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Novel type global function aircraft outer lighting controller

A full-featured controller technology, applied in lighting devices, light sources, electric light sources, etc., can solve the problems of increased weight of control boxes and increased complexity of maintenance and maintenance, and achieve light weight, high reliability, and simple maintenance Effect

Active Publication Date: 2013-04-10
SHANGHAI AVIATION ELECTRIC
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It is not difficult to see that such a separate design will not only increase the weight of the control box, but also increase the complexity of maintenance and maintenance.

Method used

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  • Novel type global function aircraft outer lighting controller
  • Novel type global function aircraft outer lighting controller

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Embodiment Construction

[0018] The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0019] See figure 1 , figure 1 Shown is a new type of full-featured external lighting controller, which is characterized in that: comprising,

[0020] An anti-collision light control unit, used to control the anti-collision light;

[0021] An aerial refueling lamp control unit, used to control the aerial refueling lamp;

[0022] A navigation light control unit, used to control the navigation lights;

[0023] A formation light control unit, used to control the formation lights;

[0024] One RSS422 decoding and digital logic unit;

[0025] The anti-collision light control unit, air refueling light control unit, navigation light control unit and formation light control unit are connected through a bus.

[0026] The production process is as follows:

[0027] ① Install the anti-collision light control panel unit 6 on the base plate 7;

[0028] ② In...

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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 [0001] The invention relates to an aircraft equipment cabin external lighting controller, in particular to a control processor that transmits control information to the external lighting controller through a data line, and the external lighting controller lights up navigation lights, formation lights, Anti-collision lights, aerial refueling lights and other off-board lighting. Background technique [0002] The control boxes of the external lighting fixtures on some Chinese aircraft are all made separately into navigation light control boxes, formation light control boxes, and anti-collision light control boxes. It is not difficult to see that such a separate design will not only increase the weight of the control box, but also increase the complexity of maintenance and maintenance. Contents of the invention [0003] The purpose of the present invention is to solve the problems in the prior art, and propose a new type of full-function external lighting con...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H05B37/02
Inventor 金正祥郑俊毛红光
Owner SHANGHAI AVIATION ELECTRIC
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