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A power supply control circuit and method for a civil aircraft display controller

A technology of power control circuit and display controller, which is applied in computer control, program control, general control system, etc., can solve the problems of display controller power-on failure, high power consumption of the display, and failure of single-chip microcomputer to collect, etc., to achieve high security Requirements for performance level, reduce system power consumption and size, and prevent damage

Active Publication Date: 2020-07-10
LUOYANG INST OF ELECTRO OPTICAL EQUIP OF AVIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The single-chip microcomputer must scan continuously every cycle, and at the same time use the CPU and GPU at the same time, and the GPU does not use low power consumption mode, and the power consumption of the display is relatively large
At the same time, the instantaneous high current generated by abnormal conditions such as lightning strikes will directly break down the optocoupler, and the single-chip microcomputer cannot collect the key signal, which will cause the display controller to fail to power on.

Method used

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  • A power supply control circuit and method for a civil aircraft display controller
  • A power supply control circuit and method for a civil aircraft display controller
  • A power supply control circuit and method for a civil aircraft display controller

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Embodiment Construction

[0022] Embodiments of the present invention are described in detail below, and the embodiments are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.

[0023] Such as figure 1 As shown, the power supply control circuit of the civil aircraft display controller in this embodiment includes: light guide plate 10, signal isolation acquisition circuit 20, FPGA and related configuration circuit 30, GPU and related configuration circuit 40, interface circuit 50, PMIC power supply circuit 60 , an optocoupler 70 and a power conversion module 80 .

[0024] After the display controller is powered on, the power conversion module 80 outputs a power signal 1 to the FPGA and related configuration circuits 30 . After the power-on button on the light guide plate 10 is pressed, the power-on button signal 1 is output. After the signal isolation and acquisition circuit, the FPGA judges that the button is pressed, and then scans ...

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Abstract

The invention provides a power supply control circuit and method for a civil aircraft display controller. After the display controller is powered on, a power supply conversion module outputs a power supply signal to an FPGA and a related configuration circuit. After a power on key on a light guide plate is pressed, a power on key signal is output. After the signal passes through a signal isolationacquisition circuit, the FPGA scans a keyboard and calculates the key value. If a key is the power on key, the key time is timed, and after the time reaches a fixed value, a power on signal is output. The power on signal passes through an opto-isolator, and then is output to the power supply conversion module. The power supply conversion module inputs the power supply signal to a PMIC power supply circuit and an interface circuit. The PMIC power supply circuit inputs a GPU power supply signal to a GPU and the related configuration circuit. The display controller is powered on to enter a normal operation mode. According to the power supply control circuit and method for the civil aircraft display controller, the power supply control circuit is effectively prevented from being damaged by abnormal electrical stress; the power consumption and volume of the system are reduced; and the high security level requirement of a civil aircraft is satisfied.

Description

technical field [0001] The invention belongs to the technical field of display driving in civil airborne display equipment, and relates to a power supply control circuit and method for a display controller of a civil aircraft. Background technique [0002] The display controller realizes the control operation of itself and its related cross-linking equipment through the buttons on the light guide plate. Traditional display controller power control circuits include: light guide plate, power module, optocoupler, single-chip microcomputer, CPU, GPU and DC / DC power supply. The key signal is input to the single-chip microcomputer through the optocoupler, and the single-chip microcomputer scans the key input periodically, adopts the progressive scanning method, and obtains the key value of the key through delay anti-shake. The single-chip microcomputer must scan continuously every cycle, and at the same time use the CPU and GPU at the same time, and the GPU does not use low power...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/25257
Inventor 李明明陈哨东杨冉赵慧慧
Owner LUOYANG INST OF ELECTRO OPTICAL EQUIP OF AVIC
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