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Touch control type control panel assembly system of aircraft cockpit

A control panel and cockpit technology, which is applied in the field of aircraft cockpit control, can solve the problems of large number of equipment and heavy weight, and achieve the effects of optimizing cost, simplifying design and weight, and reducing the number of equipment and system weight

Inactive Publication Date: 2022-05-27
SHANGHAI AVIATION ELECTRIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention aims to solve the problem of a large number of equipment and heavy weight caused by the integration of a large number of operating switches and indicating devices in the traditional control panel assembly, and provides a new type of aircraft cockpit touch control panel assembly system based on the touch screen And human-computer interaction technology, it has a design guarantee level and safety comparable to traditional control panel components, thereby improving the system integration and intelligence level of the control panel component system

Method used

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  • Touch control type control panel assembly system of aircraft cockpit
  • Touch control type control panel assembly system of aircraft cockpit
  • Touch control type control panel assembly system of aircraft cockpit

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Embodiment Construction

[0025] The present invention will be further described in detail below through specific embodiments in conjunction with the accompanying drawings. It should be noted here that the descriptions of these embodiments are used to help the understanding of the present invention, but do not constitute a limitation of the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0026] See figure 1 , the touch control panel assembly system in this embodiment includes three touch control panel assemblies. They are respectively identified as touch control panel assembly #1, touch control panel assembly #2, and touch control panel assembly #3. The functions implemented by the three touch control panel components are the same and function as backups for each other. Three touch control panel assemblies are installed in a "pin" shap...

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Abstract

The invention discloses an aircraft cockpit touch control type control panel assembly system which comprises one or more touch control type control panel assemblies, and each touch control panel assembly is provided with a touch screen unit and a processor unit. The touch screen unit is used for providing a graphical control related to driving control and converting a touch action of an operator on the graphical control into a corresponding touch signal, and the processor unit is used for receiving the touch signal from the touch screen unit and outputting a corresponding control instruction according to the touch signal. The control panel assembly has the beneficial effects that the design guarantee level and safety equivalent to those of a traditional control panel assembly are achieved, and therefore the system integration level and the intelligent level of a control panel assembly system are improved.

Description

technical field [0001] The present invention relates to aircraft cockpit controls, and more particularly, to an aircraft cockpit touch control panel assembly system. Background technique [0002] Existing implementation techniques for control panel assemblies, including microprocessor-based digital implementations, inevitably design and install several control panel assemblies in the top panel area of ​​the aircraft cockpit. Among them, each control board assembly integrates dozens of operation switches for controlling aircraft systems, such as push switches, rotary switches, toggle switches, etc. The control panel assembly and operating switches are arranged in a plane on the top panel area of ​​the cockpit. The functional division of control panel assemblies and the placement of operating switches vary significantly by aircraft model and are generally completely redesigned. Even for the same aircraft model, the control panel components in the cockpit top panel area will ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F3/04883
CPCG06F3/04883
Inventor 李欣翁营
Owner SHANGHAI AVIATION ELECTRIC
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