KR20170024886A - Aeronautical light system and aeronautical light system controlling method - Google Patents

Aeronautical light system and aeronautical light system controlling method Download PDF

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Publication number
KR20170024886A
KR20170024886A KR1020150120456A KR20150120456A KR20170024886A KR 20170024886 A KR20170024886 A KR 20170024886A KR 1020150120456 A KR1020150120456 A KR 1020150120456A KR 20150120456 A KR20150120456 A KR 20150120456A KR 20170024886 A KR20170024886 A KR 20170024886A
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South Korea
Prior art keywords
voltage
discharge lamp
input voltage
isolation transformer
magnitude
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KR1020150120456A
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Korean (ko)
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KR101797815B1 (en
Inventor
이남석
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한국공항공사
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V23/00—Arrangement of electric circuit elements in or on lighting devices
    • F21V23/02—Arrangement of electric circuit elements in or on lighting devices the elements being transformers, impedances or power supply units, e.g. a transformer with a rectifier
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21K—NON-ELECTRIC LIGHT SOURCES USING LUMINESCENCE; LIGHT SOURCES USING ELECTROCHEMILUMINESCENCE; LIGHT SOURCES USING CHARGES OF COMBUSTIBLE MATERIAL; LIGHT SOURCES USING SEMICONDUCTOR DEVICES AS LIGHT-GENERATING ELEMENTS; LIGHT SOURCES NOT OTHERWISE PROVIDED FOR
    • F21K9/00—Light sources using semiconductor devices as light-generating elements, e.g. using light-emitting diodes [LED] or lasers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21—LIGHTING
    • F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V23/00—Arrangement of electric circuit elements in or on lighting devices
    • F21V23/003—Arrangement of electric circuit elements in or on lighting devices the elements being electronics drivers or controllers for operating the light source, e.g. for a LED array
    • H05B37/02—
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B41/00—Circuit arrangements or apparatus for igniting or operating discharge lamps
    • H05B41/14—Circuit arrangements
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
    • H05B41/00—Circuit arrangements or apparatus for igniting or operating discharge lamps
    • H05B41/14—Circuit arrangements
    • H05B41/26—Circuit arrangements in which the lamp is fed by power derived from dc by means of a converter, e.g. by high-voltage dc
    • F21W2101/06—

Abstract

An air navigation system and an air navigation system control method are disclosed. An aviation equalization system according to an embodiment of the present invention includes an isolation transformer disposed corresponding to each of aviation equalization and oscillating a voltage, and an input voltage determining unit for determining an input voltage value according to the type of the aviation equalization, Wherein the control unit controls the magnitude of the voltage to be supplied to the aviation equalization, and when the aviation equalizer is a discharge lamp, .

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an air-conditioning lighting system and an air-

The present invention relates to an aviation equalization system and a method of controlling an aviation equalization system for lighting a discharge lamp such as a fluorescent lamp as an aviation equalization.

In general, an aviation equalization system can refer to an illumination facility to assist in safe navigation by controlling the aerial lighting (lamp) installed at airports, airports or airplanes during takeoff and landing of aircraft.

Unlike the parallel circuit used in the home, the aviation equalization system is implemented as a constant current circuit that changes the voltage according to the load in order to maintain constant brightness (constant current) in each airplane regardless of power loss due to distance .

The load (lamp) connected to the aviation equalization series circuit can utilize the power induced in the secondary winding of the isolation transformer magnetically coupled to the primary winding of the isolation transformer for aviation equalization.

Resistive loads such as incandescent bulbs and halogen lamps have been mainly used as aerial lighting, but recently, LED lamps with LED driving devices have also been used.

However, the aviation equalization series circuit can not directly turn on the discharge lamp (fluorescent lamp) corresponding to the surface light source by the voltage and the current for driving the point light source such as the incandescent lamp or the halogen lamp and it is difficult to use the discharge lamp as the load have.

Accordingly, in order to connect the discharge lamp to the aviation equalization series circuit, it is required to develop a separate device capable of converting and supplying the power in consideration of the characteristics of the load called the discharge lamp.

In the embodiment of the present invention, various types of aviation equipments are provided for convenience by converting and supplying voltages in consideration of the characteristics of each aviation equipments for lighting of aviation equipments connected in series in an aviation equilibrium system supplying constant current power. So that they can be used in connection with each other.

In addition, the embodiment of the present invention can also provide an aviation equalization of at least one of a point light source, an LED lamp, and a discharge lamp by adjusting a voltage adjusted in consideration of the type of aviation lighting through a dedicated driving apparatus, So that the equalization can be simultaneously turned on.

It is another object of the present invention to provide an air-conditioning system having a driving device dedicated to a discharge lamp capable of supplying an input voltage required for lighting a discharge lamp.

In the embodiment of the present invention, when the discharge lamp is used as an aerial lighting in an aerial lighting system for supplying a constant current power, the input voltage value for lighting the discharge lamp is determined, and the magnitude of the voltage oscillated in the insulation transformer is inputted to the input (Boosted) according to the voltage value, and supplies the discharge lamp to the discharge lamp.

Further, an embodiment of the present invention aims to rectify an AC voltage induced at both ends of a discharge lamp connected in series to a secondary winding of an insulation transformer to a discharge voltage (DC voltage) and supply the same to the discharge lamp.

An aviation equalization system according to an embodiment of the present invention includes an isolation transformer disposed corresponding to each of aviation equalization and oscillating a voltage, and an input voltage determining unit for determining an input voltage value according to the type of the aviation equalization, Wherein the control unit controls the magnitude of the voltage to be supplied to the aviation equalization, and when the aviation equalizer is a discharge lamp, .

According to another aspect of the present invention, there is provided a method of controlling an air-conditioning system including the steps of oscillating a voltage through an isolation transformer disposed corresponding to each of aerial lighting, determining an input voltage value according to a type of the air- Determining the input voltage value so as to be at least boosted with respect to the magnitude of the voltage at the time of oscillation when the air-conditioning lamp is a discharge lamp, adjusting the magnitude of the oscillated voltage according to the input voltage value, .

The aerial lighting system according to another embodiment of the present invention includes a constant current regulator and a dedicated driving device for using a discharge lamp such as a fluorescent lamp in a secondary cable of the insulation transformer and a serial cable, The exclusive drive apparatus includes a voltage rectifying section for generating a voltage, a voltage raising section for raising the voltage level in accordance with the input voltage value, and an electronic circuit for generating a resonance frequency necessary for driving the discharge lamp with a boosted voltage.

According to an embodiment of the present invention, in order to turn on an aviation equalization connected in series in an aviation equalization system that supplies a constant current power source, by converting and supplying a voltage in consideration of characteristics of each aviation equalization, It is possible to make it possible to connect and use it according to convenience.

In addition, according to an embodiment of the present invention, by supplying a voltage adjusted in consideration of the type of aviation equalization through a dedicated driving device to at least one of the point light source, the LED lamp, and the discharge lamp, Can be turned on at the same time.

According to an embodiment of the present invention, it is possible to provide an aviation equalization system having a drive device dedicated to a discharge lamp capable of supplying an input voltage necessary for lighting a discharge lamp.

According to an embodiment of the present invention, when the discharge lamp is used as an aerial lighting in an aviation equalization system that supplies a constant current power, an input voltage value for lighting the discharge lamp is determined, and the magnitude of the voltage (Boosted) in accordance with the input voltage value and supplying the discharge lamp with the discharge lamp, the discharge lamp can be easily turned on. According to an embodiment of the present invention, an alternating voltage generated at both ends of a discharge lamp connected in series to the secondary winding of the isolation transformer may be rectified to a voltage (DC voltage) and supplied to the discharge lamp.

According to an embodiment of the present invention, when at least one point light source of the incandescent lamp or the halogen lamp is used for aviation lighting, the input voltage value is determined so that the magnitude of the voltage at the starting point is maintained, The point light source can be directly connected through the isolation transformer and can be easily lighted.

According to an embodiment of the present invention, when the LED lamp is used as an airplane, an input voltage value is determined so as to be at least reduced in magnitude from the voltage at the oscillation time point, and a voltage adjusted (decompressed) The LED lamp can be easily turned on by supplying it as an LED lamp.

1 is a block diagram illustrating an internal configuration of an air-conditioning system according to an embodiment of the present invention.
2 is a diagram showing the overall connection relationship of the air-conditioning system according to an embodiment of the present invention.
3 is a diagram showing an example of the internal configuration of the dedicated drive apparatus in the air-conditioning system according to the embodiment of the present invention.
4 is a diagram showing another example of the internal configuration of the dedicated drive apparatus in the air-conditioning system according to the embodiment of the present invention.
5 is a diagram showing an example of a double voltage rectifying circuit.
6 is a diagram showing an example of an electronic circuit for generating a resonance frequency.
7 is a flowchart illustrating a procedure of a method of controlling an air-conditioning system according to an embodiment of the present invention.

Hereinafter, an apparatus and method for updating an application program according to an embodiment of the present invention will be described in detail with reference to the accompanying drawings. However, the present invention is not limited to or limited by the embodiments. Like reference symbols in the drawings denote like elements.

1 is a block diagram illustrating an internal configuration of an air-conditioning system according to an embodiment of the present invention.

Referring to FIG. 1, an aerial lighting system 100 according to an embodiment of the present invention may include an isolation transformer 110 and a dedicated driving apparatus 120.

The isolation transformer 110 is disposed corresponding to each of the aerial lighting (lamp) 101 to oscillate (induce) a voltage.

Here, the aerial lighting 101 may be at least one of a point light source such as an incandescent lamp or a halogen lamp, or a surface light source such as a discharge lamp (e.g., a fluorescent lamp) or an LED lamp.

For example, the air conditioning system 100 may include an isolation transformer 110 corresponding to the number of the air conditioning 101 and may connect the air conditioning 101 and the isolation transformer 110, respectively.

The isolation transformer 110 is connected in series with a constant current regulator CCR which supplies a constant current to the primary winding of the isolation transformer 110 and is connected in series with the airborne equalization 101 in the secondary winding of the isolation transformer 110, Lt; / RTI > If the aerial lighting 101 is a discharge lamp, the discharge lamp may be connected in series with the secondary winding of the isolation transformer 110.

Also, the isolation transformer 110 may constitute a loop circuit through a constant current regulator and a serial cable, which supply a constant current to the aerial lighting system 100.

The dedicated drive device 120 adjusts the voltage generated by the isolation transformer 110 in consideration of the characteristics of the load (resistance) of each of the aerial equalization 101 and supplies power to each aerial equalization 101, (Not shown).

The dedicated driving apparatus 120 determines the input voltage value according to the type of the aerial lighting 101, adjusts the magnitude of the oscillated voltage according to the input voltage value, and supplies the adjusted voltage to the air lighting system 101.

For example, the dedicated drive device 120 determines the input voltage value so that when the aerial lighting 101 is a discharge lamp, it is at least boosted above the magnitude of the voltage at the oscillation time.

That is, the dedicated driving apparatus 120 can easily turn on the discharge lamp by adjusting (increasing) the magnitude of the voltage oscillated in the isolation transformer 110 according to the input voltage value and supplying it to the discharge lamp. At this time, the dedicated driving apparatus 120 may rectify the alternating voltage induced at both ends of the discharge lamp connected in series to the secondary winding of the isolation transformer 110 to a discharge voltage (DC voltage) and supply the discharge lamp.

Hereinafter, the dedicated driving apparatus 120 will be described with reference to FIG.

3 is a diagram showing an example of the internal configuration of the dedicated drive apparatus in the air-conditioning system according to the embodiment of the present invention.

FIG. 3 shows a dedicated driving apparatus 120, 300 including a discharge lamp 304 and implemented as one body.

The dedicated driving apparatuses 120 and 300 may include a voltage rectifying unit 301, a voltage raising unit 302, an electronic circuit 303 and a discharge lamp 304.

The voltage rectifying unit 301 can rectify the voltage by full-wave rectification, convert it into a DC voltage, and supply it to both ends of the discharge lamp 304. Where the discharge lamp 304 may be connected in series with the secondary winding of the isolation transformer 110.

The boosting unit 302 may boost the DC voltage using a voltage doubler rectifying circuit so that the magnitude of the boosted DC voltage is included in the range set by the input voltage value.

5 is a diagram showing an example of a double voltage rectifying circuit.

FIG. 5 shows one example of a voltage doubler rectifying circuit for boosting a DC voltage.

The voltage multiplying rectifier is a circuit that obtains a DC output voltage close to the input AC voltage by using a rectifier and a capacitor. As shown in FIG. 5, the voltage multiplying rectifier is composed of an on-wave voltage rectification and a half- . The voltage doubler rectifier circuit can be used where the load current is relatively small because the output voltage suddenly decreases when the load current increases to some extent.

The boost section 302 is controlled within a predetermined range (for example, 2.8 A to 6.6 A) for a constant current supplied by a constant current regulator (not shown) connected in series to the primary winding of the isolation transformer 110 The DC voltage can be stepped up by adjusting the circuit constant so that the discharge lamp 304 is turned on.

The electronic circuit 303 can generate the resonance frequency necessary for driving the discharge lamp 304 by using the boosted DC voltage as the input voltage. An example of the electronic circuit 303 that generates a resonance frequency necessary for driving / lighting the discharge lamp 207 with the boosted voltage is shown in Fig.

6 is a diagram showing an example of an electronic circuit for generating a resonance frequency.

The electronic circuit for generating the resonance frequency may be a kind of resonance circuit and may refer to a circuit connected so that the electrostatic energy of the capacitor C and the electromagnetic energy of the inductance L can be freely converted.

As shown in Fig. 6, the electronic circuit for generating the resonance frequency may be composed of a series resonance circuit in which a capacitor and an induction unit are connected in series and a parallel resonance circuit in which they are connected in parallel.

The electronic circuit for generating the resonance frequency becomes electrically resonant at a specific frequency determined by the value of the coil and the capacitor. Such a resonance may be a condition in which the current of the RLC circuit becomes the maximum when the inductive reactance and the capacitive reactance are the same, and the specific frequency at the resonance may be the resonance frequency.

As described above, according to the embodiment of the present invention, it is possible to provide an aviation equalization system having a drive device dedicated to a discharge lamp capable of supplying an input voltage necessary for lighting a discharge lamp.

According to the embodiment, the dedicated drive device 120 can determine the input voltage value so that when the aerial lighting 101 is an LED lamp, it is at least reduced in magnitude than the magnitude of the voltage at the oscillation time. Accordingly, the aviation equalization system 100 can supply the LED lamp with a voltage adjusted (reduced in pressure) according to the input voltage value, thereby easily controlling the lighting of the LED lamp.

In addition, the dedicated driving apparatus 120 may determine the input voltage value such that the magnitude of the voltage at the oscillation time is maintained when the aerial lighting 101 is a point light source such as an incandescent lamp or a halogen lamp. In this case, the aviation equalization system 100 can be easily turned on by directly connecting the point light source through the isolation transformer.

As described above, according to the embodiment of the present invention, in order to turn on the air lighting system 101 connected in series in the air conditioning system supplying the constant current power, So that various types of aviation equipments 101 can be connected and used conveniently without limitation.

According to an embodiment of the present invention, a voltage adjusted in consideration of the type of the aerial lighting 101 through the dedicated driving device 120 is supplied to at least one of the point light source, the LED lamp, and the discharge lamp, So that each of the air-conditioning lights 101 driven by different voltages can be lighted simultaneously.

2 is a diagram showing the overall connection relationship of the air-conditioning system according to an embodiment of the present invention.

2, an aerial lighting system 200 according to an embodiment of the present invention has a series circuit connected in series through a primary winding of an isolation transformer 203, 204, 205, and supplies a constant current to the series circuit And a constant current regulator (CCR, 201).

Specifically, the aviation equalization system 200 includes a constant current regulator 201, a serial cable 202, an isolation transformer 203, 204, 205, an incandescent or halogen lamp 206, a discharge lamp 207, an LED lamp 208, A dedicated drive device 209 for the lamp 207, and a dedicated drive device 210 for the LED lamp 208. [

The constant current regulator 201 serves to supply a constant current necessary for lighting of the air-conditioning lighting. The constant current regulator 201 is connected to the primary winding of the isolation transformers 203, 204, 205 through the serial cable 202 to constitute a loop circuit.

The aviation equalization system 200 can control lighting by supplying a constant current to at least one aerial equalization connected in series. The aerial lighting may be an incandescent lamp or a halogen lamp 206, a discharge lamp (e.g., a fluorescent lamp) 207, and an LED lamp 208.

Each of the aerial equalizations may be coupled in series with the secondary windings of correspondingly disposed isolation transformers 203, 204, 205.

For example, the incandescent bulb or the halogen lamp 206 may be directly connected to the secondary winding of the isolation transformer 203 without a separate dedicated drive device.

The LED lamp 208 is connected in series to the secondary winding of the isolation transformer 205 through the dedicated drive unit 210 and the dedicated drive unit 210 supplies power for lighting the LED lamp 208 .

The discharge lamp 207 is connected in series to the secondary winding of the isolation transformer 204 through a dedicated drive unit 209 and the dedicated drive unit 209 is connected to the alternating current The voltage is converted into a DC voltage by full-wave rectification, and the DC voltage can be boosted by using two kinds of voltage doubler rectifying circuits shown in Fig.

The dedicated drive unit 209 supplies power to the discharge lamp 207 using the boosted DC voltage to generate a resonance frequency required for lighting the discharge lamp 207. [ An example of an electronic circuit that generates a resonance frequency required for driving / lighting the discharge lamp 207 with a boosted voltage is shown in Fig.

The dedicated driving apparatus 209 can raise the voltage so that the boosted voltage is included in the set range (e.g., 90%) of the input voltage value determined according to the type of aviation equalization (i.e., the discharge lamp 207).

The dedicated drive unit 209 also adjusts the circuit constants so that the discharge lamp 207 is lit within a predetermined current range (2.8 A to 6.6 A) for the primary winding of the isolation transformer 204, By boosting, it is possible to maintain a constant brightness in each aerial lighting connected in series.

Here, the dedicated drive device 209 may be embodied as an integral type including a discharge lamp 207. [

4 is a diagram showing another example of the internal configuration of the dedicated drive apparatus in the air-conditioning system according to the embodiment of the present invention.

Referring to FIG. 4, the dedicated driving device 400 may be implemented as an integrated type including a discharge lamp 406.

Specifically, the dedicated driving apparatus 400 includes an EMI filter (line filter) 401, a rectifying circuit 402, an oscillating circuit (Driver) 403, an inverter circuit 404, a resonant circuit 405, and a discharge lamp 406 ). ≪ / RTI > In addition, the dedicated drive device 400 may further include a commercial AC power source (220 V 60 Hz) and a surge suppression circuit.

The EMI filter 401 removes the noise in the power line and the rectifying circuit 402 can be composed of a rectifier and a power factor corrector (PFC). The PFC is a power generated in the process of converting an AC voltage to a DC voltage Loss can be reduced.

The oscillation circuit 403 generates an AC voltage using a commercial AC power source and the inverter circuit 404 converts the AC voltage to a DC voltage and the resonance circuit 405 generates a resonance frequency necessary for driving the discharge lamp 406 Can be generated.

Hereinafter, the operation flow of the air-conditioning system 100 according to the embodiments of the present invention will be described in detail with reference to FIG.

7 is a flowchart illustrating a procedure of a method of controlling an air-conditioning system according to an embodiment of the present invention.

The air-conditioning system control method according to the present embodiment can be performed by the air-conditioning system 100 described above.

Referring to FIG. 7, in step 710, the aerial equalization system 100 oscillates voltage through an isolation transformer disposed corresponding to each of the aerial equalizations.

Here, the aerial lighting may be at least one of a point light source such as an incandescent lamp or a halogen lamp, or a surface light source such as a discharge lamp (e.g., a fluorescent lamp) or an LED lamp.

For example, the air-conditioning system 100 may include an isolation transformer corresponding to the number of air-conditioning equalizations and may connect the air-conditioning equalization and isolation transformers, respectively.

The isolation transformer may be connected in series with the constant current regulator (CCR), which supplies a constant current, to the primary winding of the isolation transformer, and may be connected in series with the aerial equalization to the secondary winding of the isolation transformer. In the case of an aviation equalizer discharge lamp, the discharge lamp may be connected in series with the secondary winding of the isolation transformer.

In addition, the isolation transformer can constitute a loop circuit through a constant current regulator and a serial cable, which supply a constant current to the aviation equalization system 100.

In step 720, the aviation equalization system 100 determines an input voltage value according to the type of aviation equalization and, in step 730, adjusts the magnitude of the oscillated voltage according to the input voltage value, It supplies by lighting.

The aviation equalization system 100 can illuminate the aviation equalization by adjusting the voltage generated by the isolation transformer in consideration of the characteristics of the load (resistance) of each aviation equalization and supplying power to each aviation equalization.

For example, the aviation equalization system 100 may determine the input voltage value such that the voltage is at least boosted with respect to the magnitude of the voltage at the oscillation time, when it is an aviation equalizer discharge lamp.

That is, the aviation equalization system 100 can adjust the magnitude of the voltage generated in the isolation transformer according to the input voltage value (boost) and supply it to the discharge lamp, thereby easily lighting the discharge lamp.

At this time, the aviation equalization system 100 can rectify the alternating voltage generated at both ends of the discharge lamp connected in series to the secondary winding of the isolation transformer to a discharge voltage (DC voltage) and supply the discharge lamp.

As described above, according to the embodiment of the present invention, it is possible to provide the air-conditioning system 100 having the driving device dedicated to the discharge lamp capable of supplying the input voltage necessary for lighting the discharge lamp.

In addition, according to an embodiment of the present invention, in order to illuminate aviation lighting connected in series in the aviation equalization system 100 that supplies a constant current power source, by converting and supplying voltages in consideration of the characteristics of each aviation lighting, It is possible to connect the lighting system to the lighting system without any restriction, and to control the lighting of each air conditioning system driven by different voltages at the same time.

100: Flight lighting system
110: Isolation transformer
120: dedicated drive device
101: Aviation lighting

Claims (14)

An isolation transformer arranged corresponding to each of the aviation equalization and oscillating the voltage; And
A control unit that determines an input voltage value according to the type of aviation equalization and adjusts the magnitude of the oscillated voltage according to the input voltage value,
Lt; / RTI >
When the air-conditioning lamp is a discharge lamp,
The dedicated drive apparatus includes:
The input voltage value is determined so as to be at least boosted with respect to the magnitude of the voltage at the oscillation time
Aeronautical lighting system. The method according to claim 1,
The discharge lamp being connected in series to a secondary winding of the isolation transformer,
The dedicated drive apparatus includes:
A voltage rectifying part for rectifying the voltage by full-wave rectification to convert it into a DC voltage, and supplying the DC voltage to both ends of the discharge lamp
Wherein the air conditioning system comprises: 3. The method of claim 2,
The dedicated drive apparatus includes:
A step-up voltage step-up circuit that boosts the direct-current voltage by using a voltage-doubler rectifying circuit and includes a magnitude of the step-up direct-current voltage within a range set by the input voltage value,
Further comprising: The method of claim 3,
The voltage-
The DC voltage is stepped up by adjusting the circuit constant so that the discharge lamp is turned on within a predetermined range for the constant current supplied by the constant current regulator connected in series with the primary winding of the isolation transformer
Aeronautical lighting system. The method of claim 3,
The dedicated drive apparatus includes:
And an electronic circuit for generating a resonance frequency required for driving the discharge lamp, using the boosted DC voltage as an input voltage
Further comprising: The method according to claim 1,
When the aviation lighting device is an LED lamp,
The dedicated drive apparatus includes:
And determines the input voltage value so as to be at least reduced in magnitude from the magnitude of the voltage at the oscillation time
Aeronautical lighting system. The method according to claim 1,
In the case where the air conditioner is an incandescent lamp or a halogen lamp,
The dedicated drive apparatus includes:
The input voltage value is determined so that the magnitude of the voltage at the oscillation time is maintained
Aeronautical lighting system. The method according to claim 1,
Wherein the isolation transformer comprises:
A constant current regulator for supplying a constant current, and a constant current regulator for constituting a loop circuit through a serial cable
Aeronautical lighting system. Oscillating the voltage through an isolation transformer arranged corresponding to each of the air-to-air equalizations;
Determining the input voltage value according to the type of aviation equalization and determining the input voltage value so that when the aviation equalizer discharge lamp is boosted at least the magnitude of the voltage at the oscillation time point; And
Adjusting the magnitude of the oscillated voltage according to the input voltage value and supplying it to the aviation equalization
Gt; a < / RTI > 10. The method of claim 9,
In the case of a discharge lamp connected in series with the secondary winding of the isolation transformer,
Wherein the step of supplying to the air-
A step of full-wave rectifying the voltage to convert it into a direct current voltage and supplying it to both ends of the discharge lamp
Gt; a < / RTI > 11. The method of claim 10,
Wherein the step of supplying to the air-
Boosting the DC voltage by using a voltage doubler rectifying circuit so that the magnitude of the boosted DC voltage is included within a range set by the input voltage value
≪ / RTI > 11. The method of claim 10,
Wherein the step of supplying to the air-
Adjusting the circuit constant so as to step up the DC voltage so that the discharge lamp is turned on within a predetermined range of the constant current supplied by the constant current regulator connected in series with the primary winding of the isolation transformer
≪ / RTI > 13. The method according to claim 11 or 12,
Wherein the step of supplying to the air-
Generating a resonance frequency necessary for driving the discharge lamp by using the boosted DC voltage as an input voltage,
≪ / RTI > 10. The method of claim 9,
Connecting the isolation transformer and a constant current regulator for supplying a constant current with a serial cable to construct a loop circuit
≪ / RTI >
KR1020150120456A 2015-08-26 2015-08-26 Aeronautical light system and aeronautical light system controlling method KR101797815B1 (en)

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KR102007968B1 (en) 2018-07-30 2019-08-06 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013623A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013625A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013626A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013624A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof

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US20050030192A1 (en) * 2003-08-08 2005-02-10 Weaver James T. Power supply for LED airfield lighting
JP4556029B2 (en) 2007-11-19 2010-10-06 東芝ライテック株式会社 Discharge lamp lighting device and lighting fixture

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KR102007968B1 (en) 2018-07-30 2019-08-06 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013623A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013625A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013626A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof
KR20200013624A (en) 2019-07-31 2020-02-07 한화시스템 주식회사 Airfield light module and airfield light apparatus comprising thereof

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