CN204452938U - Flying platform is searched and rescued in low latitude - Google Patents
Flying platform is searched and rescued in low latitude Download PDFInfo
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- CN204452938U CN204452938U CN201520094161.1U CN201520094161U CN204452938U CN 204452938 U CN204452938 U CN 204452938U CN 201520094161 U CN201520094161 U CN 201520094161U CN 204452938 U CN204452938 U CN 204452938U
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Abstract
A kind of low latitude is searched and rescued flying platform and is comprised umbrella wing system, and be connected with skeleton below it, this skeleton be provided with passenger cabin system, Landing Gear System, direction control system and emergency survival system, its rear portion is provided with power system, and front portion is provided with communication control system; Life checking system; Shielded frame; GPS position fixing system; And ground receiving station, wherein, described GPS position fixing system is connected with Communication Control system with life checking system, and described communication control system is connected with ground receiving station communication.This flying platform have maneuvering performance good, fly flexible, simple to operate, safe and reliable, the GPS position information collected and vital sign information are real-time transmitted to ground receiving station through communication facilities by the microcontrol processor of flying platform system, ground rescue group after learning the location information of disaster affected people, thus can implement to rescue timely.
Description
Technical field
The utility model belongs to life and searches and rescues field, and particularly flying platform is searched and rescued in a kind of low latitude.
Background technology
In recent years, the accidents such as the disaster of China, all kinds of Accidents Disasters happen occasionally, because the geographical environmental condition in disaster scenes such as earthquakes is severe, space constraint is larger, the aerocraft being similar to helicopter cannot perform to respective advantage, thus directly can have influence on the efficiency of ground rescue.
Therefore, in order to solve many deficiencies and the defect of above-mentioned prior art, be necessary that studying a kind of low latitude searches and rescues flying platform.
Utility model content
Consider at least one the problems referred to above and complete the utility model, and an object of the present utility model is to provide a kind of low latitude to search and rescue flying platform, the soft vane-type aircraft that flying platform have employed suitable low-latitude flying is searched and rescued in this low latitude, and be equipped with life check implement, when system flies over search and rescue region, the vital sign information collected by microcontrol processor and GPS position information, through communication device transfers to ground receiving station, be convenient to catch wounded position in time effectively to be rescued.Wherein, flying platform is searched and rescued in this low latitude, it is characterized in that comprising:
Umbrella wing system, is connected with skeleton below it, this skeleton is provided with passenger cabin system, Landing Gear System, direction control system and emergency survival system, and its rear portion is provided with power system, and front portion is provided with communication control system;
Life checking system;
Shielded frame;
GPS position fixing system; With
Ground receiving station, wherein, described GPS position fixing system is connected with communication control system with life checking system, and described communication control system is connected with ground receiving station communication.
This flying platform has that maneuvering performance is good, many advantages such as flexible, simple to operate, safe and reliable of flying, many fields such as it also can be applicable to take photo by plane, forest monitoring, electric inspection process, agricultural are sowed.Its flight theory depends on the power propeller increased at the afterbody of parasol, when platform along ground short-range slide lift-off after, aircraft is then against the thrust flight forward of motor, and the direction controlling of flight can be controlled the receipts of parafoil operating rope by direction control system such as left and right pedal rod or be put realization.Aircraft in flight course, its flight speed, or fall can by adjustment power motor throttle control.
According to the utility model on the other hand, described life checking system is connected with GPS position fixing system.
According to the utility model on the other hand, described flying platform also comprises display unit, and this display unit is connected with life checking system.
According to the utility model on the other hand, with the human life characteristic matching prestored after described life checking system detects vital signs, after the match is successful, control described flying platform by direction control system and again search this position, just corresponding GPS information is sent to communication control system when twice search result is consistent.
According to the utility model on the other hand, described GPS information is sent to ground receiving station by described communication control system.
Compared with prior art, the beneficial effects of the utility model are:
Flight job platform maneuvering performance, stability and aeroperformance are all relatively good, and its coasting distance taken off is short, and can carry out extreme low-altitude job task very easily; This search and rescue flight system performs in low latitude search and rescue task at search and rescue region, when detecting device detects the relevant information of vital sign, control system will the vital sign data collected and corresponding GPS position information real-time Transmission to ground rescue group, thus disaster affected people is rescued timely, also improve the efficiency that ground is searched and rescued simultaneously.
Accompanying drawing explanation
Fig. 1 is the structural representation of searching and rescuing flying platform according to the low latitude of the utility model preferred embodiment.
Fig. 2 is the fundamental diagram of searching and rescuing flying platform according to the low latitude of another preferred embodiment of the utility model.
In figure, 1. umbrella wing system, 2. life checking system, 3. power system, 4. passenger cabin system, 5. Landing Gear System, 6. emergency survival system, 7. directional control pedals rod, 8. communication control system, 9. shielded frame, 10.GPS position fixing system.
Detailed description of the invention
Below in conjunction with accompanying drawing; by preferred embodiment, preferred forms of the present utility model is described; here detailed description of the invention is to explain the utility model; and should not be construed as restriction of the present utility model; when not departing from spirit of the present utility model and essential scope; can make various changes and modifications, these all should be included within protection domain of the present utility model.
Embodiment 1
See Fig. 1-2, the utility model provides a kind of low latitude and searches and rescues flying platform.Such as, this low latitude is searched and rescued flying platform and can be comprised: umbrella wing system 1, is connected with skeleton below it, this skeleton is provided with passenger cabin system 4, Landing Gear System 5, direction control system 7 and emergency survival system 6, its rear portion is provided with power system 3, and front portion is provided with communication control system 8; Life checking system 2; Shielded frame 9; GPS position fixing system 10; And ground receiving station, wherein, described GPS position fixing system 10 is connected with communication control system 8 with life checking system 2, and described communication control system 8 is connected with ground receiving station communication.
This flying platform has that maneuvering performance is good, many advantages such as flexible, simple to operate, safe and reliable of flying, many fields such as it also can be applicable to take photo by plane, forest monitoring, electric inspection process, agricultural are sowed.Its flight theory depends on the power propeller increased at the afterbody of parasol, when platform along ground short-range slide lift-off after, aircraft is then against the thrust flight forward of motor, and the direction controlling of flight can be controlled the receipts of parafoil operating rope by direction control system such as left and right pedal rod or be put realization.Aircraft in flight course, its flight speed, or fall can by adjustment power motor throttle control.
Preferably, described life checking system 2 is connected with GPS position fixing system 10, with the human life characteristic matching prestored after described life checking system 2 detects vital signs, after the match is successful, just excite GPS position fixing system 10 that GPS information is sent to communication control system.
Preferably, described flying platform also comprises display unit, and this display unit is connected with life checking system 2, with the human life characteristic matching prestored after described life checking system detects vital signs, shows on the display unit after the match is successful.
Preferably, with the human life characteristic matching prestored after described life checking system 2 detects vital signs, after the match is successful, control described flying platform by direction control system and again search this position, just corresponding GPS information is sent to communication control system when twice search result is consistent.
Preferably, described GPS information is sent to ground receiving station by described communication control system 8.
Preferably, after power system 3 startup of aircraft, the lift of the thrust that motor produces and parafoil 1 can make whole flight system go up to the air along the distance that ground taxi one is shorter, and the heading after lift-off and attitude are pedaled rod 7 about can being trampled by pin and regulated.In flight course, life check implement 2 detects the ground life-information below flight site in real time, go to navigate to by GPS position fixing system 10 position that vital sign information occurs, then gather its vital signs information and location information through communication control system 8 and be transmitted to ground receiving station, when ground rescue group receives rescue location information, disaster-stricken location site can be arrived in timely, thus improve the rescue efficiency after calamity.
In Fig. 2, after life detection equipment senses the electric field that human body ulf electric wave is formed, communication control system passes to ground station under gathering the locating information of this information and GPS.
Preferably, additionally provide a kind of low latitude and search and rescue flying platform, be the flight system carrying GPS position fixing system and life check implement, its composition includes umbrella wing system 1, life checking system 2, power system 3, passenger cabin system 4, Landing Gear System 5, emergency survival system 6, direction control system 7, communication control system 8, shielded frame 9 and GPS position fixing system 10.
Be understandable that, the utility model employing maneuvering performance is good, safety is high, be suitable for the flying platform of the advantage such as hedgehopping and flexible operation, and carry GPS position fixing system, life check implement and other communication facilitiess on board the aircraft.GPS position fixing system is used in real time location and searches and rescues the location information of point, and life check implement is used for detecting the vital sign information of searching and rescuing point in real time, and communication facilities is used for the mutual of aerial and ground data.Carry out in search and rescue process at search and rescue region, the GPS position information collected and vital sign information are real-time transmitted to ground receiving station through communication facilities by the microcontrol processor of searching and rescuing flying platform system, ground rescue group after learning the location information of disaster affected people, thus can implement to rescue timely.
The utility model is not limited to above-mentioned specific embodiment.Be understandable that, when not departing from spirit of the present utility model and essential scope, can make various changes and modifications, these all should be included within protection domain of the present utility model.
Claims (3)
1. a flying platform is searched and rescued in low latitude, it is characterized in that comprising:
Umbrella wing system, is connected with skeleton below it, this skeleton is provided with passenger cabin system, Landing Gear System, direction control system and emergency survival system, and its rear portion is provided with power system, and front portion is provided with communication control system;
Life checking system;
Shielded frame;
GPS position fixing system; With
Ground receiving station, wherein, described GPS position fixing system is connected with communication control system with life checking system, and described communication control system is connected with ground receiving station communication.
2. flying platform is searched and rescued in low latitude according to claim 1, it is characterized in that described life checking system is connected with GPS position fixing system.
3. flying platform is searched and rescued in low latitude according to claim 2, and it is characterized in that described flying platform also comprises display unit, this display unit is connected with life checking system.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520094161.1U CN204452938U (en) | 2015-02-10 | 2015-02-10 | Flying platform is searched and rescued in low latitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520094161.1U CN204452938U (en) | 2015-02-10 | 2015-02-10 | Flying platform is searched and rescued in low latitude |
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| CN204452938U true CN204452938U (en) | 2015-07-08 |
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| CN201520094161.1U Active CN204452938U (en) | 2015-02-10 | 2015-02-10 | Flying platform is searched and rescued in low latitude |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104608929A (en) * | 2015-02-10 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Low-altitude rescue flight platform |
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2015
- 2015-02-10 CN CN201520094161.1U patent/CN204452938U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104608929A (en) * | 2015-02-10 | 2015-05-13 | 襄阳宏伟航空器有限责任公司 | Low-altitude rescue flight platform |
| CN104608929B (en) * | 2015-02-10 | 2016-09-07 | 襄阳宏伟航空器有限责任公司 | Flying platform is searched and rescued in low latitude |
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