Attack angle indication dimming and carrier landing indication dimming system based on data bus control

An angle of attack and landing technology, applied in the field of dimming systems, can solve problems such as the inability to meet the needs of new carrier-based aircraft, and achieve the effects of improving human-machine efficiency, ensuring reliability, and aircraft landing safety.

Active Publication Date: 2020-06-16
SHANGHAI AVIATION ELECTRIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Whether the system can work normally in harsh environments is directly related to the landing safety of carrier-based aircraft. The traditional angle of attack indication and landing indication system can no longer meet the needs of new carrier-based aircraft. It is urgent to design a data bus-controlled angle of attack indication and dimming and landing indication and dimming system

Method used

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  • Attack angle indication dimming and carrier landing indication dimming system based on data bus control
  • Attack angle indication dimming and carrier landing indication dimming system based on data bus control

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Embodiment Construction

[0016] 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 understand the present invention, but are not intended to limit 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 constitute a conflict with each other.

[0017] See figure 1 , the angle of attack indication dimming and landing indication dimming system controlled by the data bus is composed of a central processing unit, a state control drive unit, a dimming drive unit, and a landing indication power supply drive unit.

[0018] The central processing unit consists of two CPUs that receive the limit information of the aircraft through two bus paths, and perform information sharing and information comparison thro...

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PUM

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Abstract

The invention discloses an attack angle indication dimming and carrier landing indication dimming system based on data bus control. The system comprises a left attack angle indicator, a right attack angle indicator, a carrier landing indication device, a central processing unit, a dimming driving unit, a state control driving unit, and a carrier landing indication power source driving circuit; thecentral processing unit is provided with a first CPU and a second CPU; the first CPU and the second CPU respectively receive the limit information of an airplane through two bus paths; and information sharing and information comparison are carried out between the first CPU and the second CPU through a CAN bus; the dimming driving unit is provided with a first dimming circuit and a second dimmingcircuit; the state control driving unit is provided with a first driving circuit and a second driving circuit. With the attack angle indication dimming and carrier landing indication dimming system based on data bus control of the invention adopted, dual-redundancy bus control attack angle indication and carrier landing indication are realized.

Description

technical field [0001] The invention relates to the field of dimming systems, in particular, an angle of attack indication dimming and landing indication dimming system based on data bus control. Background technique [0002] Approach angle of attack indication and landing indication are important indication tools for aircraft landing, and data bus is an important means to realize information transmission on aircraft. In order to safely and reliably realize the angle of attack indication and landing indication through bus control, and at the same time carry out stepless brightness adjustment of the angle of attack indication and day and night brightness control of the landing indication, a data bus based angle of attack indication and landing indication with dimming function is designed. Landing instruction system. When the aircraft lands, the landing commander obtains accurate information on the angle of attack of the aircraft and whether the landing hook is lowered accord...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H05B47/10B64F1/20
CPCB64F1/20Y02B20/40
Inventor 段敬琳夏小春黄玮
Owner SHANGHAI AVIATION ELECTRIC
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