CN112591130A - Aircraft landing indicating device and using method thereof - Google Patents
Aircraft landing indicating device and using method thereof Download PDFInfo
- Publication number
- CN112591130A CN112591130A CN202011439226.3A CN202011439226A CN112591130A CN 112591130 A CN112591130 A CN 112591130A CN 202011439226 A CN202011439226 A CN 202011439226A CN 112591130 A CN112591130 A CN 112591130A
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- China
- Prior art keywords
- lamp
- aircraft
- controller
- aircraft landing
- pole
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/02—Systems using the reflection of electromagnetic waves other than radio waves
- G01S17/06—Systems determining position data of a target
- G01S17/08—Systems determining position data of a target for measuring distance only
Abstract
The invention discloses an aircraft landing indicating device and a using method thereof, and the aircraft landing indicating device comprises a base, a lamp post, a lamp holder and an indicating lamp, wherein the lamp post is arranged in the middle of the upper end of the base, the lamp holder is arranged in the lamp post, the indicating lamp is arranged on the lamp holder, a lamp shade is arranged on one side of the indicating lamp, a photosensitive sensor is arranged above the lamp shade, an overhaul lamp is arranged on one side of the lamp shade, radiating holes are formed in two side walls of the lamp post, and a dust screen is arranged in the radiating holes. Has the advantages that: according to the invention, by arranging the radar and the signal transmitter, when the radar detects the aircraft, a detection signal is transmitted to the controller, the controller enables the signal transmitter to work, and the transmitted signal can be transmitted to the instrument panel of the aircraft, at the moment, the signal transmitter can be used as a positioning reference point, a driver can better operate the aircraft according to the position of the reference point, so that the aircraft can accurately land in the middle of the runway, and the practicability of the device is improved.
Description
Technical Field
The invention relates to the technical field of aircraft landing indicating devices, in particular to an aircraft landing indicating device and a using method thereof.
Background
An aircraft is an apparatus that flies in the atmosphere or in the outer space of the atmosphere (space). Aircraft fall into 3 categories: aircraft, spacecraft, rockets, and missiles. Flying in the atmosphere is referred to as an aircraft, such as a balloon, airship, airplane, etc. They fly by the static buoyancy of air or the aerodynamic force generated by the relative movement of air, and need an indicating device to guide and indicate the aircraft in the landing process.
Present aircraft landing indicating device is because can't carry out accurate direction to the aircraft in the course of the work, and then lead to the aircraft to be falling the easy off tracking of in-process, the reducing means practicality, secondly, present aircraft landing indicating device is in the use because the luminance of pilot lamp is unadjustable, and then when aircraft and device are more and more near, the highlight of pilot lamp causes the amazing and forms the glare to driver's eyes easily, and then cause the influence to driver operation aircraft, furthermore, present aircraft landing indicating device is when needs overhaul, need arrange one by one, not only waste time, and increase staff's work load, reduce maintenance efficiency, consequently, an aircraft landing indicating device is urgently needed to solve current problem.
Disclosure of Invention
The present invention is directed to solving the above problems and providing an aircraft landing indicating device and method of use.
The invention realizes the purpose through the following technical scheme:
an aircraft landing indicating device comprises a base, a lamp pole, a lamp holder and an indicating lamp, wherein the lamp pole is arranged in the middle of the upper end of the base, the lamp holder is arranged in the lamp pole, the indicating lamp is arranged on the lamp holder, a lamp shade is arranged on one side of the indicating lamp, a photosensitive sensor is arranged above the lamp shade, an overhaul lamp is arranged on one side of the lamp shade, radiating holes are formed in two side walls of the lamp pole, a dustproof net is arranged in the radiating holes, a radiating fan is arranged on one side of the indicating lamp, a controller is arranged on the other side of the indicating lamp, a radar is arranged on the upper end of the lamp pole, a radar protective cover is arranged on the outer side of the radar, a signal transmitter is arranged on one side of the radar, a laser range finder is arranged on the, the improved mosquito repelling device comprises an access door, a lamp pole, a lamp post, a pull handle, a connecting seat, a reinforcing rod, a fixing hole, a fixing bolt and a hook, wherein the access door is connected with the lamp pole through a hinge, the pull handle is arranged on one side wall of the access door, a reflective sticker is arranged below the access door, the connecting seat is arranged at the upper end of one side wall of the lamp pole, the mosquito repelling device is arranged on the connecting seat, the reinforcing rod is arranged between the lamp pole and the base, the fixing hole is formed in the.
Further, the lamp pole with the lamp stand welding, the lamp stand with the lamp pole passes through the screw connection, the pilot lamp with the lamp stand passes through threaded connection, the lamp shade with the lamp pole passes through the draw-in groove and is connected.
Through the technical scheme, the indicator light guides the landing of the aircraft, and meanwhile, the lamp shade protects the indicator light.
Further, the photosensitive sensor with the lamp pole passes through the draw-in groove to be connected, overhaul the lamp with the lamp pole passes through the draw-in groove to be connected.
Through above-mentioned technical scheme, in the device working process, photosensitive sensor can real-time detection whether the pilot lamp works, works as when the pilot lamp is out of work, just with detected signal transmission to in the controller, controller control the maintenance lamp lights, when the staff overhauls, can confirm fast which the pilot lamp needs to be changed, improves maintenance efficiency.
Further, the louvre is formed in on the lamp pole, the dust screen with the louvre passes through the draw-in groove and is connected, the heat dissipation fan with the lamp stand passes through the screw connection, the controller with the lamp stand passes through the screw connection.
Through the technical scheme, in the working process of the device, the heat generated by the device is quickly discharged out of the device through the heat dissipation holes by the heat dissipation fan, and meanwhile, external dust can be prevented from entering the device through the dust screen.
Furthermore, the radar is connected with the lamp pole through a clamping groove, and the signal transmitter is connected with the lamp pole through the clamping groove.
Through the technical scheme, when the radar detects the aircraft, just will detect signal transmission to in the controller, the controller makes signal transmitter work to the signal that sends can transmit to the panel board of aircraft, at this moment, signal transmitter alright regard as a location reference point, and the driver can come better operation aircraft according to the position of reference point, makes its accurate landing in the runway centre.
Furthermore, the laser range finder with the lamp pole passes through the draw-in groove and is connected, the wire casing with the lamp pole passes through the screw connection, the fastener with the wire casing passes through the buckle and is connected.
Through above-mentioned technical scheme, but laser range finder real-time detection aircraft is to the distance of device, when the distance is more and more near, just arrives signal transmission in the controller, the controller control the luminance of pilot lamp prevents because of pilot lamp luminance is stronger and causes the amazing to driver's eyes, avoids causing the glare simultaneously, guarantees that the aircraft descends safely.
Furthermore, the access door with the lamp pole rotates to be connected, the pull handle with the access door passes through the screw connection.
Through the technical scheme, the access door is opened, so that the maintenance of workers can be facilitated.
Further, the reflecting sticker is adhered to the lamp pole, the connecting seat is connected with the lamp pole through screws, and the mosquito dispeller is connected with the connecting seat through screws.
Through above-mentioned technical scheme, when the aircraft fell on the runway, the reflection of light subsides can lead the gliding of aircraft, the mosquito repellant can drive the mosquito.
Further, the reinforcing rod is welded with the lamp post and the base, the fixing hole is formed in the base, the fixing bolt is connected with the fixing hole through threads, and the hook is connected with the lamp post through a screw.
Through the technical scheme, the fixing hole with fixing bolt combines together and can be with the device quick fixation, the couple can be convenient for hang the bar of guarding against when the runway overhauls.
The invention has the beneficial effects that:
1. in order to solve the problem that the existing aircraft landing indicating device is easy to deflect in the falling process due to the fact that the aircraft cannot be accurately guided in the working process, and the practicability of the device is reduced, the invention is provided with the radar and the signal transmitter, when the radar detects the aircraft, a detection signal is transmitted to the controller, the controller enables the signal transmitter to work, and the transmitted signal can be transmitted to an instrument panel of the aircraft, at the moment, the signal transmitter can be used as a positioning reference point, a driver can better operate the aircraft according to the position of the reference point, the aircraft can be accurately landed in the middle of a runway, and the practicability of the device is improved;
2. in order to solve the problem that the brightness of an indicating lamp of the existing aircraft landing indicating device can not be adjusted in the using process, and further when the aircraft and the device are closer and closer, strong light of the indicating lamp easily stimulates eyes of a driver and forms glare, so that the aircraft operation by the driver is influenced, the laser range finder is arranged, the laser range finder can detect the distance from the aircraft to the device in real time, when the distance is closer and closer, a signal is transmitted to a controller, the controller controls the brightness of the indicating lamp, the stimulation to the eyes of the driver due to the strong brightness of the indicating lamp is prevented, meanwhile, the glare is avoided, and the safe landing of the aircraft is ensured;
3. in order to solve the problems that the existing aircraft landing indicating device needs to be checked one by one when needing to be overhauled, not only is time wasted, but also the workload of workers is increased, and the overhauling efficiency is reduced.
Drawings
FIG. 1 is a front view of an aircraft landing indicating device of the present invention;
FIG. 2 is a cross-sectional view of a light pole of an aircraft landing indicator assembly of the present invention;
FIG. 3 is a cross-sectional view of a base of an aircraft landing indicating device of the present invention;
FIG. 4 is a block circuit diagram of a controller of an aircraft landing indication device in accordance with the present invention.
The reference numerals are explained below:
1. a base; 2. fixing the bolt; 3. reflecting light; 4. hooking; 5. an access door; 6. overhauling the lamp; 7. a photosensitive sensor; 8. a radar; 9. a connecting seat; 10. a mosquito dispeller; 11. a lamp shade; 12. an indicator light; 13. pulling a handle; 14. a lamp post; 15. a reinforcing bar; 16. heat dissipation holes; 17. a heat dissipation fan; 18. a laser range finder; 19. a signal transmitter; 20. a controller; 21. a lamp socket; 22. a dust screen; 23. a wire slot; 24. a wire clamp 25 and a fixing hole; 26. a hinge; 27. provided is a radar shield.
Detailed Description
The invention will be further described with reference to the accompanying drawings in which:
as shown in fig. 1-4, an aircraft landing indicating device comprises a base 1, a lamp post 14, a lamp holder 21 and an indicator light 12, wherein the lamp post 14 is arranged in the middle of the upper end of the base 1, the lamp holder 21 is arranged in the lamp post 14, the indicator light 12 is arranged on the lamp holder 21, a lamp shade 11 is arranged on one side of the indicator light 12, a photosensitive sensor 7 is arranged above the lamp shade 11, an overhaul lamp 6 is arranged on one side of the lamp shade 11, radiating holes 16 are arranged on both side walls of the lamp post 14, a dust screen 22 is arranged in the radiating holes 16, a radiating fan 17 is arranged on one side of the indicator light 12, a controller 20 is arranged on the other side of the indicator light 12, a radar 8 is arranged on the upper end of the lamp post 14, a radar protective cover 27 is arranged on the outer side of the radar 8, a signal emitter 19, the utility model discloses a lamp stand, including lamp stand 21, wire casing 23, be provided with fastener 24 on the wire casing 23, 11 below of lamp shade are provided with access door 5, access door 5 with lamp pole 14 passes through hinge 26 and connects, be provided with pull handle 13 on the 5 lateral walls of access door, 5 below of access door is provided with reflection of light subsides 3, 14 a lateral wall upper end of lamp pole is provided with connecting seat 9, be provided with mosquito repellant 10 on the connecting seat 9, lamp pole 14 with be provided with stiffener 15 between the base 1, be provided with fixed orifices 25 on the base 1, be provided with fixing bolt 2 in the fixed orifices 25, be provided with couple 4 on 14 another lateral wall of lamp pole.
In this embodiment, the lamp pole 14 with the welding of lamp stand 21, lamp stand 21 with the lamp pole 14 passes through the screw connection, pilot lamp 12 with the lamp stand 21 passes through threaded connection, lamp shade 11 with the lamp pole 14 passes through the draw-in groove and is connected, pilot lamp 12 leads for the descending of aircraft, and simultaneously lamp shade 11 is right pilot lamp 12 protects.
In this embodiment, photosensitive sensor 7 with lamp pole 14 passes through the draw-in groove and connects, overhaul lamp 6 with lamp pole 14 passes through the draw-in groove and connects, and in the device course of operation, photosensitive sensor 7 can real-time detection whether pilot lamp 12 works, works as pilot lamp 12 is out of work, just arrives with detected signal transmission in controller 20, controller 20 control overhaul lamp 6 lights, when the staff overhauls, can confirm fast which pilot lamp 12 needs to be changed, improves maintenance efficiency.
In this embodiment, the heat dissipation holes 16 are formed in the lamp post 14, the dust screen 22 is connected with the heat dissipation holes 16 through a clamping groove, the heat dissipation fan 17 is connected with the lamp holder 21 through screws, the controller 20 is connected with the lamp holder 21 through screws, in the working process of the device, the heat generated by the device is quickly discharged out of the heat dissipation holes 16 through the heat dissipation fan 17, and meanwhile, the dust screen 22 can prevent external dust from entering the device.
In this embodiment, radar 8 with lamp pole 14 passes through the draw-in groove and connects, signal transmitter 19 with lamp pole 14 passes through the draw-in groove and connects, works as when radar 8 detects the aircraft, just will detect signal transmission to in controller 20, controller 20 makes signal transmitter 19 work to the signal that sends can transmit the panel board of aircraft, at this moment, signal transmitter 19 alright regard as a location reference point, and the driver can come better operation aircraft according to the position of reference point, makes its accurate landing in the middle of the runway.
In this embodiment, laser range finder 18 with lamp pole 14 passes through the draw-in groove and connects, wire casing 23 with lamp pole 14 passes through screwed connection, fastener 24 with wire casing 23 passes through the buckle and connects, but laser range finder 18 real-time detection aircraft reaches the distance of device, and when the distance is more and more near, just reach signal transmission in controller 20, controller 20 control the luminance of pilot lamp 12 prevents because of pilot lamp 12 luminance is stronger and causes the amazing to driver's eyes, avoids causing the glare simultaneously, guarantees that the aircraft descends safely.
In this embodiment, reflection of light subsides 3 with lamp pole 14 bonds, connecting seat 9 with lamp pole 14 passes through screwed connection, mosquito repellant 10 with connecting seat 9 passes through screwed connection, and when the aircraft fell on the runway, reflection of light subsides 3 can lead the gliding of aircraft, mosquito repellant 10 can drive the mosquito.
In this embodiment, the access door 5 with the lamp pole 14 is rotated and is connected, the pull handle 13 with the access door 5 passes through the screw connection, will the access door 5 is opened, can be convenient for the staff to overhaul.
In this embodiment, the stiffener 15 with the lamp pole 14 and the base 1 is all welded, the fixed orifices 25 shaping in on the base 1, fixing bolt 2 with the fixed orifices 25 passes through threaded connection, couple 4 with the lamp pole 14 passes through screwed connection, the fixed orifices 25 with fixing bolt 2 combines together and can be with the device fast fixed, couple 4 can be convenient for hang the warning and give up the strip when the runway overhauls.
A method for using an aircraft landing indicating device comprises the following steps: the device is quickly fixed on bases which are prepared on two sides of a runway through the fixing bolts 2 and the fixing holes 25, then a power line is connected with the lamp holder 21 to supply power for the device, meanwhile, the wire clamp 24 can fix the power line in the wire slot 23, at the moment, the indicator lamp 12 is lightened to guide an aircraft, in the indicating process of the device, when the radar 8 detects the aircraft, a detection signal is transmitted to the controller 20, the controller 20 enables the signal transmitter 19 to work, the sent signal is transmitted to an instrument panel of the aircraft, at the moment, the signal transmitter 19 can be used as a positioning reference point, a driver can better operate the aircraft according to the position of the reference point to accurately land in the middle of the runway, and meanwhile, the laser range finder 18 can detect the distance from the aircraft to the device in real time, when the distance is closer, the signal is transmitted to the controller 20, the controller 20 controls the brightness of the indicator light 12, the stimulation to the eyes of the driver due to the strong brightness of the indicator light 12 is prevented, meanwhile, glare is avoided, the safe landing of the aircraft is ensured, when the aircraft lands on a runway, the reflective sticker 3 can guide the sliding of the aircraft, in the working process of the device, the heat generated by the device is quickly discharged out of the device through the heat dissipation holes 16 by the heat dissipation fan 17, meanwhile, the dust screen 22 can prevent external dust from entering the device, the photosensitive sensor 7 can detect whether the indicator light 12 works or not in real time, when the indicator light 12 does not work, the detection signal is transmitted to the controller 20, the controller 20 controls the maintenance light 6 to light up, when a worker maintains, but the rapid determination which pilot lamp 12 needs to be changed, improves maintenance efficiency, and will access door 5 is opened, and the staff of can being convenient for overhauls, in addition, mosquito repellant 10 can be driven the mosquito, stiffener 15 is right lamp pole 14 is consolidated, couple 4 can be convenient for hang the police and give up the strip when the runway overhauls.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (10)
1. An aircraft landing indication device, characterized by: the lamp comprises a base (1), a lamp post (14), a lamp holder (21) and an indicator light (12), wherein the lamp post (14) is arranged in the middle of the upper end of the base (1), the lamp holder (21) is arranged in the lamp post (14), the indicator light (12) is arranged on the lamp holder (21), a lamp shade (11) is arranged on one side of the indicator light (12), a photosensitive sensor (7) is arranged above the lamp shade (11), an overhaul lamp (6) is arranged on one side of the lamp shade (11), radiating holes (16) are formed in two side walls of the lamp post (14), a dust screen (22) is arranged in each radiating hole (16), a radiating fan (17) is arranged on one side of the indicator light (12), a controller (20) is arranged on the other side of the indicator light (12), a radar (8) is arranged on the upper end of the lamp post (14), and, the anti-mosquito lamp is characterized in that a signal transmitter (19) is arranged on one side of the radar (8), a laser range finder (18) is arranged on the other side of the radar (8), a wire slot (23) is formed in the lower portion of the lamp holder (21), a wire clamp (24) is arranged on the wire slot (23), an access door (5) is arranged on the lower portion of the lamp shade (11), the access door (5) is connected with the lamp pole (14) through a hinge (26), a pull handle (13) is arranged on one side wall of the access door (5), a reflective sticker (3) is arranged below the access door (5), a connecting seat (9) is arranged at the upper end of one side wall of the lamp pole (14), a mosquito dispeller (10) is arranged on the connecting seat (9), a reinforcing rod (15) is arranged between the lamp pole (14) and the base (1), a fixing hole (25) is formed in the base (1), a fixing bolt, and a hook (4) is arranged on the other side wall of the lamp post (14).
2. An aircraft landing indication device according to claim 1, wherein: the lamp post (14) is welded with the lamp holder (21), the lamp holder (21) is connected with the lamp post (14) through screws, the indicator lamp (12) is connected with the lamp holder (21) through threads, and the lampshade (11) is connected with the lamp post (14) through a clamping groove.
3. An aircraft landing indication device according to claim 1, wherein: the photosensitive sensor (7) is connected with the lamp pole (14) through a clamping groove, and the maintenance lamp (6) is connected with the lamp pole (14) through the clamping groove.
4. An aircraft landing indication device according to claim 1, wherein: louvre (16) shaping in on lamp pole (14), dust screen (22) with louvre (16) pass through the draw-in groove and connect, heat dissipation fan (17) with lamp stand (21) pass through the screw connection, controller (20) with lamp stand (21) pass through the screw connection.
5. An aircraft landing indication device according to claim 1, wherein: the radar (8) is connected with the lamp pole (14) through a clamping groove, and the signal transmitter (19) is connected with the lamp pole (14) through the clamping groove.
6. An aircraft landing indication device according to claim 1, wherein: the laser range finder (18) with the lamp pole (14) passes through the draw-in groove and is connected, wire casing (23) with lamp pole (14) pass through the screw connection, fastener (24) with wire casing (23) pass through the buckle and are connected.
7. An aircraft landing indication device according to claim 1, wherein: the access door (5) is rotationally connected with the lamp post (14), and the pull handle (13) is connected with the access door (5) through a screw.
8. An aircraft landing indication device according to claim 1, wherein: the light reflecting sticker (3) is adhered to the lamp pole (14), the connecting seat (9) is connected with the lamp pole (14) through screws, and the mosquito dispeller (10) is connected with the connecting seat (9) through screws.
9. An aircraft landing indication device according to claim 1, wherein: the lamp post is characterized in that the reinforcing rod (15) is welded with the lamp post (14) and the base (1), the fixing hole (25) is formed in the base (1), the fixing bolt (2) is in threaded connection with the fixing hole (25), and the hook (4) is in threaded connection with the lamp post (14).
10. A method of using an aircraft landing indication device, for use in an aircraft landing indication device as claimed in any one of claims 1 to 9, wherein: the device is quickly fixed on bases which are prepared on two sides of a runway through the fixing bolts (2) and the fixing holes (25), then a power line is connected with the lamp holder (21) to supply power for the device, meanwhile, the wire clamp (24) can fix the power line in the wire groove (23), the indicator lamp (12) is lightened to guide an aircraft, in the indicating process of the device, when the radar (8) detects the aircraft, a detection signal is transmitted to the controller (20), the controller (20) enables the signal transmitter (19) to work, the transmitted signal can be transmitted to an instrument panel of the aircraft, at the moment, the signal transmitter (19) can be used as a positioning reference point, a driver can better operate the aircraft according to the position of the reference point to accurately land the aircraft in the middle of the runway, meanwhile, the laser range finder (18) can detect the distance from the aircraft to the device in real time, when the distance is closer and closer, signals are transmitted to the controller (20), the controller (20) controls the brightness of the indicator light (12), the situation that the eyes of a driver are irritated due to the fact that the brightness of the indicator light (12) is stronger is prevented, glare is avoided, the aircraft is guaranteed to land safely, when the aircraft lands on a runway, the light reflecting sticker (3) can guide the aircraft to slide is avoided, in the working process of the device, the heat generated by the device is quickly discharged out of the device through the heat dissipation holes (16) by the heat dissipation fan (17), meanwhile, the dust screen (22) can prevent external dust from entering the device, the photosensitive sensor (7) can detect whether the indicator light (12) works in real time, and when the indicator light (12) does not work, just will detect signal transmission arrives in controller (20), controller (20) control maintenance lamp (6) light, when the staff overhauls, but quick determination which pilot lamp (12) need be changed, improve maintenance efficiency, and will access door (5) are opened, the staff's of can being convenient for overhaul, in addition, mosquito repellant (10) can be driven the mosquito, stiffener (15) are right lamp pole (14) are consolidated, couple (4) can be convenient for hang the police and give up the strip when the runway overhauls.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011439226.3A CN112591130A (en) | 2020-12-07 | 2020-12-07 | Aircraft landing indicating device and using method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011439226.3A CN112591130A (en) | 2020-12-07 | 2020-12-07 | Aircraft landing indicating device and using method thereof |
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| CN112591130A true CN112591130A (en) | 2021-04-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011439226.3A Pending CN112591130A (en) | 2020-12-07 | 2020-12-07 | Aircraft landing indicating device and using method thereof |
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| EP0220752A2 (en) * | 1985-09-20 | 1987-05-06 | D.R.I.M. Limited | Ground control method at an aerodrome for vehicles, and arrangement for carrying out this method |
| CN206723982U (en) * | 2017-05-09 | 2017-12-08 | 中山市思科瑞迪安全设备有限公司 | One kind take off landing indicator lamp |
| CN206861424U (en) * | 2017-06-07 | 2018-01-09 | 郭群群 | A kind of night unmanned plane aid projector |
| CN108662545A (en) * | 2018-05-16 | 2018-10-16 | 长春众鼎科技有限公司 | Automobile brake lamp brightness control system and its control method |
| CN208544437U (en) * | 2018-04-25 | 2019-02-26 | 重庆万明扬建设工程有限公司 | A kind of novel airport is into low beam light directing system |
| CN109404819A (en) * | 2018-12-11 | 2019-03-01 | 汪传佳 | A kind of easy road lamp device for solving failure |
| CN209795851U (en) * | 2019-04-28 | 2019-12-17 | 昆山蒲公英智能科技有限公司 | Auxiliary landing lighting device for unmanned aerial vehicle |
| CN210027949U (en) * | 2018-03-22 | 2020-02-07 | 北京京东尚科信息技术有限公司 | Aircraft landing indicating device and aircraft |
| CN111746816A (en) * | 2020-05-18 | 2020-10-09 | 陈穗 | Airplane landing auxiliary device and landing method |
-
2020
- 2020-12-07 CN CN202011439226.3A patent/CN112591130A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1092821A (en) * | 1965-02-02 | 1967-11-29 | Richard Thomas Cella | Instrument landing system |
| EP0220752A2 (en) * | 1985-09-20 | 1987-05-06 | D.R.I.M. Limited | Ground control method at an aerodrome for vehicles, and arrangement for carrying out this method |
| CN206723982U (en) * | 2017-05-09 | 2017-12-08 | 中山市思科瑞迪安全设备有限公司 | One kind take off landing indicator lamp |
| CN206861424U (en) * | 2017-06-07 | 2018-01-09 | 郭群群 | A kind of night unmanned plane aid projector |
| CN210027949U (en) * | 2018-03-22 | 2020-02-07 | 北京京东尚科信息技术有限公司 | Aircraft landing indicating device and aircraft |
| CN208544437U (en) * | 2018-04-25 | 2019-02-26 | 重庆万明扬建设工程有限公司 | A kind of novel airport is into low beam light directing system |
| CN108662545A (en) * | 2018-05-16 | 2018-10-16 | 长春众鼎科技有限公司 | Automobile brake lamp brightness control system and its control method |
| CN109404819A (en) * | 2018-12-11 | 2019-03-01 | 汪传佳 | A kind of easy road lamp device for solving failure |
| CN209795851U (en) * | 2019-04-28 | 2019-12-17 | 昆山蒲公英智能科技有限公司 | Auxiliary landing lighting device for unmanned aerial vehicle |
| CN111746816A (en) * | 2020-05-18 | 2020-10-09 | 陈穗 | Airplane landing auxiliary device and landing method |
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Application publication date: 20210402 |
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