CN109035875B - Visual directional guiding device applied to airport runway - Google Patents
Visual directional guiding device applied to airport runway Download PDFInfo
- Publication number
- CN109035875B CN109035875B CN201811199207.0A CN201811199207A CN109035875B CN 109035875 B CN109035875 B CN 109035875B CN 201811199207 A CN201811199207 A CN 201811199207A CN 109035875 B CN109035875 B CN 109035875B
- Authority
- CN
- China
- Prior art keywords
- control unit
- lamp
- electrically connected
- lamp body
- unit
- Prior art date
- 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.)
- Active
Links
- 230000000007 visual effect Effects 0.000 title claims abstract description 22
- 239000011521 glass Substances 0.000 claims abstract description 5
- 238000012544 monitoring process Methods 0.000 claims description 21
- 230000003287 optical effect Effects 0.000 claims description 12
- 238000001514 detection method Methods 0.000 claims description 5
- 230000011664 signaling Effects 0.000 claims description 3
- 230000002159 abnormal effect Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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 invention provides a visual directional guiding device applied to an airport runway, which is respectively arranged at two sides of the airport runway and comprises: the bottom mounting plate is provided with a supporting rod, and the supporting rod is detachably arranged on the bottom mounting plate through a flange plate; the power supply box is arranged on the supporting rod, and a power supply and a controller are arranged in the power supply box; the guide lamp body sets up the top of bracing piece, a window has been seted up on the lateral wall of guide lamp body, be provided with transparent glass in the window, the guide lamp body includes: the stepping motor is arranged at the center of the top of the base, and the rotating shaft of the stepping motor is vertically arranged at the top of the stepping motor. The visual directional guiding device provided by the invention is used at night at an airport, and can indicate the main traveling direction to a pilot, so that the pilot can visually distinguish the runway environment and can be helped to align the runway when the aircraft travels to a preset point.
Description
Technical Field
The invention relates to the field of airport light guiding devices, in particular to a visual directional guiding device applied to an airport runway.
Background
According to the technical standard of the civil helicopter flight field, the helicopter is used at night, and when the main approach direction is necessary to be indicated to pilots and the conditions allow, an approach lighting system is preferably arranged. The approach light system is a kind of navigation light, and is used for providing visual reference of runway entrance position and direction under the condition of night or low-visibility approach of an airplane. The approach light is mounted at the approach end of the runway to enable the pilot to visually discern the runway environment and help the pilot align the runway when the approach of the aircraft reaches a predetermined point. The approach lighting system consists of a central line lamp with a distance of 30M and a transverse line lamp with a distance of 90M from the side line of FATO, wherein the length of the transverse line lamp is 18M, and the transverse line lamp is preferably arranged on a horizontal straight line, is perpendicular to the line where the central line lamp is positioned and is bisected by the line. The horizontal row lamps are composed of two lamps at two sides of a central line respectively, the distance is 4.5M, the central line lamps can be 3 or more than 3, but the arrangement area of the lamp close to a lamplight system is large, and the lamp is more and is not applicable to all airports.
Disclosure of Invention
The invention provides a visual directional guiding device applied to an airport runway, and aims to solve the problem that pilots align the runway when the aircraft travels to a preset point.
In order to achieve the above object, an embodiment of the present invention provides a visual directional guiding device applied to an airport runway, which is respectively disposed at two sides of the airport runway, comprising:
the bottom mounting plate is arranged on the ground, a supporting rod is arranged on the bottom mounting plate, and the supporting rod is detachably arranged on the bottom mounting plate through a flange plate;
the power supply box is arranged on the supporting rod, and a power supply and a controller are arranged in the power supply box;
the guide lamp body sets up the top of bracing piece, a window has been seted up on the lateral wall of guide lamp body, be provided with transparent glass in the window, the guide lamp body includes:
the base is arranged at the top of the supporting rod, and the guide lamp body is fixedly arranged on the supporting rod through the base;
the stepping motor is arranged at the center of the top of the base, and a rotating shaft of the stepping motor is vertically arranged at the top of the stepping motor;
the optical reflector is fixedly arranged on the stepping motor through a rotating mechanism, is arranged on the rotating mechanism at a first preset angle and faces upwards;
the upper cover plate is arranged at the top of the guide lamp body, a pressing sheet is sleeved outside the upper cover plate, a lamp source is fixed at the central position of the upper cover plate through the pressing sheet, and the lamp source penetrates through the upper cover plate;
the lamp cap is arranged at the top of the upper cover plate and covers the lamp source.
The guide lamp body is internally provided with a sensor, the sensor is arranged on the stepping motor, a first end of the sensor is electrically connected with the stepping motor, and a second end of the sensor is electrically connected with the controller.
The guiding lamp body is internally provided with a square tube, the square tube is internally provided with an electric wire for connecting the sensor and the controller, and the square tube is internally provided with an electric wire for connecting a lamp source and a power supply.
Wherein the controller comprises:
the first end of the first control unit is electrically connected with the monitoring unit and is used for receiving the monitoring signal sent by the monitoring unit;
the first lamp brightness control unit is electrically connected with the second end of the first control unit and is used for receiving a first control signal sent by the first control unit according to the monitoring signal and adjusting the brightness of the lamp source according to the first control signal;
the first motor control unit is electrically connected with the third end of the first control unit and is used for receiving a second control signal sent by the first control unit according to the monitoring signal and controlling the rotating speed of the motor according to the second control signal.
The first control unit, the first lamp brightness control unit and the first motor control unit are arranged in a power box at the first side of the airport runway.
Wherein the controller further comprises:
the signal synchronization unit is electrically connected with the fourth end of the first control unit and is used for receiving a first control signal and a second control signal sent by the first control unit;
the first end of the second control unit is electrically connected with the signal synchronization unit and is used for receiving a first control signal and a second control signal sent by the signal synchronization unit;
the second lamp brightness control unit is electrically connected with the second end of the second control unit and is used for receiving a first control signal sent by the second control unit and adjusting the brightness of the lamp source according to the first control signal;
and the second motor control unit is electrically connected with a third end of the second control unit and is used for receiving a second control signal sent by the second control unit and controlling the rotating speed of the motor according to the second control signal.
The second control unit, the second lamp brightness control unit and the second motor control unit are all arranged in a power supply box of the visual orientation guiding device at the second side of the airport runway.
The signal synchronization unit is further configured to receive a feedback signal sent by the second control unit, and send the feedback signal to the first control unit.
The first control unit is further configured to send the received feedback signal to the monitoring unit.
Wherein the controller further comprises:
the current detection unit is electrically connected with the fifth end of the first control unit and is used for detecting the current running condition of the controller.
The scheme of the invention has the following beneficial effects:
the visual directional guiding device provided by the invention is used at night at an airport, and can indicate the main traveling direction to a pilot, so that the pilot can visually distinguish the runway environment and can be helped to align the runway when the aircraft travels to a preset point.
Drawings
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a schematic view of the internal structure of the present invention;
FIG. 3 is a side view of the internal structure of the present invention;
fig. 4 is a schematic diagram of the circuit connection of the present invention.
[ reference numerals description ]
1-a bottom mounting plate; 2-a flange plate; 3-a power box; 4-supporting rods; 5-guiding the lamp body; 6-a lamp cap; 7-fixing clips; 8-a stepper motor; 9-rotating shaft; 10-a rotation mechanism; 11-an optical reflector; 12-a base; 13-window; 14-an upper cover plate; 15-tabletting; 16-a light source; 17-sensor; 18-square tubes; 19-connecting column.
Detailed Description
In order to make the technical problems, technical solutions and advantages to be solved more apparent, the following detailed description will be given with reference to the accompanying drawings and specific embodiments.
The invention provides a visual directional guiding device applied to an airport runway, aiming at the problem that the existing pilot aligns the runway when the airplane runs to reach a preset point.
As shown in fig. 1 to 3, an embodiment of the present invention provides a visual directional guide device applied to an airport runway, respectively disposed at both sides of the airport runway, comprising: the bottom mounting plate 1 is arranged on the ground, a supporting rod 4 is arranged on the bottom mounting plate 1, and the supporting rod 4 is detachably arranged on the bottom mounting plate 1 through a flange plate 2; the power supply box 3 is arranged on the supporting rod 4, and a power supply and a controller are arranged in the power supply box 3; the guide lamp body 5 is arranged at the top of the supporting rod 4, a window 13 is formed in the side wall of the guide lamp body 5, transparent glass is arranged in the window 13, and the guide lamp body 5 comprises: the base 12 is arranged at the top of the supporting rod 4, and the guide lamp body 5 is fixedly arranged on the supporting rod 4 through the base 12; the stepping motor 8 is arranged at the center of the top of the base 12, and a rotating shaft 9 of the stepping motor 8 is vertically arranged at the top of the stepping motor 8; the optical reflector 11 is fixedly arranged on the stepping motor 8 through a rotating mechanism 10, the optical reflector 11 is arranged on the rotating mechanism 10 at a first preset angle, and the reflecting surface of the optical reflector 11 faces upwards; the upper cover plate 14 is arranged at the top of the guide lamp body 5, a pressing sheet 15 is sleeved outside the upper cover plate 14, a lamp source 16 is fixed at the center position of the upper cover plate 14 through the pressing sheet 15, and the lamp source 16 is arranged on the upper cover plate 14 in a penetrating manner; a lamp cap 6 is disposed on top of the upper cover plate 14 to cover the lamp source 16.
The main and auxiliary lamps of the visual directional guide device disclosed by the embodiment of the invention have the same structure and are respectively arranged at two sides of an airport runway and comprise a guide lamp body 5, a power supply box 3, a lamp body bracket and a lamp cap 6; the lamp cap 6 is used for covering the lamp source 16 and has the function of water resistance; a stepping motor 8 is arranged in the guide lamp body 5, the stepping motor 8 is positioned at the center of the base 12, the optical reflector 11 is fixed on the rotating mechanism 10 at an inclined angle, the rotating mechanism 10 is connected with the stepping motor 8 through a rotating shaft 9, a lamp source 16 is fixed in the middle of the upper cover plate 14 through a pressing plate 15 and is positioned right above the optical reflector 11, and lamplight is focused on the center of the optical reflector 11 through a middle hole of the upper cover plate 14 to reflect light to form a light beam; when the stepping motor 8 rotates, the optical reflector 11 also rotates, and the light beam formed on the optical reflector 11 rotates around the rotation shaft 9 as a center of a circle and irradiates through the transparent glass on the side wall of the guiding lamp body 5.
The guiding lamp body 5 is internally provided with a sensor 17, the sensor 17 is arranged on the stepping motor 8, a first end of the sensor 17 is electrically connected with the stepping motor 8, and a second end of the sensor 17 is electrically connected with the controller.
The guiding lamp body 5 is internally provided with a square tube 18, the square tube 18 is internally provided with an electric wire for connecting the sensor 17 and the controller, and the square tube 18 is internally provided with an electric wire for connecting the lamp source 16 and the power supply.
The sensor 17 according to the above embodiment of the present invention is located on the motor so as to acquire a signal and control the rotation speed; the lamp source 16, the optical reflector 11, the stepping motor 8, the rotating mechanism 10 and the sensor 17 are assembled and then are arranged in the guiding lamp body 5; the bottom of the guiding lamp body 5 is provided with a connecting column 19, the connecting column 19 is rotationally connected with the supporting rod 4, and the direction of the guiding lamp body 5 can be freely adjusted; the power box is fixed on the supporting rod 4 through a fixing clamp 7, and the direction of the power box 3 can be freely adjusted.
The visual directional guiding device according to the above embodiment of the present invention is divided into a main and auxiliary lamp structure, in which the rotation directions of the driving motors of the main and auxiliary lamps are opposite, the running directions of the rotating light beams are opposite, the time when the light beams of the main and auxiliary lamps reach the position of the lamp body window 13 is consistent, when the pilot is at the position deviated from the runway, the light beams of which side lamp firstly scan the pilot, the visual is firstly flashed, and the light beams of the other side are rotated at a certain angle to scan the pilot and then flashed.
Wherein the controller comprises: the first end of the first control unit is electrically connected with the monitoring unit and is used for receiving the monitoring signal sent by the monitoring unit; the first lamp brightness control unit is electrically connected with the second end of the first control unit and is used for receiving a first control signal sent by the first control unit according to the monitoring signal and adjusting the brightness of the lamp source 16 according to the first control signal; the first motor control unit is electrically connected with the third end of the first control unit and is used for receiving a second control signal sent by the first control unit according to the monitoring signal and controlling the rotating speed of the motor according to the second control signal.
The first control unit, the first lamp brightness control unit and the first motor control unit are all arranged in the power box 3 at the first side of the airport runway.
Wherein the controller further comprises: the signal synchronization unit is electrically connected with the fourth end of the first control unit and is used for receiving a first control signal and a second control signal sent by the first control unit; the first end of the second control unit is electrically connected with the signal synchronization unit and is used for receiving a first control signal and a second control signal sent by the signal synchronization unit; the second lamp brightness control unit is electrically connected with the second end of the second control unit, and is used for receiving a first control signal sent by the second control unit and adjusting the brightness of the lamp source 16 according to the first control signal; and the second motor control unit is electrically connected with a third end of the second control unit and is used for receiving a second control signal sent by the second control unit and controlling the rotating speed of the motor according to the second control signal.
The second control unit, the second lamp brightness control unit and the second motor control unit are all arranged in the power box 3 of the visual orientation guiding device on the second side of the airport runway.
The signal synchronization unit is further configured to receive a feedback signal sent by the second control unit, and send the feedback signal to the first control unit.
The first control unit is further configured to send the received feedback signal to the monitoring unit.
Wherein the controller further comprises: the current detection unit is electrically connected with the fifth end of the first control unit and is used for detecting the current running condition of the controller.
The controller according to the above embodiment of the present invention is composed of a first control unit, the first lamp brightness control unit, the first motor control unit, the second lamp brightness control unit, the second motor control unit, a signal synchronization unit and a current detection unit, where the first control unit receives a signal from a local or remote monitoring unit, and sets the brightness level of the main lamp source 16 through the first lamp brightness control unit, and simultaneously controls the stepper motor 8 to perform variable speed rotation through the first motor control unit, and then sends a first control signal and a second control signal to the second control unit through the signal synchronization unit, and the second control unit respectively controls the second lamp brightness control unit to set the brightness level of the auxiliary lamp source 16 and control the stepper motor 8 to perform variable speed rotation according to the first control signal and the second control signal, and the second control unit may also send a feedback signal to the first control unit through the signal synchronization unit, and the first control unit receives the feedback signal, and sends the remote status information of the system to the client of the remote monitoring unit; when the current detection unit detects that the system operation current is abnormal or feedback information of the second controller is not received for 5 times continuously in the operation process, the system immediately stops operation, and abnormal information is reported to the remote monitoring unit.
While the foregoing is directed to the preferred embodiments of the present invention, it will be appreciated by those skilled in the art that various modifications and adaptations can be made without departing from the principles of the present invention, and such modifications and adaptations are intended to be comprehended within the scope of the present invention.
Claims (4)
1. Visual directional guide devices applied to airport runways are respectively arranged on two sides of the airport runways, and are characterized by comprising:
the bottom mounting plate is arranged on the ground, a supporting rod is arranged on the bottom mounting plate, and the supporting rod is detachably arranged on the bottom mounting plate through a flange plate;
the power supply box is arranged on the supporting rod, and a power supply and a controller are arranged in the power supply box;
the guide lamp body sets up the top of bracing piece, a window has been seted up on the lateral wall of guide lamp body, be provided with transparent glass in the window, the guide lamp body includes:
the base is arranged at the top of the supporting rod, and the guide lamp body is fixedly arranged on the supporting rod through the base;
the stepping motor is arranged at the center of the top of the base, and a rotating shaft of the stepping motor is vertically arranged at the top of the stepping motor;
the optical reflector is fixedly arranged on the stepping motor through a rotating mechanism, is arranged on the rotating mechanism at a first preset angle and faces upwards;
the upper cover plate is arranged at the top of the guide lamp body, a pressing sheet is sleeved outside the upper cover plate, a lamp source is fixed at the central position of the upper cover plate through the pressing sheet, and the lamp source penetrates through the upper cover plate;
the lamp cap is arranged at the top of the upper cover plate and covers the lamp source;
a sensor is arranged in the guide lamp body, the sensor is arranged on the stepping motor, a first end of the sensor is electrically connected with the stepping motor, and a second end of the sensor is electrically connected with the controller;
the guiding lamp body is internally provided with a square tube, the square tube is internally provided with an electric wire for connecting the sensor and the controller, and the square tube is internally provided with an electric wire for connecting a lamp source and a power supply;
the controller includes:
the first end of the first control unit is electrically connected with the monitoring unit and is used for receiving the monitoring signal sent by the monitoring unit;
the first lamp brightness control unit is electrically connected with the second end of the first control unit and is used for receiving a first control signal sent by the first control unit according to the monitoring signal and adjusting the brightness of the lamp source according to the first control signal;
the first motor control unit is electrically connected with the third end of the first control unit and is used for receiving a second control signal sent by the first control unit according to the monitoring signal and controlling the rotating speed of the motor according to the second control signal;
the first control unit, the first lamp brightness control unit and the first motor control unit are arranged in a power supply box of the visual orientation guiding device at the first side of the airport runway;
wherein the controller further comprises:
the signal synchronization unit is electrically connected with the fourth end of the first control unit and is used for receiving a first control signal and a second control signal sent by the first control unit;
the first end of the second control unit is electrically connected with the signal synchronization unit and is used for receiving a first control signal and a second control signal sent by the signal synchronization unit;
the second lamp brightness control unit is electrically connected with the second end of the second control unit and is used for receiving a first control signal sent by the second control unit and adjusting the brightness of the lamp source according to the first control signal;
the second motor control unit is electrically connected with a third end of the second control unit and is used for receiving a second control signal sent by the second control unit and controlling the rotating speed of the motor according to the second control signal;
the second control unit, the second lamp brightness control unit and the second motor control unit are all arranged in a power supply box of the visual orientation guiding device at the second side of the airport runway.
2. The visual directional guide device applied to an airport runway of claim 1, wherein said signal synchronizing unit is further configured to receive a feedback signal from said second control unit and transmit said feedback signal to said first control unit.
3. Visual directional guide device for use on an airport runway according to claim 2 wherein the first control unit is further adapted to send the received feedback signal to the monitoring unit.
4. The visual directional guide device for use on an airport runway of claim 1, wherein the controller further comprises:
the current detection unit is electrically connected with the fifth end of the first control unit and is used for detecting the current running condition of 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 CN109035875A (en) | 2018-12-18 |
| CN109035875B true CN109035875B (en) | 2024-03-08 |
Family
ID=64613124
Family Applications (1)
| 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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109035875B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110364033B (en) * | 2019-05-15 | 2020-08-25 | 江苏星华机场设施有限公司 | Airport ground plane guidance system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN207213810U (en) * | 2017-09-15 | 2018-04-10 | 深圳市欧士照明科技有限公司 | A kind of LED floodlight of specular removal |
| 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 |
-
2018
- 2018-10-15 CN CN201811199207.0A patent/CN109035875B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN207213810U (en) * | 2017-09-15 | 2018-04-10 | 深圳市欧士照明科技有限公司 | A kind of LED floodlight of specular removal |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109035875A (en) | 2018-12-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109035875B (en) | Visual directional guiding device applied to airport runway | |
| CN109548250B (en) | Landing lamp and taxi lamp debugging and calibrating system and method | |
| KR102384816B1 (en) | Night landing guidance system using gyro sensor | |
| KR101708423B1 (en) | crosswalk lighting equipment | |
| US20180370653A1 (en) | Takeoff and landing assist apparatus for flight vehicle, and flight device | |
| CN208938353U (en) | Visual orientation guide device applied to airfield runway | |
| US2155295A (en) | Airport lighting system | |
| JP4124090B2 (en) | Guide light device | |
| CN108621916B (en) | Intelligent headlamp and its control method | |
| CN111547259A (en) | Method for guiding helicopter to land by using light guide system | |
| US5136288A (en) | Method and installation for providing alignment guidance to an aircraft in the approach stage | |
| RU2397115C1 (en) | Aircraft landing system | |
| KR102378204B1 (en) | Aeronautical light aids for vertical take-off and landing | |
| CN210721855U (en) | Novel signal lamp convenient to turn to and adjust | |
| CN208797472U (en) | A kind of thread-laying device | |
| US3813657A (en) | Glide slope indicator | |
| US3701969A (en) | Optical failsafe airplane landing guidance system | |
| US5200748A (en) | Path guidance indication apparatus for vehicles or craft | |
| CN204130000U (en) | A kind of automobile follow-up steering headlight teaching demonstrating table | |
| CN209248772U (en) | Pedestrian traffic lamp | |
| CN101639989B (en) | Visual sliding berthing approaching light column guide device of airplane berth system | |
| WO2011073846A1 (en) | Optical device for indicating the glide angle of aircraft | |
| RU174351U1 (en) | AIRCRAFT LASER LANDING SYSTEM | |
| JPH11201753A (en) | Setting method and device for marking laser reference | |
| KR101940956B1 (en) | A traffic police mannequin |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |