CN207366742U - A kind of life-detection system based on unmanned plane - Google Patents
A kind of life-detection system based on unmanned plane Download PDFInfo
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- CN207366742U CN207366742U CN201721268136.6U CN201721268136U CN207366742U CN 207366742 U CN207366742 U CN 207366742U CN 201721268136 U CN201721268136 U CN 201721268136U CN 207366742 U CN207366742 U CN 207366742U
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Abstract
The utility model belongs to unmanned plane applied technical field; specifically provide a kind of life-detection system based on unmanned plane; life-information after calamity is detected by radar life-detection instrument of the carry on unmanned plane, is made of six rotor wing unmanned aerial vehicles, GPS module, protective cradle, radar life-detection instrument, antenna, unmanned controller, posture display, Minitype hand-held computer controller.Solve the problems, such as in rescue and relief work that artificial detection efficient is low, danger zone rescue personnel is unable to reach, it is convenient, efficient, accurate to have the advantages that.
Description
Technical field
The utility model belongs to unmanned plane applied technical field, specifically provides and is given birth to by radar of the carry on unmanned plane
Life survey meter detects life-information after calamity, solve in rescue and relief work artificial detection efficient lowly, danger zone rescue personnel
Problem is unable to reach, saves rescue personnel, improves rescue efficiency, it is convenient, efficient, accurate to have the characteristics that.
Background technology
The life-detection system detects life-information after calamity by radar life-detection instrument of the carry on unmanned plane, solves
Manually detection efficient of having determined in rescue work is low, danger zone rescue personnel is unable to reach problem, avoids causing second accident,
Rescue personnel is saved, improves rescue efficiency.
In traditional Post disaster relief work, the generally hand-held life-detection instrument of rescue personnel carries out life detection, so not
Substantial amounts of manpower and materials, and inefficiency are only expended, the region rescue personnel of some of complex danger is difficult to reach, or even causes
Second accident, consumes the rescue time of preciousness.Recently as the fast development of unmanned plane so that in emergency repair rescue all
It can see the figure of unmanned plane.But unmanned plane is mainly used for surveying overall condition in work at present, afterwards further according to overall feelings
Condition formulates rescue method.Life-detection instrument is still carried by rescue personnel mostly, does not improve rescue efficiency fundamentally.
For such case, radar life-detection instrument of the present invention by carry on unmanned plane is special to detect life after calamity
Sign, its result of detection can real-time Transmission give Minitype hand-held computer controller.User when in use, is responsible for manipulation six by a people respectively
Rotor wing unmanned aerial vehicle and a people are responsible for operational observations Minitype hand-held computer controller, using unmanned plane is portable, maneuverability, is applicable in model
The characteristics of wide is enclosed, efficient and accurate life detection can be carried out to calamity rear region, finds vital signs at the first time, meanwhile,
It can be detected with round-the-clock running, save the rescue time of preciousness.User can set automatic covering by unmanned controller
Scan pattern, the pattern can carry out specific region blanket type scanning.Solve in rescue work that artificial detection efficient is low, danger
Danger zone domain rescue personnel is unable to reach problem, avoids causing second accident, and it is convenient, efficient, accurate to have the characteristics that.
Utility model content
The utility model solves artificial detection efficient in earthquake relief, and lowly and in danger zone disaster relief personnel can not reach
To the problem of.
For this reason, the utility model provides a kind of life-detection system based on unmanned plane, including：Six rotor wing unmanned aerial vehicles,
GPS module, radar life-detection instrument, protective cradle, antenna, unmanned controller, posture display, the control of Minitype hand-held computer
Device.Wherein, GPS module is installed at the top of six rotor wing unmanned aerial vehicles；Protective cradle is used for placing and protecting radar life-detection instrument；My god
Line is installed on unmanned plane machine frame inside；Unmanned controller is used for operating six rotor wing unmanned aerial vehicles, its top posture display can be with
Real-time display items flying quality；Minitype hand-held computer controller can control and receive the detection of radar life-detection instrument to believe
Number.
The operating frequency of antenna is 2.4GHz, gain 5dB.
The GPS module selects NEO-6M modules, positioning accuracy 5m.
The protective cradle is made of elastomeric material.
The radar life-detection instrument detection range is 30m.
The Minitype hand-held computer controller is connected with control radar life-detection instrument by radio.
The beneficial effects of the utility model：Including six rotor wing unmanned aerial vehicles, GPS module, protective cradle, radar life detection
Instrument, antenna, unmanned controller, posture display, Minitype hand-held computer controller composition.Can at any time, everywhere with it is round-the-clock into
Row life detection, and specific region can be scanned by blanket type automatically, human resources are saved, solve hazardous area in earthquake relief
The problem of domain personnel are unable to reach, detection efficient is low.
The present invention is described in further details below with reference to attached drawing.
Brief description of the drawings
Fig. 1 is the utility model embodiment principle schematic diagram；
Fig. 2 is the unmanned plane partial schematic diagram of Fig. 1；
Fig. 3 is control and the monitoring side schematic diagram of Fig. 1.
1 description of symbols of attached drawing：1st, six rotor wing unmanned aerial vehicle；2nd, GPS module；3rd, radar life-detection instrument；4th, protective cradle；5、
Antenna；6th, unmanned controller；7th, posture display；8th, Minitype hand-held computer controller.
Embodiment
As shown in Figure 1, Figure 2 and Figure 3, it is a kind of structure diagram of the life-detection system based on unmanned plane, including：Six
Rotor wing unmanned aerial vehicle 1, GPS module 2, radar life-detection instrument 3, protective cradle 4, antenna 5, unmanned controller 6, posture display
7th, Minitype hand-held computer controller 8.Wherein, GPS module 2 is installed on the top of six rotor wing unmanned aerial vehicle 1；Protective cradle 4 is used for placing
And protect radar life-detection instrument 3；Antenna 5 is installed on unmanned plane machine frame inside；Unmanned controller 6 be used for operate six rotors without
Man-machine 1, its top posture display 7 can be with real-time display items flying quality；Minitype hand-held computer controller 8 can control and
Receive the detectable signal of radar life-detection instrument 3.
5 working frequency of antenna is 2.4GHz, gain 5dB.
The GPS module 2 selects NEO-6M modules, and positioning accuracy is not more than 5m.
The protective cradle 4 is made of elastomeric material.
3 detection range of radar life-detection instrument is 30m.
The Minitype hand-held computer controller 8 is connected with control radar life-detection instrument 3 by radio.
Six rotor wing unmanned aerial vehicles 1 have long endurance, medium negative using six axis power suit of SIGMA Summit SS6P-ARF1
The characteristics of carrying with the operation of a variety of environment；GPS module 2 uses outstanding science and technology GPS-G2；Radar life-detection instrument 3 uses LEADER
The SDHT16S351S000S2584 radar detection apparatus of Scan；User need first to be respectively started when in use unmanned controller 6,
Six rotor wing unmanned aerial vehicles 1, wait posture display 7 successful connection occur；Compass calibration operation must be carried out after successful connection：Hand
Six rotor wing unmanned aerial vehicle 1 liftoff 1~2 meter is held, keeps horizontal attitude to rotate horizontally 360 degree, keep vertical posture horizontal rotation respectively
360 degree, until (for the sake of safety, GPS signal strength need to be more than 9 can just take off normal display gps signal, no in posture display 7
It can not then ensure positioning and the hovering function of six rotor wing unmanned aerial vehicles 1)；Radar life-detection instrument 3 is opened, waits Minitype hand-held computer
Controller 8 and 3 successful match of radar life-detection instrument；Radar life-detection instrument 3 is positioned in protective cradle 4, you can take off
Detection；After taking off, result of detection can be observed by Minitype hand-held computer controller 8, can then start alarm if any vital signs
Notification mechanisms；User can manipulate unmanned plane during flying state by unmanned controller 5, and can set automatic covering scanning mould
Formula, the pattern can pair radius X (<=5) carry out blanket type scanning in kilometer range, user can to the sweep speed of aircraft,
Height is configured (this function uses the preceding building or other objects that need to be ensured surrounding and be not above set flying height) respectively.
Solve the problems, such as that danger zone personnel are unable to reach in earthquake relief, detection efficient is low, have convenient, efficient, accurate
Feature.
The foregoing examples are only illustrative of the present invention, does not form the limitation to protection scope of the present invention, all
It is to be belonged to the same or similar design of the present invention within protection scope of the present invention.
Claims (6)
- A kind of 1. life-detection system based on unmanned plane, it is characterised in that including：Six rotor wing unmanned aerial vehicles (1), GPS module (2), Radar life-detection instrument (3), protective cradle (4), antenna (5), unmanned controller (6), posture display (7), Minitype hand-held Computer controller (8)；Wherein, GPS module (2) is installed at the top of six rotor wing unmanned aerial vehicles (1)；Protective cradle (4) is used for placing simultaneously Protect radar life-detection instrument (3)；Antenna (5) is installed on unmanned plane machine frame inside；Unmanned controller (6) is used for operating six rotations Wing unmanned plane (1), its top posture display (7) can be with real-time display items flying quality；Minitype hand-held computer controller (8) It can control and receive the detectable signal of radar life-detection instrument (3).
- A kind of 2. life-detection system based on unmanned plane according to claim 1, it is characterised in that：The antenna (5) working frequency is 2.4GHz, gain 5dB.
- A kind of 3. life-detection system based on unmanned plane according to claim 1, it is characterised in that：The GPS moulds Block (2) selects NEO-6M modules, and positioning accuracy is not more than 5m.
- A kind of 4. life-detection system based on unmanned plane according to claim 1, it is characterised in that：The protection branch Frame (4) is made of elastomeric material.
- A kind of 5. life-detection system based on unmanned plane according to claim 1, it is characterised in that：The radar life It is 30m to order survey meter (3) detection range.
- A kind of 6. life-detection system based on unmanned plane according to claim 1, it is characterised in that：The miniature hand Computer controller (8) is held to connect by radio with control radar life-detection instrument (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721268136.6U CN207366742U (en) | 2017-09-29 | 2017-09-29 | A kind of life-detection system based on unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721268136.6U CN207366742U (en) | 2017-09-29 | 2017-09-29 | A kind of life-detection system based on unmanned plane |
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| Publication Number | Publication Date |
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| CN207366742U true CN207366742U (en) | 2018-05-15 |
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| CN201721268136.6U Active CN207366742U (en) | 2017-09-29 | 2017-09-29 | A kind of life-detection system based on unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107526078A (en) * | 2017-09-29 | 2017-12-29 | 蒙城县永腾微行掌智能科技有限责任公司 | A kind of life-detection system based on unmanned plane |
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2017
- 2017-09-29 CN CN201721268136.6U patent/CN207366742U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107526078A (en) * | 2017-09-29 | 2017-12-29 | 蒙城县永腾微行掌智能科技有限责任公司 | A kind of life-detection system based on unmanned plane |
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Address after: 233500 South District of Mengcheng County Economic Development Zone, Bozhou City, Anhui Province, East of Jingwu Road Patentee after: Mengcheng Yongshun Intelligent Technology Co., Ltd. Address before: 233500 South District of Mengcheng County Economic Development Zone, Bozhou City, Anhui Province, East of Jingwu Road Patentee before: Mengcheng Yongteng incog palm intelligent technology limited liability company |