CN207191432U - Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters - Google Patents
Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters Download PDFInfo
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- CN207191432U CN207191432U CN201721219362.5U CN201721219362U CN207191432U CN 207191432 U CN207191432 U CN 207191432U CN 201721219362 U CN201721219362 U CN 201721219362U CN 207191432 U CN207191432 U CN 207191432U
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Abstract
The utility model discloses a kind of public security waters to rescue four rotor wing unmanned aerial vehicles,Including fuselage,Load,The fuselage includes body cover,There are RTK modules on the body cover,There is fuselage main body under the body cover,There is cantilever in the fuselage main body,Brushless electric machine is installed on the cantilever,Blade is housed on the brushless electric machine,There is GPS navigation module the fuselage main body side,The GPS navigation module is arranged on a Carbon fibe pipe,There is screw threads for fastening button under the Carbon fibe pipe,The load includes load connecting plate,There is antenna beside the load connecting plate,There is undercarriage around the load,There is ultrasonic wave module under the undercarriage,There is draw off gear on the load connecting plate,Draw off gear extension pipe is connected under the draw off gear,Described draw off gear extension pipe one end presss from both sides equipped with folding and unfolding,The folding and unfolding folder is lower to set lifebuoy.Simple in construction, flying quality stabilization, wind loading rating is strong, practical, cruising time is long, flying speed is fast.
Description
Technical field
The utility model belongs to unmanned plane field, and in particular to rescues four rotor wing unmanned aerial vehicles in a kind of public security waters.
Background technology
In the rescue operations of public security waters, the problem of being commonly encountered, has positioning inaccurate, and speed of suing and labouring is slow, and such as run into it is multiple fall
During water personnel, attend to one thing and lose sight of another, and waters is rescued and very big danger is brought to public security rescuer, it is impossible to effective fast accurate
Give drowning people deliver lifebuoy, to public security waters rescue bring great puzzlement, due to waters rescue environment particularity, often
Strong wind, light rain are often accompanied by, without smooth landing site of rule etc., so also higher to the equipment requirement of this special operation
, endurance also requires longer, and the flight stability and operating characteristics each side of aircraft have higher requirement.
The Chinese patent of Patent No. (CN106081111A), particular content are：One kind rescue unmanned plane, including fuselage,
Grasping mechanism, putting module, lifebuoy, it is characterised in that：Described grasping mechanism is arranged on the bottom plate lower surface of fuselage；Institute
The putting module stated is arranged on the bottom plate lower surface of fuselage；Described lifebuoy is arranged on putting module, described fuselage
Including bottom plate, 3 motor, 3 propellers, power module, rocking arm, the first electric cylinders, control module, camera, described confession
Energy module is fixedly mounted on bottom plate upper surface；Described rocking arm is hinged on the hinge stent of bottom plate afterbody.
The Chinese patent of Patent No. (CN106864698A), particular content are：A kind of intelligence for being used to succour drowning person
Type unmanned plane, including deliverance apparatus, deliverance apparatus, which includes gas main, some branch pipes and some rescue units, rescue unit, to be included
Retractor device, retractor device include shell, and telescopic component is provided with shell, and telescopic component includes the 3rd motor and flexible list
Member, telescopic unit include the 3rd drive shaft and sleeve pipe, and some ventilation units are provided with gas main, and ventilation unit includes the second driving
Motor, buffer stopper, driver framework, connecting rod and plugging block.
The Chinese patent of Patent No. (CN106741733A), particular content are：It is a kind of jettisoning by several times lifebuoy carry and
Unmanned plane, wherein, lifebuoy carry of jettisoninging by several times includes：Link, the support frame on link, it is enclosed on support frame
Lifebuoy group, the bottom of link is provided with mounting seat, steering wheel and high-definition camera, the output gear of steering wheel is provided with mounting seat
A reel is coaxially installed with wheel.When drawstring on reel inwardly pulls on the top of two layers of support feet, two layers
The bottom of support feet is turned out holding up the layer lifebuoy second from the bottom of lifebuoy group, and the bottom of base layer support pin, which inwardly rotates, releases
Put the layer lifebuoy last of lifebuoy group.
The Chinese patent of Patent No. (CN106143918A), particular content are：A kind of lifebuoy delivers unmanned plane, including
Frame, delivery module, it is characterised in that：Described delivery module is symmetrically mounted on both sides below the matrix of frame；Described machine
Frame include matrix, camera, load port, 2 motor racks, 4 brushless electric machines, 4 propellers, power module, control module, plus
Strengthening tendons, described camera are fixedly mounted on the mounting bracket of matrix side.
Above-mentioned patent designs complicated, and cruising time is short, is not easy to dismount, cumbersome, it is impossible to realizes well
Unmanned plane flies delivery automatically, and positioning is inaccurate, and wind loading rating is poor, it is difficult to ensures fast and effectively water life-saving action, therefore, needs
A kind of easy to use, four rotor wing unmanned aerial vehicles are rescued in practical public security waters, insufficient present in above-mentioned patent to solve.
Utility model content
The purpose of this utility model be that to solve the above problems and provide a kind of public security waters rescue four rotors without
It is man-machine.
The utility model is achieved through the following technical solutions above-mentioned purpose：
Four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters, including fuselage, load, the fuselage include body cover, the machine
Body, which covers, is provided with RTK modules, and the body cover is arranged with fuselage main body, and cantilever is provided with the fuselage main body, described
Brushless electric machine is installed on cantilever, blade is housed on the brushless electric machine, the fuselage main body side is provided with GPS navigation mould
Block, the GPS navigation module are arranged on a Carbon fibe pipe, and the Carbon fibe pipe is arranged with screw threads for fastening button, the load
Pocket includes load connecting plate, and antenna is provided with beside the load connecting plate, is provided with undercarriage around the load, described
Fall and ultrasonic wave module is installed under frame, draw off gear is provided with the load connecting plate, is connected to receive under the draw off gear
Device extension pipe is put, described draw off gear extension pipe one end presss from both sides equipped with folding and unfolding, and the folding and unfolding folder is lower to set lifebuoy.
After unmanned plane is powered, by the antenna and outside earth station and radio station intercommunication, data real-time, interactive is realized.
In order to further improve performance, the RTK is arranged on the body cover, increases the positioning accurate accuracy of unmanned plane,
And the RTK is arranged on to the signal interference that it also avoid flying control on the body cover, the RTK tail ends are provided with lock knot
Structure, the body cover form flip structure with the fuselage main body.
In order to further improve performance, four cantilevers are set, the cantilevered distal end is provided with four brushless electricity
Machine, the cantilever are integrally formed with the fuselage main body, and material is Carbon fibe, overall structural strength are added, also certain
In degree.
In order to further improve performance, the routine navigation function of the GPS navigation module increase unmanned plane, the GPS is led
Model plane block by the Carbon fibe pipe support lengthen, avoid fly control signal interference, and described Carbon fibe pipe one end with it is described
Screw threads for fastening button is connected, and facilitates the body cover to cover tightly fastening.
In order to further improve performance, the draw off gear and the antenna are arranged on the load connecting plate.
In order to further improve performance, the folding and unfolding folder is linked to be by the draw off gear extension pipe and the draw off gear
One entirety, by lengthening, cause to interfere when avoiding the undercarriage from launching the lifebuoy.
In order to further improve performance, a lifebuoy inflated is clipped under the folding and unfolding folder, is improved in waters
Efficiency during rescue action.
In order to further improve performance, the undercarriage shares four groups, and uses aircraft aluminum matter, enhances takeoff and landing
When stability.
In order to further improve performance, by the ultrasonic wave module, the height on actual measurement aircraft and ground.
Beneficial effect is：The utility model is designed reasonably, simple in construction, flying quality is stable, wind loading rating is strong, is easy to
Carry, be easy to dismount, it is practical, by flight control technique, unmanned plane autonomous flight, cruising time length, flying speed can be made
It hurry up, complete water life-saving action in time, by positioners such as GPS, precisely launch, increase substantially search and rescue effect waterborne
Rate, the ability and level of significant increase rapidly and efficiently search and rescue waterborne, effectively reduces search and rescue risk waterborne.
Brief description of the drawings
Fig. 1 is the dimensional structure diagram that four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters described in the utility model；
1st, fuselage；2nd, load；3rd, body cover；4th, fuselage main body；5th, blade；6th, brushless electric machine；7th, cantilever；8th, screw threads for fastening
Button；9th, Carbon fibe pipe；10th, GPS navigation module；11st, RTK modules；12nd, antenna；13rd, ultrasonic wave module；14th, draw off gear；15、
Draw off gear extension pipe；16th, folding and unfolding is pressed from both sides；17th, lifebuoy；18th, undercarriage；19th, load connecting plate.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings：
As shown in figure 1, four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters, including fuselage 1, load 2, fuselage 1 include fuselage
Lid 3, RTK modules 11 being provided with body cover 3, RTK modules 11 are used to improve accurate data degree during aircraft flight mapping operation, and
It is space-saving above body cover 3, isolate the interference of aircraft battery and dynamical system to it again, the tail end of RTK modules 11 is set
Lock structure is equipped with, body cover 3 is formed flip structure with fuselage main body 4, body cover 3 is arranged with fuselage main body 4, fuselage master
Four cantilevers 7 are provided with body 4, for every cantilever 7 into being symmetrical arranged, adjacent two at an angle of 90, and one is provided with every cantilever 7
Individual brushless electric machine 6, blade 5 is housed on brushless electric machine 6, the side of fuselage main body 4 is provided with GPS navigation module 10, GPS navigation module
10 are arranged on a Carbon fibe pipe 9, and GPS navigation module 10 is increased into extraction by Carbon fibe pipe 9, has isolated winged control and system
Signal interference caused by signal, Carbon fibe pipe 9 are arranged with screw threads for fastening button 8, the one end of Carbon fibe pipe 9 and screw threads for fastening button 8
It is connected, facilitates body cover 3 to cover tightly fastening, load 2 includes load connecting plate 19, and the side of load connecting plate 19 is provided with antenna
12, by antenna 12 and outside earth station and radio station intercommunication, data real-time, interactive is realized, undercarriage 18 is provided with around load 2,
Undercarriage 18 shares four groups, and uses aircraft aluminum matter, enhances stability during takeoff and landing, is provided with undercarriage 18 super
Sound wave module 13, by ultrasonic wave module 13, the height on actual measurement aircraft and ground.Draw off gear is provided with load connecting plate 19
14, draw off gear extension pipe 15 is connected under draw off gear 14, by the lengthening of draw off gear extension pipe 15, avoids undercarriage 18
Cause to interfere when launching lifebuoy 17, the one end of draw off gear extension pipe 15 passes through turning for draw off gear 14 equipped with folding and unfolding folder 16
16 times setting lifebuoys 17 are pressed from both sides in the dynamic folding for driving folding and unfolding folder 16, folding and unfolding, and when program, which starts, delivers, draw off gear 14, which rotates, to be made
Obtain folding and unfolding folder 16 to open, and lifebuoy 17 is effectively cast in success.
General principle, principal character and advantage of the present utility model has been shown and described above.The technical staff of the industry
It should be appreciated that the utility model is not restricted to the described embodiments, the simply explanation described in above-described embodiment and specification is originally
The principle of utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model also has various change
And improvement, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model requires protection scope
Defined by appended claims and its effect thing.
Claims (9)
1. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters, it is characterised in that：Including fuselage, load, the fuselage includes fuselage
Cover, be provided with RTK modules on the body cover, the body cover is arranged with fuselage main body, is provided with the fuselage main body
Cantilever, brushless electric machine is installed on the cantilever, blade is housed, the fuselage main body side is provided with the brushless electric machine
GPS navigation module, the GPS navigation module are arranged on a Carbon fibe pipe, and the Carbon fibe pipe is arranged with screw threads for fastening
Button, the load include load connecting plate, are provided with antenna beside the load connecting plate, are provided with and rise and fall around the load
Frame, ultrasonic wave module is installed under the undercarriage, is provided with draw off gear on the load connecting plate, under the draw off gear
Draw off gear extension pipe is connected to, described draw off gear extension pipe one end presss from both sides equipped with folding and unfolding, and the folding and unfolding folder is lower to set lifebuoy.
2. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：The RTK modules
It is arranged on the body cover, the RTK modules are connected by screw with the body cover, and tail end is provided with lock structure, institute
State body cover and form flip structure with the fuselage main body.
3. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：It is provided with four institutes
Cantilever, one brushless electric machine of every installation are stated, four cantilevers are integrally formed with the fuselage main body, and material is Carbon fiber
Dimension.
4. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：The fuselage main body
Side is provided with GPS navigation module, and the GPS navigation module is linked to be one by the Carbon fibe pipe and the screw threads for fastening button
Body.
5. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：The load connection
Plate is equipped with the draw off gear and the antenna.
6. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：The draw off gear
One entirety is linked to be by the draw off gear extension pipe and folding and unfolding folder, the draw off gear and the brushless electric machine pass through
Unmanned machine battery is integrally powered.
7. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：Under the folding and unfolding folder
Clip the lifebuoy.
8. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：The undercarriage is total to
There are four groups, and use aircraft aluminum matter.
9. four rotor wing unmanned aerial vehicles are rescued in a kind of public security waters according to claim 1, it is characterised in that：Under the undercarriage
Side is equipped with the ultrasonic wave module, surveys the height on aircraft and ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721219362.5U CN207191432U (en) | 2017-09-22 | 2017-09-22 | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721219362.5U CN207191432U (en) | 2017-09-22 | 2017-09-22 | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207191432U true CN207191432U (en) | 2018-04-06 |
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ID=61786648
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721219362.5U Active CN207191432U (en) | 2017-09-22 | 2017-09-22 | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436246A (en) * | 2018-11-12 | 2019-03-08 | 黄永文 | A kind of water survival is anti-to be trembled around lock unmanned plane |
| CN109436245A (en) * | 2018-11-12 | 2019-03-08 | 黄永文 | A kind of water survival is anti-to be trembled around lock unmanned plane |
| CN110104138A (en) * | 2019-04-26 | 2019-08-09 | 山东理工职业学院 | A kind of waters deliverance apparatus |
| CN111661280A (en) * | 2020-06-03 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Be applied to unmanned aerial vehicle rescue device of emergent relief of disaster |
| WO2022110240A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Unmanned aerial vehicle for water rescue |
-
2017
- 2017-09-22 CN CN201721219362.5U patent/CN207191432U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109436246A (en) * | 2018-11-12 | 2019-03-08 | 黄永文 | A kind of water survival is anti-to be trembled around lock unmanned plane |
| CN109436245A (en) * | 2018-11-12 | 2019-03-08 | 黄永文 | A kind of water survival is anti-to be trembled around lock unmanned plane |
| CN109436245B (en) * | 2018-11-12 | 2020-11-06 | 中枢物联网科技(嘉兴)有限公司 | Anti lock unmanned aerial vehicle that winds of trembling of lifesaving on water |
| CN110104138A (en) * | 2019-04-26 | 2019-08-09 | 山东理工职业学院 | A kind of waters deliverance apparatus |
| CN111661280A (en) * | 2020-06-03 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Be applied to unmanned aerial vehicle rescue device of emergent relief of disaster |
| WO2022110240A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Unmanned aerial vehicle for water rescue |
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