CN105427677A - Distance display system of airplane berth guiding device - Google Patents
Distance display system of airplane berth guiding device Download PDFInfo
- Publication number
- CN105427677A CN105427677A CN201510976452.8A CN201510976452A CN105427677A CN 105427677 A CN105427677 A CN 105427677A CN 201510976452 A CN201510976452 A CN 201510976452A CN 105427677 A CN105427677 A CN 105427677A
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- CN
- China
- Prior art keywords
- display screen
- distance display
- digital
- progress bar
- microprocessor
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
Abstract
The invention belongs to the field of airplane berth guiding equipment and specifically relates to a distance display system of an airplane berth guiding device. The system comprises a microprocessor, a display screen controller, a power source, a digital distance display screen and a progress bar distance display screen, wherein the display screen controller and the power source are connected with the microprocessor; the display screen controller is respectively connected to the digital distance display screen and the progress bar distance display screen; the digital distance display screen comprises a first LED installation plate; the first LED installation plate is equipped with a digital indicator light display part constituted of a light emitting diode; the progress bar distance display screen comprises a second LED installation plate; the second LED installation plate is equipped with a plurality of bar-shaped indicator light display parts constituted of light emitting diodes; the microprocessor is also connected to a laser radar; the power source is a mains supply or a lithium battery or a storage battery; and the storage battery is connected to a solar cell panel. The system provided by the invention has the advantages of comprehensive functions, high safety and reliability, a rational structure and visual display.
Description
Technical field
The invention belongs to aircraft docking guidance apparatus field, especially relate to a kind of aircraft docking guidance device distance display system.
Background technology
Current aircraft docking guidance equipment is the distance value by display screen display digital form for pilot provides distance to guide, digitized display can show range information accurately, but its change due to displaying contents completes instantaneously, pilot cannot experience the speed that aircraft advances intuitively.
Summary of the invention
The problem to be solved in the present invention is to provide a kind of complete function, safe and reliable, rational in infrastructure, the aircraft docking guidance device distance display system of intuitive display.
For solving the problems of the technologies described above, the technical solution used in the present invention is: a kind of aircraft docking guidance device distance display system, comprise microprocessor, displaying screen controller, power supply, digital Distance display screen and progress bar formula distance display screen, described displaying screen controller is all connected with microprocessor with power supply, and described displaying screen controller is connected with progress bar formula distance display screen with digital Distance display screen respectively; Described digital Distance display screen comprises a LED installing plate, a described LED installing plate is provided with the digital pilot lamp display section be made up of light emitting diode, described progress bar formula distance display screen comprises the 2nd LED installing plate, described 2nd LED installing plate is arranged the some articles of formula pilot lamp display sections be made up of light emitting diode; Described microprocessor is also connected with laser radar.
Described power supply is civil power or lithium battery or accumulator.
Described accumulator is connected with solar panel.
Owing to adopting technique scheme, when displaying screen controller receives after laser radar is transferred to the range information of microprocessor, range information directly can be shown in the mode of numeral by digital Distance display screen, also can draw by computing the display length that progress bar is corresponding, and allow the bar formula pilot lamp display section of corresponding length light.When the range information change that displaying screen controller receives, digital Distance display screen displaying contents changes, progress bar display length also changes thereupon, the bar formula pilot lamp display section i.e. change of distance progress bar length can allow pilot experience the distance of aircraft advance intuitively, realize distance display accurately at distance procedure for displaying and allow pilot experience the change of speed, outer also in the display adding distance progress bar at the range information of display digital form, a kind of effect being similar to analog dial plate is played in the length change of distance progress bar, the speed of its length change represents the speed of aircraft advance, allow pilot can from perception aircraft advance speed instinctively like this, thus make it better control pace.In addition, the present invention can adopt solar panel to power, safe and reliable, environmental protection.
The invention has the beneficial effects as follows: there is complete function, safe and reliable, rational in infrastructure, the advantage of intuitive display.
Accompanying drawing explanation
Below by with reference to accompanying drawing describe the present invention particularly in conjunction with example, advantage of the present invention and implementation will be more obvious, wherein content shown in accompanying drawing is only for explanation of the present invention, and does not form restriction of going up in all senses of the present invention, in the accompanying drawings:
Fig. 1 is structured flowchart of the present invention
In figure:
1, microprocessor 2, displaying screen controller 3, power supply
4, digital Distance display screen 5, progress bar formula distance display screen 6, a LED installing plate
7, the 2nd LED installing plate 8, laser radar 9, accumulator
10, solar panel
Embodiment
As shown in Figure 1, a kind of aircraft docking guidance of the present invention device distance display system, comprise microprocessor 1, displaying screen controller 2, power supply 3, digital Distance display screen 4 and progress bar formula distance display screen 5, described displaying screen controller 2 is all connected with microprocessor 1 with power supply 3, and described displaying screen controller 2 is connected with progress bar formula distance display screen 5 with digital Distance display screen 4 respectively; Described digital Distance display screen 4 comprises a LED installing plate 6, a described LED installing plate 6 is provided with the digital pilot lamp display section be made up of light emitting diode, described progress bar formula distance display screen 5 comprises the 2nd LED installing plate 7, described 2nd LED installing plate 7 is arranged the some articles of formula pilot lamp display sections be made up of light emitting diode; Described microprocessor 1 is also connected with laser radar 8; Described power supply 3 is accumulator 9; Described accumulator 9 is connected with solar panel 10.
When displaying screen controller 2 receives after laser radar 8 is transferred to the range information of microprocessor, range information directly can be shown in the mode of numeral by digital Distance display screen 4, also can draw by computing the display length that progress bar is corresponding, and allow the bar formula pilot lamp display section of corresponding length light.When the range information change that displaying screen controller 2 receives, digital Distance display screen 4 displaying contents changes, the progress bar display length of progress bar formula distance display screen 5 also changes thereupon, the bar formula pilot lamp display section i.e. change of distance progress bar length can allow pilot experience the distance of aircraft advance intuitively, realize distance display accurately at distance procedure for displaying and allow pilot experience the change of speed, outer also in the display adding distance progress bar at the range information of display digital form, a kind of effect being similar to analog dial plate is played in the length change of distance progress bar, the speed of its length change represents the speed of aircraft advance, allow pilot can from perception aircraft advance speed instinctively like this, thus make it better control pace.In addition, the present invention can adopt solar panel 10 to power, safe and reliable, environmental protection.
Above embodiments of the invention have been described in detail, but described content being only preferred embodiment of the present invention, can not being considered to for limiting practical range of the present invention.All equalizations done according to the scope of the invention change and improve, and all should still belong within this patent covering scope.
Claims (3)
1. an aircraft docking guidance device distance display system, it is characterized in that: comprise microprocessor, displaying screen controller, power supply, digital Distance display screen and progress bar formula distance display screen, described displaying screen controller is all connected with microprocessor with power supply, and described displaying screen controller is connected with progress bar formula distance display screen with digital Distance display screen respectively; Described digital Distance display screen comprises a LED installing plate, a described LED installing plate is provided with the digital pilot lamp display section be made up of light emitting diode, described progress bar formula distance display screen comprises the 2nd LED installing plate, described 2nd LED installing plate is arranged the some articles of formula pilot lamp display sections be made up of light emitting diode; Described microprocessor is also connected with laser radar.
2. aircraft docking guidance device distance display system according to claim 1, is characterized in that: described power supply is civil power or lithium battery or accumulator.
3. aircraft docking guidance device distance display system according to claim 2, is characterized in that: described accumulator is connected with solar panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510976452.8A CN105427677A (en) | 2015-12-21 | 2015-12-21 | Distance display system of airplane berth guiding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510976452.8A CN105427677A (en) | 2015-12-21 | 2015-12-21 | Distance display system of airplane berth guiding device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105427677A true CN105427677A (en) | 2016-03-23 |
Family
ID=55505850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510976452.8A Pending CN105427677A (en) | 2015-12-21 | 2015-12-21 | Distance display system of airplane berth guiding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105427677A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106251711A (en) * | 2016-08-24 | 2016-12-21 | 桂林信通科技有限公司 | A kind of aircraft docking guidance and distance display and information system |
| CN106976567A (en) * | 2017-01-11 | 2017-07-25 | 天津华德宝航翼光电科技有限公司 | A kind of aircraft autonomous parking direction guides dynamic display system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4184655A (en) * | 1976-09-29 | 1980-01-22 | Anderberg Nils E | Parking guidance system for aircraft |
| JPH09207896A (en) * | 1996-02-09 | 1997-08-12 | Nec Corp | Apron guiding system |
| CN102252619A (en) * | 2011-04-21 | 2011-11-23 | 中国民航大学 | Displacement distance measuring and displaying system in airplane berthing process |
| CN103786893A (en) * | 2014-01-24 | 2014-05-14 | 中国民用航空总局第二研究所 | Aircraft berthing automatic guide method and device based on laser ranging technology |
| CN205211192U (en) * | 2015-12-21 | 2016-05-04 | 天津华德宝航翼光电科技有限公司 | Aircraft berth guiding device is apart from display system |
-
2015
- 2015-12-21 CN CN201510976452.8A patent/CN105427677A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4184655A (en) * | 1976-09-29 | 1980-01-22 | Anderberg Nils E | Parking guidance system for aircraft |
| JPH09207896A (en) * | 1996-02-09 | 1997-08-12 | Nec Corp | Apron guiding system |
| CN102252619A (en) * | 2011-04-21 | 2011-11-23 | 中国民航大学 | Displacement distance measuring and displaying system in airplane berthing process |
| CN103786893A (en) * | 2014-01-24 | 2014-05-14 | 中国民用航空总局第二研究所 | Aircraft berthing automatic guide method and device based on laser ranging technology |
| CN205211192U (en) * | 2015-12-21 | 2016-05-04 | 天津华德宝航翼光电科技有限公司 | Aircraft berth guiding device is apart from display system |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106251711A (en) * | 2016-08-24 | 2016-12-21 | 桂林信通科技有限公司 | A kind of aircraft docking guidance and distance display and information system |
| CN106976567A (en) * | 2017-01-11 | 2017-07-25 | 天津华德宝航翼光电科技有限公司 | A kind of aircraft autonomous parking direction guides dynamic display system |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160323 |