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Integrated avionics system for light aircrafts

A comprehensive avionics, light and small technology, applied in the transmission system, digital transmission system, control/regulation system, etc., can solve the problem of poor reliability and maintainability, affecting the safety and separation of the airborne avionics system that affects aircraft attendance. The mechanical structure of the type instrument is complex and other problems, so as to reduce the use and maintenance costs, reduce the incidence of human errors, and improve the attendance rate and safety.

Inactive Publication Date: 2017-05-31
石家庄飞机工业有限责任公司
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AI Technical Summary

Problems solved by technology

The mechanical structure of the discrete instrument is complicated, and the reliability and maintainability are poor, which affects the attendance rate of the aircraft and the safety of the airborne avionics system
[0004] There are problems such as technical protection, design coordination, development cycle and after-sales operation guarantee when assembling foreign integrated avionics systems

Method used

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  • Integrated avionics system for light aircrafts
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Embodiment Construction

[0036] Combine below Figure 1~Figure 2 The working principle and process of the present invention will be further described with examples.

[0037] Such as Figure 1~Figure 2As shown, this embodiment relates to an integrated avionics system for light and small aircraft, which includes a navigation subsystem, a communication subsystem and an indication / record subsystem;

[0038] The communication subsystem includes an audio control board, a VHF radio and an earphone microphone assembly; the VHF radio includes a first VHF radio and a second VHF radio; the first VHF radio and the second VHF radio The first VHF antenna and the second VHF antenna are respectively connected to the two VHF stations;

[0039] The instruction / record subsystem includes a main flight display, a multi-function display, an integrated processor, an engine parameter collector and an airframe state collector; the integrated processor includes a first integrated processor and a second integrated processor; ...

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PUM

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Abstract

The invention discloses an integrated avionics system for light aircrafts, and belongs to the field of integrated avionics systems of aircrafts. The integrated avionics system comprises a navigation subsystem, a communication subsystem and an indicating / recording subsystem; the communication subsystem comprises an audio control panel, a very high frequency station and an earphone microphone component; the indicating / recording subsystem comprises a primary flight display, a multifunctional display, an integrated processor, an engine parameter collector and an aircraft body state collector; the navigation subsystem comprises a flight environment monitoring system, a posture and direction control system and a radio navigation control system; the integrated avionics system disclosed by the invention can replace the original discrete instrument, reduce the incidence of human errors, improve the utilization rate of indicating contents of the indicating system, reduce the use and maintenance costs of general aircrafts, improve the attendance and the security of the general aircrafts and satisfy the client demands.

Description

technical field [0001] The invention relates to an integrated avionics system for light and small aircraft, which belongs to the field of aircraft integrated avionics systems. Background technique [0002] At present, most of the light and small aircraft independently designed and developed in China are discrete instrument configurations, and a small number of light and small aircraft equipped with foreign integrated avionics systems are still in the research and development stage. [0003] Drivers only need specific information at any given time, and the utilization of discrete instruments and their indications is low. The mechanical structure of the discrete instrument is complicated, and its reliability and maintainability are poor, which affects the attendance rate of the aircraft and the safety of the airborne avionics system. [0004] There are problems such as technical protection, design cooperation, development cycle and after-sales operation guarantee when assembl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/40G05D1/08
CPCH04L12/40006G05D1/0808H04L2012/4028
Inventor 杨志芳崔章栋孙凤琴王嘉为张明辉
Owner 石家庄飞机工业有限责任公司
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