CN212637960U - Aircraft guiding device under runway pollution condition - Google Patents
Aircraft guiding device under runway pollution condition Download PDFInfo
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- CN212637960U CN212637960U CN202022066194.9U CN202022066194U CN212637960U CN 212637960 U CN212637960 U CN 212637960U CN 202022066194 U CN202022066194 U CN 202022066194U CN 212637960 U CN212637960 U CN 212637960U
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Abstract
The utility model relates to the technical field of airplane berthing, and discloses an airplane guide device under the condition of runway pollution, which comprises an inspection unit and an information input terminal, the output end of the checking unit is respectively connected with the receiving end of the fault analysis unit and the receiving end of the information transmission unit through signals, the output end of the information transmission unit is in signal connection with the receiving end of the central processing unit, the output end of the central processing unit is in signal connection with the receiving end of the fault evaluation unit, the airplane guiding device under the condition of runway pollution comprises a temperature acquisition unit, a wind direction acquisition unit, an air pressure acquisition unit and a visibility acquisition unit through the interior of a weather information acquisition unit, the interior of the runway information acquisition unit comprises a roughness acquisition unit, a surface temperature acquisition unit and a surface dry and wet acquisition unit, the effectiveness of the weather information and the road surface condition information on the takeoff and landing of the airplane is increased through the weather information and the road surface condition information.
Description
Technical Field
The utility model relates to an aircraft berth technical field specifically is an aircraft guiding device under runway pollution condition.
Background
In the taking-off and landing process of the airplane, the runway can cause great threat to the safety of the flight under the condition of being polluted, the airframe is damaged if the potential hazard is light, the air crash is caused if the potential hazard is heavy, and the airplane is damaged and the people are killed, so that in order to ensure the safety of the flight, pollutants on the runway must be timely found and identified, corresponding treatment is carried out according to the threat level, and the pollutant of the airplane taking off and landing by using the runway is checked to ensure the safety performance of the airplane.
Through retrieval, Chinese patent No. CN103675939B discloses a runway pavement monitoring device and method based on point cloud detection, wherein a laser scanning device continuously emits detection laser to a monitoring area, a three-dimensional point cloud image of the surface of a runway is generated at a fixed period T, the scanning data of the laser scanning device is uploaded to a processor in real time, a monitoring algorithm is operated on the point cloud image data to monitor whether an invasive foreign object exists, if the suspected invasive foreign object is monitored, the analysis and the processing of the data are completed in the processor, according to the suspected invasive foreign object coordinate obtained by the monitoring algorithm, the processor selects a nearest camera to point to the object position, and shoots an image/video signal for manual confirmation, and if the suspected alarm is not cleared; if the foreign matter is confirmed manually, the operation of manually removing the invasive foreign matter is executed, and the alarm is eliminated after the foreign matter is removed.
However, the runway of the airplane is not checked in detail, and various index information on the runway is also monitored, which easily causes great safety hazards to other aircrafts.
SUMMERY OF THE UTILITY MODEL
Technical scheme
Report to the runway pollutant that can be quick for realizing the aforesaid, can also gather various important information fast, ensure the safety purpose of other airplanes, the utility model provides a following technical scheme: an aircraft guiding device under the condition of runway pollution comprises an inspection unit and an information input terminal, wherein the output end of the inspection unit is respectively in signal connection with the receiving end of a fault analysis unit and the receiving end of an information transmission unit, the output end of the information transmission unit is in signal connection with the receiving end of a central processing unit, the output end of the central processing unit is in signal connection with the receiving end of a fault evaluation unit, the output end of the fault evaluation unit is respectively in signal connection with the receiving end of a weather information acquisition unit and the receiving end of a runway information acquisition unit, the output end of the weather information acquisition unit is in signal connection with the receiving end of an information sending unit, the output end of the information sending unit is in signal connection with the receiving end of an information receiving unit, the output end of the information receiving unit is in signal connection with the receiving end of an information comparison unit, and the output end of the, the output end of the information checking unit is respectively in signal connection with the receiving end of the emergency processing unit and the receiving end of the information confirming unit.
Furthermore, the output end of the central processing unit is also in signal connection with the receiving end of the information display unit.
Furthermore, the output end of the runway information acquisition unit is also in signal connection with the receiving end of the information sending unit.
Furthermore, the interior of the inspection unit comprises a retraction unit, a brake unit and a wheel unit.
Further, the inside of weather information acquisition unit includes temperature acquisition unit, humidity acquisition unit, wind direction acquisition unit, atmospheric pressure acquisition unit and visibility acquisition unit.
Furthermore, the runway information acquisition unit comprises a roughness acquisition unit, a surface temperature acquisition unit and a surface dry and wet acquisition unit.
Further, the output end of the information input terminal is in signal connection with the receiving end of the information receiving unit.
Advantageous effects
Compared with the prior art, the utility model provides an aircraft guiding device under runway pollution condition possesses following beneficial effect:
1. the aircraft guiding device under the condition of runway pollution inspects the landing gear system of the aircraft in detail through the retraction unit, the brake unit and the wheel unit in the inspection unit, so that the components of the aircraft are prevented from being damaged, and the use safety of the aircraft is improved.
2. This aircraft guiding device under runway pollution condition, the inside through weather information acquisition unit includes temperature acquisition unit, humidity acquisition unit, wind direction acquisition unit, atmospheric pressure acquisition unit and visibility acquisition unit, and the inside of runway information acquisition unit includes roughness acquisition unit, surface temperature acquisition unit and the wet acquisition unit of surface futilely, increases the validity of weather information and road surface condition information to the takeoff and landing of aircraft through these.
Drawings
FIG. 1 is a system diagram of the present invention;
FIG. 2 is a diagram of the inspection unit of the present invention;
FIG. 3 is a diagram of a weather information collecting unit of the present invention;
fig. 4 is the runway information collection unit diagram of the present invention.
In the figure: 1-checking unit, 2-information input terminal, 3-fault analysis unit, 4-information transmission unit, 5-central processing unit, 6-information display unit, 7-fault evaluation unit, 8-weather information acquisition unit, 9-runway information acquisition unit, 10-information sending unit, 11-information receiving unit, 12-information comparison unit, 13-information checking unit, 14-emergency processing unit, 15-information confirmation unit, 16-retraction unit, 17-brake unit, 18-airplane wheel unit, 19-temperature acquisition unit, 20-humidity acquisition unit, 21-wind direction acquisition unit, 22-air pressure acquisition unit, 23-visibility acquisition unit, 24-roughness acquisition unit, 24-weather information analysis unit, 9-runway information acquisition unit, 10-information sending unit, 11-information receiving unit, 12-information comparison unit, 13-information checking unit, 14-emergency processing unit, 15-information, 25-surface temperature acquisition unit, 26-surface dry and wet acquisition unit.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, an airplane guiding device under runway pollution condition includes an inspection unit 1 and an information input terminal 2, an output end of the inspection unit 1 is respectively in signal connection with a receiving end of a fault analysis unit 3 and a receiving end of an information transmission unit 4, an output end of the information transmission unit 4 is in signal connection with a receiving end of a central processing unit 5, an output end of the central processing unit 5 is in signal connection with a receiving end of a fault evaluation unit 7, an output end of the fault evaluation unit 7 is respectively in signal connection with a receiving end of a weather information collection unit 8 and a receiving end of a runway information collection unit 9, an output end of the weather information collection unit 8 is in signal connection with a receiving end of an information sending unit 10, an output end of the information sending unit 10 is in signal connection with a receiving end of an information receiving unit 11, an output end of the information receiving unit 11 is, the output end of the information comparing unit 12 is signal-connected to the receiving end of the information collating unit 13, and the output end of the information collating unit 13 is signal-connected to the receiving end of the emergency processing unit 14 and the receiving end of the information confirming unit 15, respectively.
The output end of the central processing unit 5 is also in signal connection with the receiving end of the information display unit 6, so that the fault information of the fault aircraft can be rapidly displayed, and a faster and better solution is required.
Wherein, the output end of the runway information acquisition unit 9 is also in signal connection with the receiving end of the information sending unit 10.
The inspection unit 1 comprises a retractable unit 16, a brake unit 17 and a wheel unit 18, wherein the retractable unit 16, the brake unit 17 and the wheel unit 18 are all parts with the highest fault level in the aircraft landing gear system.
Wherein, the inside of weather information acquisition unit 8 includes temperature acquisition unit 19, humidity acquisition unit 20, wind direction acquisition unit 21, atmospheric pressure acquisition unit 22 and visibility acquisition unit 23, can learn the weather condition near runway fast, conveniently makes accurate effectual instruction to the aircraft.
The runway information acquisition unit 9 includes a roughness acquisition unit 24, a surface temperature acquisition unit 25 and a surface dry and wet acquisition unit 26, so that conditions on the runway can be quickly known, and accurate and effective instructions can be conveniently made for the airplane.
The output end of the information input terminal 2 is in signal connection with the receiving end of the information receiving unit 11, so that the airport can be conveniently and accurately and effectively communicated with the airplane to be landed, and the safety of the airplane to be landed is ensured.
The utility model discloses a theory of operation and use flow: when pollutants are found on the runway, a crew firstly carries out detailed inspection on a receiving and releasing unit 16, a braking unit 17 and a wheel unit 18 of a landing airplane, when a fault occurs in the inspected equipment, fault information is respectively transmitted to a fault analysis unit 3 and an information transmission unit 4, the information transmission unit 4 transmits the fault information and an analysis result to a central processing unit 5, the central processing unit 5 transmits the fault analysis result to a fault evaluation unit 7 to evaluate the fault, whether the normal take-off and landing of the airplane on the runway are influenced or not is judged, the environment around the pollutants on the runway is monitored through a weather information acquisition unit 8 and a runway information acquisition unit 9, the monitored information is transmitted to an airport unit system and the airplane ready to take-off and land, and the take-off and landing of the airplane are determined according to the information, but also activates the emergency processing unit 14 upon confirmation of the message to prevent an accident.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. An aircraft guiding device in case of runway contamination, comprising an inspection unit (1) and an information input terminal (2), characterized in that: the output end of the inspection unit (1) is respectively in signal connection with the receiving end of the fault analysis unit (3) and the receiving end of the information transmission unit (4), the output end of the information transmission unit (4) is in signal connection with the receiving end of the central processing unit (5), the output end of the central processing unit (5) is in signal connection with the receiving end of the fault evaluation unit (7), the output end of the fault evaluation unit (7) is respectively in signal connection with the receiving end of the weather information acquisition unit (8) and the receiving end of the runway information acquisition unit (9), the output end of the weather information acquisition unit (8) is in signal connection with the receiving end of the information sending unit (10), the output end of the information sending unit (10) is in signal connection with the receiving end of the information receiving unit (11), and the output end of the information receiving unit (11) is in signal connection with the receiving end of the information comparison unit (12), the output end of the information comparison unit (12) is in signal connection with the receiving end of the information checking unit (13), and the output end of the information checking unit (13) is in signal connection with the receiving end of the emergency processing unit (14) and the receiving end of the information confirmation unit (15) respectively.
2. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the output end of the central processing unit (5) is also in signal connection with the receiving end of the information display unit (6).
3. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the output end of the runway information acquisition unit (9) is also in signal connection with the receiving end of the information sending unit (10).
4. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the inspection unit (1) comprises a storage unit (16), a brake unit (17) and a wheel unit (18) inside.
5. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the inside of weather information acquisition unit (8) includes temperature acquisition unit (19), humidity acquisition unit (20), wind direction acquisition unit (21), atmospheric pressure acquisition unit (22) and visibility acquisition unit (23).
6. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the runway information acquisition unit (9) comprises a roughness acquisition unit (24), a surface temperature acquisition unit (25) and a surface dry and wet acquisition unit (26) inside.
7. An aircraft guidance device in the event of a contamination of a runway according to claim 1, characterised in that: the output end of the information input terminal (2) is in signal connection with the receiving end of the information receiving unit (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022066194.9U CN212637960U (en) | 2020-09-18 | 2020-09-18 | Aircraft guiding device under runway pollution condition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022066194.9U CN212637960U (en) | 2020-09-18 | 2020-09-18 | Aircraft guiding device under runway pollution condition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212637960U true CN212637960U (en) | 2021-03-02 |
Family
ID=74762305
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022066194.9U Expired - Fee Related CN212637960U (en) | 2020-09-18 | 2020-09-18 | Aircraft guiding device under runway pollution condition |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212637960U (en) |
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2020
- 2020-09-18 CN CN202022066194.9U patent/CN212637960U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder |
Address after: No. 1519, Moganshan Road, Liangzhu street, Yuhang District, Hangzhou City, Zhejiang Province, 310012 Patentee after: ZHEJIANG INSTITUTE OF COMMUNICATION Address before: No.42 Jiaogong Road, Hangzhou, Zhejiang Province Patentee before: ZHEJIANG INSTITUTE OF COMMUNICATION |
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| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: No. 1515, Moganshan Road, Liangzhu street, Yuhang District, Hangzhou City, Zhejiang Province, 310012 Patentee after: ZHEJIANG INSTITUTE OF COMMUNICATION Address before: No. 1519, Moganshan Road, Liangzhu street, Yuhang District, Hangzhou City, Zhejiang Province, 310012 Patentee before: ZHEJIANG INSTITUTE OF COMMUNICATION |
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| CP02 | Change in the address of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210302 Termination date: 20210918 |
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| CF01 | Termination of patent right due to non-payment of annual fee |