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Airplane airborne display unit

An airborne display and aircraft technology, which is applied to the casing with display/control unit, aircraft parts, closed casing, etc., can solve the problems of increasing aircraft weight cost and equipment cost, etc.

Pending Publication Date: 2020-10-30
AVIC SHANGHAI AERONAUTICAL MEASUREMENT CONTROLLING RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Generally, traditional airborne display devices meet the high vibration requirements of the aircraft by wrapping a large number of metal structures or selecting military-grade liquid crystal modules. However, this design method undoubtedly increases the weight and equipment costs of the aircraft. Therefore, it is necessary to design And install a set of aircraft onboard display unit, which can facilitate pilots to quickly and accurately look up information, and achieve the purpose of reducing flight weight and pilot workload

Method used

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  • Airplane airborne display unit
  • Airplane airborne display unit
  • Airplane airborne display unit

Examples

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Embodiment

[0022] see Figure 1 to Figure 3 As shown, an aircraft on-board display unit shown in this embodiment includes a touch liquid crystal module 1 , a front case installation structure 2 , a reinforced rear case 3 and the like. The purpose to be achieved in this embodiment is: 1. Make the developed aircraft onboard display unit more anti-vibration effect than traditional displays, and achieve the goal of airborne application; 2. Reduce the use of metal structures for heat dissipation, so that the aircraft onboard display The overall weight of the unit is more optimized, achieving the goal of reducing the weight of airborne products, and at the same time saving production costs to a large extent.

[0023] For the first purpose, the touch liquid crystal module 1 shown in this embodiment includes a capacitive touch screen and a liquid crystal screen, and the capacitive touch screen and the liquid crystal screen are bonded by adopting a full lamination process to play the role of fixi...

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PUM

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Abstract

The invention discloses an airplane airborne display unit which comprises a touch liquid crystal module (1), a front shell mounting structure (2) and a reinforced rear shell (3). The touch liquid crystal module (1) comprises a capacitive touch screen and a liquid crystal screen, and the capacitive touch screen and the liquid crystal screen are bonded by adopting a full bonding process; the part, making contact with the touch liquid crystal module (1), of the front shell mounting structure (2) is buffered and fixed through conductive foam glue. And the reinforced rear shell (3) and the front shell mounting structure (2) are fixed through peripheral screws. According to the invention, the integrally reinforced airborne display unit is adopted, so that the developed airplane airborne displayunit has a better anti-vibration effect than a traditional display, and an airborne application target is achieved.

Description

technical field [0001] The invention belongs to the field of on-board display equipment of civil aircraft, and relates to an on-board display unit of an aircraft installed in a cockpit in an aircraft cabin. Background technique [0002] Aircraft on-board display unit is an operating carrier used to assist pilots to consult flight manuals or charts during flight. It mainly provides auxiliary flight information for pilots, reducing flight weight and pilot workload. Generally, the traditional airborne display devices meet the high vibration requirements of the aircraft by wrapping a large number of metal structures or selecting military-grade liquid crystal modules, but this design method undoubtedly increases the weight and equipment costs of the aircraft, so it is necessary to design And installing a set of aircraft onboard display unit can facilitate pilots to quickly and accurately look up information, and achieve the purpose of reducing flight weight and pilot workload. ...

Claims

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Application Information

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IPC IPC(8): G02F1/1333H05K5/02H05K5/00G06F3/044B64D43/00
CPCG02F1/13338G02F1/133382H05K5/0217H05K5/0004H05K5/0017B64D43/00G06F3/044
Inventor 张超黄建民宋志超黄小亮
Owner AVIC SHANGHAI AERONAUTICAL MEASUREMENT CONTROLLING RES INST
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