CN109035875A - Visual orientation guide device applied to airfield runway - Google Patents
Visual orientation guide device applied to airfield runway Download PDFInfo
- Publication number
- CN109035875A CN109035875A CN201811199207.0A CN201811199207A CN109035875A CN 109035875 A CN109035875 A CN 109035875A CN 201811199207 A CN201811199207 A CN 201811199207A CN 109035875 A CN109035875 A CN 109035875A
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- Prior art keywords
- control unit
- signal
- guide device
- airfield runway
- lamp
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- 230000000007 visual effect Effects 0.000 title claims abstract description 27
- 239000011521 glass Substances 0.000 claims abstract description 6
- 238000012544 monitoring process Methods 0.000 claims description 20
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 11
- 230000007246 mechanism Effects 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 7
- 238000007689 inspection Methods 0.000 claims 1
- 241001347978 Major minor Species 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 241001465382 Physalis alkekengi Species 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V14/00—Controlling the distribution of the light emitted by adjustment of elements
- F21V14/04—Controlling the distribution of the light emitted by adjustment of elements by movement of reflectors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/003—Arrangement of electric circuit elements in or on lighting devices the elements being electronics drivers or controllers for operating the light source, e.g. for a LED array
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
Abstract
The present invention provides a kind of visual orientation guide devices applied to airfield runway, it is respectively arranged at the two sides of airfield runway, it include: bottom mounting plate, setting is having a support rod on the bottom mounting plate, and the support rod is removably mounted on the bottom mounting plate by a ring flange；Power supply box, setting are provided with power supply and controller on the support rod, and in the power supply box；Guide lamp body, the top of the support rod is set, a window is offered on the side wall of the guidance lamp body, transparent glass is provided in the window, the guidance lamp body includes: stepper motor, the center of the base top is set, and the rotary shaft of the stepper motor is vertically arranged in the top of stepper motor.Visual orientation guide device provided by the present invention can indicate main direction of travel to pilot, enable pilot visually to differentiate runway environment, pilot is helped to be aligned runway when aircraft advances and reaches predetermined point in airport night use.
Description
Technical field
The present invention relates to airfield light guide device field, in particular to a kind of visual orientation applied to airfield runway draws
Lead device.
Background technique
According to civil helicopter field flying field technical standard, airport night use, when it is necessary to indicate to lead to pilot
Want into nearly direction and conditions permit when, approach light sys tem is preferably set.Approach light sys tem is one kind of navigational lighting aid, for flying
Machine is in night or low visibility into providing the visual reference of runway threshold position and direction in nearly situation.It is mounted on into low beam light
Runway into proximal end, enable pilot visually to differentiate runway environment, help pilot in aircraft into the nearly predetermined point that reaches
When be aligned runway.Approach light sys tem is made of the middle-line lamp of spacing 30M and the Cross Bar away from the sideline FATO 90M, Cross Bar
Length is 18M, is preferably arranged on a horizontal linear, and institute is vertical online and divided equally by it with middle-line lamp.Cross Bar should be by center
Each two lamp groups in line two sides are at spacing is that 3 or 3 or more, but approach light sys tem setting area can be used in 4.5M. middle-line lamp
Larger, lamps and lanterns are more and are not suitable for all airports.
Summary of the invention
The present invention provides a kind of visual orientation guide devices applied to airfield runway, and its purpose is to solve to fly
Member is when aircraft advances and reaches predetermined point the problem of alignment runway.
In order to achieve the above object, the embodiment provides a kind of visual orientation guidance applied to airfield runway
Device is respectively arranged at the two sides of airfield runway, comprising:
Bottom mounting plate, on the ground, setting is having a support rod on the bottom mounting plate, and the support rod is logical for setting
A ring flange is crossed to be removably mounted on the bottom mounting plate；
Power supply box, setting are provided with power supply and controller on the support rod, and in the power supply box；
Lamp body is guided, the top of the support rod is set, offers a window on the side wall of the guidance lamp body, it is described
Transparent glass is provided in window, the guidance lamp body includes:
The top of the support rod is arranged in pedestal, the pedestal, and the guidance lamp body is fixedly mounted by the pedestal
On the support rod；
Stepper motor, is arranged in the center of the base top, and the rotary shaft of the stepper motor is vertically arranged in
The top of stepper motor；
Optic reflector, the optic reflector is fixedly mounted on the stepper motor by a rotating mechanism, described
Optic reflector is arranged on the rotating mechanism in the first predetermined angle, and the reflective of the optic reflector sets upwardly
It sets；
Upper cover plate, is arranged in the top of the guidance lamp body, and the outer cover of the upper cover plate is equipped with a tabletting, the upper cover
The center of plate is fixed with a lamp source by the tabletting, and the lamp source is threaded through on the upper cover plate；
The top of the upper cover plate is arranged in the crown top of burner, covers the lamp source.
Wherein, a sensor is provided in the guiding lamp body, the sensor is arranged on the stepper motor, described
The first end of sensor is electrically connected with the stepper motor, and the second end of the sensor is electrically connected with the controller.
Wherein, it is additionally provided with a square tube in the guiding lamp body, is provided in the square tube for connecting the sensor
With the electric wire of the controller, the electric wire for connecting lamp source and power supply is additionally provided in the square tube.
Wherein, the controller includes:
The first end of first control unit, the first control unit is electrically connected with monitoring unit, for receiving the prison
Control the monitoring signal that unit issues；
The second of first lamp brightness control unit, the first lamp brightness control unit and the first control unit
End electrical connection, the first control signal issued for receiving the first control unit according to the monitoring signal, and according to institute
State the brightness that first control signal adjusts the lamp source；
The third end of first motor control unit, the first motor control unit and the first control unit is electrically connected
It connects, the second control signal issued for receiving the first control unit according to the monitoring signal, and according to described second
Control signal controls the revolving speed of the motor.
Wherein, the first control unit, the first lamp brightness control unit and the first motor control unit
It is arranged in the power supply box of the first side of airfield runway.
Wherein, the controller further include:
Signal synchronization unit, the signal synchronization unit is electrically connected with the 4th end of the first control unit, for connecing
Receive first control signal and second control signal that the first control unit issues；
The first end of second control unit, second control unit is electrically connected with the signal synchronization unit, for connecing
Receive first control signal and second control signal that the signal synchronization unit issues；
The second of second lamp brightness control unit, the second lamp brightness control unit and second control unit
End electrical connection, the first control signal issued for receiving second control unit, and according to the first control signal tune
The brightness of the whole lamp source；
Second motor control unit, second motor control unit and the third end of second control unit are electrically connected
It connects, the second control signal issued for receiving second control unit, and according to second control signal control
The revolving speed of motor.
Wherein, second control unit, the second lamp brightness control unit and second motor control unit
It is arranged in the power supply box of visual orientation guide device of airfield runway second side.
Wherein, the signal synchronization unit is also used to receive the feedback signal that second control unit issues, and by institute
It states feedback signal and is sent to the first control unit.
Wherein, the feedback signal that the first control unit is also used to receive is sent to the monitoring unit.
Wherein, the controller further include:
Current detecting unit, the current detecting unit are electrically connected with the 5th end of the first control unit, the electricity
Stream detection unit is used to detect the current running condition of the controller.
Above scheme of the invention have it is following the utility model has the advantages that
Visual orientation guide device provided by the present invention can indicate main row to pilot in airport night use
Into direction, pilot is enabled visually to differentiate runway environment, helps pilot when aircraft advances and reaches predetermined point pair
Neat runway.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is schematic diagram of internal structure of the invention；
Fig. 3 is internal structure side view of the invention；
Fig. 4 is circuit connection diagram of the invention.
[description of symbols]
1- bottom mounting plate；2- ring flange；3- power supply box；4- support rod；5- guides lamp body；The 6- crown top of burner；7- fixing clamp；8-
Stepper motor；9- rotary shaft；10- rotating mechanism；11- optic reflector；12- pedestal；13- window；14- upper cover plate；15- pressure
Piece；16- lamp source；17- sensor；18- square tube；19- connecting column.
Specific embodiment
To keep the technical problem to be solved in the present invention, technical solution and advantage clearer, below in conjunction with attached drawing and tool
Body embodiment is described in detail.
The present invention provides aiming at the problem that existing pilot alignment runway when aircraft advances and reaches predetermined point
A kind of visual orientation guide device applied to airfield runway.
As shown in Figure 1 to Figure 3, the embodiment provides a kind of visual orientations applied to airfield runway to guide dress
It sets, is respectively arranged at the two sides of airfield runway, comprising: bottom mounting plate 1, setting on the ground, are set on the bottom mounting plate 1
Setting is having a support rod 4, and the support rod 4 is removably mounted on the bottom mounting plate 1 by a ring flange 2；Power supply
Case 3, setting are provided with power supply and controller on the support rod 4, and in the power supply box 3；Lamp body 5 is guided, is arranged in institute
The top of support rod 4 is stated, a window 13 is offered on the side wall of the guidance lamp body 5, is provided with transparent glass in the window 13
Glass, the guidance lamp body 5 includes: pedestal 12, and the top of the support rod 4 is arranged in the pedestal 12, and the guidance lamp body 5 is logical
The pedestal 12 is crossed to be fixedly mounted on the support rod 4；The center at 12 top of pedestal is arranged in stepper motor 8,
The rotary shaft 9 of the stepper motor 8 is vertically arranged in the top of stepper motor 8；Optic reflector 11, the optic reflector 11
It is fixedly mounted on the stepper motor 8 by a rotating mechanism 10, the optic reflector 11 is arranged in the first predetermined angle
On the rotating mechanism 10, and the reflective surface of the optic reflector 11 is set up；Upper cover plate 14 is arranged in the guidance
The outer cover at the top of lamp body 5, the upper cover plate 14 is equipped with a tabletting 15, and the center of the upper cover plate 14 passes through the pressure
Piece 15 is fixed with a lamp source 16, and the lamp source 16 is threaded through on the upper cover plate 14；The upper cover plate 14 is arranged in the crown top of burner 6
Top covers the lamp source 16.
The major-minor modulated structure of visual orientation guide device described in the above embodiment of the present invention is consistent, is separately positioned on machine
The two sides of field runway include guidance lamp body 5, power supply box 3, bracket of lamp body and the crown top of burner 6；The crown top of burner 6 is for covering the lamp
Source 16, and play the role of waterproof；A stepper motor 8 is provided in the guidance lamp body 5, the stepper motor 8 is located at pedestal
12 center, the inclined angle of the optic reflector 11 are fixed on rotating mechanism 10, and rotating mechanism 10 passes through rotation
Axis 9 is connect with stepper motor 8, and lamp source 16 is fixed on the centre of upper cover plate 14 by tabletting 15, just positioned at optic reflector 11
Top, light are focused on the center of optic reflector 11 by the interstitial hole of upper cover plate 14, light are reflected away, and light is formed
Beam；When stepper motor 8 rotates, the optic reflector 11 is also rotated with, and the light beam formed on optic reflector 11 is to revolve
Shaft 9 is center of circle rotation, is shone out through the transparent glass on guidance 5 side wall of lamp body.
Wherein, a sensor 17 is provided in the guidance lamp body 5, the sensor 17 is arranged in the stepper motor 8
On, the first end of the sensor 17 is electrically connected with the stepper motor 8, the second end of the sensor 17 and the controller
Electrical connection.
Wherein, it is additionally provided with a square tube 18 in the guidance lamp body 5, be provided in the square tube 18 for connecting the biography
The electric wire of sensor 17 and the controller is additionally provided with the electric wire for connecting lamp source 16 Yu power supply in the square tube 18.
Sensor 17 described in the above embodiment of the present invention is located on motor, to obtain signal, controls revolving speed；It is described
Lamp source 16, optic reflector 11, stepper motor 8, rotating mechanism 10 and sensor 17 are packed into guidance lamp body 5 after assembling；It is described
The bottom of guidance lamp body 5 is provided with a connecting column 19, and the connecting column 19 is rotatablely connected with support rod 4, the guidance lamp body 5
Direction can freely adjust；The power pack is fixed on the support rod 4 by a fixing clamp 7, and the power supply box 3 can also be with
Free adjustment direction.
Visual orientation guide device described in the above embodiment of the present invention is divided into major-minor modulated structure, the driving electricity of major-minor lamp
Machine direction of rotation on the contrary, rotary light beam traffic direction also just on the contrary, major-minor lamp light beam reach 13 position of lamp body window time
Be consistent, when pilot be in drift off the runway which side when, the light beam of which side lamp just first strafes pilot, and vision is first glistened,
In addition the light beam on one side will rotate by a certain angle, and just strafe pilot, rear to glisten.
Wherein, the controller includes: first control unit, first end and the monitoring unit electricity of the first control unit
Connection, the monitoring signal issued for receiving the monitoring unit；First lamp brightness control unit, first lamp brightness
Control unit is electrically connected with the second end of the first control unit, for receiving the first control unit according to the monitoring
The first control signal that signal issues, and adjust according to the first control signal brightness of the lamp source 16；First motor control
Unit processed, the first motor control unit is electrically connected with the third end of the first control unit, for receiving described first
The second control signal that control unit is issued according to the monitoring signal, and the motor is controlled according to the second control signal
Revolving speed.
Wherein, the first control unit, the first lamp brightness control unit and the first motor control unit
It is arranged in the power supply box 3 of the first side of airfield runway.
Wherein, the controller further include: signal synchronization unit, the signal synchronization unit and the first control unit
The electrical connection of the 4th end, the first control signal and second control signal issued for receiving the first control unit；Second
The first end of control unit, second control unit is electrically connected with the signal synchronization unit, same for receiving the signal
Walk first control signal and second control signal that unit issues；Second lamp brightness control unit, second lamp brightness
Control unit is electrically connected with the second end of second control unit, the first control issued for receiving second control unit
Signal processed, and adjust according to the first control signal brightness of the lamp source 16；Second motor control unit, second electricity
Machine control unit is electrically connected with the third end of second control unit, second issued for receiving second control unit
Signal is controlled, and controls the revolving speed of the motor according to the second control signal.
Wherein, second control unit, the second lamp brightness control unit and second motor control unit
It is arranged in the power supply box 3 of the visual orientation guide device of airfield runway second side.
Wherein, the signal synchronization unit is also used to receive the feedback signal that second control unit issues, and by institute
It states feedback signal and is sent to the first control unit.
Wherein, the feedback signal that the first control unit is also used to receive is sent to the monitoring unit.
Wherein, the controller further include: current detecting unit, the current detecting unit and the first control unit
The electrical connection of the 5th end, the current detecting unit is used to detect the current running condition of the controller.
Controller described in the above embodiment of the present invention is controlled single by first control unit, first lamp brightness
First, the described first motor control unit, second control unit, the second lamp brightness control unit, second electricity
Machine control unit, signal synchronization unit and current detecting unit composition, the first control unit, which receives, comes from Local or Remote
Monitoring unit signal, and by the first lamp brightness control unit set king light lamp source 16 brightness degree, pass through simultaneously
The first motor control unit control stepper motor 8 carries out speed-changing rotation, then is controlled by signal synchronization unit to described second
Unit processed sends first control signal and second control signal, and second control unit is according to the first control signal and institute
Second control signal is stated, controls brightness degree and control that the second lamp brightness control unit sets secondary lamp lamp source 16 respectively
Stepper motor 8 processed carries out speed-changing rotation, and second control unit can also send feedback signal extremely by signal synchronization unit
First control unit, first control unit receive the feedback signal, and the long journey status information of system is sent to long-range monitoring
The client of unit；In the process of running when current detecting unit detects system running current exception or continuous 5 times are not received
To the feedback information of second controller, then system stops running immediately, and exception information is reported to remote monitoring unit.
The above is a preferred embodiment of the present invention, it is noted that for those skilled in the art
For, without departing from the principles of the present invention, it can also make several improvements and retouch, these improvements and modifications
It should be regarded as protection scope of the present invention.
Claims (10)
1. a kind of visual orientation guide device applied to airfield runway, is respectively arranged at the two sides of airfield runway, feature exists
In, comprising:
Bottom mounting plate, on the ground, setting is having a support rod on the bottom mounting plate, and the support rod passes through one for setting
Ring flange is removably mounted on the bottom mounting plate；
Power supply box, setting are provided with power supply and controller on the support rod, and in the power supply box；
Lamp body is guided, the top of the support rod is set, offers a window, the window on the side wall of the guidance lamp body
It is inside provided with transparent glass, the guidance lamp body includes:
The top of the support rod is arranged in pedestal, the pedestal, and the guidance lamp body is fixedly mounted on institute by the pedestal
It states on support rod；
Stepper motor, is arranged in the center of the base top, and the rotary shaft of the stepper motor is vertically arranged in stepping
The top of motor；
Optic reflector, the optic reflector are fixedly mounted on the stepper motor by a rotating mechanism, the optics
Reflector is arranged on the rotating mechanism in the first predetermined angle, and the reflective surface of the optic reflector is set up；
The top of the guidance lamp body is arranged in upper cover plate, and the outer cover of the upper cover plate is equipped with a tabletting, the upper cover plate
Center is fixed with a lamp source by the tabletting, and the lamp source is threaded through on the upper cover plate；
The top of the upper cover plate is arranged in the crown top of burner, covers the lamp source.
2. the visual orientation guide device according to claim 1 applied to airfield runway, which is characterized in that the guidance
Be provided with a sensor in lamp body, the sensor is arranged on the stepper motor, the first end of the sensor with it is described
Stepper motor electrical connection, the second end of the sensor are electrically connected with the controller.
3. the visual orientation guide device according to claim 2 applied to airfield runway, which is characterized in that the guidance
It is additionally provided with a square tube in lamp body, the electric wire for connecting the sensor and the controller, institute are provided in the square tube
State the electric wire being additionally provided in square tube for connecting lamp source and power supply.
4. the visual orientation guide device according to claim 2 applied to airfield runway, which is characterized in that the control
Device includes:
The first end of first control unit, the first control unit is electrically connected with monitoring unit, single for receiving the monitoring
The monitoring signal that member issues；
The second end electricity of first lamp brightness control unit, the first lamp brightness control unit and the first control unit
Connection, the first control signal issued for receiving the first control unit according to the monitoring signal, and according to described the
One control signal adjusts the brightness of the lamp source；
First motor control unit, the first motor control unit are electrically connected with the third end of the first control unit, are used
Believe in the second control signal that the reception first control unit is issued according to the monitoring signal, and according to second control
The revolving speed of number control motor.
5. the visual orientation guide device according to claim 4 applied to airfield runway, which is characterized in that described first
Control unit, the first lamp brightness control unit and the first motor control unit are arranged at the first side of airfield runway
Visual orientation guide device power supply box in.
6. the visual orientation guide device according to claim 4 applied to airfield runway, which is characterized in that the control
Device further include:
Signal synchronization unit, the signal synchronization unit is electrically connected with the 4th end of the first control unit, for receiving
State the first control signal and second control signal of first control unit sending；
The first end of second control unit, second control unit is electrically connected with the signal synchronization unit, for receiving
State the first control signal and second control signal of signal synchronization unit sending；
The second end electricity of second lamp brightness control unit, the second lamp brightness control unit and second control unit
Connection, the first control signal issued for receiving second control unit, and institute is adjusted according to the first control signal
State the brightness of lamp source；
Second motor control unit, second motor control unit are electrically connected with the third end of second control unit, are used
In the second control signal that reception second control unit issues, and the motor is controlled according to the second control signal
Revolving speed.
7. the visual orientation guide device according to claim 6 applied to airfield runway, which is characterized in that described second
Control unit, the second lamp brightness control unit and second motor control unit are arranged at airfield runway second side
Visual orientation guide device power supply box in.
8. the visual orientation guide device according to claim 6 applied to airfield runway, which is characterized in that the signal
Synchronization unit is also used to receive the feedback signal that second control unit issues, and the feedback signal is sent to described the
One control unit.
9. the visual orientation guide device according to claim 8 applied to airfield runway, which is characterized in that described first
The feedback signal that control unit is also used to receive is sent to the monitoring unit.
10. the visual orientation guide device according to claim 4 applied to airfield runway, which is characterized in that the control
Device processed further include:
Current detecting unit, the current detecting unit are electrically connected with the 5th end of the first control unit, the electric current inspection
Survey the current running condition that unit is used to detect the controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811199207.0A CN109035875B (en) | 2018-10-15 | 2018-10-15 | Visual directional guiding device applied to airport runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811199207.0A CN109035875B (en) | 2018-10-15 | 2018-10-15 | Visual directional guiding device applied to airport runway |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109035875A true CN109035875A (en) | 2018-12-18 |
| CN109035875B CN109035875B (en) | 2024-03-08 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811199207.0A Active CN109035875B (en) | 2018-10-15 | 2018-10-15 | Visual directional guiding device applied to airport runway |
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| Country | Link |
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| CN (1) | CN109035875B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110364033A (en) * | 2019-05-15 | 2019-10-22 | 浦江会亿智能科技有限公司 | A kind of airport ground aircraft guidance system |
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| CN208938353U (en) * | 2018-10-15 | 2019-06-04 | 湖南辰东科技有限公司 | Visual orientation guide device applied to airfield runway |
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| CN102478186A (en) * | 2010-11-30 | 2012-05-30 | 海洋王照明科技股份有限公司 | Automatic directionally regulated lamp fitting |
| CN103307505A (en) * | 2012-03-13 | 2013-09-18 | 刘胜 | Irradiation range-adjustable high-efficiency light-emitting diode (LED) airport runway center line light |
| CN204879923U (en) * | 2015-09-11 | 2015-12-16 | 中国人民解放军空军勤务学院 | Airport runway pilot lamp |
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| CN110364033A (en) * | 2019-05-15 | 2019-10-22 | 浦江会亿智能科技有限公司 | A kind of airport ground aircraft guidance system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109035875B (en) | 2024-03-08 |
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