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Aircraft aid landing system and centering guide method

An aircraft and centerline technology, which is applied to aircraft landers and other directions to achieve the effects of simple application, long life and strong operability

Active Publication Date: 2015-01-28
CSSC SYST ENG RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to effectively solve the deficiencies of the existing landing runway guidance methods, the present invention provides an aircraft landing aiding system and a landing aiding centering guidance method that utilizes different luminous colors, different luminous angles of lamps and lamps, and a specific arrangement of lamps.

Method used

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  • Aircraft aid landing system and centering guide method

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Embodiment Construction

[0034] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0035] figure 1 It is a plan view of the landing aid system of the present invention. The system includes rear end line light 1, first type boundary light 2 on the left side, second type boundary light 3 on the left side, third type boundary light 4 on the left side, first type boundary light 5 on the right side, and second type boundary light type on the right side Light 6, right third boundary light 7, center line light 8, head end line light 9. The system features different light colors, as well as different light arrangements. The purpose of this design is to use different colors of lights, according to different layouts, to make the emitted light overlap and overlap, and the overlapping areas are different, and the lights seen in different areas are different, indicating that the distance from the center line of the slideway is different...

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Abstract

The invention discloses an aircraft aid landing system and a centering guide method. The aircraft aid landing system is characterized in that head and tail end line lamps and left and right side border lamps are arranged to form a landing area; the border lamps have three colors arranged in a staggered way; one of the three colors is the same as center line lamps. Moreover, the emergent azimuth of the border lamps in the same color as the center line lamps ranges from 0 degree to a certain inward angle, and the emergent azimuth of the border lamps in different colors from the center line lamps ranges from 0 degree to a certain outward angle; the center line lamps emit light toward the left and the right. The specific divergence angles and relative positions of the lamps in different colors can ensure that an aviator clearly sees and accurately distinguishes the colors of light in the effective action distance, and relative deviation information of a centering position is provided for the aviator intuitively further. The method is applied easily, conveniently, quickly and accurately, the used auxiliary facilities are simple in structure and high in reliability and operability, and the method can serve as a good centering guide method for aircraft landing.

Description

technical field [0001] The invention belongs to the technical field of aircraft landing aids, and in particular relates to an aircraft landing aiding system and a landing aiding centering and guiding method using light signals as indications. Background technique [0002] With the development of modern transportation, the safety requirements for transportation facilities are getting higher and higher. In order to ensure the safety of citizens and property, strengthening work has been carried out in many aspects. Airplanes are also increasingly prominent in the means of transportation, and the number of aircrafts and flight routes are gradually increasing. Most of the aircraft fly at night, according to relevant data, at night or in low visibility conditions, it has a great impact on the safe landing of the aircraft. During the approach of the aircraft along the glideslope, early knowledge of the relative deviation position information from the runway centerline and timely a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D45/08
Inventor 张珺张泽帮高斌赵煜
Owner CSSC SYST ENG RES INST