CN108124368A - A kind of aviation obstruction light system - Google Patents

A kind of aviation obstruction light system Download PDF

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Publication number
CN108124368A
CN108124368A CN201611065838.4A CN201611065838A CN108124368A CN 108124368 A CN108124368 A CN 108124368A CN 201611065838 A CN201611065838 A CN 201611065838A CN 108124368 A CN108124368 A CN 108124368A
Authority
CN
China
Prior art keywords
module
obstruction light
power
singlechip
chip computer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201611065838.4A
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Chinese (zh)
Inventor
宋文康
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Liaoning East Eagle Aviation Equipment Polytron Technologies Inc
Original Assignee
Liaoning East Eagle Aviation Equipment Polytron Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Liaoning East Eagle Aviation Equipment Polytron Technologies Inc filed Critical Liaoning East Eagle Aviation Equipment Polytron Technologies Inc
Priority to CN201611065838.4A priority Critical patent/CN108124368A/en
Publication of CN108124368A publication Critical patent/CN108124368A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B47/00Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
    • H05B47/20Responsive to malfunctions or to light source life; for protection
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05BELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B47/00Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
    • H05B47/10Controlling the light source

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  • Circuit Arrangement For Electric Light Sources In General (AREA)

Abstract

The present invention relates to a kind of aeronautical beacons to have field, and in particular to a kind of aviation obstruction beacon and its control method.Aviation obstruction beacon and its control method are provided, kind cable need not be set up, can the work information of obstruction light be fed back into master control platform in time.Including the first controller and second controller, first controller includes power module one, power module one is connected with DC conversion modules one, DC conversion modules one are connected with the first one-chip computer module, first one-chip computer module and display module, key-press module is connected with wireless receiving module, the second controller includes power module two, power module two is connected with DC conversion modules two, DC conversion modules two are connected with second singlechip module, second singlechip module and wireless transmitter module, obstruction light is connected, obstruction light is connected by inverter circuit module with power module two, power module two is connected with voltage detection module, voltage detection module is connected with second singlechip module.

Description

A kind of aviation obstruction light system
Technical field
The present invention relates to a kind of aeronautical beacons to have field, and in particular to a kind of aviation obstruction light system.
Background technology
It is to identify the extraordinary lamps and lanterns of barrier that aviation obstruction beacon, which is also known as navigational lighting aid equipment, is under the jurisdiction of navigational lighting aid equipment row Industry, aviation obstruction beacon are the lamp kind scopes under it.In order to otherwise varied with general purpose headlamp, aviation obstruction beacon is not It is always on but glittering, for aero-obstruction lantern with low light intensity to be always on, middle light intensity navigation obstacle lamp is sudden strain of a muscle with high light intensity navigation obstacle lamp Light, flash frequency is not less than 20 times per minute, not higher than 70 times per minute.The effect of aviation obstruction beacon is exactly to show structures Profile, enable the height and profile of aircraft operators disturbance in judgement object, play a warning role.At present, the boat of domestic application Empty obstruction light is all using fixedly mounted, and when installation all needs to set up cable to power, existing technology there are adverse circumstances or Person's human factor may damage cable, the shortcomings that aviation obstruction beacon is caused not flicker normally;Traditional aviation obstruction beacon It if influence of breaking down uses, can only manually regular visit find, such crossed just is known ask for a long time The generation of topic.At night if you need in particular circumstances, such as non-airport environment is risen for still further aspect, passenger plane or helicopter , it is necessary to flexibly complete the instruction work of special runway according to extreme terrain using aviation obstruction beacon when flying or force-landing.
The content of the invention
The present invention provides a kind of aviation obstruction light system aiming at defect existing in the prior art, kind frame is not required If the work information of obstruction light can be fed back to master control platform by cable in time.
To achieve the above object, the present invention adopts the following technical scheme that, described including the first controller and second controller First controller includes power module one, and power module one is connected with DC conversion modules one, DC conversion modules one and first One-chip computer module is connected, and the first one-chip computer module is connected with display module, key-press module and wireless receiving module, second control Device processed includes power module two, and power module two is connected with DC conversion modules two, DC conversion modules two and second singlechip Module is connected, and second singlechip module is connected with wireless transmitter module, obstruction light, and obstruction light passes through inverter circuit module and power supply Module two is connected, and power module two is connected with voltage detection module, and voltage detection module is connected with second singlechip module.
As a preferred embodiment of the present invention, the power module one includes vehicle power supply module and host accumulator mould Block.
As another preferred embodiment of the present invention, the power module is second is that slave battery module.
As another preferred embodiment of the present invention, the power module one is single to first by DC conversion modules one Piece machine module for power supply, the first one-chip computer module are received the information of wireless transmitter module by wireless receiving module, realized to obstacle The real-time monitoring and control of lamp operating status, and testing result is shown by display module, it can be to first by key-press module One-chip computer module is controlled;Power module two is by DC conversion modules two to second singlechip module for power supply, the second monolithic Machine module sends the information of obstruction light to wireless receiving module by wireless transmitter module, and power module two passes through inverter circuit Module is powered to obstruction light, and voltage detection module detects the operating mode from electromechanical source and sends that information to second singlechip mould Block.
As another preferred embodiment of the present invention, first one-chip computer module and second singlechip module use STM32 series monolithics.
Advantageous effect of the present invention compared with prior art.
The present invention is divided into the first controller and second controller two parts, and each power supply power supply for having oneself by oneself of two parts can To save the process for setting up cable, prevent from influencing the work of obstruction light due to the damage of cable.
In addition, the working condition and voltage status of second singlechip module real time monitoring obstruction light, information are passed through wireless Transmitting module is timely feedbacked to the wireless receiving module of the first controller so that the first one-chip computer module is accused by display module Know staff, the operating status of obstruction light can be carried out concentrating real-time monitoring.
Description of the drawings
The present invention will be further described with reference to the accompanying drawings and detailed description.The scope of the present invention not only limits to In the statement of herein below.
Fig. 1 is the first controller principle block diagram of the present invention.
Fig. 2 is second controller functional block diagram of the present invention.
Specific embodiment
As shown in Figs. 1-2, as shown in drawings, a kind of movable type aviation obstruction light system, including the first controller and Two controllers, first controller include power module one, and power module one is connected with DC conversion modules one, direct current conversion Module one is connected with the first one-chip computer module, the first one-chip computer module and display module, key-press module and wireless receiving module phase Even, the second controller includes power module two, and power module two is connected with DC conversion modules two, DC conversion modules two It is connected with second singlechip module, second singlechip module is connected with wireless transmitter module, obstruction light, and obstruction light passes through inversion electricity Road module is connected with power module two, and power module two is connected with voltage detection module, voltage detection module and second singlechip Module is connected.
The power module one includes vehicle power supply module and host battery module, and power module is second is that slave accumulator Module.
In the present invention, wireless receiving module and wireless transmitter module can be realized and several aviation obstruction beacons transported at a distance The real-time monitoring and control of row state and operating voltage.
Power module one is powered by the first controller to the first one-chip computer module, and the first one-chip computer module is by wirelessly connecing The information that module receives wireless transmitter module is received, the real-time monitoring and control to obstruction light operating status is realized, and passes through display Module shows testing result, and the first one-chip computer module can be controlled by key-press module.
By DC conversion modules two to second singlechip module for power supply, second singlechip module will hinder power module two The information of lamp is hindered to send wireless receiving module to by wireless transmitter module, power module two is by inverter circuit module to obstacle Lamp is powered, and voltage detection module detects the operating mode from electromechanical source and sends that information to second singlechip module.
As another preferred embodiment of the present invention, first one-chip computer module and second singlechip module use STM32 series monolithics.
The present invention is divided into the first controller and second controller two parts, and each power supply power supply for having oneself by oneself of two parts can To save the process for setting up cable, prevent from influencing the work of obstruction light due to the damage of cable.
In addition, the working condition and voltage status of second singlechip module real time monitoring obstruction light, information are passed through wireless Transmitting module is timely feedbacked to the wireless receiving module of the first controller so that the first one-chip computer module is informed by display module Staff can carry out concentrating real-time monitoring to the operating status of obstruction light.
It is understood that above with respect to the specific descriptions of the present invention, it is merely to illustrate the present invention and is not limited to this The described technical solution of inventive embodiments, it will be understood by those of ordinary skill in the art that, still the present invention can be carried out Modification or equivalent substitution, to reach identical technique effect;As long as meeting using needs, all protection scope of the present invention it It is interior.

Claims (5)

  1. A kind of 1. aviation obstruction light system, including the first controller and second controller, which is characterized in that first controller Including power module one, power module one is connected with DC conversion modules one, one and first one-chip computer module of DC conversion modules It is connected, the first one-chip computer module is connected with display module, key-press module and wireless receiving module, and the second controller includes electricity Source module two, power module two are connected with DC conversion modules two, and DC conversion modules two are connected with second singlechip module, the Two one-chip computer modules are connected with wireless transmitter module, obstruction light, and obstruction light is connected by inverter circuit module with power module two, Power module two is connected with voltage detection module, and voltage detection module is connected with second singlechip module.
  2. 2. a kind of aviation obstruction light system according to claim 1, it is characterised in that:The power module one includes vehicle-mounted Power module and host battery module.
  3. 3. a kind of aviation obstruction light system according to claim 1, it is characterised in that:The power module is second is that slave stores Battery module.
  4. 4. a kind of aviation obstruction light system according to claim 1, it is characterised in that:The power module one is by straight It flows modular converter one to power to the first one-chip computer module, the first one-chip computer module receives wireless transmission mould by wireless receiving module The information of block realizes the real-time monitoring and control to obstruction light operating status, and shows testing result by display module, passes through Key-press module can control the first one-chip computer module;Power module two is by DC conversion modules two to second singlechip Module for power supply, second singlechip module send the information of obstruction light to wireless receiving module, power supply by wireless transmitter module Module two is powered by inverter circuit module to obstruction light, and voltage detection module detects the operating mode from electromechanical source and sends out the information Give second singlechip module.
  5. 5. a kind of aviation obstruction light system according to claim 1, it is characterised in that:First one-chip computer module and Second singlechip module uses STM32 series monolithics.
CN201611065838.4A 2016-11-28 2016-11-28 A kind of aviation obstruction light system Pending CN108124368A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611065838.4A CN108124368A (en) 2016-11-28 2016-11-28 A kind of aviation obstruction light system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611065838.4A CN108124368A (en) 2016-11-28 2016-11-28 A kind of aviation obstruction light system

Publications (1)

Publication Number Publication Date
CN108124368A true CN108124368A (en) 2018-06-05

Family

ID=62223811

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611065838.4A Pending CN108124368A (en) 2016-11-28 2016-11-28 A kind of aviation obstruction light system

Country Status (1)

Country Link
CN (1) CN108124368A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109413821A (en) * 2018-10-26 2019-03-01 北京首航艾启威节能技术股份有限公司 Novel aviation obstruction light controller and control method
CN113840427A (en) * 2021-09-16 2021-12-24 安徽智芯能源科技有限公司 Aviation obstruction light control system based on alternating current and direct current high-voltage power transmission tower

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109413821A (en) * 2018-10-26 2019-03-01 北京首航艾启威节能技术股份有限公司 Novel aviation obstruction light controller and control method
CN109413821B (en) * 2018-10-26 2024-02-23 首航高科能源技术股份有限公司 Aviation obstruction light controller and control method
CN113840427A (en) * 2021-09-16 2021-12-24 安徽智芯能源科技有限公司 Aviation obstruction light control system based on alternating current and direct current high-voltage power transmission tower

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Application publication date: 20180605

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