CN208828107U - A kind of multiple no-manned plane terminal airspace control device - Google Patents
A kind of multiple no-manned plane terminal airspace control device Download PDFInfo
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- CN208828107U CN208828107U CN201821400732.XU CN201821400732U CN208828107U CN 208828107 U CN208828107 U CN 208828107U CN 201821400732 U CN201821400732 U CN 201821400732U CN 208828107 U CN208828107 U CN 208828107U
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Abstract
The utility model discloses a kind of multiple no-manned plane terminal airspace control devices, belong to unmanned plane terminal airspace control technical field, a kind of multiple no-manned plane terminal airspace control device, including control patrol aviation device and the on-board data box being mounted on unmanned plane, managing patrol aviation device includes four rotor aircraft shells, equally distributed main flying wing there are four being fixedly connected on four rotor aircraft shells, the protecting frame to match with main flying wing is fixedly connected on four rotor aircraft shells, the lower end of four rotor aircraft shells is fixedly connected with multiple alighting carriages, the lower end of alighting carriage is fixedly connected with resilient cushion, the downside of four rotor aircraft shells is equipped with high-definition camera, it may be implemented reasonably to manage multiple no-manned plane airport, it can be realized by installing airborne data box additional, versatility is high, it is easy to be promoted the security and stability on multiple no-manned plane airport, Meanwhile being easy to improve the processing speed of emergency case.
Description
Technical field
The utility model relates to unmanned plane terminal airspaces to manage technical field, more specifically to a kind of multiple no-manned plane
Terminal airspace control device.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, unmanned plane
By application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+
Industrial application is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country also in actively extension industrial application and develops unmanned plane
Technology.
Since unmanned plane and common aircraft have biggish difference, in the control of multiple no-manned plane terminal airspace with
Can also there be biggish difference on existing airport, and universal and quantity recently as unmanned plane is increased, many personal and single
Position is owned by unmanned plane, especially personal small drone, often there is black winged phenomenon, that is, without relevant departments
Approval unmanned plane near airports fly, the normal takeoff and landing order on airport can be seriously affected, in addition, unmanned plane due to
There is no the operation of pilot and judgement, the requirement degree to ground wireless control system is higher, when a failure occurs, it is easy to go out
The case where existing airport paralysis, it will cause large effect.
Summary of the invention
1. technical problems to be solved
Aiming at the problems existing in the prior art, the purpose of this utility model is to provide a kind of multiple no-manned plane terminal airspaces
Control device, it may be implemented reasonably to manage multiple no-manned plane airport, can be realized by installing airborne data box additional, general
Property it is high, be easy to be promoted the security and stability on multiple no-manned plane airport, meanwhile, be easy to improve the processing speed of emergency case.
2. technical solution
To solve the above problems, the utility model adopts the following technical scheme.
A kind of multiple no-manned plane terminal airspace control device including control patrol aviation device and is mounted on airborne on unmanned plane
Data box, the control patrol aviation device include four rotor aircraft shells, are fixedly connected with four on the four rotor aircrafts shell
A equally distributed main flying wing is fixedly connected with the protecting frame to match with main flying wing on the four rotor aircrafts shell,
The lower end of the four rotor aircrafts shell is fixedly connected with multiple alighting carriages, and the lower end of the alighting carriage, which is fixedly connected with, to be subtracted
Shake pad, the downside of the four rotor aircrafts shell are equipped with high-definition camera, the high-definition camera and four rotor aircraft shells it
Between be connected with holder, the lower end of the four rotor aircrafts shell is fixedly connected with multiple equally distributed device sets columns, it can
Multiple no-manned plane airport is reasonably managed with realizing, can be realized by installing airborne data box additional, versatility is high, is easy to be promoted
The security and stability on multiple no-manned plane airport, meanwhile, it is easy to improve the processing speed of emergency case.
Further, the control patrol aviation device is waterproof construction, is connected with secondary flying wing on described device collection zygostyle
When encountering rainy equal weather, managing will not intake in patrol aviation device, when control patrol aviation device compels to be down in water, pass through
Controlling secondary flying wing can be such that control patrol aviation device exercises on the water surface, take convenient for recycling.
Further, it is fixedly connected on the four rotor aircrafts shell there are four equally distributed air bag, and safe
Air bag is located between two adjacent protecting frames, and air bag, protection four wings flight can be triggered when encountering hard hit
Device shell is not damaged.
Further, the side of the on-board data box is equipped with connector, connects between the on-board data box and connector
It is connected to connecting line, the power output end connection of the connecting line and unmanned plane can connect the power supply of on-board data box and unmanned plane
It connects, versatility is stronger.
Further, multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence normal nothing
Man-machine takeoff and landing.
3. beneficial effect
Compared with the prior art, utility model has the advantages that
(1) this programme may be implemented reasonably to manage multiple no-manned plane airport, can be real by installing airborne data box additional
Existing, versatility is high, is easy to be promoted the security and stability on multiple no-manned plane airport, meanwhile, it is easy to improve the processing speed of emergency case.
(2) control patrol aviation device is waterproof construction, and secondary flying wing is connected on device sets column when encountering rain equal days
When gas, managing will not intake in patrol aviation device, can by controlling secondary flying wing when control patrol aviation device compels to be down in water
It exercises control patrol aviation device on the water surface, takes convenient for recycling.
Equally distributed air bag there are four being fixedly connected on (3) four rotor aircraft shells, and air bag distinguishes position
Between two adjacent protecting frames, air bag can be triggered when encountering hard hit, four rotor aircraft shells of protection not by
Damage.
(4) side of on-board data box is equipped with connector, and connecting line is connected between on-board data box and connector, connects
The connection of the power output end of line and unmanned plane, can connect the power supply of on-board data box and unmanned plane, versatility is stronger.
(5) multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence taking off for normal unmanned plane
And landing.
Detailed description of the invention
Fig. 1 is the bottom substance schematic diagram of the control patrol aviation device of the utility model；
Fig. 2 is the superstructure schematic diagram of the control patrol aviation device of the utility model；
Fig. 3 is that the data of the utility model transmit box structure schematic diagram；
Fig. 4 is that the data of the utility model transmit box mounted configuration schematic diagram；
Fig. 5 is the unmanned plane approach area structure top view of the utility model；
Fig. 6 is sectional view at A-A in Fig. 5；
Fig. 7 is sectional view at B-B in Fig. 5；
Fig. 8 is the systematic schematic diagram of the utility model.
Figure label explanation:
1 four rotor aircraft shells, 2 main flying wings, 3 protecting frames, 4 alighting carriages, 5 resilient cushions, 6 high-definition cameras, 7 safety
Air bag, 8 device sets columns, 9 secondary flying wings, 10 holders, 11 on-board data boxes, 12 connectors, 13 connecting lines.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model；The technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe；Obviously；The described embodiments are only a part of the embodiments of the utility model；Rather than whole
Embodiment, based on the embodiments of the present invention；Those of ordinary skill in the art are without making creative work
Every other embodiment obtained；It fall within the protection scope of the utility model.
In the description of the present invention, it should be noted that term " on ", "lower", "inner", "outside" " top/bottom end " etc.
The orientation or positional relationship of instruction is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of description the utility model
It is described with simplifying, rather than the device or element of indication or suggestion meaning must have a particular orientation, with specific orientation structure
It makes and operates, therefore should not be understood as limiting the present invention.In addition, term " first ", " second " are only used for description mesh
, it is not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " being provided with ", " be arranged/connect ", " connection " etc., shall be understood in a broad sense, such as " connection ", may be a fixed connection, can also be with
It is to be detachably connected, or be integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, it can also be with
Indirectly connected through an intermediary, it can be the connection inside two elements.For the ordinary skill in the art, may be used
The concrete meaning of above-mentioned term in the present invention is understood with concrete condition.
Embodiment 1:
Fig. 3-4, a kind of multiple no-manned plane terminal airspace control device, including control device and managing and control system are please referred to, is managed
Device includes the on-board data box 11 managing patrol aviation device and being mounted on unmanned plane, and the side of on-board data box 11, which is equipped with, to be connected
Connector 12 is connected with connecting line 13, the power output end of connecting line 13 and unmanned plane between on-board data box 11 and connector 12
On-board data box 11, can connect by connection with the power supply of unmanned plane, and versatility is stronger,
Referring to Fig. 8, being mounted on satellite positioning module, flight control modules and peace in unmanned plane and on-board data box 11
Full control module, managing and control system include that ground telemetering and letter biography system, unmanned aerial vehicle onboard telemetering and letter biography system, defence type are detected
Early warning system and black winged aircraft interference system, ground telemetering manages control tower with ground with letter biography system and operation remote control center is equal
Signal connection, satellite positioning module, flight control modules and safety control module with unmanned aerial vehicle onboard telemetering and letter biography system
Signal connection, ground telemetering pass system signal with letter with unmanned aerial vehicle onboard telemetering with letter biography system and connect, and manage patrol aviation device
With ground telemetering with letter biography system and unmanned aerial vehicle onboard telemetering with letter biography system equal signal connect, ground telemetering with believe biography system and
Managing patrol aviation device includes defence type detecting and early warning system and black winged aircraft interference system, defence type detecting and early warning system
Including aircraft figure biography and remote signal receiver, black winged aircraft interference system includes electromagnetic interference emission device, ground telemetering
It is two-way encrypted data transmission between letter biography system and unmanned aerial vehicle onboard telemetering and letter biography system and control patrol aviation device,
Managing between patrol aviation device and on-board data and unmanned aerial vehicle onboard telemetering and letter biography system is two-way encrypted data transmission, can be mentioned
High security.
Control patrol aviation device includes four rotor aircraft shells 1, fixed company on four rotor aircraft shells 1 referring to FIG. 1-2,
It connects there are four equally distributed main flying wing 2, is fixedly connected with the guarantor to match with main flying wing 2 on four rotor aircraft shells 1
Frame 3 is protected, 3 pairs of protecting frame main flying wings 2 have protective action, and the lower end of four rotor aircraft shells 1 is fixedly connected with multiple landing branch
Frame 4, the lower end of alighting carriage 4 are fixedly connected with resilient cushion 5, and resilient cushion 5 can reduce vibration when landing, four rotor aircraft shells
1 downside is equipped with high-definition camera 6, holder 10 is connected between high-definition camera 6 and four rotor aircraft shells 1, holder 10 can
Make high-definition camera 6 be not susceptible to shake, be easy to improve the quality of acquisition image, the lower end of four rotor aircraft shells 1 is fixed to be connected
Multiple equally distributed device sets columns 8 are connected to, the figure biography and remote signal receiver and electromagnetism managed on patrol aviation device are done
It disturbs transmitter to be respectively positioned in device sets column 8, convenient for emitting and receiving signal, control patrol aviation device is waterproof construction, device
Secondary flying wing 9 is connected on collection zygostyle 8 when encountering rainy equal weather, managing will not intake in patrol aviation device, when control is patrolled
When patrolling aircraft and compeling to be down in water, it can make to manage patrol aviation device by controlling secondary flying wing 9 and be exercised on the water surface, convenient for recycling
Take, this function can be achieved by the prior art by those skilled in the art, be fixedly connected on four rotor aircraft shells 1 there are four
Equally distributed air bag 7, and air bag 7 is located between two adjacent protecting frames 3, when encountering hard hit
Air bag 7 can be triggered, four rotor aircraft shells 1 of protection are not damaged.
Please refer to Fig. 5-7, multiple control patrol aviation device flight positions are respectively positioned on outside clearance zone, will not influence it is normal nobody
The takeoff and landing of machine.
Unmanned plane carries out signal connection by unmanned aerial vehicle onboard telemetering and letter biography system and ground telemetering and letter biography system, by
Staff manages the state of flight of unmanned plane in ground control control tower, and is carried out by operation remote control center to unmanned plane
It controls and operates, wherein satellite positioning module can determine position and the height of unmanned plane, and flight control modules can control unmanned plane
Navigation, safety control module can prevent that unmanned plane from colliding or the generation of other fortuitous events, this management-control method are equal
It is similar with civil aviation control technology for the prior art, it can be realized by those skilled in the art.
Airborne data box 11 is installed on unmanned plane, on-board data box 11 can be used as the Beck-up Control System of unmanned plane, when
When the included control system of unmanned plane fails, on-board data box 11 can play a role automatically, meanwhile, on-board data box 11 can be by nothing
Man-machine flying quality is stored into cloud server in real time, and on-board data box 11 is made to play the function of cloud black box, and thing occurs
After therefore, the loss of flying quality not will cause.
Position of multiple control patrol aviation devices outside clearance zone close to airport is uniformly flown, defence type detecting and early warning system
The position of unmanned plane can be determined by receiving unmanned plane figure biography and remote signal, when received signal belongs to the unmanned plane in control
When, black winged aircraft interference system will not be triggered, when received signal is unknown signaling, and the normal of unmanned plane is will affect and flies
When row, it can be defaulted as black winged aircraft, the black winged aircraft lift-off such as do not need, after black winged aircraft booting in the short time
It was found that and be accurately positioned, while black winged aircraft interference system can be triggered, black winged aircraft interference system can pass through electromagnetic interference
Transmitter carries out accurate electromagnetic interference, adjust automatically electricity according to information such as working frequency, the directions of the black winged aircraft detected
Magnetic disturbance frequency and direction realize that black winged aircraft expelling and force-landing in prevention and control region；Ground telemetering and letter biography system can be
This function is played in approach area, will not influence normal unmanned plane during flying.
When ground telemetering and letter pass system jam, control patrol aviation device can play temporary control function, temporarily
When safeguard unmanned plane airport order.
High-definition camera 6 is installed on control patrol aviation device, it can be by the picture of shooting or realtime video transmission to cloud
Server, ground control control tower and operation remote control center, convenient for handling emergency in time or being supervised to airport surrounding enviroment
It surveys.
This programme may be implemented reasonably to manage unmanned plane using dual system, can be real by installing airborne data box additional
Existing, versatility is high, is easy to be promoted the security and stability on multiple no-manned plane airport；Using multiple control patrol aviation devices outside clearance zone
It goes on patrol on duty, can prevent black winged situation from upsetting the normal order on multiple no-manned plane airport, meanwhile, it is easy to improve the place to emergency case
Manage speed.
It is described above；The only preferable specific embodiment of the utility model；But the protection scope of the utility model is not
It is confined to this；Anyone skilled in the art is within the technical scope disclosed by the utility model；It is practical according to this
Novel technical solution and its improvement design is subject to equivalent substitution or change；It should all cover in the protection scope of the utility model
It is interior.
Claims (5)
1. a kind of multiple no-manned plane terminal airspace control device, including control patrol aviation device and the airborne number being mounted on unmanned plane
According to box (11), it is characterised in that: the control patrol aviation device includes four rotor aircraft shells (1), outside four rotor aircraft
It is fixedly connected on shell (1) there are four equally distributed main flying wing (2), is fixedly connected on the four rotor aircrafts shell (1)
The lower end of the protecting frame (3) to match with main flying wing (2), the four rotor aircrafts shell (1) is fixedly connected with multiple landing
The lower end of bracket (4), the alighting carriage (4) is fixedly connected with resilient cushion (5), the downside of the four rotor aircrafts shell (1)
Equipped with high-definition camera (6), it is connected with holder (10) between the high-definition camera (6) and four rotor aircraft shells (1), it is described
The lower end of four rotor aircraft shells (1) is fixedly connected with multiple equally distributed device sets columns (8).
2. a kind of multiple no-manned plane terminal airspace control device according to claim 1, it is characterised in that: the control patrol
Aircraft is waterproof construction, and secondary flying wing (9) are connected on described device collection zygostyle (8).
3. a kind of multiple no-manned plane terminal airspace control device according to claim 1, it is characterised in that: four wings flight
Be fixedly connected on device shell (1) there are four equally distributed air bag (7), and air bag (7) be located at two it is adjacent
Protecting frame (3) between.
4. a kind of multiple no-manned plane terminal airspace control device according to claim 1, it is characterised in that: the on-board data
The side of box (11) is equipped with connector (12), is connected with connecting line between the on-board data box (11) and connector (12)
(13), the connecting line (13) connect with the power output end of unmanned plane.
5. a kind of multiple no-manned plane terminal airspace control device according to claim 1, it is characterised in that: multiple control
Patrol aviation device flight position is respectively positioned on outside clearance zone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821400732.XU CN208828107U (en) | 2018-08-29 | 2018-08-29 | A kind of multiple no-manned plane terminal airspace control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821400732.XU CN208828107U (en) | 2018-08-29 | 2018-08-29 | A kind of multiple no-manned plane terminal airspace control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208828107U true CN208828107U (en) | 2019-05-07 |
Family
ID=66311025
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821400732.XU Active CN208828107U (en) | 2018-08-29 | 2018-08-29 | A kind of multiple no-manned plane terminal airspace control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208828107U (en) |
-
2018
- 2018-08-29 CN CN201821400732.XU patent/CN208828107U/en active Active
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