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A cockpit touch screen tuning control system

A tuning control, touch screen technology, applied in the field of cockpit control, can solve the problems of inconvenient on-board real-time monitoring and health management analysis, multiple cockpit space and cost, occupied aircraft load, etc., to achieve online status monitoring function, reduce Cabling complexity, reducing the effect of connecting cables

Active Publication Date: 2021-05-04
CETC AVIONICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Using this method, firstly, there are many cables, the wiring is more complicated, and it takes up the load of the aircraft; secondly, it is controlled through an independent tuning device, and the control data is not connected to the network, which is inconvenient for real-time monitoring and health management analysis on the airborne; finally , the cockpit usually needs to be equipped with two to three independent tuning control devices, which require more cockpit space and cost than touch screen tuning control devices

Method used

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  • A cockpit touch screen tuning control system

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Effect test

Embodiment 1

[0023] like figure 1 A cockpit touchscreen tuning control system shown, including:

[0024] Touch screen: provide touch screen control program man-machine interface;

[0025] Integrated Modular Avionics IMA: resident tuning control application and display manager for touchscreen responsiveness and tuning control;

[0026] Flight management system FMS: realize the tuning control of the controlled terminal, mainly the tuning control of the navigation station;

[0027] Remote data interface unit RDIU: used for data forwarding, conversion of A429 data and AFDX data;

[0028] Controlled terminal: implement actions and feedback status according to the data instructions forwarded by the remote data interface unit RDIU;

[0029] AFDX switch: Provide path routing for data communication among touch screen, integrated modular avionics equipment IMA, flight management system FMS, and remote data interface unit RDIU. Two remote data interface units RDIU can be set to realize redundant ...

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PUM

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Abstract

The invention discloses a cockpit touch screen tuning control system, including a touch screen; IMA: resident tuning control application program and display management program to realize the response and tuning control to the touch screen; flight management system FMS: realize the tuning control of the controlled terminal ; Remote data interface unit RDIU: used for data forwarding, conversion of A429 data and AFDX data; controlled terminal: implement actions and feedback status according to the data instructions forwarded by RDIU; AFDX switch: provide path routing for data communication between the above devices. Using the touch screen to realize the display of the control interface and the reception of control commands can reduce the connection cables between devices, reduce the complexity of wiring, save hardware setting costs, and reduce the size of the tuning control system; realize data forwarding through the AFDX network, The tuning control data is uploaded to the network, which can facilitate data monitoring, save cables, reduce the size of the tuning control system, realize online status monitoring, and increase data transmission speed.

Description

technical field [0001] The invention relates to the technical field of cockpit control, in particular to a cockpit touch screen tuning control system. Background technique [0002] The cockpit tuning control system is an important part of the aircraft, which mainly realizes the control of the airborne communication station, navigation station and surveillance station. The traditional cockpit tuning control system uses an independent tuning control device to control the aircraft. The pilot controls the airborne radio station through the panel of the tuning control device. The tuning device communicates directly with the controlled radio station through a cable connection. Using this method, firstly, there are many cables, the wiring is more complicated, and it takes up the load of the aircraft; secondly, it is controlled through an independent tuning device, and the control data is not connected to the network, which is inconvenient for real-time monitoring and health managem...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D43/00B64D47/00H04L29/08
CPCB64D43/00B64D47/00H04L67/025H04L67/12
Inventor 罗斌刘天华崔凯姚待艳
Owner CETC AVIONICS
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