Top control panel for aircraft cockpit and installation method thereof

Abstract

The invention relates to a top control panel for an aircraft cockpit and an installation method thereof. The top control panel comprises a shell and a plurality of control panels, wherein the shell is provided with a guide rail positioned in the shell, and an installation angle sheet, a connector interface and a ventilation opening which are positioned on the shell; the plurality of control panels are arranged on the guide rail in the shell in a quick connection mode; and the plurality of control panels are arranged in the shell, so that the top control panel has an integrated structure. The invention also relates to a method for installing the top control panel for the aircraft cockpit.

Description

technical field [0001] The invention relates to a cockpit top control panel for an aircraft and an installation method thereof. Background technique [0002] The top control panel is an important part of the human-machine interface in the cockpit of the aircraft. The control panel components (a panel with switches and knobs) of most important systems of the aircraft are centrally installed on the top control panel. Aircraft roof panels typically include structural connectors, rails, and multiple panel assemblies. The top control board is mainly to securely fix multiple control board components on the aircraft structure to ensure the space installation position of these control board components. The entire top control board should have sufficient strength and rigidity, and the wiring of the control board components needs to be considered Space, heat dissipation and electromagnetic shielding, etc. [0003] Traditional aircraft top control panels (see figure 1 ) generally ad...

AI Technical Summary

Problems solved by technology

[0004] 1. It is not easy to guarantee the connection strength and rigidity of assembly of parts;

[0005] 2. Parts assembly is not easy to ensure the strict control indicators such as guide rail parallelism and spacing, and the positioning of each control board component is affected by the accumulation of structural connectors and guide rail installation errors, and once the guide rail is positioned, the positioning of the control board components cannot be carried out Adjustment;

[0006] 3. It is difficult to lay the lines. After the parts are installed on the top structure of the aircraft cockpit, the internal lines of the top control panel are laid. Due to the influence of the operating environment and installation space, the laying of the lines is laborious and laborious;

[0007] 4. It is not easy to realize the overall electromagnetic shielding;

[0008] 5. It is not easy to realize the overall heat dissipation design;

[0009] 6. It is not easy to realize the display brightness uniformity of the light guide plate on the top control board;

[0010] 7. It is not easy to realize the comprehensive test of the control board components on the top control board

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