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A kind of backup control system and operation method for integrated CNI system of minicomputer

A control system and small computer technology, applied in the field of aircraft human-computer interaction control, can solve the problems that the pilot cannot, the operation is inconvenient, and the backup control box cannot be arranged for the pilot to observe and operate.

Active Publication Date: 2022-07-22
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, the cockpit of a small aircraft has a small space, and it is impossible to arrange the backup control box in the cockpit where the pilot can observe and operate easily.
Therefore, when the avionics is degraded, the display controller fails, and the pilot cannot use the upper front control panel to control, but can only control the system through the backup control box, which is inconvenient to operate.

Method used

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  • A kind of backup control system and operation method for integrated CNI system of minicomputer
  • A kind of backup control system and operation method for integrated CNI system of minicomputer

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Embodiment Construction

[0015] The following will combine figure 1 and figure 2 , clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only a specific embodiment of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0016] like figure 1 As shown, the backup control system for the integrated CNI system of the minicomputer consists of a control panel 1, a display controller 2, an integrated CNI system 3, a data bus 4 and a backup control interface box 5, and the control panel 1 includes the front control panel on the front cabin 11. The front control panel 12 on the rear cabin, the above two control panels are reserved for backup control bus interfaces. The control panel is connected to the display...

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Abstract

The invention provides a backup control system and an operation method for an integrated CNI system of a minicomputer. The system mainly includes a control panel (1), a display controller (2), an integrated CNI system (3), a data bus (4) and a backup The control interface box (5), the control panel (1) is connected with the display controller (2), the backup control interface box (5) through the data bus (4), the display controller (2), the backup control interface box (5) and the The integrated CNI system (3) is connected through the data bus (4), and the backup control button (6) on the operation control panel (1) is operated to switch between backup and normal operation. The above system and operation method have simple equipment composition and convenient operation, and are very suitable for minicomputers.

Description

technical field [0001] The invention belongs to the field of aircraft man-machine interactive operation control, in particular to a backup control system and an operation method for a small computer integrated CNI system. Background technique [0002] In the field of aeronautical radio communication, navigation and identification (Communicate Navigate Identify, CNI for short), pilots need to conduct frequent man-machine interaction operations according to the airport data, navigation station information and aircraft status in the airspace where they are located, and adjust the communication channel, frequency and mode in real time. , compass working frequency and mode, TACAN working channel and mode, instrument landing working channel, microwave landing working channel and mode, air traffic control response code and other information. For this reason, corresponding control equipment needs to be installed in the aircraft cockpit to facilitate the control of the integrated CNI...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D47/00
CPCB64D47/00
Inventor 王顺亮邹辉朱亚萍李晓乐郭云蒋伟李迪张爱茹陈英余奎
Owner JIANGXI HONGDU AVIATION IND GRP