CN108320410A - A kind of aviation for aerial cable warns ball system - Google Patents
A kind of aviation for aerial cable warns ball system Download PDFInfo
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- CN108320410A CN108320410A CN201810309224.9A CN201810309224A CN108320410A CN 108320410 A CN108320410 A CN 108320410A CN 201810309224 A CN201810309224 A CN 201810309224A CN 108320410 A CN108320410 A CN 108320410A
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- China
- Prior art keywords
- warning
- unit
- shell
- aerial cable
- global shell
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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
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B5/00—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied
- G08B5/22—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission
- G08B5/36—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission using visible light sources
- G08B5/38—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission using visible light sources using flashing light
-
- 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
- H02G7/00—Overhead installations of electric lines or cables
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- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Emergency Alarm Devices (AREA)
Abstract
The present invention relates to low-latitude flying aircrafts to warn field, ball system is warned more particularly, to a kind of aviation for aerial cable, to solve the complexity of installation process and using the uncontrolled property of process, make whole installation process save trouble and labor, while increasing the intelligent effect of its application.This system includes that high voltage induction takes electric unit, including mutual inductor and power-supply controller of electric, and wherein mutual inductor is open-type structure, grasps and is fitted on the aerial cable crossed inside warning global shell and obtains electric energy；Support unit is grasped and is fitted on the aerial cable crossed inside warning global shell, for global shell will to be warned tightly fixed with aerial cable；Information process unit, the energy information for taking the output signal and LED light-emitting caution units of electric unit for handling high voltage induction；LED light-emitting caution units are installed on for half built-in in warning global shell；Global shell is warned, global shell will be warned to be fixed on aerial cable for passing through support unit.
Description
Technical field
The present invention relates to low-latitude flying aircrafts to warn field, is warned more particularly, to a kind of aviation for aerial cable
Ball system.
Background technology
With the fast development of General Aviation, domestic navigation accident happens occasionally, and ascendant trend year by year is presented in recent years,
Between 2014 to 4 years 2017, domestic generation 6,12,23 and more than 40 respectively plays general aviation accident, wherein is related to
The accident that aircraft is breasted the tape is up to 15, dead 18 people.According to incompletely statistics, aerial cable is still that all purpose aircraft low latitude flies at present
Capable No.1 danger.In addition, navigation is breasted the tape, aircraft accident also easily causes the damage of national grid circuit, or even causes serious
Power outage brings larger impact to national economy and social development.Therefore, it is necessary to a kind of effective precautionary measures to prevent accident
Generation.According to states such as International Civil Aviation Organization (ICAO), Federal Aviation management board (FAA) and China Civil Aviation offices (CAAC)
Corresponding policy that border and each Economic Growth of Civil Aviation Transportation relevant industrial department formulate, clear stipulaties low latitude cable should install flight obstacle mark
Will.Currently used way is to install aviation warning ball additional on the cable of low latitude, because spheroid form has uniform force, keeps flat
It weighs, avoid substantially swinging, the protection effect advantages such as preferably, the abrasion to aerial cable can be effectively reduced.
The aviation warning ball of domestic and international overhead transmission line installation is broadly divided into two types, and the first kind is mounted to aerial earth wire
Or on OPGW cables, warning function is provided by itself larger volume and conspicuous color；Second class is on the basis of preceding a kind of
It installs lighting apparatus additional, increases the effect of active light-emitting caution.Lighting apparatus can warn ball to be combined into one with aviation, integral installation
In on aerial condutor, also ball can be warned to separate with aviation, it is separately installed on aerial condutor.The first kind fills for non-luminescent warning
It sets, can only be played a warning role between daytime, then without effect, such setting of part improvement under night or bad weather condition
It is standby, by installing reflective tape, speculum or reflecting coating etc. additional outside sphere, wish to meet night flight needs with this, but practical
On can not but meet civil aircraft night low-latitude flying to effective identification of aerial cable requirement.In addition, such equipment is long
It is easily faded with rear outer surface, influences using effect.Second class is self light emitting warning device, external technology and relevant device
Existing defects in practical applications fail to be widely applied.Often spininess is existing to constructing for domestic technology and relevant device
The big machinery of field or the large vessel etc. of streamway, and play the role of a kind of external force damage prevention protection to aerial cable, equally
Requirement of the civil aviaton to aerial cable light intensity, flicker frequency and beam distribution etc. cannot be met.Now it is applied to make somebody a mere figurehead by existing
The common disadvantage of all aviations warning ball equipment on cable is summarized as follows：
Most products market assessment is not high, and service life falls short of, and is easily damaged aerial cable, leads to power grid O＆M list
Position installation wish is not strong.
Invention content
The technical problem to be solved by the present invention is to：In view of the problems of the existing technology, it provides a kind of for overhead line
The aviation of cable warns ball system.
Further, by the way that multigroup warning lamp unit is arranged and the color of warning lamp unit is arranged, warning effect is improved；
The non-luminescent caution device of the prior art is overcome to cannot be satisfied the movable warning demand of night flying；Existing self light emitting warning equipment
Luminescent color, beam distribution, flash duration, flicker frequency, brightness etc. do not meet civil aviaton's industry and warn dress to aviation
The problems such as technology set requires.
Further, by the way that power-supply controller of electric is arranged, overcome prior art warning light system poor work stability：Such as：
Existing Current Mutual Inductance electricity getting device poor work stability, is vulnerable to the influence of line current, and line short high current can puncture
The problems such as equipment, line current is too small and can not work normally, poor reliability.
Further, by positioning function in information process unit, overcome later maintenance and management inconvenient：Existing apparatus
It cannot achieve low-latitude flying cultural obstacle location information acquisition function and working state of device on-line monitoring and back-stage management
Function.After leading to equipment damage, O＆M unit cannot be found in time, and position cannot accurately determine, it is easier to which initiation accident etc. is asked
Topic.
The technical solution adopted by the present invention is as follows：
A kind of aviation warning ball system for aerial cable includes：
High voltage induction takes electric unit, is arranged and is fixed in system inner cavity, is obtained from the aerial cable inside warning global shell
Electromagnetic induction energy is taken, and exports electric energy；
Support unit is arranged and is fixed in system inner cavity, grasps and is fitted in and crosses making somebody a mere figurehead inside warning global shell
On cable, for that global shell will be warned to be fixed with aerial cable；
Information process unit, is arranged and is fixed in system inner cavity, and electric unit is taken for handling and exporting high voltage induction
The energy information of output signal and LED light-emitting caution units；
LED light-emitting caution units are installed on for half built-in in warning global shell；
Global shell is warned, global shell will be warned to be fixed on aerial cable for passing through support unit, keep warning ball system
System balance.
Further, the support unit is at least 2n, is evenly distributed on high voltage induction and takes electric unit and warning ball
On aerial cable between shell, n is more than or equal to 1.The support unit includes upper half component and lower half component, wherein upper half
Component is formed such that the hollow knot that support unit is grasped and is fitted on the aerial cable of warning global shell inside with lower half component
Structure；First junction is connected by hinge mode；The second junction of support unit is located at tight in bolts assemblies slot by one end
Hoop formula connector is fixed on aerial cable so that warning global shell is fixed on aerial cable；Wherein the first junction, second
Junction refers to upper and lower half structure junction.The effect of support unit, which is arranged, is：High voltage induction, which can be fixed, takes electric unit in frame
It is not overturn on ceases to be busy cable, prevents aviation warning ball from loosening and even fall.
Further, it includes mutual inductor and power-supply controller of electric that the high pressure, which takes electric unit,；Wherein mutual inductor includes that electric current is mutual
Sensor and the bolts assemblies slot being arranged on current transformer；The upper and lower half hitch of current transformer is configured to so that high pressure takes
Electric unit is fitted in the hollow groove of aerial cable；Bolts assemblies slot is arranged in upper and lower half structure edge；High voltage induction takes electricity
The first junction of unit passes through hinge connection；High voltage induction takes the second junction of electric unit to be located in bolts assemblies slot by one end
Hooped type connector be fixed on aerial cable；Support unit includes upper half component and lower half component, wherein upper half component with
Lower half component is formed such that support unit grasps and is fitted in the hollow structure inside warning global shell on aerial cable；First
Junction passes through hinge connection；The second junction of support unit is located at the hooped type connector in bolts assemblies slot by one end and consolidates
It is scheduled on aerial cable so that warning global shell is fixed on aerial cable；Wherein the first junction, the second junction refer to
Upper and lower half structure junction；Specific first junction can be that symmetrical side or the first junction second connect with the second junction
Place is met not in symmetrical side.Effect is：High voltage induction, which can be fixed, takes electric unit not overturn on aerial cable, prevents aviation from warning ball
It loosens and even falls.
Further, the warning global shell is the upper half-shell and housing lower half of mirror image, upper half-shell
And the first junction of housing lower half, by hinge connection, the second junction of upper half-shell and housing lower half passes through locker
Formula connector connects.Specific first junction and the second junction can be the second junctions of symmetrical side or the first junction
Not in symmetrical side；Structure symmetrical above and below is conducive to the setting of aviation warning ball stabilization on aerial cable, prevents aviation from warning
Ball, which loosens, even to be fallen.
Further, the high voltage induction takes the power-supply controller of electric of electric unit, information process unit to be located at lower housing cavity
In one support plate of interior setting or on the lower shell surface of warning global shell；It is described to incude the mutual inductor for taking electric unit, support
Unit bottom end is fixed in another support plate being arranged in lower housing cavity or on the lower shell surface of warning global shell；Support plate
It is provided in plane parallel to the ground in warning global shell.The effect reached is：High voltage induction takes electric unit, information processing list
Member is more stabilized in warning global shell so that entire aviation warning ball is not easy to overturn, it is not easy to which generation, which loosens, even to be fallen
The case where.
Further, the warning global shell is sphere；The support plate is plectane；Wherein radius of sphericity range is 30-
150cm；The warning global shell material is metal alloy compositions.
Further, LED light-emitting cautions unit includes m group warning lamp units, and p groups are arranged in warning global shell upper half-shell
M-p group warning lamp units are respectively set in warning lamp unit, housing lower half；Wherein m is equal to 2p or p and is not equal to m-p.
Further, the m=2；With sphere bottom at the top of the sphere, that is, warn global shell upper half-shell top under
One group of half built-in warning lamp unit is respectively set in half shell bottom end.
Further, the aerial cable passes across at the circular hole of warning ball system exterior surface, and circular hole was located at
In the plane parallel to the ground of center point.
Further, the warning spherical shell external surface is set as different colours, is arranged at intervals on aerial cable.Reach
Effect be：Meet the movable warning demand of day flight；The color of ball is warned by the way that aviation is arranged, and improves the identification of warning ball
Degree.
Further, further include Cloud Server, described information processing unit is remotely connect with Cloud Server；Information processing list
The work state information of LED light-emitting caution units is sent to Cloud Server by member in real time, and Cloud Server can be right according to these data
The working condition of specific aviation warning ball is monitored, and can be positioned to it when information process unit breaks down.
Reaching effect is：Solving the problems, such as that product function is single causes user to be unwilling to install, and most products market assessment is not high,
The effect of eye-catching warning only between daytime causes power grid O＆M unit installation wish not strong.In addition, after equipment damage, O＆M unit
It cannot find in time, position cannot accurately determine, it is easier to the problem of causing accident.By information process unit, solve well
It has determined the above problem.
In conclusion by adopting the above-described technical solution, the beneficial effects of the invention are as follows：
1, the present invention has carried out modularized design, and compact overall structure is easy for installation, avoids common aerial cable boat
Empty alarming device is easier, rapid in the complexity installed；
2, the LED light-emitting caution units of this system use 3 paths of LEDs chip light sources, extend service life, while by matching
Light design and control system ensure that luminescent color, beam distribution, flash frequency, flash model, synchronous flashing, duty ratio, from
The low environment luminance threshold setting etc. for starting photosensitive switch meets civil aviaton's requirement；
3, this system is by information process unit, energy fast-positioning device specific location and its working condition, in time actively
Reporting fault information is convenient for remote monitoring and maintenance management, realizes low-latitude flying for aerial cable flight obstacle mark
Real demand, while can also play the role of well protect electric power cable, for safeguard people's life and national wealth peace
It is complete to create value.
Power-supply controller of electric and information process unit warn global shell center of gravity relative to entire warning ball system weight very little
Stablize, has and do not change the stress structure of aerial cable under the action of the wind, the effect of aerial cable fatigue will not be accelerated.
This system has carried out modularized design, and compact overall structure is easy for installation, avoids common aerial cable aviation
Alarming device is easier, rapid in the complexity installed；This system ensure that luminous by light distribution design and control system
The low environment luminance threshold of color, beam distribution, flash frequency, flash model, synchronous flashing, duty ratio, self-starting photosensitive switch
Value setting etc. meets the technology requirement of civil aviaton's professional standard；This system uses GPS positioning module, can fast-positioning device tool
Body position and its working condition, timely active reporting fault message are convenient for remote monitoring and maintenance management, realize low-latitude flying
For the real demand of aerial cable flight obstacle mark, while can also play the role of protecting electric power cable well,
To safeguard that people's life and national wealth create safely value.
Description of the drawings
Examples of the present invention will be described by way of reference to the accompanying drawings, wherein：
Fig. 1 is internal system structure and connected mode schematic diagram.
Fig. 2 is this system high-level schematic functional block diagram.
Fig. 3 a are locker formula interface unit position and schematic diagram.
Fig. 3 b are locker formula interface unit structural front views.
Fig. 4 is the mutual inductor and locker formula interface unit structural front view that induction takes electric unit.
Fig. 5 a are the mutual inductor front views that induction takes electric unit.
Fig. 5 b are the upward views for the mutual inductor that induction takes electric unit.
Fig. 5 c are the vertical views for the mutual inductor that induction takes electric unit.
Fig. 5 d are the left views for the mutual inductor that induction takes electric unit.
Fig. 5 e are the right views for the mutual inductor that induction takes electric unit.
Fig. 6 is support unit structural front view.
Fig. 7 a are the front views of support unit.
Fig. 7 b are the upward views of support unit.
Fig. 7 c are the vertical views of support unit.
Fig. 7 d are the left views of support unit.
Fig. 7 e are the right views of support unit.
1- warns global shell 2- mutual inductor 3- power-supply controller of electric
4- information process unit 5- warning lamp unit A 6- warning lamp unit Bs
7- light source controller 8- luminous component 9- hooped type interface units
10- support unit 11- locker formula interface unit 12- temperature sensors
A- bolt b- handles
Specific implementation mode
All features disclosed in this specification or disclosed all methods or in the process the step of, in addition to mutually exclusive
Feature and/or step other than, can combine in any way.
Any feature disclosed in this specification unless specifically stated can be equivalent or with similar purpose by other
Alternative features are replaced.That is, unless specifically stated, each feature is an example in a series of equivalent or similar characteristics
.
One, this system forms：
This system include high voltage induction take electric unit, information process unit, LED light-emitting cautions unit, support unit and
Warn global shell.
1, high voltage induction takes electric unit：
11) it includes that the mutual inductor of bolts assemblies slot is arranged (i.e. in two structural portions of original setting that high voltage induction, which takes electric unit,
Divide and (is named as half structure (or top half, as shown in Figure 4) and lower half structure (or lower half portion, as shown in Figure 4))
Current transformer on the basis of, increase by the bolts assemblies slot that two structures can be fixed together) and power-supply controller of electric, mutual inductor
It grasps and is fitted on the aerial cable crossed inside warning global shell, electromagnetic induction energy is obtained from aerial cable, and lead to
Cross the stable electric energy of power-supply controller of electric output；Mutual inductor shape is not fixed.Mutual inductor be open-type take can mutual inductor or other
The mutual inductor of identical function；Power-supply controller of electric reaches effect：The unstable line that can will be acquired by high voltage induction unit
Road electric energy is converted into stable can be used to ensure that, and the electric energy that information process unit and LED light-emitting caution units work normally for a long time is defeated
Enter.
12) high voltage induction takes electric unit to be fixed on the center for warning global shell inner transverse end face wire channel, can
To be fitted closely with aerial cable by hooped type interface unit.Power-supply controller of electric takes energy mutual inductor 2 to connect by conducting wire with open-type,
At its upper position, and it is placed in the circular shelf set in aluminum spherical housing and fixes.High voltage induction takes electric unit to obtain
After obtaining electromagnetic induction energy, high voltage induction is taken the electric energy that electric unit exports through over commutation, filtering, charge and discharge fulgurite by power-supply controller of electric
The processing such as reason, are converted into stable output voltage and electric current.
13) high voltage induction take the power-supply controller of electric of electric unit, information process unit be located at setting support plate on or
Person warns the inner surface of global shell.
2, support unit：
1), support unit quantity：
Support unit is at least 2n, is evenly distributed on high voltage induction and takes making somebody a mere figurehead between electric unit and warning global shell
On cable, n is more than or equal to 1.
Specially：
When support unit is two, it is arranged and takes electric unit in high voltage induction and warn the aerial cable between global shell
On.
When support unit is four, takes the survey of electric unit two to be evenly distributed in high voltage induction and two support units are set.
2), support unit material：Metal alloy compositions, such as aluminium alloy.
3), support unit shape：Grasp and be fitted in cross it is hollow, just on the aerial cable inside warning global shell
The bodies such as cube, cylinder shape (as shown in figure 4, cylindrical shape), concrete structure is described as：Support unit is by the two of upper and lower mirror symmetry
Part forms, and upper and lower two parts (as shown in fig. 6, upper and lower half point) are connected by hooped type connector, specially side be by
Hinge-type interface unit connects, and the other side is connected by hooped type interface unit.
Support unit is fitted closely using hooped type interface unit with aerial cable, hooped type connector (as described in Figure 4)
Bolt including handle, in bolts assemblies slot and the fixing end in bolts assemblies slot；Handle turns with bolt one end
Dynamic connection (such as hinged)；The bolt other end is rotatablely connected (such as articulated manner realization) with fixing end；The fixing end setting
In up or down half structure fitting groove；When hooped type connector fastens, handle correspond to fastening on taking electric unit half structure or
Under support unit or at upper half structure；When handle unclamps, then hooped type connector unclamps.Support unit warns spherical shell with aviation
Body securely connects, and after ensureing that the aerial cable in support unit is securely locked, entire shell will not all move, will not be to frame
Ceases to be busy cable damages, the phenomenon that being fallen off after avoiding this system from being used for a long time.
Such as：Support unit is two, and there are three hooped type interface units, in addition to two for support unit to be fixed on
Outside aerial cable, there are one being taken on electric unit positioned at high voltage induction, electric unit is taken for secure lock high voltage induction, make its with
Aerial cable holding fits closely state.High voltage induction takes the mutual inductor of electric unit to be connect with warning global shell, also functions to guarantee
Warning global shell will not move on aerial cable.It is fixed that high voltage induction, which takes the relative position of electric unit and support unit,
's.
3, information process unit；
Including information acquisition unit, main control unit, host computer management software unit and GPRS communication units.
31) information process unit hardware includes information acquisition unit, main control unit and GPRS communication units, information processing list
First hardware installation is simultaneously fixed in the cavity of 1 housing lower half of shell, and is placed in the circular shelf set in shell and is fixed.It is upper
Machine management software unit is communicated by agreement with main control unit.The importation of information process unit hardware by conducting wire with
Power-supply controller of electric connects.
Information acquisition unit can be by the LED light source operating voltage and operating current of the warning lamp unit of aerial cable conducting wire
Real time information and high voltage induction take the output current of electric unit and output voltage information collection and transfer data to master control
Unit is sampled；
32) main control unit realizes the control, calculating, communication management of entire information process unit.
33) host computer management software unit includes the two kinds of human-computer interaction interfaces in the ends PC or mobile phone terminal and operation program；For
Remote control.
34) GPRS communication units by GPRS communication modules and main control unit communicate, and information process unit can lead to
It crosses GPRS module and is connected to internet, after networking, information process unit will be actively connected to specified Cloud Server, then carry out
Data exchange, including upload information data download control command etc..User is connected to cloud by host computer management software unit
Server inquires instant data information or publication control command, the long-range real time monitoring realized to this system.
4, LED light-emitting cautions unit：
P group half built-in warning lamp units, housing lower half is arranged in warning global shell upper half-shell in m group warning lamp units
M-p group half built-in warning lamp units are respectively set；Wherein m is equal to 2p or p and is not equal to m-p；
Work as m=2p and is divided into two kinds when p group warning lamp units are respectively set with housing lower half in warning global shell upper half-shell
Situation：
When p is odd number, one group of warning lamp unit is respectively set with housing lower half central point in upper half-shell, remaining p-1 is a
Warning lamp unit is uniformly distributed evenly around upper half-shell or housing lower half central point, and m is more than or equal to 0.
When p is even number, p warning lamp unit is uniformly respectively in upper half-shell or housing lower half；
When p is not equal to m-p, when p group warning lamp units are respectively set with housing lower half in warning global shell upper half-shell, point
For following several situations：
1) when warning global shell upper half-shell or odd number group half built-in warning lamp unit is arranged in upper half-shell；Upper half shell
One group of half built-in warning lamp unit is respectively set in body and housing lower half central point, remaining p-1 warning lamp unit evenly around
Upper half-shell or the uniform half built-in distribution of housing lower half central point, m are more than or equal to 0.
2) when warning global shell upper half-shell or even number set half built-in warning lamp unit is arranged in upper half-shell, even number set
The uniform half built-in of warning lamp unit is respectively in upper half-shell or housing lower half；
Warning lamp unit includes that light source controller 7 and luminous component 8 form, and wherein luminous component includes LED chip, glass
Lens, lampshade, radiator structure.LED chip uses spare management design, specially three tunnels, wherein be work LED chip all the way,
In addition two-way is spare LED chip, and after the LED chip that works breaks down, light source controller can switch and enable spare in time
LED chip to ensure the longer work service life of warning lamp unit, and provides sufficient repair phase buffer and is convenient for maintenance personnel
Timely more exchange device.Light source controller is connect with m group warning lamp units respectively, provides the stabilized driving voltage and electric current of m groups, is protected
Hinder its normal work.In addition, also controlling flash frequency, flash model, synchronous flashing, the duty ratio of m group warning lamp unit light sources
And the low environment luminance threshold of setting self-starting photosensitive switch.Glass lens is semicircle sphere, and it is empty to form closing with lampshade bottom surface
Between, LED chip is formed in glass lens and bottom surface in enclosure space.Lampshade also forms an enclosure space with lampshade bottom surface.
Upper housing lower half is all made of luminous component and lampshade is placed outside warning global shell and radiator structure and other component are built in warning
The assembling form of the half built-in of global shell.Radiator structure is aluminum material, and heat output channel is provided for LED chip work,
It is at normal operating conditions.
Such as：As m=0, warning lamp is respectively set with housing lower half least significant end in warning global shell upper half-shell top
Unit A and B；
It is a sphere when warning global shell, when upper half-shell top and housing lower half are all hemispheres, warning lamp list
First A and the luminous component of warning lamp unit B is external and radiator structure built-in i.e. half is embedded is mounted on warning global shell.
LED light source A and LED light source B technical parameters having the same and performance, respectively half built-in be fixed on warning spherical shell
At the circular hole of two longitudinal terminal surfaces (top and bottom end) of the upper and lower hemispheres of body case 1, and luminous component is external.With conventional white light
The red optics light distribution part of chip collocation is compared, and the efficiency of light energy utilization higher of this luminous component is more energy saving.In addition, LED chip point
For 3 tunnels, 1 tunnel is work LED chip, remaining two-way is spare LED chip, and the power that uses per paths of LEDs chip is 8W, is shone strong
Degree is not less than 400cd.Light source controller be used for the flash frequency of LED light source A and LED light source B, flash model, synchronous flashing,
Duty ratio, self-starting photosensitive switch low environment luminance threshold be managed, and by main control unit and GPRS communication units, build
Vertical contacting with host computer management software unit, realization remote monitoring.The importation of light source controller and information process unit
The output par, c of hardware is connected by conducting wire, and the output par, c of light source controller is connect with LED light source A and LED light source B.Light source
Controller is placed in the circular shelf set in aluminum spherical housing and solid together with information process unit hardware and power-supply controller of electric
It is fixed.
As m=1, warning lamp unit A is respectively set with housing lower half least significant end in warning global shell upper half-shell top
And B, it then warns and is uniformly arranged 2 warning lamp units respectively on global shell upper half-shell top and housing lower half.
5, global shell is warned.
51) structure：It is described warning global shell be mirror image upper half-shell and housing lower half, upper half-shell with
And housing lower half connects (such as Fig. 3 a and 3b) by locking clip adapter.
52) material：It is metal material, such as aluminum material etc..
53)：Warn global shell in addition to the stress structure of aerial cable under the action of the wind is not changed, frame will not be accelerated
The effect of empty cable fatigue, while playing the role of protecting ball interior electronic component, improving its service life.Warn spherical shell
Trepanning at the upper half-shell top end surface and housing lower half bottom end face of body, for being embedded in LED luminescence units and it being kept to shine
Component is external.It is diametrically symmetrical at it in upper half-shell and housing lower half calmodulin binding domain CaM to warn the fixed structure of global shell
Position at be arranged two interface units, one be hinge-type interface unit, one be locker formula interface unit.
The lock clip adapter includes handle, the fixing buckle in a half shell is arranged, lock and is arranged at the other half
The bearing of shell, handle one end are rotatablely connected with bearing upper end, and lock one end is fixed on the support；When warning global shell closing connects
When connecing, the lock other end is socketed on fixing buckle, then compresses handle；When unclamping handle, lock is removed from fixing buckle
When, warning global shell separation；One half shell refers to upper and lower half shell；Another half shell refers to upper and lower half shell.
54) the warning spherical shell external surface is set as different colours, is arranged at intervals on aerial cable.
Wherein, the high voltage induction takes the power-supply controller of electric of electric unit, information process unit to be located in lower housing cavity and sets
In the support plate set or on the lower shell surface of warning global shell.
Induction takes the mutual inductor of electric unit, support unit bottom end to be fixed in another support plate being arranged in lower housing cavity
Or on the lower shell surface of warning global shell.
Wherein, acrylic resin paint of the warning spherical shell external surface coating by baking process processing, color are boat
Empty red white or orange (interval installation different colours sphere is more advantageous to warning effect between daytime).
Two, on the basis of one, aviation warning ball system further includes being arranged to take electric unit and information processing list in high voltage induction
The power-supply controller of electric of member takes electric unit to export energy value for controlling high voltage induction.Power-supply controller of electric takes with open-type can mutual inductance
Device connects, and the voltage and current for providing the high stability for meeting actual demand exports, and ensures information process unit and LED hairs
The normal work of light alarm unit.
Three, aviation warning ball system further includes Cloud Server, and described information processing unit and Cloud Server are long-range
Connection；The information of voltage of LED light-emitting caution units is sent to Cloud Server by information process unit in real time, works as information process unit
When failure, Cloud Server can warn ball to position specific aviation according to these data.
Four, aerial cable was located in the plane parallel to the ground of warning global shell central point.
Five, further include temperature sensor, temperature sensor is fixed on aerial cable, detects temperature information in real time, is transmitted
To information process unit.
Six, installation process：
Step 1 will warn upper half-shell, housing lower half and the locker formula interface unit of global shell to unclamp, wherein on unclamping
The locker formula interface unit of half shell, housing lower half keeps lock clip adapter rotatable, makes upper and lower the half of warning global shell
Discrete state is presented in shell；Hooped type interface unit is unclamped, high voltage induction is opened and takes electric unit and support unit；Aerial cable is horizontal
It is placed through at the circular hole of warning ball system exterior surface, and circular hole was located at the parallel to the ground of warning global shell center point and puts down
On face；Subsequently enter step 2；
High voltage induction is taken electric unit and support unit to be sleeved on aerial cable by step 2, locks hooped type interface unit；
It will be taken at the output signal of electric unit and the information of the energy information of LED light-emitting caution units for handling and exporting high voltage induction
Unit is managed to be arranged in warning spherical shell intracoelomic cavity；LED light-emitting caution units are installed on alarming lamp casing surface for half built-in
On；The upper-lower casing of global shell will be warned to close, and locker formula interface unit is locked.
The invention is not limited in specific implementation modes above-mentioned.The present invention, which expands to, any in the present specification to be disclosed
New feature or any new combination, and disclose any new method or process the step of or any new combination.
Claims (10)
1. a kind of aviation for aerial cable warns ball system, it is characterised in that including：
High voltage induction takes electric unit, is arranged and is fixed in system inner cavity, and electricity is obtained from the aerial cable inside warning global shell
Magnetic induction energy, and export electric energy；
Support unit is arranged and is fixed in system inner cavity, grasps and is fitted in the aerial cable crossed inside warning global shell
On, for that global shell will be warned to be fixed with aerial cable；
Information process unit is arranged and is fixed in system inner cavity, the output of electric unit is taken for handling and exporting high voltage induction
The energy information of signal and LED light-emitting caution units；
LED light-emitting caution units are installed on warning global shell for half built-in；
Global shell is warned, global shell will be warned to be fixed on aerial cable for passing through support unit, keep warning ball system flat
Weighing apparatus.
2. aviation according to claim 1 warns ball system, it is characterised in that the support unit is at least 2n, uniformly
It is distributed in high voltage induction to take electric unit and warn on the aerial cable between global shell, n is more than or equal to 1；The support unit
Including upper half component and lower half component, wherein upper half component is formed such that support unit grasps and is fitted in police with lower half component
Show the hollow structure on aerial cable inside global shell；First junction is connected by hinge mode；Support unit second connects
The place of connecing is located at the hooped type connector in bolts assemblies slot by one end and is fixed on aerial cable so that warning global shell is fixed
In on aerial cable；Wherein the first junction, the second junction refer to upper and lower half structure junction.
3. aviation according to claim 1 warns ball system, it is characterised in that it includes mutual inductor and electricity that high pressure, which takes electric unit,
Source controller；Wherein mutual inductor includes current transformer and the bolts assemblies slot being arranged on current transformer；Current Mutual Inductance
The upper and lower half hitch of device is configured to so that the hollow groove that high pressure takes electric unit to be fitted in aerial cable；Bolts assemblies slot is arranged upper
At lower half structural edge；High voltage induction takes the first junction of electric unit to pass through hinge connection；High voltage induction takes electric unit second
Junction is located at the hooped type connector in bolts assemblies slot by one end and is fixed on aerial cable.
4. aviation according to claim 1 warns ball system, it is characterised in that the warning global shell is mirror symmetry knot
First junction of the upper half-shell and housing lower half of structure, upper half-shell and housing lower half passes through hinge connection, upper half shell
Second junction of body and housing lower half is by locking clip adapter connection.
5. aviation according to claim 1,2,3 or 4 warns ball system, it is characterised in that the high voltage induction takes electric unit
Power-supply controller of electric, information process unit is located in the support plate being arranged in lower housing cavity or the lower casing of warning global shell
On body surface face；The induction takes the mutual inductor of electric unit, support unit bottom end to be fixed on another be arranged in lower housing cavity
On fagging or on the lower shell surface of warning global shell；Support plate is provided in plane parallel to the ground in warning global shell.
6. aviation according to claim 5 warns ball system, it is characterised in that the warning global shell is sphere；The branch
Fagging is plectane；Wherein radius of sphericity range is 30-150cm；The warning global shell material is metal alloy compositions.
7. aviation according to claim 5 warns ball system, it is characterised in that LED light-emitting caution units include the warning of m groups
P group half built-in warning lamp units are arranged in warning global shell upper half-shell in lamp unit, and m-p groups half are respectively set in housing lower half
Embedded warning lamp unit；Wherein m is equal to 2p or p and is not equal to m-p.
8. the aviation according to claim 1,2,3,4,5 or 7 warns ball system, it is characterised in that the m=2；The ball
With sphere bottom at the top of body, that is, warns global shell upper half-shell top that one group of half built-in is respectively set with housing lower half bottom end and warn
Show lamp unit.
9. aviation according to claim 8 warns ball system, it is characterised in that the aerial cable is passed across positioned at warning
At the circular hole of ball system exterior surface, and circular hole was located in the plane parallel to the ground of center point.
10. the aviation according to claim 1,2,3,4,5,7 or 9 warns ball system, it is characterised in that further include cloud service
Device, described information processing unit are remotely connect with Cloud Server；Information process unit is in real time by the work of LED light-emitting caution units
Status information is sent to Cloud Server, and Cloud Server can warn the working condition of ball to supervise specific aviation according to these data
Control, and it can be positioned when information process unit breaks down.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810309224.9A CN108320410A (en) | 2018-04-09 | 2018-04-09 | A kind of aviation for aerial cable warns ball system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810309224.9A CN108320410A (en) | 2018-04-09 | 2018-04-09 | A kind of aviation for aerial cable warns ball system |
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| CN108320410A true CN108320410A (en) | 2018-07-24 |
Family
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| CN201810309224.9A Pending CN108320410A (en) | 2018-04-09 | 2018-04-09 | A kind of aviation for aerial cable warns ball system |
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| CN110491049A (en) * | 2019-08-20 | 2019-11-22 | 国网四川省电力公司电力科学研究院 | The transmission line of electricity external force damage prevention of energy is taken to warn ball based on equipotential |
| CN110867032A (en) * | 2019-11-22 | 2020-03-06 | 林田霞 | Electricity-saving aviation warning ball for power line |
| CN113497431A (en) * | 2021-07-28 | 2021-10-12 | 国网江苏省电力有限公司南通供电分公司 | Induction electricity taking type overhead line warning ball with ice and snow removing function |
| WO2023096619A1 (en) * | 2021-11-23 | 2023-06-01 | Yildiz Teknik Universitesi | An illuminated warning sphere |
| WO2024172781A1 (en) * | 2023-05-10 | 2024-08-22 | Bursa Uludağ Üni̇versi̇tesi̇ | Lighting system for the warning sphere |
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