CN103037588A - Novel type global function aircraft outer lighting controller - Google Patents
Novel type global function aircraft outer lighting controller Download PDFInfo
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- CN103037588A CN103037588A CN201210572995XA CN201210572995A CN103037588A CN 103037588 A CN103037588 A CN 103037588A CN 201210572995X A CN201210572995X A CN 201210572995XA CN 201210572995 A CN201210572995 A CN 201210572995A CN 103037588 A CN103037588 A CN 103037588A
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Abstract
The invention discloses a novel type global function aircraft outer lighting controller which is characterized by comprising an anti-collision light control unit, a flight-refuel light control unit, a navigation light control unit, a formation light control unit and an RSS422 decoding and digital logic unit, wherein the anti-collision light control unit is used for controlling an anti-collision light, the flight-refuel light control unit is used for controlling a flight-refuel light, the navigation light control unit is used for controlling a navigation light and the formation light control unit is used for controlling a formation light. The anti-collision light control unit, the flight-refuel light control unit, the navigation light control unit and the formation light control unit are all connected with a bus through the RSS422 decoding and digital logic unit. Due to the structure, a navigation light control box, a formation light control box and an anti-collision light control box are integrated, and thereby the weight of a device is light, maintenance is easy, reliability is high and use requirements of military severe environment are met.
Description
Technical field
The present invention relates to airplane equipment cabin aircraft exterior lighting controller, belong to especially a kind of control processor and by data wire control information is transferred to the aircraft exterior lighting controller, the aircraft exterior lighting controller is lighted respectively the machine outer lamps such as navigation lights, formation light, anticollision beacon, air refuelling lamp according to control information.
Background technology
The control box of the aircraft exterior lighting light fixture on China's aircraft that has now all is separately to make navigation lights control box, formation light control box, anticollision beacon control box.Be not difficult to find out, such split design not only can cause the increase of control box weight, and has also increased complexity in maintenance and maintenance.
Summary of the invention
The present invention seeks to solve the problems of the prior art, a kind of novel global function aircraft exterior lighting controller is proposed, to adapt to round-the-clock high-intensity combat duty requirement, make the ground maintenance personnel can simply maintain and change product, also to alleviate as much as possible simultaneously the weight of product.
To achieve these goals, the present invention is achieved in that a kind of novel global function aircraft exterior lighting controller, it is characterized in that: comprise,
One anticollision beacon control unit is used for the control anticollision beacon;
One air refuelling lamp control unit is used for control air refuelling lamp;
One navigation lights control unit is used for the control navigation lights;
One formation light control unit is used for the control formation light;
One RSS422 decoding and digital logic unit;
Described anticollision beacon control unit, air refuelling lamp control unit, navigation lights control unit, formation light control unit all are connected with bus with digital logic unit by described RSS422 decoding.
Specifically, described anticollision beacon control unit comprises anticollision beacon power supply side, front-end module, direct voltage module, driver module, friendly pattern, blind mode, the direct voltage module respectively with friendly mode unit;
Described air refuelling lamp control unit comprises that air refuelling lamp feeder ear, front-end module, direct voltage module and brightness regulation module, brightness regulation module connect described air refuelling lamp;
Described navigation lights control unit, comprise, navigation lights power supply side, front-end module, direct voltage module, driver module, ground traction mode circuit, friendly mode unit and blind mode unit, friendly mode unit and blind mode list connect respectively described navigation lights;
Described formation light control unit, comprise, formation light power supply side, filtering peak surge unit, DC/AC inversion module, power amplifier module, mode switching unit, brightness adjusting unit, friendly mode unit and blind mode unit, friendly mode unit is connected with described formation light with the blind mode unit.
Advantage of the present invention: with navigation lights control box, formation light control box, anticollision beacon control box All-in-One, so that weight of equipment is light, easy to maintenance, reliability is high, and can satisfy the instructions for use of military adverse circumstances.
Description of drawings
Accompanying drawing 1 is mechanical structure schematic diagram of the present invention.
Accompanying drawing 2 is electrical block diagram of the present invention.
Embodiment
Below in conjunction with drawings and Examples the present invention is elaborated.
See also Fig. 1, a kind of novel global function aircraft exterior lighting controller shown in Figure 1 is characterized in that: comprise,
One anticollision beacon control unit is used for the control anticollision beacon;
One air refuelling lamp control unit is used for control air refuelling lamp;
One navigation lights control unit is used for the control navigation lights;
One formation light control unit is used for the control formation light;
One RSS422 decoding and digital logic unit;
Described anticollision beacon control unit, air refuelling lamp control unit, navigation lights control unit, formation light control unit connect by bus.
Manufacturing process is as follows:
1. anticollision beacon control board unit 6 is installed on the base plate 7;
2. signal controlling plate unit 2 is installed on the right plate 3;
3. 422 decoding deck unit 4 are installed in front side board 5;
4. inverter voltage change-over panel unit 9 is installed in left plate 8;
Formation light, air refuelling lamp control board unit 11 are installed in back side panel 10.
Please again referring to Fig. 2, shown in Figure 2 is the circuit structure of this creation: the anticollision beacon control unit comprises anticollision beacon power supply side, front-end module, direct voltage module, driver module, friendly pattern, blind mode, the direct voltage module respectively with friendly mode unit;
Described air refuelling lamp control unit comprises that air refuelling lamp feeder ear, front-end module, direct voltage module and brightness regulation module, brightness regulation module connect described air refuelling lamp;
Described navigation lights control unit, comprise, navigation lights power supply side, front-end module, direct voltage module, driver module, ground traction mode circuit, friendly mode unit and blind mode unit, friendly mode unit and blind mode list connect respectively described navigation lights;
Described formation light control unit, comprise, formation light power supply side, filtering peak surge unit, DC/AC inversion module, power amplifier module, mode switching unit, brightness adjusting unit, friendly mode unit and blind mode unit, friendly mode unit is connected with described formation light with the blind mode unit.
RS422 decoding and digital logic unit are 422 bus control signals (brightness regulation, flicker frequency, the pattern control) decodings of will send on the machine and by certain logical circuit generation control signal, control respective transistor and electric component on each sub-function module, are realized the output of each sub-function module of control with signal loading.After receiving one of them sub-function module conditioning signal, RS422 decoding and digital logic unit latch output with the processing signals of a upper sub-function module, to guarantee the independent regulation function between each sub-function module.This unit is reserved with the simulation test port simultaneously, when this Port detecting behind analog test signal, will control all lighting apparatus and carry out work with minimum power state, to make things convenient for the regular maintenance of this equipment.
Below only expressed embodiments of the present invention, it describes comparatively concrete and detailed, but can not therefore be construed as limiting the scope of the patent.Should be pointed out that for the person of ordinary skill of the art, without departing from the inventive concept of the premise, can also make some distortion and improvement, these all belong to protection scope of the present invention.Therefore, the protection range of patent of the present invention should be as the criterion with claims.
Claims (2)
1. novel global function aircraft exterior lighting controller is characterized in that: comprises,
One anticollision beacon control unit is used for the control anticollision beacon;
One air refuelling lamp control unit is used for control air refuelling lamp;
One navigation lights control unit is used for the control navigation lights;
One formation light control unit is used for the control formation light;
One RSS422 decoding and digital logic unit;
Described anticollision beacon control unit, air refuelling lamp control unit, navigation lights control unit, formation light control unit all are connected with bus with digital logic unit by described RSS422 decoding.
2. a kind of novel global function aircraft exterior lighting controller according to claim 1, it is characterized in that: described anticollision beacon control unit comprises anticollision beacon power supply side, front-end module, direct voltage module, driver module, friendly mode unit and blind mode unit, and friendly mode unit is connected with described anticollision beacon with the blind mode unit and is connected;
Described air refuelling lamp control unit comprises that air refuelling lamp feeder ear, front-end module, direct voltage module and brightness regulation module, brightness regulation module connect described air refuelling lamp;
Described navigation lights control unit, comprise, navigation lights power supply side, front-end module, direct voltage module, driver module, ground traction mode circuit, friendly mode unit and blind mode unit, friendly mode unit and blind mode list connect respectively described navigation lights;
Described formation light control unit, comprise, formation light power supply side, filtering peak surge unit, DC/AC inversion module, power amplifier module, mode switching unit, brightness adjusting unit, friendly mode unit and blind mode unit, friendly mode unit is connected with described formation light with the blind mode unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210572995.XA CN103037588B (en) | 2012-12-26 | 2012-12-26 | A kind of new global function aircraft exterior lighting controller |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210572995.XA CN103037588B (en) | 2012-12-26 | 2012-12-26 | A kind of new global function aircraft exterior lighting controller |
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| Publication Number | Publication Date |
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| CN103037588A true CN103037588A (en) | 2013-04-10 |
| CN103037588B CN103037588B (en) | 2017-08-08 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654241A (en) * | 2013-11-21 | 2015-05-27 | 上海航空电器有限公司 | Operation and control integrated aircraft exterior lighting control box |
| CN105398579A (en) * | 2015-12-02 | 2016-03-16 | 上海航空电器有限公司 | Light guide system of oil receiving opening for boom type air refueling |
| CN105554934A (en) * | 2015-12-02 | 2016-05-04 | 上海航空电器有限公司 | Control circuit of dual-mode combination navigation light and control method thereof |
| CN115589654A (en) * | 2022-11-03 | 2023-01-10 | 上海东风照明器材有限公司 | Circuit design of outdoor lighting control box |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654241A (en) * | 2013-11-21 | 2015-05-27 | 上海航空电器有限公司 | Operation and control integrated aircraft exterior lighting control box |
| CN105398579A (en) * | 2015-12-02 | 2016-03-16 | 上海航空电器有限公司 | Light guide system of oil receiving opening for boom type air refueling |
| CN105554934A (en) * | 2015-12-02 | 2016-05-04 | 上海航空电器有限公司 | Control circuit of dual-mode combination navigation light and control method thereof |
| CN115589654A (en) * | 2022-11-03 | 2023-01-10 | 上海东风照明器材有限公司 | Circuit design of outdoor lighting control box |
| CN115589654B (en) * | 2022-11-03 | 2023-08-08 | 上海东风照明器材有限公司 | Circuit design of off-board illumination control box |
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| Publication number | Publication date |
|---|---|
| CN103037588B (en) | 2017-08-08 |
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