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Device and method for head-up display in integrated avionics equipment

A technology of integrated avionics and head-up display, applied in the field of integrated avionics, can solve the problems of single control mode, inability to adapt to application scenarios, single display mode, etc., and achieve the effect of meeting the needs of use

Active Publication Date: 2018-09-21
CHENGDU HERMES TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, there is currently no complete head-up display device for general aviation aircraft
Some existing head-up display devices often have a single control mode, which cannot meet the different requirements of pilots for displaying various data and interactive interfaces on the head-up display device
For example, due to the unique language and unit of the page display, it cannot adapt to different application scenarios and cannot be easily switched; and the display mode is single, and the complexity of the data displayed in different flight stages is the same

Method used

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  • Device and method for head-up display in integrated avionics equipment
  • Device and method for head-up display in integrated avionics equipment
  • Device and method for head-up display in integrated avionics equipment

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Embodiment Construction

[0019] In the following, the present invention will be further described in detail in conjunction with the accompanying drawings and embodiments, so as to make the purpose, technical solutions and advantages of the present invention more clear. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0020] According to the embodiment of the present invention, the device for head-up display in integrated avionics equipment can adopt an all-in-one device with a multi-channel data interface, a processor and a display device; Under control, one of the three control modes NORM, TEXT and FPM is used to display the corresponding display interface; among them, the display interface corresponding to the NORM control mode is used to display complete flight data and pictures; the display interface corresponding to the TEXT control mode is used for Displays the main flight information, inclu...

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Abstract

The invention discloses a device and method for head-up display in integrated avionics equipment. The device can achieve the fast switching of data head-up display of the integrated avionics equipmentunder various application scenarios by controlling mode switching, corresponding display modes are applied for different flight phases, so that the display efficiency is high, and extension and upgrade are easy. The device comprises multiple data interfaces, a processor and a display device; the display device is used for adopting a display interface corresponding to the display in a first control mode, second control mode and third control mode under the control of the processor according to control instructions input by the data interfaces or user's selection for a rotary knob on a displaydevice panel; data displayed by the display interface corresponding to the first control module is more than that displayed by the display interface corresponding to the second control mode; and datadisplayed by the display interface corresponding to the third control mode is less than that displayed by the display interface corresponding to the second control mode.

Description

technical field [0001] The invention relates to the technical field of integrated avionics, in particular to a device and method for head-up display in integrated avionics equipment. Background technique [0002] In modern aircraft, the processing unit is usually used to uniformly process the information of various avionics equipment on the aircraft, combine the equipment with the same or similar functions into one component, comprehensively display the relevant parameters on the display device, and display the related parameters in each avionics equipment The relevant information is transmitted through the on-board data bus, so that the performance of all avionics on the entire aircraft can reach a higher level. Such a system is called an integrated avionics system. [0003] The integrated avionics system includes a variety of equipment with many functions, such as integrated display control unit, data interface unit, dual redundant air data system, INS / GNSS integrated navi...

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Application Information

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IPC IPC(8): B64D43/00
CPCB64D43/00
Inventor 李明罗涛汪坤王强杨宏伟尹彦清于宝强
Owner CHENGDU HERMES TECH