CN106532572A - Flying cable as well as wiring system and method - Google Patents
Flying cable as well as wiring system and method Download PDFInfo
- Publication number
- CN106532572A CN106532572A CN201710001107.1A CN201710001107A CN106532572A CN 106532572 A CN106532572 A CN 106532572A CN 201710001107 A CN201710001107 A CN 201710001107A CN 106532572 A CN106532572 A CN 106532572A
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- aircraft
- flight
- mounting interface
- unit
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- 238000000034 method Methods 0.000 title claims abstract description 19
- 238000010276 construction Methods 0.000 claims abstract description 37
- 230000004044 response Effects 0.000 claims description 9
- 238000012544 monitoring process Methods 0.000 claims description 7
- 230000007613 environmental effect Effects 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 2
- 230000008092 positive effect Effects 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 9
- 238000004891 communication Methods 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 230000005520 electrodynamics Effects 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 244000144992 flock Species 0.000 description 2
- 230000000977 initiatory effect Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 235000013311 vegetables Nutrition 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000001617 migratory effect Effects 0.000 description 1
- 238000010295 mobile communication Methods 0.000 description 1
- 230000001151 other effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
- H02G1/04—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables for mounting or stretching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Abstract
The invention provides a flying cable as well as a wiring system and method thereof, relating to the technical field of unmanned flying equipment. The flying cable comprises a cable body, wherein flight vehicles capable of carrying the cable body to fly are arranged on the cable body. The flying cable as well as the wiring system and method have the advantages and positive effects that the flying cable is safe and efficient and can be reused; the degree of automation of cable laying is increased; the working hours of the constructors in the environment with low safety is reduced; the engineering construction progress is greatly increased; the construction period is ensured; the construction cost is reduced.
Description
Technical field
The present invention relates to unmanned flight's equipment technical field.
Background technology
When emergency is speedily carried out rescue work, generally require first to survey the basic condition of devastated, then need to connect disaster-stricken position with
The water in the external world, electricity, communication line, are so easy to the rescue work in later stage.The work for connecting circuit at present generally needs to rescue people
Member and relief car collaboration are carried out, it is contemplated that often cause mountain after secondary disaster, such as flood are tended to occur or caused after calamity
Body landslide, mud-rock flow etc., this mode security are low, accident risk occur high.Also, for needing operation of ascending a height in the disaster relief
Situation, operating environment security is low.
Meanwhile, during power circuit Poling Construction, it is often necessary to across roomy river, mountain region, forest belt, various voltages
The facilities such as the power circuit of grade, highway, high-speed railway, green house of vegetables.During construction, some locations are relatively complicated, people
Power difficulty of construction is larger.And often thing is spanned because cause specific difficulty of construction is very big.Across high ferro, high speed, green house of vegetables
Difficulty is bigger, and damages, coordinative construction expense, the expense of leap are all the inevitable expenses for occurring, therefore the generally great number of generation
Across taking, crop compensation expense and across thing indemnity for damage expense, bring huge Jing to power construction investment enterprise and construction enterprises
Also the duration is delayed while Ji loss.Meanwhile, the manpower construction also low problem of faced one operating environment security.
The content of the invention
It is an object of the invention to：Overcome the deficiencies in the prior art, there is provided a kind of flight formula cable and utilize flight formula line
Cable lays the wiring system of power circuit, communication line etc., wiring method.
To realize above-mentioned target, the invention provides following technical scheme:
A kind of flight formula cable, including cable main body, are provided with the cable main body and can carry the flight of cable body
Aircraft.
Further, multiple aircraft are provided with cable main body.
Further, the power source of aircraft in the following way one or more：Mode one, arranges electricity on board the aircraft
Source；Mode two, arranges flight power interface in cable main body, and flight power interface is connected with aircraft electrical, by the interface
Obtain power supply；Mode three, arranges flight power source special, electrical connection power source special and aircraft.
Further, it is provided with to enter as fulcrum force using supported underneath face in cable main body and cable main body is supported
Supporting construction, by the supporting construction adjust cable main body position.
Further, be provided with buoyancy aid in the supporting construction, by supporting construction described in buoyancy aid can using the water surface as
Support face provides support force.
Further, ground structure is provided with cable main body.
Further, also including alarm unit, the alarm unit is used for more than the power source of monitoring of environmental information and aircraft
Amount information, and the information of acquisition is sent to into flying vehicles control center, flying vehicles control center is according to the information adjustment for receiving
The flight of aircraft.
Further, including the first aircraft, first aircraft includes that flying power unit, cable main body connection are single
Unit, and the winged control unit of navigation of control flight parameter.
Further, including the second aircraft, second aircraft includes that flying power unit, cable main body connection are single
Unit, and the flight response unit in response to controlling to be flown.
Further, including the first aircraft and the second aircraft, the first flying vehicles control flight parameter, described second
Aircraft is flown in response to the control of the first aircraft.
Further, the flying platform of aircraft is rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella wing structure
Or flapping wing structure.
Further, also including recognition unit, the recognition unit is recognized simultaneously by gathering image information and/or audio-frequency information
Judge the position of destination.
Further, also including wireless positioning unit, the destination locations are provided with wireless signal Transmit-Receive Unit, the nothing
Line positioning unit gathers the signal of wireless messages Transmit-Receive Unit, recognizes and judge the position of destination.
Further, the interface position unit of the wiring point mounting interface information for obtaining destination is provided with aircraft.
Further, mounting interface fixed structure and mounting interface embedded structure, the mounting interface are provided with aircraft
For cable is positioned on mounting interface or mounting interface near zone, the mounting interface embedded structure is used for fixed structure
Cable connector is arranged in erection joint.
Present invention also offers a kind of wiring system of flight formula cable, including：Aforesaid flight formula cable；Initial solid point
Stationary interface, for the initial side of fixed cable.
Present invention also offers a kind of wiring method of flight formula cable, comprises the steps：Fixed flight formula cable
Initial side；Flight formula cable is flown to wiring point position by aircraft thereon.
Further, the step of flight formula cable is flown to wiring point position by aircraft thereon includes：Flight formula
Positioning unit on cable or ground control station at least one obtains the positional information that wiring point is located；According to the position letter for obtaining
The breath control flight formula cable flies to wiring point position.
Further, the interface position unit of the wiring point mounting interface information for obtaining destination is provided with aircraft, with
And mounting interface fixed structure and mounting interface embedded structure, include the step of wiring point upper fixed line cable：Interface position list
Unit obtains the positional information of wiring point mounting interface；Cable landing is accordingly carried to aircraft according to the positional information control for obtaining
To mounting interface position；Cable is positioned on mounting interface or the neighbouring area of mounting interface by mounting interface fixed structure
Domain；Cable connector is arranged in erection joint by mounting interface embedded structure.
Further, be provided with alarm unit on flight formula cable, by the alarm unit be used for monitoring of environmental information and
The power source balance information of aircraft, and the information of acquisition is sent to into flying vehicles control center；The alarm unit is monitored
When environment is unsuitable for continuing flight and/or not enough power source surplus, alarm signal is sent to flying vehicles control center；Aircraft control
Course line and/or the flight quantity of aircraft of the center processed according to the information adjustment aircraft for receiving.
The present invention is due to using above technical scheme, compared with prior art, having the following advantages that and good effect：This
The flight formula cable of invention, it is safe and efficient, can reuse.Change in rescue and relief work or region with a varied topography construction
When can only by manpower shoulder draw the back of the body shoulder, make a difficult journey laying power circuit, the method for communication line, improve to a certain extent from
It is dynamic to be turned into industry, the time that workmen works in the low environment of security is reduced, engineering construction progress is greatly improved, is protected
The duration has been demonstrate,proved, construction cost has been reduced.
Description of the drawings
Fig. 1 is the structural representation of flight formula cable provided in an embodiment of the present invention.
Fig. 2 is the structural representation of the flight formula cable with supporting construction provided in an embodiment of the present invention.
Fig. 3 is the structural representation of the flight formula cable including the first aircraft provided in an embodiment of the present invention.
Fig. 4 is that the structure of the flight formula cable including the first aircraft and the second aircraft provided in an embodiment of the present invention is shown
It is intended to.
Fig. 5 is the function structure chart of flight formula cable provided in an embodiment of the present invention.
Fig. 6 is the flow chart of wiring method provided in an embodiment of the present invention.
In figure, label is as follows：
Cable main body 100；
Aircraft 200, flying power unit 210, cable main body connection unit 220, supporting construction 230, buoyancy aid 240.
Specific embodiment
The flight formula cable and wiring system, method provided to the present invention below in conjunction with the drawings and specific embodiments is made into one
Step is described in detail.It should be noted that the combination of technical characteristic or technical characteristic described in following embodiments should not be by
It is considered isolated, they can be mutually combined so as to reach superior technique effect.In the accompanying drawing of following embodiments, respectively
The identical label that accompanying drawing occurs represents identical feature or part, can be applicable in different embodiments.Therefore, once it is a certain
It is defined in Xiang Yi accompanying drawing, then which need not be further discussed in subsequent accompanying drawing.
It should be noted that, depicted structure, ratio, size etc. in this specification institute accompanying drawing, only to coordinate explanation
Content disclosed in book, so that those skilled in the art understands and reads, is not limited to invent enforceable restriction bar
Part, the modification of any structure, the change of proportionate relationship or the adjustment of size are not affecting to invent effect and the institute's energy that can be generated
Under the purpose reached, all should fall in the range of the disclosed technology contents of invention can be covered.The side of being preferable to carry out of the present invention
The scope of formula includes other realization, wherein can not press it is shown or discuss order, including according to involved function by
Basic mode simultaneously or in the opposite order, carrys out perform function, and this should be by the skill of embodiments of the invention art
Art personnel understood.
For known to person of ordinary skill in the relevant, technology, method and apparatus may be not discussed in detail, but suitable
In the case of, the technology, method and apparatus should be considered the part for authorizing specification.Institute that is shown here and discussing
In having example, any occurrence should be construed as merely exemplary, not as restriction.Therefore, exemplary embodiment
Other examples can have different values.
Embodiment
Fig. 1 is the structural representation of flight formula cable provided in an embodiment of the present invention.
It is shown in Figure 1, a kind of flight formula cable, including cable main body 100, being provided with the cable main body 100 can
Carry the aircraft 200 of cable body flight.
Cable is the general designation of electric wire, optical cable, cable and other items.The purposes of cable has a lot, is mainly used in control and installs, connects
The multiple action such as connect equipment, transmit electric power, being common and indispensable a kind of thing in daily life.Line alleged by the present invention
Cable body, including electric wire, cable, optical cable etc., which is commonly used for instrument, instrument, intercommunication, monitoring, control and installs, electrical equipment,
Instrument, the signal transmission of power distribution equipment, control, measurement, cable television, broadband networks private cable, telephone communication and radio set
Junction box wiring use of standby connection and telephony wiring net etc..
Aircraft, refers to the apparatus that can be flown, and in embodiments of the present invention, its specifically unmanned plane, is to utilize nothing
The not manned aircraft that line electrical remote control equipment and the presetting apparatus provided for oneself are manipulated.The aircraft arranged in the cable main body,
It can also be multiple that can be one, can be adjusted according to the length of cable, weight etc..During using multiple aircraft, can
Collaboration flight between multiple aircraft is made, the mode of flight is adjusted according to flight environment of vehicle.The mode of the flight, including during flight
The shape of cable main body, attitude, height etc..
Aircraft includes flying power unit, and flying power unit includes flying platform and power source.
Flying platform can be using rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella wing structure or flapping wing structure
Deng.Flight dynamic devices can adopt piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching type or jet-propelled, this enforcement
Power set in example adopt electrodynamic type engine.
Power source can be in the following way one or more.
Mode one, arranges power supply on board the aircraft.Power source is provided by the power supply such as battery that aircraft is carried.Make
For for example and not limitation, power supply can be the battery in aircraft, and battery is electrically connected with the power set of flying wing
Connect.It is easily understood that in the case that charging head is provided with battery, charging circuit can be arranged on the circuit board of charging head, be filled
Circuit is for being charged for battery when battery electric quantity is not enough.The charging circuit is known to those skilled in the art,
For example, charging circuit includes voltage reduction module, rectification module and the filtration module being sequentially connected, and the voltage reduction module is for by outside
Power supply High Level AC Voltage is converted into low-voltage AC, the rectification module for low-voltage AC is converted into low-voltage DC,
The filtration module is for being filtered to the direct current after rectification.The circuit board of charging head can also be included with overvoltage and mistake
The Voltage stabilizing module of stream protective effect, prevents overvoltage or excessively stream from causing the damage of circuit components.The Voltage stabilizing module is this area
Well known to technical staff, here is omitted.
Mode two, arranges flight power interface in cable main body, and flight power interface is connected with aircraft electrical, by this
Interface obtains power supply.It is typically powered in view of cable itself, flight power interface can be set on cable directly, fly
Power interface is connected with aircraft electrical, obtains power supply by the interface.Certainly, the current type for being needed according to aircraft, can be with
The equipment such as current converter and/or rectifier is set on power interface.
Mode three, arranges flight power source special, electrical connection power source special and aircraft.Flight Special electric is set in addition
Source, which is not arranged in aircraft sheet, also not against cable main body.
In this enforcement, preferred employing mode two provides power source.In view of security, it is provided with cable main body and connects
Ground structure is used as safety device.It is unrestricted as an example, the wire that electric current is introduced the earth is such as set in cable main body,
In electrical equipment leak or overtension, electric current can pass through the wire of ground connection and enter the earth, play a part of safeguard protection.
Another embodiment provides the structure of the flight formula cable with supporting construction.Being provided with cable main body can be below
Square supporting surface enters the supporting construction being supported to cable main body as fulcrum force, adjusts cable sheet by the supporting construction
The position of body.With this, during the flight of flight formula cable, the grounding, cable is suitably reduced to other objects in environment
The impact for causing.
The supporting construction arranged below cable main body be solid support thing, such as support bar, bracing frame etc..Referring to Fig. 2 institutes
Show, the supporting construction 230 realized as fulcrum force is provided with using lower section supporting surface below cable main body 100, in flight formula
During cable flies and/or grounds, the position of electric wire can be adjusted by the supporting construction 230.As an example rather than limit
System, shown supporting construction 230 can be mounted in cable main body, or preset on the support surface.For front
Person, typically can be arranged on supporting construction in cable main body by hinge, control supporting construction when needed with respect to cable sheet
Hang down after body rotation；For the latter, flight formula cable preferentially arranges flight road according to the position that supporting construction is located in flight
Footpath, cable accurately can be placed in supporting construction top.
In view of needing to cross over the water surface during flight, further, buoyancy aid can be set in the supporting construction, it is described floating
Body enables the supporting construction to provide support force as supporting surface using the water surface.
In another embodiment, flight formula cable also include alarm unit, the alarm unit be used for monitoring of environmental information and
The power source balance information of aircraft, and the information of acquisition is sent to into flying vehicles control center, flying vehicles control center according to
The information for receiving adjusts the flight of aircraft.The flying vehicles control center, it is unrestricted as an example, can be aircraft
The flight controller of itself, or it is placed in the ground control station on ground.
For the aircraft of flight formula cable, can itself be provided with control system, can intelligently plan, adjust itself
And/or the collaboration flight of other aircraft Intelligent flight device, or itself there is no control system, need according to ground or
The combination of aircraft, or two groups of aircraft above that the control of other equipment is flown.Fig. 3 is the embodiment of the present invention
The structural representation of the flight formula cable including the first aircraft for providing.Fig. 4 is provided in an embodiment of the present invention including first
The structural representation of the flight formula cable of aircraft and the second aircraft.
Referring to Fig. 3, the first aircraft 200 is itself to be provided with the aircraft of control system, including flying power unit
210th, cable main body connection unit 220, and the winged control unit (not shown) of navigation of control flight parameter.
Referring to Fig. 4, second aircraft 200 itself does not have control system, needs according to ground or other equipment
Control is flown, including flying power unit 210, cable main body connection unit 220, and flown in response to control
Flight response unit.
One group of first aircraft and/or one group of second aircraft can be set in cable main body.Referring to Fig. 4, when including the
When one flight 200 and the second aircraft 200, it is preferred that by the first flying vehicles control flight parameter, second aircraft
Control in response to the first aircraft is flown.Thus, imitate the Nature in migratory bird moving when flock of birds flying method, first
Aircraft follows the first aircraft similar to leading bird, the second aircraft, similar to the flock of birds for following leading bird flying, in flight
It is middle to keep certain formation effectively utilize air-flow, reduce aloft energy ezpenditure.
In another embodiment, also include recognition unit to accurately judge that the position of destination on flight formula cable.
The recognition unit, can recognize and judge the position at electrical equipment place by gathering image information and/or audio-frequency information.Make
For for example and not limitation, image mechanism and image identification unit be such as set on board the aircraft, outdoor scene is gathered by image mechanism
Image, judges positional information after image identification unit recognizes image.Collection audio-frequency information structure can be installed in
Carry-on microphone.
The method of identifying purpose position, in addition to collection image information and/or audio-frequency information, can also pass through wireless location side
Formula, can arrange wireless positioning unit on the aircraft of flight formula cable, corresponding, be provided with wireless on the destination locations
Signal transmitting and receiving unit, the wireless positioning unit gather the signal of wireless messages Transmit-Receive Unit, recognize and judge destination locations
Position.Location technology common at present mainly has PPD location technologies, gps satellite to position, bluetooth positioning, WIFI network are positioned,
Big Dipper positioning, GPRS/CDMA mobile communication technologies positioning etc..As a example by being commonly used based on mobile terminal positioning technology at present, should
The principle of location technology is：The Base Transmitter signal of multiple known locations, institute's transmission signal carry relevant with base station location
Characteristic information, after mobile terminal receives these signals, determines itself and the geometry site between each base station, and according to phase
Closing algorithm carries out positioning estimation to its own position, so as to obtain the positional information of itself.
Certainly, above-mentioned two groups of identification structures also can be set simultaneously, so can selects suitable according to flight environment of vehicle such as weather
Mode obtain destination locations information.Unrestricted as an example, such as in foggy weather, poor visibility is known using image
During other effect on driving birds is not good, the RM of audio-frequency information identification or wireless location can be adopted.
Further, in the present embodiment, on aircraft, it is provided with the interface of the wiring point mounting interface information for obtaining destination
Positioning unit, and mounting interface fixed structure and mounting interface embedded structure, the mounting interface fixed structure is for by line
Cable is positioned on mounting interface or mounting interface near zone, and the mounting interface embedded structure is for cable connector is arranged on
In erection joint.
May need one end of cable or certain medium position are fixed on the mounting interface of some wiring point during wiring
On, it is therefore desirable to the interface position unit of the charging inlet positional information of electrical equipment can be accurately acquired.In interface position
Cable can be positioned on mounting interface by mounting interface fixed structure after the positional information of unit acquisition mounting interface
Or mounting interface near zone, then cable connector is arranged in erection joint by mounting interface embedded structure.The peace
Attaching mouth fixed structure, it is unrestricted as an example, can be gripper, sucker, preferred magnechuck；The mounting interface is embedding
Enter structure, it is unrestricted as an example, can be telescopic elements or collapsible element, in cable connector alignment mounting interface institute
Postpone in place, cable connector is inserted and installed by control contractable element or foldable member elongation.Fig. 5 shows
A kind of function structure chart of the flight formula cable with support function, alarm function, identification function and interface installation function of example,
Each unit is arranged to realize corresponding function.
Another embodiment of the present invention provides a kind of wiring system of flight formula cable, including：It is aforesaid with flight
The flight formula cable of device, and starting point fixed interface, for the initial side of fixed cable.According to the needs that wiring is installed,
Wiring point mounting interface can also be set, for cable is fixed on wiring point position.
Referring to Fig. 6, another embodiment of the present invention additionally provides a kind of wiring method of flight formula cable, including following step
Suddenly.
S100, the initial side of fixed flight formula cable.It is unrestricted as an example, than if desired on two power towers
During erecting power lines road, one end of cable is fixed first on a power tower.The initiating terminal, which includes but is not limited to cable
Initial end, unrestricted as an example, the wiring of a cable is divided into continuous three phases, phase III by such as user
Initiating terminal can be second stage clearing end, and the initial end of the clearing end of second stage non-cable.
S200, flight formula cable are flown to wiring point position by aircraft thereon.
In the present embodiment, include the step of flight formula cable is flown to wiring point position by aircraft thereon：Fly
Positioning unit on line cable or ground control station at least one obtains the positional information that wiring point is located；According to the position for obtaining
The confidence breath control flight formula cable flies to wiring point position.
In the present embodiment, the interface position list of the wiring point mounting interface information for obtaining destination on aircraft, is provided with
Unit, and mounting interface fixed structure and mounting interface embedded structure, include the step of wiring point upper fixed line cable：Interface is fixed
Bit location obtains the positional information of wiring point mounting interface；Positional information control according to obtaining accordingly carries cable to aircraft
It drop to mounting interface position；Cable is positioned on mounting interface by mounting interface fixed structure or mounting interface is attached
Near field；Cable connector is arranged in erection joint by mounting interface embedded structure.
Further, when alarm unit is provided with flight formula cable, believed for monitoring of environmental by the alarm unit
The power source balance information of breath and aircraft, and the information of acquisition is sent to into flying vehicles control center；The alarm unit prison
When measuring environment and being unsuitable for continuing flight and/or power source surplus not enough, alarm signal is sent to flying vehicles control center；Flight
Course line and/or the flight quantity of aircraft of the device control centre according to the information adjustment aircraft for receiving.
Foregoing description is only the description to present pre-ferred embodiments, not any restriction to the scope of the invention, this
The scope of bright preferred embodiment includes other realization, wherein work(can not be performed by order that is shown or discussing
Energy.Any change that the those of ordinary skill in field of the present invention is done according to the disclosure above content, modification, belong to claims
Protection domain.
Claims (15)
1. a kind of flight formula cable, including cable main body, it is characterised in that：It is provided with the cable main body and can carries cable sheet
The aircraft of body flight.
2. flight formula cable is arrived according to claim 1, it is characterised in that：The power source of aircraft in the following way one
Plant or various,
Mode one, arranges power supply on board the aircraft；
Mode two, arranges flight power interface in cable main body, and flight power interface is connected with aircraft electrical, by the interface
Obtain power supply；
Mode three, arranges flight power source special, electrical connection power source special and aircraft.
3. flight formula cable is arrived according to claim 1, it is characterised in that：Being provided with cable main body can be with supported underneath face
Enter the supporting construction being supported to cable main body as fulcrum force, the position of cable main body is adjusted by the supporting construction
Put.
4. flight formula cable is arrived according to claim 3, it is characterised in that：Buoyancy aid is provided with the supporting construction, is passed through
Supporting construction described in buoyancy aid can provide support force as supporting surface using the water surface.
5. flight formula cable is arrived according to claim 1, it is characterised in that：Ground structure is provided with cable main body.
6. flight formula cable is arrived according to claim 1, it is characterised in that：Also include alarm unit, the alarm unit is used
In the power source balance information of monitoring of environmental information and aircraft, and the information of acquisition is sent to into flying vehicles control center, is flown
Hang Qi control centres adjust the flight of aircraft according to the information for receiving.
7. flight formula cable is arrived according to claim 1, it is characterised in that：The aircraft is multiple, including the first flight
Device, first aircraft include flying power unit, cable main body connection unit, and the navigation of control flight parameter flies control
Unit.
8. flight formula cable is arrived according to claim 1, it is characterised in that：The aircraft is multiple, including the second flight
Device, second aircraft include flying power unit, cable main body connection unit, and in response to flying that control is flown
Row response unit.
9. flight formula cable is arrived according to claim 1, it is characterised in that：The aircraft is multiple, including the first flight
Device and the second aircraft, the first flying vehicles control flight parameter, control of second aircraft in response to the first aircraft
System is flown.
10. flight formula cable is arrived according to claim 1, it is characterised in that：It is provided with aircraft,
Obtain the interface position unit of the wiring point mounting interface information of destination；
And mounting interface fixed structure and mounting interface embedded structure, the mounting interface fixed structure is for cable is positioned
On mounting interface or mounting interface near zone, the mounting interface embedded structure is for cable connector is connect installed in installation
On head.
11. a kind of wiring systems of flight formula cable, it is characterised in that include：
Flight formula cable any one of claim 1-10；
Starting point fixed interface, for the initial side of fixed cable.
12. a kind of wiring methods of flight formula cable, it is characterised in that including step：
The initial side of fixed flight formula cable；
Flight formula cable is flown to wiring point position by aircraft thereon.
13. wiring methods according to claim 12, it is characterised in that：
The step of flight formula cable is flown to wiring point position by aircraft thereon includes that flight formula cable or ground are controlled
Positioning unit at least one of system station obtains the positional information that wiring point is located；
The flight formula cable is controlled according to the positional information for obtaining to fly to wiring point position.
14. methods according to claim 12, it is characterised in that：
The interface position unit of the wiring point mounting interface information for obtaining destination is provided with aircraft, and mounting interface is admittedly
Fixed structure and mounting interface embedded structure, include the step of wiring point upper fixed line cable,
Interface position unit obtains the positional information of wiring point mounting interface；
Positional information control according to obtaining accordingly carries cable to aircraft and drop to mounting interface position；
Cable is positioned on mounting interface or mounting interface near zone by mounting interface fixed structure；
Cable connector is arranged in erection joint by mounting interface embedded structure.
15. methods according to claim 12, it is characterised in that：Alarm unit is provided with flight formula cable, by institute
Alarm unit is stated for monitoring of environmental information and the power source balance information of aircraft, and the information of acquisition is sent to into aircraft
Control centre；
When the alarm unit monitors that environment is unsuitable for continuing flight and/or not enough power source surplus, in flying vehicles control
The heart sends alarm signal；
Course line and/or the flight quantity of aircraft of the flying vehicles control center according to the information adjustment aircraft for receiving.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710001107.1A CN106532572B (en) | 2017-01-03 | 2017-01-03 | Flight formula cable and wiring system, wiring method |
Applications Claiming Priority (1)
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| CN201710001107.1A CN106532572B (en) | 2017-01-03 | 2017-01-03 | Flight formula cable and wiring system, wiring method |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6115505A (en) * | 1984-06-29 | 1986-01-23 | 昭和電線電纜株式会社 | Method of extending aerial transmission line |
| CN101039138A (en) * | 2006-03-13 | 2007-09-19 | 阎跃军 | Cable-fed floating information transceiver system |
| CN203553761U (en) * | 2013-11-13 | 2014-04-16 | 禹城市供电公司 | Cable supporting river-crossing device |
| CN204304316U (en) * | 2015-01-05 | 2015-04-29 | 河南华通电缆有限公司 | Overhead line installation |
| CN206340903U (en) * | 2017-01-03 | 2017-07-18 | 上海量明科技发展有限公司 | Flight formula cable and wiring system |
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2017
- 2017-01-03 CN CN201710001107.1A patent/CN106532572B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6115505A (en) * | 1984-06-29 | 1986-01-23 | 昭和電線電纜株式会社 | Method of extending aerial transmission line |
| CN101039138A (en) * | 2006-03-13 | 2007-09-19 | 阎跃军 | Cable-fed floating information transceiver system |
| CN203553761U (en) * | 2013-11-13 | 2014-04-16 | 禹城市供电公司 | Cable supporting river-crossing device |
| CN204304316U (en) * | 2015-01-05 | 2015-04-29 | 河南华通电缆有限公司 | Overhead line installation |
| CN206340903U (en) * | 2017-01-03 | 2017-07-18 | 上海量明科技发展有限公司 | Flight formula cable and wiring system |
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| CN106532572B (en) | 2018-09-18 |
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