CN207625811U - Emergency communication UAV system and emergency communication system - Google Patents
Emergency communication UAV system and emergency communication system Download PDFInfo
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- CN207625811U CN207625811U CN201721869436.XU CN201721869436U CN207625811U CN 207625811 U CN207625811 U CN 207625811U CN 201721869436 U CN201721869436 U CN 201721869436U CN 207625811 U CN207625811 U CN 207625811U
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Abstract
A kind of emergency communication UAV system of the utility model embodiment offer and emergency communication system, the emergency communication UAV system include unmanned plane, base station, cable and power generator；The base station is mounted on the unmanned plane, to arrive in the object height of target location by plane with the unmanned plane, and passes through the communication near target location described in the communication recovery between ground base station；The cable is arranged between the unmanned plane and the power generator, and it is connect respectively with the unmanned plane and the power generator, so that the power generator provides electric energy by the cable for the unmanned plane, it is ensured that the unmanned plane can be stopped vacantly for a long time.The network recovery of the emergency communication UAV system is efficient, can improve the rescue efficiency of disaster area rescue operations, reduces the loss of disaster area resident.
Description
Technical field
The utility model is related to communication network recovery technology fields, in particular to a kind of emergency communication unmanned plane system
System and emergency communication system.
Background technology
With the continuous development of communication network technology, the application of communication network is more extensive.For now, for building
The GCF ground communication facility of communication network can be seriously damaged, cause when encountering the natural calamities such as earthquake, flood, mud-rock flow
Communication network interrupts.
Therefore, it is the concrete condition for understanding disaster area in time, needs the communication network for restoring disaster area as soon as possible, improves rescue
Efficiency, but the communication network being destroyed is often because of the reasons such as GCF ground communication facility complexity is huge, Operation and Maintenance difficulty is big, it can not
It is resumed in a short time, makes the emergency team 5 in entire disaster area rescue operations that can not speedily carry out rescue work what is obtained now within first time
Field information is sent to speedily carry out rescue work floor manager portion and rear emergency center in real time, to influence the rescue of entire rescue operations
Efficiency easily causes heavy losses.
Utility model content
In order to overcome above-mentioned deficiency in the prior art, the purpose of this utility model is to provide it is a kind of using unmanned plane into
The emergency communication UAV system and emergency communication system that row urgency communication restores.The network of the emergency communication UAV system
Restore efficient, the rescue efficiency of disaster area rescue operations can be improved, reduces the loss of disaster area resident.
For emergency communication UAV system, the utility model preferred embodiment provides a kind of emergency communication unmanned plane
System.The emergency communication UAV system includes unmanned plane, base station, cable and power generator；
The base station is mounted on the unmanned plane, to arrive in the object height of target location by plane with the unmanned plane,
And pass through the communication near target location described in the communication recovery between ground base station；
The cable is arranged between the unmanned plane and the power generator, and respectively with the unmanned plane and the hair
Electric installation connects, so that the power generator provides electric energy by the cable for the unmanned plane, it is ensured that the unmanned plane can
It is hanging for a long time to stop.The emergency communication UAV system by unmanned plane by the base station communicated with ground base station carry to
At the object height of target location, and the network coverage is carried out to the target location by the network signal that the base station discharges,
To restore the communication network near the target location within the extremely short time, improves entire speedily carrying out rescue work for disaster area rescue operations and rescue
Efficiency is helped, the loss of disaster area resident is reduced.
In the utility model preferred embodiment, be provided with stand-by power supply on above-mentioned unmanned plane, the stand-by power supply with
The unmanned plane is electrically connected, for providing electric energy to the hanging unmanned plane when the power generator is out of service, really
It protects the unmanned function and continues hovering in the air.
For emergency communication system, the utility model preferred embodiment provides a kind of emergency communication system.It is described to answer
Anxious communication system includes dispatching control center, GCS Ground Communication System and above-mentioned emergency communication UAV system；
The dispatching control center is connect with the UAV Communication in the emergency communication UAV system, is used for described
Unmanned plane sends dispatch command, is arrived in by plane to the object height of target location according to the dispatch command with controlling the unmanned plane；
The GCS Ground Communication System includes ground base station, the base station communication of the ground base station and the UAV flight,
For after the object height that the unmanned plane arrives in the target location by plane, being carried out to the target location by the base station
The network coverage, to restore the communication near the target location.
In the utility model preferred embodiment, above-mentioned emergency communication system further includes positioning device, and the positioning is set
It is standby to be arranged on the unmanned plane, it is positioned for the flight path to the unmanned plane, obtains the position of the unmanned plane
Change information.
In the utility model preferred embodiment, above-mentioned positioning device is communicated with the dispatching control center, by institute
Rheme sets change information and is sent to the dispatching control center, makes the dispatching control center according to the change in location information pair
The dispatch command is adjusted.
In the utility model preferred embodiment, above-mentioned dispatching control center includes computing device, the computing device
Including display device and flight remote control；
The display device is used for according to the change in location information and map on the spot, to the unmanned plane in the map
In position shown；
The flight remote control is used to generate the dispatch command for the state of flight for controlling the unmanned plane.
In the utility model preferred embodiment, above-mentioned dispatching control center further includes elevating mechanism, the elevator
Structure needs the elevator of the unmanned plane to be flown by controlling carrying for placing the unmanned plane, the dispatching control center
Structure is lifted, and the unmanned plane is made to be moved to out of described dispatching control center outside the dispatching control center.
In the utility model preferred embodiment, in above-mentioned dispatching control center and the emergency communication UAV system
Power generator be set in a moveable vehicle.
In the utility model preferred embodiment, above-mentioned dispatching control center is electrically connected with the power generator, with
Control power supply state of the power generator to the unmanned plane.
In the utility model preferred embodiment, the waterproofing grade of above-mentioned unmanned plane is not less than IP65 grades.
In terms of existing technologies, the emergency communication UAV system and answer that the utility model preferred embodiment provides
Anxious communication system has the advantages that：The network recovery of the emergency communication UAV system is efficient, can improve calamity
The rescue efficiency of area's rescue operations reduces the loss of disaster area resident.Specifically, the emergency communication UAV system includes
Unmanned plane, base station, cable and power generator, the base station are mounted on the unmanned plane, to be arrived in by plane with the unmanned plane
The object height of target location, and pass through the communication near target location described in the communication recovery between ground base station；It is described
Cable is arranged between the unmanned plane and the power generator, and is connect respectively with the unmanned plane and the power generator,
So that the power generator provides electric energy by the cable for the unmanned plane, it is ensured that the unmanned plane can be hanging for a long time
It stops.The emergency communication UAV system is carried the base station communicated with ground base station to the mesh of target location by unmanned plane
At absolute altitude degree, and the network coverage is carried out to the target location by the network signal that the base station discharges, to extremely short
Restore the communication network near the target location in time, improve the rescue efficiency of entire disaster area rescue operations, reduces
The loss of disaster area resident.
To enable the above objects, features, and advantages of the utility model to be clearer and more comprehensible, the utility model cited below particularly compared with
Good embodiment, and coordinate appended attached drawing, it is described in detail below.
Description of the drawings
It, below will be to required use in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
Attached drawing be briefly described, it should be understood that the following drawings illustrates only some embodiments of the utility model, therefore should not be by
Regard the restriction to the utility model claims protection domain as, for those of ordinary skill in the art, is not paying
Under the premise of creative work, other relevant attached drawings are can also be obtained according to these attached drawings.
Fig. 1 is a kind of composition schematic diagram for the emergency communication system that the utility model preferred embodiment provides.
One kind of emergency communication UAV system shown in Fig. 1 that Fig. 2 provides for the utility model preferred embodiment
Block diagram.
Emergency communication UAV system is another shown in Fig. 1 that Fig. 3 provides for the utility model preferred embodiment
Kind block diagram.
A kind of box of dispatching control center shown in Fig. 1 that Fig. 4 provides for the utility model preferred embodiment shows
It is intended to.
A kind of block diagram of computing device shown in Fig. 4 that Fig. 5 provides for the utility model preferred embodiment.
A kind of structural schematic diagram of elevating mechanism shown in Fig. 4 that Fig. 6 provides for the utility model preferred embodiment.
Icon：10- emergency communication systems；100- emergency communication UAV system；110- unmanned planes；The base stations 120-；130-
Power generator；140- stand-by power supplies；200- dispatching control centers；300- GCS Ground Communication Systems；400- positioning devices；210- is calculated
Equipment；211- display devices；212- flight remote controls；213- memories；214- storage controls；215- processors；220-
Elevating mechanism；310- ground base stations.
Specific implementation mode
It is new below in conjunction with this practicality to keep the purpose, technical scheme and advantage of the utility model embodiment clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Usually here described in attached drawing and
The component of the utility model embodiment shown can be arranged and be designed with a variety of different configurations.
Therefore, the detailed description of the embodiments of the present invention to providing in the accompanying drawings is not intended to limit requirement below
The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained without creative efforts, all
Belong to the range of the utility model protection.
It should be noted that：Similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined, then it further need not be defined and explained in subsequent attached drawing in a attached drawing.
It is in the description of the present invention, it should be noted that term "center", "upper", "lower", "left", "right", " perpendicular
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, or
The utility model product using when the orientation or positional relationship usually put, be merely for convenience of description the utility model and letter
Change description, do not indicate or imply the indicated device or element must have a particular orientation, with specific azimuth configuration and
Operation, therefore should not be understood as limiting the present invention.
In addition, the terms such as term "horizontal", "vertical", " pendency " are not offered as requiring component abswolute level or pendency, and
It is that can be slightly tilted.It is not to indicate the structure if "horizontal" refers to only that its direction is more horizontal with respect to for "vertical"
It has to fully horizontally, but can be slightly tilted.
In the description of the present invention, it should also be noted that, unless otherwise clearly defined and limited, term " is set
Set ", " installation ", " connected ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection,
Or it is integrally connected；It can be mechanical connection, can also be electrical connection；It can be directly connected, intermediary can also be passed through
It is indirectly connected, can be the connection inside two elements.For the ordinary skill in the art, it can be managed with concrete condition
Solve the concrete meaning of above-mentioned term in the present invention.
How providing one kind can communicate in quick-recovery disaster area soon, improve the rescue efficiency of disaster area rescue operations, reduce
The emergency communication system of the loss of disaster area resident is to those skilled in the art the technical issues of being badly in need of solving.
Below in conjunction with the accompanying drawings, it elaborates to some embodiments of the utility model.In the absence of conflict, under
Feature in the embodiment and embodiment stated can be combined with each other.
Fig. 1 is please referred to, is a kind of composition signal for the emergency communication system 10 that the utility model preferred embodiment provides
Figure.In the utility model embodiment, the emergency communication system 10 is used to restore disaster area communication network within the extremely short time,
To improve the rescue efficiency of entire disaster area rescue operations, the loss of disaster area resident is reduced, is the security of the lives and property of resident
It provides safeguard.Specifically, in the present embodiment, the emergency communication system 10 includes emergency communication UAV system 100, scheduling
Control centre 200 and GCS Ground Communication System 300, the emergency communication system 10 by the emergency communication UAV system 100,
The dispatching control center 200 and the GCS Ground Communication System 300 carry out fast quick-recovery, so that calamity to the communication network in disaster area
Emergency team 5 in the area scene field data that will can speedily carry out rescue work in real time is sent to speedily carry out rescue work floor manager portion and rear emergency center,
To improve the rescue efficiency of disaster area rescue operations, the loss of disaster area resident is reduced.
In the present embodiment, the emergency communication UAV system 100 may include unmanned plane 110 and base station 120, described
GCS Ground Communication System 300 includes ground base station 310, the base station 120 in the emergency communication UAV system 100 and the ground
Ground base station 310 in communication system 300 communicates to connect, to get the ground base station 310 from the ground base station 310
Releasable network signal, and the ground base station 310 is coordinated to form a communication network.
Wherein, the base station 120 is mounted on the unmanned plane 110, with the unmanned plane 110 with arriving in target by plane
Point object height after, the network signal got based on the communication with the ground base station 310, to the target location into
The row network coverage, to rapidly restore the communication near the target location.
In the present embodiment, the number of the ground base station 310 can be multiple, and the base station 120 is with the nothing
Man-machine 110 when flying into the network coverage of the ground base station 310, will carry out communication link with corresponding ground base station 310
It connects, the relay for serving as the ground base station 310, to increase the network coverage of the ground base station 310, from
And realize and the network coverage is carried out to the target location, restore the communication near the target location.
In the present embodiment, the dispatching control center 200 is for controlling the flight progress of the unmanned plane 110
System.Specifically, the dispatching control center 200 is communicated to connect with the unmanned plane 110, is adjusted with being sent to the unmanned plane 110
Degree instruction, controls the unmanned plane 110 and is arrived in by plane to the object height of the target location according to the dispatch command.Wherein, institute
It can be that the control unmanned plane 110 carries out diving flight to state dispatch command, can also be to control the unmanned plane 110 to be climbed
Rise flight, can also be that the control unmanned plane 110 carries out rolling flight, can also be the control unmanned plane 110 forward, to
A left side is flown to the right, and specific dispatch command is generated in the dispatching control center 200 according to demand by operating personnel.
In the present embodiment, the dispatching control center 200 is set in a moveable vehicle, and the vehicle can carry
The dispatching control center 200 is moved, for example, carry the dispatching control center 200 enter disaster area scene after, the tune
Degree control centre 200 can start to be scheduled the unmanned plane 110 after the vehicle parking.
In the present embodiment, the target location can be target disaster area rescue point, can also be that target communication is established a little,
The object height of the target location is the height on Ullage ground in the target location.What the unmanned plane 110 can fly
Object height ranging from 50m~150m.
Fig. 2 is please referred to, is emergency communication UAV system shown in Fig. 1 of the utility model preferred embodiment offer
A kind of 100 block diagram.In the utility model embodiment, the emergency communication UAV system 100 can also include
Power generator 130 and cable, the cable are arranged between the power generator 130 and the unmanned plane 110, and respectively with institute
It states unmanned plane 110 and the power generator 130 connects, so that the power generator 130 is the unmanned plane by the cable
110 provide electric energy, it is ensured that the unmanned plane 110 can vacantly be detained for a long time.
In the present embodiment, the power generator 130 can be set to the dispatching control center 200 on same vehicle,
And with the dispatching control center 200 be electrically connected, under the control of the dispatching control center 200 to the unmanned plane
110 are powered, i.e., the dispatching control center 200 can while the flight progress to the unmanned plane 110 controls,
Control power supply state of the power generator 130 to the unmanned plane 110.
Fig. 3 is please referred to, is emergency communication UAV system shown in Fig. 1 of the utility model preferred embodiment offer
100 another block diagram.In the utility model embodiment, the emergency communication UAV system 100 can also wrap
Stand-by power supply 140 is included, the stand-by power supply 140 is arranged on the unmanned plane 110, and is electrically connected with the unmanned plane 110,
For providing electric energy to the hanging unmanned plane 110 when the power generator 130 is out of service, it is ensured that the unmanned plane
110 can continue hovering in the air.Specifically, when 130 unmanned plane 110 of the power generator needs the base
When 120 holdings of standing maintain the communication of the target location, the stand-by power supply 140 can be by way of providing electric energy, it is ensured that
The hovering continuation of the journey of the unmanned plane 110；It is described when 130 unmanned plane 110 of the power generator needs to land
Stand-by power supply 140 can be by way of providing electric energy, it is ensured that the unmanned plane 110 being capable of safe landing.In the present embodiment, institute
Power generator 130 is stated while providing electric energy to the unmanned plane 110, can also be charged to the stand-by power supply 140.
Referring once again to Fig. 1, in the present embodiment, the emergency communication system 10 can also include positioning device 400, institute
It states positioning device 400 to be arranged on the unmanned plane 110, positions, obtain for the flight path to the unmanned plane 110
The change in location information of the unmanned plane 110.
In the present embodiment, the positioning device 400 is communicated to connect with the dispatching control center 200, will be described fixed
The change in location information for the unmanned plane 110 that position equipment 400 navigates to is sent to the dispatching control center 200, so that institute
It states dispatching control center 200 to be adjusted the dispatch command according to the change in location information, enables the unmanned plane 110
It enough arrives in by plane to the object height of target location, to be led to the target location by the base station 120 on the unmanned plane 110
Letter is restored.
Fig. 4 is please referred to, is dispatching control center 200 shown in Fig. 1 of the utility model preferred embodiment offer
A kind of block diagram.In the utility model embodiment, the dispatching control center 200 includes computing device 210 and lifting
Mechanism 220.
Wherein, the computing device 210 is used to send scheduling to the unmanned plane 110 according to the change in location information and refer to
It enables, to control the flight path of the unmanned plane 110, the unmanned plane 110 is enable to arrive in by plane to the object height of target location.
The computing device 210 includes display device 211 and flight remote control 212, and the display device 211 is used for according to institute's rheme
Change information and on the spot map are set, position of the unmanned plane 110 in the map is shown；The flight remote control dress
212 dispatch command for generating the state of flight for controlling the unmanned plane 110 is set, so that the unmanned plane 110 is arrived in by plane to institute
State the object height of target location.Wherein, the state of flight include the flying speed of the unmanned plane 110, heading and
State of flight.
In the present embodiment, the display device 211 includes a display screen, and the display device 211 passes through the display
Screen shows position of the unmanned plane 110 on the spot in map；The flight remote control 212 includes that a flight is remotely controlled
Rocking bar, the flight remote control 212 are remotely controlled the state of flight that rocking bar controls the unmanned plane 110 by the flight.
Fig. 5 is please referred to, is one kind of computing device 210 shown in Fig. 4 of the utility model preferred embodiment offer
Block diagram.In the present embodiment, the computing device 210 can also include memory 213, storage control 214 and place
Manage device 215.Directly or indirectly electrically connect between 215 each element of the memory 213, storage control 214 and processor
It connects, to realize the transmission or interaction of data.For example, these elements can pass through one or more communication bus or signal between each other
Line, which is realized, to be electrically connected.
Wherein, the memory 213 may be, but not limited to, random access memory (Random Access
Memory, RAM), read-only memory (Read Only Memory, ROM), programmable read only memory (Programmable
Read-Only Memory, PROM) etc..Wherein, memory 213 is receiving execution for storing program, the processor 215
After instruction, described program is executed, to control the state of flight of the unmanned plane 110, and then the unmanned plane 110 is made to arrive in by plane to mark
The object height in place, and the communication of the target location is restored by the base station 120 on the unmanned plane 110.Institute
State processor 215 and other possible components to memory 213 access can under the control of the storage control 214 into
Row.
The processor 215 may be a kind of IC chip with signal handling capacity.Above-mentioned processor 215
Can be general processor, including central processing unit (Central Processing Unit, CPU), network processing unit
(Network Processor, NP) etc..
It is appreciated that structure shown in fig. 5 is only to illustrate, computing device 210 may also include it is more than shown in Fig. 5 or
Less component, or with the configuration different from shown in Fig. 5.Each component shown in Fig. 5 may be used hardware, software or its
Combination is realized.
Fig. 6 is please referred to, is one kind of elevating mechanism 220 shown in Fig. 4 of the utility model preferred embodiment offer
Structural schematic diagram.In the present embodiment, the elevating mechanism 220 is for placing unmanned plane 110.When on the elevating mechanism 220
Carrying is when needing the unmanned plane 110 to be flown, and the dispatching control center 200 can be by controlling the lifting of the elevating mechanism 220
State makes the unmanned plane 110 be moved to out of the dispatching control center 200 outside the dispatching control center 200.Wherein,
The unmanned plane 110 can be placed on the dispatching control center 200 in same vehicle when not running, and be placed on described
On elevating mechanism 220, to improve the mobile efficiency to the emergency communication system 10 and carry efficiency.
In the present embodiment, 110 waterproofing grade of the unmanned plane is high, and wind resistance is good, and it is big to carry capacity.Specifically, institute
The waterproofing grade for stating unmanned plane 110 is not less than IP65 grades, when the unmanned plane 110 can be long under the wind speed of 10m/S~15m/S
Between normal operation, the unmanned plane 110 can carry 5~10 kilograms load carry out flying for long time.In the present embodiment, described
Unmanned plane 110 may be, but not limited to, multi-rotor unmanned aerial vehicle, fixed-wing unmanned plane etc..In the present embodiment, the unmanned plane
Equipped with parachute landing system on 110, for can ensure ground staff's safety when the unmanned plane 110 is in a state of emergency, and
The equipment safety of the unmanned plane 110.
In conclusion the emergency communication UAV system provided in the utility model preferred embodiment and emergency communication system
In system, the network recovery of the emergency communication UAV system is efficient, can improve the rescue effect of disaster area rescue operations
Rate reduces the loss of disaster area resident.Specifically, the emergency communication UAV system includes unmanned plane, base station, cable and power generation
Device, the base station are mounted on the unmanned plane, to arrive in the object height of target location by plane with the unmanned plane, and are led to
Cross the communication near target location described in the communication recovery between ground base station；The cable is arranged in the unmanned plane and institute
It between stating power generator, and is connect respectively with the unmanned plane and the power generator, so that the power generator is described in
Cable provides electric energy for the unmanned plane, it is ensured that the unmanned plane can be stopped vacantly for a long time.The emergency communication unmanned plane
System is carried the base station communicated with ground base station to the object height of target location by unmanned plane, and passes through the base station
The network signal of release carries out the network coverage to the target location, attached to restore the target location within the extremely short time
Close communication network improves the rescue efficiency of entire disaster area rescue operations, reduces the loss of disaster area resident.
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 emergency communication UAV system, which is characterized in that the emergency communication UAV system includes unmanned plane, base
It stands, cable and power generator；
The base station is mounted on the unmanned plane, to arrive in the object height of target location by plane with the unmanned plane, and is led to
Cross the communication near target location described in the communication recovery between ground base station；
The cable is arranged between the unmanned plane and the power generator, and is filled respectively with the unmanned plane and the power generation
Connection is set, so that the power generator provides electric energy by the cable for the unmanned plane, it is ensured that when the unmanned plane can be long
Between hanging stop.
2. emergency communication UAV system according to claim 1, which is characterized in that be provided on the unmanned plane spare
Power supply, the stand-by power supply are electrically connected with the unmanned plane, are used for when the power generator is out of service to hanging institute
It states unmanned plane and electric energy is provided, it is ensured that the unmanned function continues hovering in the air.
3. a kind of emergency communication system, which is characterized in that the emergency communication system includes dispatching control center, ground communication system
Emergency communication UAV system described in any one of system and claim 1-2；
The dispatching control center is connect with the UAV Communication in the emergency communication UAV system, for it is described nobody
Machine sends dispatch command, is arrived in by plane to the object height of target location according to the dispatch command with controlling the unmanned plane；
The GCS Ground Communication System includes ground base station, and the base station communication of the ground base station and the UAV flight is used for
After the object height that the unmanned plane arrives in the target location by plane, network is carried out to the target location by the base station
Covering, to restore the communication near the target location.
4. emergency communication system according to claim 3, which is characterized in that the emergency communication system further includes that positioning is set
Standby, the positioning device is arranged on the unmanned plane, is positioned for the flight path to the unmanned plane, obtains described
The change in location information of unmanned plane.
5. emergency communication system according to claim 4, which is characterized in that in the positioning device and the scheduling controlling
The heart communicates, and the change in location information is sent to the dispatching control center, makes the dispatching control center according to
Change in location information is adjusted the dispatch command.
6. emergency communication system according to claim 5, which is characterized in that the dispatching control center includes calculating to set
Standby, the computing device includes display device and flight remote control；
The display device is used for according to the change in location information and map on the spot, to the unmanned plane in the map
Position is shown；
The flight remote control is used to generate the dispatch command for the state of flight for controlling the unmanned plane.
7. emergency communication system according to claim 3, which is characterized in that the dispatching control center further includes elevator
Structure, the elevating mechanism carry nobody for needing to be flown for placing the unmanned plane, the dispatching control center by controlling
The elevating mechanism of machine is lifted, and the unmanned plane is made to be moved in the scheduling controlling from the dispatching control center
Outside the heart.
8. emergency communication system according to claim 3, which is characterized in that the dispatching control center and described meet an urgent need are led to
Power generator in letter UAV system is set in a moveable vehicle.
9. emergency communication system according to claim 8, which is characterized in that the dispatching control center is filled with the power generation
Electric connection is set, to control power supply state of the power generator to the unmanned plane.
10. according to the emergency communication system described in any one of claim 3-9, which is characterized in that the unmanned plane is prevented
Water grade is not less than IP65 grades.
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| CN201721869436.XU CN207625811U (en) | 2017-12-27 | 2017-12-27 | Emergency communication UAV system and emergency communication system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201721869436.XU CN207625811U (en) | 2017-12-27 | 2017-12-27 | Emergency communication UAV system and emergency communication system |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108093389A (en) * | 2017-12-27 | 2018-05-29 | 成都科易未来光电技术有限公司 | Emergency communication UAV system and emergency communication system |
| CN110176955A (en) * | 2019-07-01 | 2019-08-27 | 北京有感科技有限责任公司 | UAV Communication base station, communication system and communication system construction method |
| CN110518955A (en) * | 2019-07-12 | 2019-11-29 | 全球能源互联网研究院有限公司 | A kind of power emergency communication system |
| CN111986518A (en) * | 2020-08-31 | 2020-11-24 | 上海大学 | Unmanned ship cooperative communication control system |
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
-
2017
- 2017-12-27 CN CN201721869436.XU patent/CN207625811U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
| CN108093389A (en) * | 2017-12-27 | 2018-05-29 | 成都科易未来光电技术有限公司 | Emergency communication UAV system and emergency communication system |
| CN110176955A (en) * | 2019-07-01 | 2019-08-27 | 北京有感科技有限责任公司 | UAV Communication base station, communication system and communication system construction method |
| CN110176955B (en) * | 2019-07-01 | 2023-08-25 | 合肥有感科技有限责任公司 | Unmanned aerial vehicle communication base station, communication system and method for constructing communication system |
| CN110518955A (en) * | 2019-07-12 | 2019-11-29 | 全球能源互联网研究院有限公司 | A kind of power emergency communication system |
| CN111986518A (en) * | 2020-08-31 | 2020-11-24 | 上海大学 | Unmanned ship cooperative communication control system |
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