CN101639989B - Visual sliding berthing approaching light column guide device of airplane berth system - Google Patents
Visual sliding berthing approaching light column guide device of airplane berth system Download PDFInfo
- Publication number
- CN101639989B CN101639989B CN2009100702677A CN200910070267A CN101639989B CN 101639989 B CN101639989 B CN 101639989B CN 2009100702677 A CN2009100702677 A CN 2009100702677A CN 200910070267 A CN200910070267 A CN 200910070267A CN 101639989 B CN101639989 B CN 101639989B
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- light
- column
- guide device
- visual
- green light
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Abstract
The invention discloses a visual sliding berthing approaching light column guide device of an airplane berth system. The device is characterized of comprising a front opening box body and two sets of light-emitting columns longitudinally installed in the box body; the two sets of the light-emitting columns are mutually installed along a transverse direction and a longitudinal direction at intervals; the light-emitting columns near the port of the box body are green light columns; the light-emitting columns installed at the inner angle part of the far end of the box body are red light columns; and the middle sections of the green light columns are cut at a certain distance. When flyers fly an airplane to berth on ground, based on light column display observed by a flight deck, and by adopting the device, the flyers judge the position of the airplane and guide the operation of the flyers to exactly berth without the guidance of ground service staffs. The device can replace the existing manual guide mode, is a safe and reliable guide mode, can save resources, and reduces operation cost, thereby being capable of obviously improving the operation efficiency of airports.
Description
[technical field]
The present invention relates to the aircraft parking system, particularly a kind of optical principle of utilizing, visual the sliding of simple in structure, stable performance, the aircraft parking system that is easy to discern stops the dipped beam column guide device.
[background technology]
Modern civil airport transportation is very busy, and aircraft also needs special personnel's channeling conduct landing when marching into the arena laggard nearly stop.Therefore, aircraft docking guidance system is a crucial system in the Civil Aviation Airport, and stopping for the safety and precise of aircraft has crucial meaning.For faster, the safer aircraft that makes is stopped to assigned address, need easier, energy-conservation automatic docking guidance system, improve the utilization rate of seat in the plane resource effectively, reduce the delay of flight, when stopping, aircraft reaches the purpose that saves time, saves resource to satisfy, thereby comprehensively improve the management level on level ground, station, airport, save operating cost.
[summary of the invention]
The objective of the invention is in order to address the above problem, and provide a kind of visual sliding of aircraft parking system to stop the dipped beam column guide device, this system utilizes visual observation guiding light beam, can make the pilot come operating aircraft to make it progressively near stop position by own visual result, final correct the stop, this system architecture is simple, dependable performance.
The present invention is for realizing goal of the invention, and the scheme that is adopted is that visual the sliding of a kind of aircraft parking system of design stops the dipped beam column guide device.It is characterized in that comprising a front opening casing and vertically be installed in two groups of Column being luminous in the casing; Described two groups of Column being luminous are installed along the horizontal and vertical segment distance of all being separated by mutually, and the Column being luminous of close casing oral area is a column of green light, and the Column being luminous that is loaded on casing far-end inner corner portion is a column of red light; And described column of green light disconnects a segment distance in the stage casing.
The invention has the beneficial effects as follows: the present invention is based on the pilot and move driving an airplane, observed light beam shows in driving cabin, and judge and instruct the operation of oneself in the own position that is driven an airplane.Thereby finish accurate stop, need not ground staff's guiding, can substitute original hand guided pattern.This mode of the present invention is different from laser, and to the not injury of people's eyes, is a safe and reliable guidance mode, can energy savings, reduce operating cost, and therefore can improve the operational efficiency on airport significantly.
[description of drawings]
Fig. 1 advances dipped beam column guide device synoptic diagram;
The corresponding shift position of column of green light synoptic diagram when Fig. 2 multiple spot is stopped the position;
Fig. 3 advances dipped beam column guide device observing effect figure.
Be described in detail with reference to accompanying drawing below in conjunction with embodiments of the invention.
[embodiment]
As shown in Figure 1, aircraft parking system of the present invention visual slides stops the dipped beam column guide device, by open front casing 3 with vertically be installed in two groups of Column being luminous in the casing etc. and form.One group of installing of close casing oral area in two groups of Column being luminous is a column of green light 2, and one group that is loaded on casing far-end interior angle position is column of red light 1.And column of green light disconnects a segment distance in the stage casing, goes to upper and lower two sections.Upper and lower two sections, the end that is connected an end with casing of column of green light are separately positioned on the mobile device 4 into interlock, with moved further and can fix.The upper and lower two sections synchronous mobile devices of column of green light are to drive leading screw by stepper motor to do rectilinear motion.
In order to be suitable for the stop needs of different type of machines, column of green light need be determined with the corresponding aircraft of guiding is corresponding with the distance of column of red light, with the accuracy that guarantees that guiding is stopped.
In addition, for the guidance light that makes red green can both be high-visible in the environment of different brightness, the brightness of described light source is adjusted after measuring ambient light brightness in real time by artificial adjustment or by light activated element automatically.
The present invention is based on the pilot at aircraft along sliding during center line L moves, observed light beam shows in driving cabin, and judges and instruct the operation of oneself in the aircraft position.Thereby finish accurate stop.This observed light beam shows, is to come out because of variation red, green glow post relative position is shown.As shown in Figure 3:
When aircraft during at position I, the pilot sees column of red light 1 preceding, column of green light 2 after, and the two apart from each other (right figure is the observed image of pilot) illustrates that aircraft need move on.
When aircraft continues to slide, when in-position II and III, the pilot still sees column of red light 1 preceding, column of green light 2 after, the two apart moves closer to, but still the no show stop position.
When aircraft taxi to position IV, when just arriving the A point, what the pilot saw is that column of red light 1 and column of green light 2 are overlapping, has promptly arrived stop position accurately.
Explanation shown in Figure 2, when for adapting to three kinds of aircrafts, when needing A, B, three stop positions of C, then column of green light need be by the mobile device 4 of interlock, and the stop needs of different aircrafts are satisfied in corresponding a, b, the c position of moving to.
Claims (5)
1. an aircraft parking system visual slides and stops the dipped beam column guide device, it is characterized in that comprising a front opening casing and vertically is installed in two groups of Column being luminous in the casing; One group of close casing oral area installation in described two groups of Column being luminous is column of green light, and one group that is loaded on casing far-end interior angle position is column of red light; And described column of green light disconnects a segment distance in the stage casing, goes to upper and lower two sections.
2. visual the sliding of aircraft parking system according to claim 1 stops the dipped beam column guide device, upper and lower two sections, the end that is connected an end with casing that it is characterized in that described column of green light, be separately positioned on the mobile device for interlock, also can fix with moved further.
3. visual the sliding of aircraft parking system according to claim 2 stops the dipped beam column guide device, it is characterized in that the upper and lower two sections synchronous mobile devices of described column of green light, is to drive leading screw by stepper motor to do rectilinear motion.
4. visual the sliding of aircraft parking system according to claim 3 stops the dipped beam column guide device, it is characterized in that described column of green light is corresponding definite with the corresponding aircraft of guiding with the distance of column of red light.
5. aircraft parking system according to claim 1 visual slides stops the dipped beam column guide device, adjusts automatically after the brightness that it is characterized in that described light source is measured ambient light brightness in real time by artificial adjustment or by light activated element.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100702677A CN101639989B (en) | 2009-08-28 | 2009-08-28 | Visual sliding berthing approaching light column guide device of airplane berth system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100702677A CN101639989B (en) | 2009-08-28 | 2009-08-28 | Visual sliding berthing approaching light column guide device of airplane berth system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101639989A CN101639989A (en) | 2010-02-03 |
| CN101639989B true CN101639989B (en) | 2011-06-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009100702677A Expired - Fee Related CN101639989B (en) | 2009-08-28 | 2009-08-28 | Visual sliding berthing approaching light column guide device of airplane berth system |
Country Status (1)
| Country | Link |
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| CN (1) | CN101639989B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102252619A (en) * | 2011-04-21 | 2011-11-23 | 中国民航大学 | Displacement distance measuring and displaying system in airplane berthing process |
| CN106448275B (en) * | 2014-12-30 | 2023-03-17 | 大连现代高技术集团有限公司 | Visualization-based real-time guiding system for airplane berthing |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4015235A (en) * | 1974-06-05 | 1977-03-29 | The Rank Organisation Limited | Aircraft parking guidance indicator |
| EP0421852A1 (en) * | 1989-10-02 | 1991-04-10 | Societe Financiere Pour L'electronique | Method and installation for azimuth guidance of an aircraft during the approach |
| CN1787946A (en) * | 2003-04-09 | 2006-06-14 | 机场标志有限公司 | Docking guidance |
| CN1799940A (en) * | 2005-12-31 | 2006-07-12 | 方殿荣 | Novel precise sea-way entering indication method and system |
| CN101405186A (en) * | 2006-01-13 | 2009-04-08 | Bwt产权公司 | Visual navigational aids based on high intensity leds |
-
2009
- 2009-08-28 CN CN2009100702677A patent/CN101639989B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4015235A (en) * | 1974-06-05 | 1977-03-29 | The Rank Organisation Limited | Aircraft parking guidance indicator |
| EP0421852A1 (en) * | 1989-10-02 | 1991-04-10 | Societe Financiere Pour L'electronique | Method and installation for azimuth guidance of an aircraft during the approach |
| CN1787946A (en) * | 2003-04-09 | 2006-06-14 | 机场标志有限公司 | Docking guidance |
| CN1799940A (en) * | 2005-12-31 | 2006-07-12 | 方殿荣 | Novel precise sea-way entering indication method and system |
| CN101405186A (en) * | 2006-01-13 | 2009-04-08 | Bwt产权公司 | Visual navigational aids based on high intensity leds |
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| Publication number | Publication date |
|---|---|
| CN101639989A (en) | 2010-02-03 |
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Granted publication date: 20110608 Termination date: 20180828 |