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Helicopter flight control system comprehensive display method

A flight control system and comprehensive display technology, applied in aircraft parts, transportation and packaging, etc., can solve problems such as absence and impact on flight safety, reduce workload, shorten maintenance time, and improve the effect of failure causes

Pending Publication Date: 2021-02-26
CHINA HELICOPTER RES & DEV INST
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  • Claims
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AI Technical Summary

Problems solved by technology

[0002] The interactive interface between the work of the helicopter flight control system and the pilot is mainly the flight control console. The flight control console without LCD screen can only be connected in mode, and the code tube digital display is available. The flight control console with LCD screen uses a certain The type electromechanical fly-by-wire flight control console is a representative, which can display information such as the working status of the flight control system and fault reporting. However, there is a common problem with the installation location of the flight control console, which is that they are not directly in front of the driver. The driver checks the status of the flight control system. All need to bow their heads, which will have a certain impact on flight safety

Method used

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  • Helicopter flight control system comprehensive display method

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Embodiment Construction

[0017] The design method involved in the present invention will be described in further detail below in conjunction with the accompanying drawings.

[0018] A design method for the comprehensive display of the helicopter flight control system, which is mainly used for the driver to monitor the working status of the flight control system during the flight, and can also be used for ground self-inspection and troubleshooting to provide status display, which can quickly locate the cause of the fault, refer to figure 1 , the comprehensive display of the helicopter flight control system is realized through the following methods and steps:

[0019] 1) Realize the position indication function of the rudder surface in the multi-function device

[0020] The flight control system of the prototype is equipped with pitch, roll, and yaw rudder position indicators, which are installed on the instrument to display the output of the flight control system in series with the rudders, and transmi...

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Abstract

The invention belongs to the technical field of helicopter flight control systems, and discloses a helicopter flight control system comprehensive display method. The helicopter flight control system is improved on the basis of an original flight control system, the working state display mode of the flight control system is comprehensively changed, control surface position indicator equipment is canceled, and control surface position indication, modal input, prompt and other information are comprehensively displayed on a multifunctional display. According to the flight control system comprehensive display design method, display information related to the flight control system is achieved on the multifunctional displayer, and a driver can check the state of the flight control system easily and pay attention to flight on the whole body.

Description

technical field [0001] The invention belongs to the technical field of helicopter flight control systems, in particular to a comprehensive display method for the helicopter flight control system. Background technique [0002] The interactive interface between the work of the helicopter flight control system and the pilot is mainly the flight control console. The flight control console without LCD screen can only be connected in mode, and the code tube digital display is available. The flight control console with LCD screen uses a certain The type electromechanical fly-by-wire flight control console is a representative, which can display information such as the working status of the flight control system and fault reporting. However, there is a common problem with the installation location of the flight control console, which is that they are not directly in front of the driver. The driver checks the status of the flight control system. All need to bow their heads, which will...

Claims

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Application Information

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IPC IPC(8): B64D43/00
CPCB64D43/00
Inventor 张浩华赵丹莉程东权
Owner CHINA HELICOPTER RES & DEV INST