CN208198834U - A kind of height rescue unmanned plane - Google Patents
A kind of height rescue unmanned plane Download PDFInfo
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- CN208198834U CN208198834U CN201820321637.4U CN201820321637U CN208198834U CN 208198834 U CN208198834 U CN 208198834U CN 201820321637 U CN201820321637 U CN 201820321637U CN 208198834 U CN208198834 U CN 208198834U
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- unmanned plane
- height rescue
- fuselage
- rescue unmanned
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- 238000005266 casting Methods 0.000 claims abstract description 27
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 4
- 239000000956 alloy Substances 0.000 claims description 3
- 238000005452 bending Methods 0.000 claims 1
- 239000005357 flat glass Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000009435 building construction Methods 0.000 description 1
- 239000006063 cullet Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000005341 toughened glass Substances 0.000 description 1
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Abstract
A kind of height rescue unmanned plane, the height rescue unmanned plane includes: fuselage；Saving casting device is connect with the fuselage, and high-pressure aerated bottle is equipped in the saving casting device；By object of jettisoninging, it is connect with the high-pressure aerated bottle；And trigger device, it is connect with the fuselage, the trigger device is arranged to trigger the saving casting device after receiving trigger signal and discharges the high-pressure aerated bottle and described by object of jettisoninging.User can discharge high-pressure aerated bottle in the trigger device on terrestrial operation remote control control unmanned plane, and high-pressure aerated bottle carries object homed on its target position of being jettisoninged, buoyant apparatus of jettisoninging into high-altitude floor.
Description
Technical field
The utility model relates to height rescue apparatus technical fields, and in particular to a kind of height rescue unmanned plane.
Background technique
Currently, urban building construction is higher and higher, to fire-fighting equipment, more stringent requirements are proposed, common aerial ladder and fire-fighting
Vehicle can not arrive at higher floor.With the development of technology, it integrates using unmanned plane or flexibly carries crucial equipment and equip, energy
Enough help is provided for the rescue in a variety of situations.For example, opening up rescue approach using unmanned plane.Existing saving casting device use environment
There is significant limitation with range, and precision is poor, using rescue unmanned plane auxiliary shooting rope or carries crucial equipment (such as
Respirator, rescue rope etc.), new approach can be created for rescue, open up escape and rescue trunk, and accurate, high efficiency.
The height rescue unmanned plane of above-mentioned crucial equipment can be launched as urgently to be resolved to high-altitude floor by designing one kind
Technical problem.
Summary of the invention
The purpose of the utility model is to provide a kind of height rescue unmanned planes, solve and are difficult in the prior art to height
Empty floor launches the technical issues of crucial equipment, realizes and accurately and efficiently launches crucial equipment to high-altitude floor.
In order to solve the above technical problems, the utility model adopts the following technical solutions: a kind of height rescue unmanned plane, institute
Stating height rescue unmanned plane includes: fuselage；Saving casting device is connect with the fuselage, and high-pressure aerated bottle is equipped in the saving casting device；Quilt
It jettisonings object, is connect with the high-pressure aerated bottle；And trigger device, the trigger device are connect with the fuselage, the triggering dress
It sets and is arranged to trigger the saving casting device after receiving trigger signal and discharges the high-pressure aerated bottle and described by object of jettisoninging.
Preferably, the object of being jettisoninged is grasp, and the grasp includes anchor body, and rear end and the high pressure of the anchor body are filled
Gas cylinder connection, the front of the anchor body are equipped with the hook-shape body of multiple lateral bends backward, and the front end of the anchor body is equipped with the broken of taper
Broken portion.
Preferably, the broken portion is titanium alloy material.
Preferably, the saving casting device has trigger, and the trigger device includes: supporting element, is connect with the fuselage；It swings
Bar, one end of the oscillating rod and the supporting element are pivotally connected, and the other end of the oscillating rod is equipped with locking portion；Steering engine, the rudder
Machine is connect with the supporting element, and the steering engine is connect with the locking portion, and the steering engine is arranged to receive the triggering letter
The locking portion is discharged after number；And elastic component, one end are connect with the supporting element, the other end is connect with the oscillating rod, works as institute
After stating the steering engine release locking portion, the elastic component is used to provide the power of triggering trigger to the oscillating rod.
Preferably, the saving casting device includes: gun body and accommodating storehouse, and the accommodating storehouse is set to the upside of the gun body, described
It accommodates and is equipped with rescue rope in storehouse, the rescue rope is connect with the grasp.
Preferably, the rear end of the anchor body is equipped with connector sleeve, and the connector sleeve and the high-pressure aerated bottle cover are closed and connected.
Preferably, the supporting element includes first support and second support, the first support and the second support
Upper end is connect with the fuselage, and the fixing end of the oscillating rod and the first support are pivotally connected, the steering engine with described second
Frame connection.
Preferably, the second support forms guide space by folded sheet, and the free end of the oscillating rod is set to described
In guide space.
Preferably, it is set on the downside of the fuselage there are two foot prop, the saving casting device is set between two foot props.
Preferably, the height rescue unmanned plane further includes camera, and the camera is connect with the fuselage.
Compared with prior art, the technical solution of the utility model embodiment has the advantages that user can be
Trigger device on terrestrial operation remote control control unmanned plane discharges high-pressure aerated bottle, and high-pressure aerated bottle carries object directive of being jettisoninged
Target position, buoyant apparatus of jettisoninging into high-altitude floor；User can obtain the image of target position by camera, accurately
Buoyant apparatus is delivered to target position；When object of being jettisoninged is grasp, the promotion of the broken portion of grasp front end in high-pressure aerated bottle
Under can be used for smashing the outer window glass of high-altitude building, and then to indoor delivery buoyant apparatus；The rear end of anchor body is equipped with connector sleeve,
Connector sleeve and the high-pressure aerated bottle cover are closed and are connected.When needing replacing high-pressure aerated bottle or replacement jettisoninged object when, use
Person, which only passes through shirtsleeve operation, can be realized purpose, saves replacing construction, improves work efficiency.
Detailed description of the invention
Fig. 1 is a kind of rearview of the height rescue unmanned plane of embodiment of the utility model；
Fig. 2 is a kind of bottom view of the height rescue unmanned plane of embodiment of the utility model；
Fig. 3 is a kind of top view of the height rescue unmanned plane of embodiment of the utility model；
Fig. 4 is a kind of left view of the height rescue unmanned plane of embodiment of the utility model；
Fig. 5 is a kind of perspective view of the height rescue unmanned plane of embodiment of the utility model；
Fig. 6 is a kind of perspective view of the height rescue unmanned plane of embodiment of the utility model；
Fig. 7 is a kind of saving casting device structural schematic diagram of the height rescue unmanned plane of embodiment of the utility model.
Fig. 8 is a kind of structural schematic diagram of the trigger device of the height rescue unmanned plane of embodiment of the utility model.
Fig. 9 is a kind of grasp of the height rescue unmanned plane of embodiment of the utility model and the connection knot of high-pressure aerated bottle
Structure schematic diagram.
Description of symbols
10 fuselage, 11 rotor
12 foot prop, 20 saving casting device
21 gun body, 211 trigger
22 accommodating 23 grasps of storehouse
231 anchor body, 232 hook-shape body
233 broken 234 connector sleeves of portion
24 trigger device, 241 oscillating rod
2411 locking portion, 242 elastic component
243 steering engine, 2431 shank
25 supporting element, 251 first support
252 second support, 2522 guide space
26 high-pressure aerated 27 rescue ropes of bottle
Specific embodiment
By explaining that the preferred embodiment of following the application, the other objects and advantages of the utility model will become clear
Chu.
As shown in Figures 1 to 4, a kind of height rescue unmanned plane, including fuselage 10, saving casting device 20, jettisoninged object and triggering
Device 24.Wherein, saving casting device 20 is connect with fuselage 10, and high-pressure aerated bottle 26 is equipped in saving casting device 20；Object and the height of being jettisoninged
Gas filling bottle 26 is pressed to connect；Trigger device 24 is connect with fuselage 10, and trigger device 24 is arranged to touch after receiving trigger signal
Hair saving casting device 20 discharges high-pressure aerated bottle 26 and described by object of jettisoninging.
User on ground can be discharged high-pressure aerated by the trigger device 24 on remote controller control unmanned plane
Bottle 26, high-pressure aerated bottle 26 carry object homed on its target position of being jettisoninged, to deliver respirator, rescue rope etc. into high-altitude floor
By object of jettisoninging.
Preferably, it is set on the downside of figure fuselage 10 there are two foot prop 12, saving casting device 20 is set between two foot props 12, unmanned plane
When in non-state of flight, foot prop 12 can fuselage 10 to unmanned plane and saving casting device 20 play a supporting role, two foot props 12
Between space play the role of accommodate saving casting device 20.
Above-mentioned height rescue unmanned plane is multi-rotor unmanned aerial vehicle, and multi-rotor unmanned aerial vehicle is that there are three revolve above for a kind of tool
The special pilotless helicopter of wing axis.It drives rotor 11 by the motor rotation on each axis, pushes away to generate and rise
Power.By changing the relative rotation speed between different rotors 11, thus it is possible to vary the size of uniaxial propulsive force, to control aircraft
Running track.
In the present embodiment, height rescue unmanned plane can also include camera, and camera is connect with fuselage 10.User can
The image of target position is obtained by camera, accurately delivers buoyant apparatus to target position.
The outer window glass of skyscraper generally uses double-deck tempered glass, needs head before above-mentioned crucial equipment of jettisoninging
First smash the outer window glass of building.In order to smash the outer window glass of skyscraper, as preferred embodiment, such as Fig. 5 to Fig. 7
Shown, object of being jettisoninged is grasp 23, and grasp 23 includes anchor body 231, and the rear end of anchor body 231 is connect with high-pressure aerated bottle 26, anchor body
231 front is equipped with the hook-shape body 232 of multiple lateral bends backward, and the front end of anchor body 231 is equipped with the broken portion 233 of taper.
Preferably, being crushed portion 233 is titanium alloy material, and titanium alloy has the characteristics that light-weight and intensity is high, hits in satisfaction
While cullet mechanical property requirements, the load of unmanned plane is alleviated.
In the present embodiment, as shown in figure 9, the rear end of anchor body 231 is equipped with connector sleeve 234, connector sleeve 234 and high-pressure aerated bottle
The connection of 26 fittings.When needing replacing high-pressure aerated bottle 26 or replacement jettisoninged object when, user only passes through shirtsleeve operation
Purpose can be realized, save replacing construction, improve work efficiency.
As shown in Figure 7 and Figure 8, saving casting device 20 has trigger 211, in order to realize the purpose of operating trigger 211, correspondingly,
Trigger device 24 includes supporting element 25, oscillating rod 241, steering engine 243 and elastic component 242；Wherein, supporting element 25 and fuselage 10 connect
It connects；One end of oscillating rod 241 and supporting element 25 are pivotally connected, and the other end of oscillating rod 241 is equipped with locking portion 2411；Steering engine 243 and branch
Support member 25 connects, and steering engine 243 is connect with locking portion 2411, and steering engine 243 is arranged to discharge locking portion after receiving trigger signal
2411；242 one end of elastic component is connect with supporting element 25, and the other end is connect with oscillating rod 241, when steering engine 243 discharges locking portion
After 2411, elastic component 242 is used to provide the power of triggering trigger 211 to oscillating rod.
As preferred embodiment, as shown in figure 8, supporting element 25 includes first support 251 and second support 252, first
The upper end of bracket 251 and second support 252 is connect with fuselage 10, and the fixing end and first support 251 of oscillating rod 241 are pivotally connected, rudder
Machine 243 is connect with second support 252.
Further, as shown in figure 8, second support 252 forms guide space 2522 by folded sheet, oscillating rod 241
Free end is set in guide space 2522.
As shown in figure 8, steering engine 243 is equipped with a telescopic shank 2431, above-mentioned locking portion 2411 has through-hole, pin
Body 2431 can pass through through-hole and lock the free end of oscillating rod 241.
Preferably, above-mentioned elastic component 242 is tension spring, one end of tension spring is connect with oscillating rod 241, the other end of tension spring
It is connect with second support 252.
The working principle of the present embodiment is: can make locking portion 2411 and the pin of oscillating rod 241 by rotating oscillating rod 241
The sealed connection of body 2431, tension spring are elongated.When needing to discharge high-pressure aerated bottle 26, user's remote controller is sent to unmanned plane
Release signal, after unmanned plane receives above-mentioned release signal, controller controls steering engine 243 for shank 2431 from locking portion
It is pulled out at 2411, locking portion 2411 is released.Tension spring pulls oscillating rod 241 to swing, so that oscillating rod 241 pushes trigger 211 to move
Dynamic, saving casting device 20 discharges high-pressure aerated bottle 26.High-pressure aerated bottle 26 sprays gas outward, and the grasp 23 for carrying its front end is penetrated outward
Out, achieve the purpose that brokenly window.
As preferred embodiment, as shown in fig. 7, saving casting device 20 includes gun body 21 and accommodating storehouse 22, accommodating storehouse 22 is set to
The upside of gun body 21, accommodating are equipped with rescue rope 27 in storehouse 22, and rescue rope 27 is connect with grasp 23.When grasp 23 projects, grasp
23 carry rescue rope 27 projects outward, and trapped person can obtain the relief goods such as descending lifeline from ground by rescue rope 27.
In the present invention, term " multiple " then refers to two or more, unless otherwise restricted clearly.Term
The terms such as " installation ", " connected ", " connection ", " fixation " shall be understood in a broad sense, for example, " connection " may be a fixed connection,
It can be and be detachably connected, or be integrally connected；" connected " can be directly connected, and can also pass through the indirect phase of intermediary
Even.For the ordinary skill in the art, it can understand above-mentioned term in the present invention as the case may be
Concrete meaning.
In the present invention, the description of term " one embodiment ", " some embodiments ", " specific embodiment " etc. means
Particular features, structures, materials, or characteristics described in conjunction with this embodiment or example are contained at least one reality of the utility model
It applies in example or example.In the present specification, schematic expression of the above terms are not necessarily referring to identical embodiment or reality
Example.Moreover, the particular features, structures, materials, or characteristics of description can be in any one or more embodiment or examples to close
Suitable mode combines.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the utility model, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on should be included within the scope of protection of this utility model.
Claims (10)
1. a kind of height rescue unmanned plane, which is characterized in that the height rescue unmanned plane includes:
Fuselage；
Saving casting device is connect with the fuselage, and high-pressure aerated bottle is equipped in the saving casting device；
By object of jettisoninging, it is connect with the high-pressure aerated bottle；And
Trigger device is connect with the fuselage, and the trigger device is arranged to trigger the throwing after receiving trigger signal
It throws device and discharges the high-pressure aerated bottle and described by object of jettisoninging.
2. height rescue unmanned plane according to claim 1, which is characterized in that the object of being jettisoninged is grasp, the anchor
Hook includes anchor body, and the rear end of the anchor body is connect with the high-pressure aerated bottle, and the front of the anchor body is equipped with multiple lateral bendings backward
Bent hook-shape body, the front end of the anchor body are equipped with the broken portion of taper.
3. height rescue unmanned plane according to claim 2, which is characterized in that the broken portion is titanium alloy material.
4. height rescue unmanned plane according to claim 1, which is characterized in that the saving casting device has trigger, the touching
Transmitting apparatus includes:
Supporting element is connect with the fuselage；
Oscillating rod, one end of the oscillating rod and the supporting element are pivotally connected, and the other end of the oscillating rod is equipped with locking portion；
Steering engine, the steering engine are connect with the supporting element, and the steering engine is connect with the locking portion, and the steering engine is arranged to connect
The locking portion is discharged after receiving the trigger signal；And
Elastic component, one end are connect with the supporting element, and the other end is connect with the oscillating rod, when the steering engine discharges the locking
Behind portion, the elastic component is used to provide the power of triggering trigger to the oscillating rod.
5. height rescue unmanned plane according to claim 2, which is characterized in that the saving casting device includes:
Gun body；With
Storehouse is accommodated, set on the upside of the gun body, rescue rope is equipped in the accommodating storehouse, the rescue rope and the grasp connect
It connects.
6. height rescue unmanned plane according to claim 2, which is characterized in that the rear end of the anchor body is equipped with connector sleeve,
The connector sleeve and the high-pressure aerated bottle cover are closed and are connected.
7. height rescue unmanned plane according to claim 4, which is characterized in that the supporting element includes first support and
The upper end of two brackets, the first support and the second support is connect with the fuselage, the fixing end of the oscillating rod and institute
First support pivot joint is stated, the steering engine is connect with the second support.
8. height rescue unmanned plane according to claim 7, which is characterized in that the second support is formed by folded sheet
The free end of guide space, the oscillating rod is set in the guide space.
9. height rescue unmanned plane according to claim 1, which is characterized in that it is set on the downside of the fuselage there are two foot prop,
The saving casting device is set between two foot props.
10. height rescue unmanned plane as claimed in any of claims 1 to 9, which is characterized in that the height rescue
Unmanned plane further includes camera, and the camera is connect with the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820321637.4U CN208198834U (en) | 2018-03-08 | 2018-03-08 | A kind of height rescue unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820321637.4U CN208198834U (en) | 2018-03-08 | 2018-03-08 | A kind of height rescue unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208198834U true CN208198834U (en) | 2018-12-07 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820321637.4U Expired - Fee Related CN208198834U (en) | 2018-03-08 | 2018-03-08 | A kind of height rescue unmanned plane |
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|---|---|
| CN (1) | CN208198834U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271668A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane in waters |
| CN110271670A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane and its lifebuoy loading device in waters |
| CN111661282A (en) * | 2020-06-18 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Life buoy releasing device based on unmanned aerial vehicle |
| CN111703576A (en) * | 2020-07-21 | 2020-09-25 | 应急管理部上海消防研究所 | A side throwing device for unmanned aerial vehicle and its operation method |
| CN112278277A (en) * | 2020-11-12 | 2021-01-29 | 重庆凯创荣智能科技有限公司 | Unmanned aerial vehicle for high-rise rescue and using method thereof |
| CN112810817A (en) * | 2021-02-19 | 2021-05-18 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
-
2018
- 2018-03-08 CN CN201820321637.4U patent/CN208198834U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271668A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane in waters |
| CN110271670A (en) * | 2019-06-18 | 2019-09-24 | 深圳高度创新技术有限公司 | Rescue unmanned plane and its lifebuoy loading device in waters |
| CN110271670B (en) * | 2019-06-18 | 2024-02-20 | 深圳高度创新技术有限公司 | Water area rescue unmanned aerial vehicle and life buoy carrying device thereof |
| CN110271668B (en) * | 2019-06-18 | 2024-10-15 | 深圳高度创新技术有限公司 | Unmanned aerial vehicle for water area rescue |
| CN111661282A (en) * | 2020-06-18 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Life buoy releasing device based on unmanned aerial vehicle |
| CN111661282B (en) * | 2020-06-18 | 2021-08-17 | 河北柒壹壹玖工业自动化技术有限公司 | Life buoy releasing device based on unmanned aerial vehicle |
| CN111703576A (en) * | 2020-07-21 | 2020-09-25 | 应急管理部上海消防研究所 | A side throwing device for unmanned aerial vehicle and its operation method |
| CN112278277A (en) * | 2020-11-12 | 2021-01-29 | 重庆凯创荣智能科技有限公司 | Unmanned aerial vehicle for high-rise rescue and using method thereof |
| CN112810817A (en) * | 2021-02-19 | 2021-05-18 | 广西一号农服航空科技有限公司 | Aerial goods hook formula unmanned aerial vehicle of jettisoninging |
| CN112810817B (en) * | 2021-02-19 | 2024-09-13 | 广西一号农服航空科技有限公司 | Aerial material hook type throwing unmanned aerial vehicle |
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| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201123 Address after: 253000 high tech entrepreneurship service center B (2-209), No. 587 Jinghua Road, songguantun sub district office, Dezhou Economic and Technological Development Zone, Shandong Province Patentee after: Dezhou Green Friends Intelligent Technology Co.,Ltd. Address before: 253000 aijiafang market 11 303, songguantun sub district office, Dezhou Economic and Technological Development Zone, Shandong Province Patentee before: SHANDONG FENDOU INFORMATION TECHNOLOGY Co.,Ltd. |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181207 Termination date: 20210308 |
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| CF01 | Termination of patent right due to non-payment of annual fee |