CN106532572B - Flight formula cable and wiring system, wiring method - Google Patents
Flight formula cable and wiring system, wiring method Download PDFInfo
- Publication number
- CN106532572B CN106532572B CN201710001107.1A CN201710001107A CN106532572B CN 106532572 B CN106532572 B CN 106532572B CN 201710001107 A CN201710001107 A CN 201710001107A CN 106532572 B CN106532572 B CN 106532572B
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- 238000000034 method Methods 0.000 title claims abstract description 19
- 238000010276 construction Methods 0.000 claims abstract description 38
- 238000009434 installation Methods 0.000 claims description 51
- 230000004044 response Effects 0.000 claims description 9
- 238000007667 floating Methods 0.000 claims description 7
- 238000012544 monitoring process Methods 0.000 claims description 7
- 230000007613 environmental effect Effects 0.000 claims description 6
- 230000007812 deficiency Effects 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 238000005516 engineering process Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 6
- 238000004891 communication Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000005520 electrodynamics Effects 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
- 230000001174 ascending effect Effects 0.000 description 1
- 230000015572 biosynthetic process 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
- 230000005611 electricity Effects 0.000 description 1
- 238000003384 imaging method 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
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Laying Of Electric Cables Or Lines Outside (AREA)
Abstract
The present invention provides flight formula cable and its wiring system, wiring methods, are related to unmanned flight's equipment technical field.The flight formula cable includes cable main body, and the aircraft that can carry the flight of cable ontology is provided in the cable main body.The flight formula cable of the present invention, it is safe and efficient, it may be reused, improve the degree of automation of cable laying, reduce the time that construction personnel works in the low environment of safety, greatly improve engineering construction progress, ensure that the duration, reduce construction cost.
Description
Technical field
The present invention relates to unmanned flight's equipment technical fields.
Background technology
When emergency is speedily carried out rescue work, generally require the basic condition for first surveying devastated, then need to connect disaster-stricken position with
Water, electricity, the communication line in the external world, are so convenient for the rescue work in later stage.The work for connecting circuit at present usually requires rescue people
Member and relief car collaboration carry out, it is contemplated that secondary disaster are tended to occur or caused after calamity, for example flood often causes mountain later
Body landslide, mud-rock flow etc., this mode safety is low, and it is high that accident risk occurs.Also, for needing operation of ascending a height in the disaster relief
The case where, operating environment safety is low.
Meanwhile during power circuit Poling Construction, it is often necessary to across roomy river, mountainous region, forest belt, various voltages
The facilities such as power circuit, highway, high-speed railway, the green house of vegetables of grade.Some locations are relatively complicated when construction, people
Power difficulty of construction is larger.And object is spanned often because cause specific difficulty of construction is very big.Across high ferro, high speed, green house of vegetables
Difficulty bigger, damages, coordinative construction take, are all the expenses unavoidably occurred across taking, therefore the usually great number of generation
Across take, crop compensation expense and cross over object indemnity for damage expense, bring huge warp to power construction investment enterprise and construction enterprises
The duration is also delayed while Ji loss.Meanwhile the manpower construction also low problem of faced one operating environment safety.
Invention content
It is an object of the invention to：It overcomes the deficiencies of the prior art and provide a kind of flight formula cable and utilizes flight formula line
Cable lays the wiring system of power circuit, communication line etc., wiring method.
To realize above-mentioned target, the present invention provides following technical solutions:
A kind of flight formula cable, including cable main body, the flight of cable ontology can be carried by being provided in the cable main body
Aircraft.
Further, multiple aircraft are provided in cable main body.
Further, the power source of aircraft in the following way one or more：Mode one, setting is electric on board the aircraft
Source；Flight power interface is arranged in mode two in cable main body, and flight power interface is connect with aircraft electrical, passes through the interface
Obtain power supply；Flight power source special is arranged in mode three, is electrically connected power source special and aircraft.
Further, being provided in cable main body can be supported using supported underneath face as fulcrum force into cable main body
Support construction, pass through the support construction adjust cable main body position.
Further, it is provided with floating body in the support construction, it can be using the water surface as branch by support construction described in floating body
Support face provides support force.
Further, it is provided with ground structure in cable main body.
Further, further include alarm unit, the alarm unit is used for more than the power source of monitoring of environmental information and aircraft
Information is measured, and the information of acquisition is sent to flying vehicles control center, flying vehicles control center is adjusted according to the information received
The flight of aircraft.
Further, including the first aircraft, first aircraft include flying power unit, cable main body connection list
Member, and the navigation of control flight parameter fly control unit.
Further, including the second aircraft, second aircraft include flying power unit, cable main body connection list
Member, and in response to controlling the flight response unit to fly.
Further, including the first aircraft and the second aircraft, the first flying vehicles control flight parameter, described second
Aircraft flies 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, further include recognition unit, the recognition unit is by acquiring image information and/or audio-frequency information identification simultaneously
Judge the position of destination.
Further, further include wireless positioning unit, the destination locations are provided with wireless signal Transmit-Receive Unit, the nothing
Line positioning unit acquires the signal of wireless messages Transmit-Receive Unit, identifies and judge the position of destination.
Further, the interface position unit for the wiring point installation interface message for obtaining destination is provided on aircraft.
Further, installation interface fixed structure and installation interface embedded structure, the installation interface are provided on aircraft
Fixed structure is used to cable being located on installation interface or installation interface near zone, the installation interface embedded structure are used for
Cable connector is mounted in erection joint.
The present invention also provides a kind of wiring systems of flight formula cable, including：Flight formula cable above-mentioned；Originate solid point
Stationary interface is used for the starting end side of fixed cable.
The present invention also provides a kind of wiring methods of flight formula cable, include the following steps：Fixed flight formula cable
Originate end side；Flight formula cable is flown by aircraft thereon to wiring point position.
Further, flight formula cable flown by aircraft thereon include to the step of wiring point position：Flight formula
Positioning unit on cable or ground control station at least one obtains the location information where wiring point；Believed according to the position of acquisition
Breath controls the flight formula cable and flies to wiring point position.
Further, the interface position unit for the wiring point installation interface message for obtaining destination is provided on aircraft, with
And interface fixed structure and installation interface embedded structure are installed, include in the step of wiring point upper fixed line cable：Interface position list
Member obtains the location information of wiring point installation interface；According to the control of the location information of acquisition accordingly cable landing is carried to aircraft
To installation interface position；Cable is located on installation interface or is installed area near interface by installing interface fixed structure
Domain；Cable connector is mounted in erection joint by installing interface embedded structure.
Further, be provided with alarm unit on flight formula cable, by the alarm unit for monitoring of environmental information and
The power source balance information of aircraft, and the information of acquisition is sent to flying vehicles control center；The alarm unit monitors
When environment is unsuitable for continuing flight and/or power source surplus deficiency, alarm signal is sent to flying vehicles control center；Aircraft control
Center processed adjusts the course line of aircraft and/or the flight quantity of aircraft according to the information received.
The present invention due to using the technology described above, compared with prior art, has the following advantages that and good effect：This
The flight formula cable of invention, it is safe and efficient, it may be reused.It changes in rescue and relief work or region with a varied topography is constructed
When can only rely on manpower shoulder draw the back of the body shoulder, make a difficult journey lay power circuit, communication line method, improve to a certain extent from
It is dynamic to be turned into industry, the time that construction personnel works in the low environment of safety is reduced, engineering construction progress is greatly improved, is protected
The duration has been demonstrate,proved, construction cost is reduced.
Description of the drawings
Fig. 1 is the structural schematic diagram of flight formula cable provided in an embodiment of the present invention.
Fig. 2 is the structural schematic diagram of the flight formula cable provided in an embodiment of the present invention with support construction.
Fig. 3 is the structural schematic diagram of the flight formula cable provided in an embodiment of the present invention for including the first aircraft.
Fig. 4 is that the structure of the flight formula cable provided in an embodiment of the present invention for including the first aircraft and the second aircraft 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.
Figure label is as follows：
Cable main body 100；
Aircraft 200, flying power unit 210, cable main body connection unit 220, support construction 230, floating body 240.
Specific implementation mode
Flight formula cable provided by the invention and wiring system, method are made into one below in conjunction with the drawings and specific embodiments
Step is described in detail.It should be noted that the combination of the technical characteristic or technical characteristic described in following embodiments should not be by
It is considered isolated, they can be combined with each other to reach superior technique effect.In the attached drawing of following embodiments, respectively
The identical label that attached drawing occurs represents identical feature or component, can be applied in different embodiments.Therefore, once it is a certain
It is defined, then it need not be further discussed in subsequent attached drawing in Xiang Yi attached drawing.
It should be noted that structure, ratio, size etc. depicted in this specification institute attached drawing, only coordinating explanation
The revealed content of book is not limited to invent enforceable restriction item so that those skilled in the art understands and reads
Part, the modification of any structure, the change of proportionate relationship or the adjustment of size are not influencing the effect of invention can be generated and institute's energy
Under the purpose reached, it should all fall in the range of the revealed technology contents of invention can be covered.The preferred implementation side of the present invention
The range of formula includes other realization, include being pressed according to involved function wherein sequence that is shown or discussing can not be pressed
Basic mode simultaneously or in the opposite order, to execute function, this should be by the skill of the embodiment of the present invention technical field
Art personnel are understood.
Technology, method and apparatus known to person of ordinary skill in the relevant may be not discussed in detail, but suitable
In the case of, the technology, method and apparatus should be considered as authorizing part of specification.Institute that is shown here and discussing
Have in example, any occurrence should be construed as merely illustrative, not as limitation.Therefore, exemplary embodiment
Other examples can have different values.
Embodiment
Fig. 1 is the structural schematic diagram of flight formula cable provided in an embodiment of the present invention.
Shown in Figure 1, a kind of flight formula cable, including cable main body 100, being provided in the cable main body 100 can
Carry the aircraft 200 of cable ontology flight.
Cable is the general designation of electric wire, optical cable, cable and other items.There are many uses of the cable, is mainly used for control installation, connects
It the multiple actions such as connects equipment, transmit electric power, being a common and indispensable thing in daily life.The so-called line of the present invention
Cable ontology, including electric wire, cable, optical cable etc. are commonly used for instrument, instrument, intercommunication, monitoring, control and install, electric appliance,
Instrument, the signal transmission of power distribution equipment, control, measurement, cable television, broadband networks private cable, telephone communication and radio are set
Junction box wiring use of standby connection and telephony wiring net etc..
Aircraft refers to the instrument that can be flown, and is specifically unmanned plane in embodiments of the present invention, is to utilize nothing
The not manned aircraft that line electrical remote control equipment and the presetting apparatus provided for oneself manipulate.The aircraft being arranged in the cable main body,
It is either one or more, it can be adjusted according to length, the weight etc. of cable.It, can when using multiple aircraft
Make to cooperate with flight between multiple aircraft, according to the mode of flight environment of vehicle adjustment flight.The mode of the flight, including when flight
Shape, posture, height of cable main body etc..
Aircraft includes flying power unit, and flying power unit includes flying platform and power source.
Rotor structure, fixed wing structure, jet-propelled structure, dirigible, umbrella wing structure or flapping wing structure can be used in flying platform
Deng.Piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle, punching type or jet-propelled, this implementation can be used in flight dynamic devices
Power plant in example uses electrodynamic type engine.
Power source may be used one or more such as under type.
Mode one, is arranged power supply on board the aircraft.The power supply such as battery carried by aircraft provides power source.Make
To be for example and not limitation, power supply can be accumulator in aircraft, and the power plant of accumulator and flying wing is electrically connected
It connects.It is easily understood that in the case that charging head is equipped with battery, can charging circuit be set on the circuit board of charging head, fill
Circuit is used to charge for battery in battery capacity deficiency.The charging circuit is known to those skilled in the art,
For example, charging circuit includes sequentially connected voltage reduction module, rectification module and filter module, the voltage reduction module is used for will be external
Power supply High Level AC Voltage is converted into low-voltage AC, and the rectification module is used to low-voltage AC being converted into low-voltage DC,
The filter module is for being filtered the direct current after rectification.The circuit board of charging head can also include with overvoltage and mistake
The Voltage stabilizing module for flowing protective effect prevents overvoltage or overcurrent from causing the damage of circuit components.The Voltage stabilizing module is this field
Well known to technical staff, details are not described herein again.
Flight power interface is arranged in mode two in cable main body, and flight power interface is connect with aircraft electrical, by this
Interface obtains power supply.In view of cable itself is typically to charge, flight power interface can be set directly on cable, flown
Power interface is connect with aircraft electrical, and power supply is obtained by the interface.Certainly, the current type needed according to aircraft, can be with
The equipment such as current converter and/or rectifier are set on power interface.
Flight power source special is arranged in mode three, is electrically connected power source special and aircraft.In addition flight Special electric is set
Source is not arranged in aircraft sheet, also not against cable main body.
In this implementation, preferred employing mode two provides power source.In view of safety, it is provided with and connects in cable main body
Ground structure is as safety device.The conducting wire that electric current is introduced to the earth is set,
In electrical equipment loophole or overtension, electric current can enter the earth by the conducting wire of ground connection, play the role of safeguard protection.
Another embodiment provides the structure of the flight formula cable with support construction.Being provided in cable main body can be following
Square supporting surface, into the support construction being supported to cable main body, cable sheet is adjusted by the support construction as fulcrum force
The position of body.Suitably reduce cable to other objects in environment during the flight of flight formula cable, the grounding with this
Caused by influence.
The support construction being arranged below cable main body is solid support object, such as supporting rod, supporting rack etc..Referring to Fig. 2 institutes
Show, 100 lower section of cable main body is provided with the support construction 230 realized using lower section supporting surface as fulcrum force, in flight formula
During cable flies and/or grounds, the position that the support construction 230 adjusts electric wire can be passed through.As an example rather than limit
System, shown support construction 230 can be mounted in cable main body, can also be to preset on the support surface.For preceding
Support construction can be generally mounted in cable main body by hinged shaft, controls support construction when needed with respect to cable sheet by person
It hangs down after body rotation；For the latter, flight formula cable is in flight preferentially according to the position setting flight road where support construction
Cable can be accurately placed in support construction top by diameter.
It may need to cross over the water surface when in view of flight, further, floating body can be set in the support construction, it is described floating
Body enables the support construction to provide support force using the water surface as supporting surface.
In another embodiment, flight formula cable further includes alarm unit, the alarm unit for monitoring of environmental information and
The power source balance information of aircraft, and the information of acquisition is sent to flying vehicles control center, flying vehicles control center according to
The flight of the information adjustment aircraft received.The flying vehicles control center can be by way of example and not limitation aircraft
The flight controller of itself can also be the ground control station for being placed in ground.
For the aircraft of flight formula cable, can itself be provided with control system, can intelligently plan, adjust itself
And/or the Intelligent flight device of other aircraft collaboration flight, can also be itself do not have control system, need according to ground or
The aircraft that the control of other equipment is flown, can also be the combination of two groups of aircraft above.Fig. 3 is the embodiment of the present invention
The structural schematic diagram of the flight formula cable including the first aircraft provided.It includes first that Fig. 4, which is provided in an embodiment of the present invention,
The structural schematic diagram 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
210, cable main body connection unit 220, and the navigation of control flight parameter fly control unit (not shown).
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 fly 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
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.In this way, imitate the Nature in migratory bird moving when flock of birds flying method, first
Aircraft is similar to leading bird, and the second aircraft follows the first aircraft, similar to the flock of birds for following leading bird flying, flying
It is middle to keep certain formation that effectively utilize air-flow, reduce energy expenditure in-flight.
In another embodiment, further include recognition unit on flight formula cable to accurately judge that the position of destination.
The recognition unit can be identified by acquisition image information and/or audio-frequency information and judge the position where electrical equipment.Make
It is for example and not limitation, such as setting camera shooting mechanism and image identification unit on board the aircraft, outdoor scene is acquired by imaging mechanism
Image judges location information after identifying image by image identification unit.Acquire audio-frequency information structure can be mounted on
Carry-on microphone.
The method of identifying purpose position also can be by wireless location side in addition to acquisition image information and/or audio-frequency information
Wireless positioning unit can be arranged in formula on the aircraft of flight formula cable, corresponding, be provided on the destination locations wireless
Signal transmitting and receiving unit, the signal of the wireless positioning unit acquisition wireless messages Transmit-Receive Unit, identifies and judges destination locations
Position.Location technology common at present mainly has PPD location technologies, GPS satellite to position, bluetooth positions, WIFI network positions,
Big Dipper positioning, the positioning of GPRS/CDMA mobile communication technologies etc..By currently used based on for mobile terminal positioning technology, it is somebody's turn to do
The principle of location technology is：The Base Transmitter signal of multiple known locations, emitted signal carry related with base station location
Characteristic information determines its geometry site between each base station, and according to phase after mobile terminal receives these signals
It closes algorithm and positioning estimation is carried out to its own position, to obtain the location information of itself.
Certainly, above-mentioned two groups of identification structures can be also set simultaneously, and it is suitable so to be selected according to flight environment of vehicle such as weather
Mode obtain destination locations information.By way of example and not limitation, such as in foggy weather, poor visibility is known using image
When not ineffective, the identification method of audio-frequency information identification or wireless location can be used.
Further, the interface for the wiring point installation interface message for obtaining destination is provided in the present embodiment, on aircraft
Positioning unit, and installation interface fixed structure and installation interface embedded structure, the installation interface fixed structure are used for line
Cable is located on installation interface or installation interface near zone, and the installation interface embedded structure is for cable connector to be mounted on
In erection joint.
The installation interface that one end of cable or some medium position are fixed on to some wiring point may be needed when wiring
On, it is therefore desirable to the interface position unit of the charging interface location information of electrical equipment can be accurately acquired.In interface position
Cable can be located on installation interface by unit after obtaining the location information for installing interface by installing interface fixed structure
Or installation interface near zone, then cable connector is mounted in erection joint by installing interface embedded structure.The peace
Attaching mouth fixed structure can be by way of example and not limitation gripper, sucker, preferably magnechuck；The installation interface is embedding
Enter structure, can be telescopic elements or collapsible element by way of example and not limitation, installation interface institute is directed in cable connector
It postpones in place, cable connector is inserted into installation interface and realizes installation 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 for the corresponding function of realization.
Another embodiment of the present invention provides a kind of wiring system of flight formula cable, including：It is above-mentioned that there is flight
The flight formula cable and starting point fixed interface of device are used for the starting end side of fixed cable.According to wiring installation needs,
Wiring point installation interface can also be set, for cable to be 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 walks as follows
Suddenly.
S100, the starting end side of fixed flight formula cable.By way of example and not limitation, it for example needs on two power towers
When erecting power lines road, one end of cable is fixed on a power tower first.The initiating terminal comprising but it is not limited to cable
Initial end, by way of example and not limitation, for example the wiring of a cable is divided into continuous three phases, phase III by user
Initiating terminal can be second stage clearing end, and the initial end of the clearing end of second stage and non-cable.
S200, flight formula cable are flown by aircraft thereon to wiring point position.
In the present embodiment, flight formula cable flown by aircraft thereon include to the step of wiring point position：Fly
Positioning unit on line cable or ground control station at least one obtains the location information where wiring point；According to the position of acquisition
Confidence breath controls the flight formula cable and flies to wiring point position.
The interface position list for the wiring point installation interface message for obtaining destination is provided in the present embodiment, on aircraft
Member, and installation interface fixed structure and installation interface embedded structure include in the step of wiring point upper fixed line cable：Interface is fixed
Bit location obtains the location information of wiring point installation interface；According to the control of the location information of acquisition accordingly cable is carried to aircraft
It drop to installation interface position；By installing, cable is located on installation interface by interface fixed structure or installation interface is attached
Near field；Cable connector is mounted in erection joint by installing interface embedded structure.
Further, when being provided with alarm unit on 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 flying vehicles control center；The alarm unit prison
When measuring environment and being unsuitable for continuing flight and/or power source surplus deficiency, alarm signal is sent to flying vehicles control center；Flight
Device control centre adjusts the course line of aircraft and/or the flight quantity of aircraft according to the information received.
Foregoing description is only the description to present pre-ferred embodiments, not to any restriction of the scope of the invention, this hair
The range of bright preferred embodiment includes other realization, wherein work(can not be executed by sequence that is shown or discussing
Energy.Any change, the modification that the those of ordinary skill in field of the present invention does according to the disclosure above content, belong to claims
Protection domain.
Claims (13)
1. a kind of flight formula cable, including cable main body, it is characterised in that：Cable sheet can be carried by being provided in the cable main body
The aircraft of body flight；
It is provided with the support construction being supported using lower section supporting surface as fulcrum force to cable main body in cable main body, passes through
The position of the support construction adjustment cable main body；
The support construction can be rotated relative to cable main body；
It is provided with floating body in the support construction, support can be provided using the water surface as supporting surface by support construction described in floating body
Power.
2. flight formula cable according to claim 1, it is characterised in that：The power source of aircraft in the following way one
Kind is a variety of,
Mode one, is arranged power supply on board the aircraft；
Mode two, is arranged flight power interface in cable main body, and flight power interface connect with aircraft electrical, connect by this
Mouth obtains power supply；
Flight power source special is arranged in mode three, is electrically connected power source special and aircraft.
3. flight formula cable according to claim 1, it is characterised in that：Ground structure is provided in cable main body.
4. flight formula cable according to claim 1, it is characterised in that：Further include alarm unit, the alarm unit is used
It is sent to flying vehicles control center in the power source balance information of monitoring of environmental information and aircraft, and by the information of acquisition, is flown
Hang Qi control centres adjust the flight of aircraft according to the information received.
5. flight formula cable according to claim 1, it is characterised in that：The aircraft be it is multiple, including first flight
Device, first aircraft include flying power unit, cable main body connection unit, and the winged control of navigation of control flight parameter
Unit.
6. flight formula cable according to claim 1, it is characterised in that：The aircraft be it is multiple, including second flight
Device, second aircraft includes flying power unit, cable main body connection unit, and is flown in response to what control was flown
Row response unit.
7. flight formula cable according to claim 1, it is characterised in that：The aircraft be it is multiple, including 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.
8. flight formula cable according to claim 1, it is characterised in that：It is provided on aircraft,
Obtain the interface position unit of the wiring point installation interface message of destination；
And installation interface fixed structure and installation interface embedded structure, the installation interface fixed structure are used to position cable
On installation interface or installation interface near zone, the installation interface embedded structure are used to cable connector being mounted on installation and connect
On head.
9. a kind of wiring system of flight formula cable, it is characterised in that including：
Flight formula cable described in any one of claim 1-8；
Starting point fixed interface is used for the starting end side of fixed cable.
10. a kind of wiring method using flight formula cable described in claim 1, it is characterised in that including step：
The starting end side of fixed flight formula cable；
Flight formula cable is flown by aircraft thereon to wiring point position.
11. wiring method according to claim 10, it is characterised in that：
Flight formula cable is flown by aircraft thereon,
Positioning unit on flight formula cable or ground control station at least one obtains the location information where wiring point；
The flight formula cable is controlled according to the location information of acquisition to fly to wiring point position.
12. according to the method described in claim 10, it is characterized in that：
The interface position unit for the wiring point installation interface message for obtaining destination is provided on aircraft, and installation interface is consolidated
Determine structure and installation interface embedded structure, include in the step of wiring point upper fixed line cable,
Interface position unit obtains the location information of wiring point installation interface；
According to the control of the location information of acquisition is corresponding installation interface position is drop to aircraft carrying cable；
Cable is located on installation interface or is installed interface near zone by installing interface fixed structure；
Cable connector is mounted in erection joint by installing interface embedded structure.
13. according to the method described in claim 10, it is characterized in that：It is provided with alarm unit on flight formula cable, passes through institute
Power source balance information of the alarm unit for monitoring of environmental information and aircraft is stated, and the information of acquisition is sent to aircraft
Control centre；
When the alarm unit monitors that environment is unsuitable for continuing flight and/or power source surplus deficiency, into flying vehicles control
The heart sends alarm signal；
Flying vehicles control center adjusts the course line of aircraft and/or the flight quantity of aircraft according to the information received.
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 |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Family Cites Families (1)
| 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 |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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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