Walk mechanism (5)；The whole height of described any damping (4) in its natural state is more than the automatic traveling mechanism (5)
Height；Multiple investigation video cameras (6) are disposed with the fuselage (1).
2. a kind of police unmanned plane of investigation type according to claim 1, it is characterised in that the support (410) is in C words
Shape.
3. a kind of police unmanned plane of investigation type according to claim 2, it is characterised in that the elastic component (430) includes
First sleeve (431), second sleeve (432), the first spring (433)；One end of first sleeve (431) is inserted into second set
In cylinder (432), and first sleeve (431) can move axially in second sleeve (432), first spring
(433) it is arranged between first sleeve (431) and the second sleeve (432), first sleeve (431) is away from second
One end of sleeve (432) is fixedly connected with the support (410), and the one of remote first sleeve (431) of the second sleeve (432)
End is fixedly connected with the universal wheel (420).
4. a kind of police unmanned plane of investigation type according to claim 3, it is characterised in that be disposed with the fuselage (1)
Poisonous gas detection device (7).
5. a kind of police unmanned plane of investigation type according to any one of Claims 1-4, it is characterised in that the investigation is taken the photograph
Camera (6) is at least one of continuous vari-focus visible light camera, thermal imaging camera, uncooled ir line video camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720341773.5U CN206634203U (en) | 2017-04-01 | 2017-04-01 | A kind of police unmanned plane of investigation type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720341773.5U CN206634203U (en) | 2017-04-01 | 2017-04-01 | A kind of police unmanned plane of investigation type |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206634203U true CN206634203U (en) | 2017-11-14 |
Family
ID=60258921
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720341773.5U Expired - Fee Related CN206634203U (en) | 2017-04-01 | 2017-04-01 | A kind of police unmanned plane of investigation type |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206634203U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107972853A (en) * | 2017-12-07 | 2018-05-01 | 佛山市神风航空科技有限公司 | Aerial photography aircraft undercarriage two level shock-damping structure |
| CN107985565A (en) * | 2017-12-07 | 2018-05-04 | 佛山市神风航空科技有限公司 | The unmanned plane undercarriage of taking photo by plane of dual shock absorption |
| CN107985566A (en) * | 2017-12-07 | 2018-05-04 | 佛山市神风航空科技有限公司 | Aerial photography aircraft undercarriage with damping auxiliary wheel |
| CN108082478A (en) * | 2017-12-16 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of early warning type unmanned plane monitors Reconnaissance system |
| CN109279017A (en) * | 2018-11-16 | 2019-01-29 | 华东理工大学 | One kind receives the foldable verification unmanned plane of type |
| CN110546476A (en) * | 2018-04-27 | 2019-12-06 | 深圳市大疆创新科技有限公司 | Folding equipment |
| CN112109879A (en) * | 2020-10-16 | 2020-12-22 | 西安羚控电子科技有限公司 | Folding wing unfolding rotating shaft mechanism |
| CN113184173A (en) * | 2021-06-07 | 2021-07-30 | 广西电网有限责任公司电力科学研究院 | VTOL fixed wing unmanned aerial vehicle with damping device |
| CN113874709A (en) * | 2019-06-20 | 2021-12-31 | 金泰克斯公司 | System and method for automated modular lighting and deployment |
-
2017
- 2017-04-01 CN CN201720341773.5U patent/CN206634203U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107985565A (en) * | 2017-12-07 | 2018-05-04 | 佛山市神风航空科技有限公司 | The unmanned plane undercarriage of taking photo by plane of dual shock absorption |
| CN107985566A (en) * | 2017-12-07 | 2018-05-04 | 佛山市神风航空科技有限公司 | Aerial photography aircraft undercarriage with damping auxiliary wheel |
| CN107972853A (en) * | 2017-12-07 | 2018-05-01 | 佛山市神风航空科技有限公司 | Aerial photography aircraft undercarriage two level shock-damping structure |
| CN108082478B (en) * | 2017-12-16 | 2021-11-16 | 深圳市翼飞鸿天无人机科技有限公司 | Early warning type unmanned aerial vehicle monitoring and investigation system |
| CN108082478A (en) * | 2017-12-16 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of early warning type unmanned plane monitors Reconnaissance system |
| CN110546476A (en) * | 2018-04-27 | 2019-12-06 | 深圳市大疆创新科技有限公司 | Folding equipment |
| CN109279017A (en) * | 2018-11-16 | 2019-01-29 | 华东理工大学 | One kind receives the foldable verification unmanned plane of type |
| CN109279017B (en) * | 2018-11-16 | 2022-04-19 | 华东理工大学 | Foldable nano unmanned aerial vehicle for verification |
| CN113874709A (en) * | 2019-06-20 | 2021-12-31 | 金泰克斯公司 | System and method for automated modular lighting and deployment |
| CN113874709B (en) * | 2019-06-20 | 2024-04-12 | 金泰克斯公司 | System and method for automated modular lighting and deployment |
| CN112109879A (en) * | 2020-10-16 | 2020-12-22 | 西安羚控电子科技有限公司 | Folding wing unfolding rotating shaft mechanism |
| CN113184173A (en) * | 2021-06-07 | 2021-07-30 | 广西电网有限责任公司电力科学研究院 | VTOL fixed wing unmanned aerial vehicle with damping device |
| CN113184173B (en) * | 2021-06-07 | 2023-04-21 | 广西电网有限责任公司电力科学研究院 | Vertical take-off and landing fixed wing unmanned aerial vehicle with damping device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20171114 Termination date: 20190401 |