CN109649674B - System and method for automatically recording time of loading and unloading wheel chock - Google Patents
System and method for automatically recording time of loading and unloading wheel chock Download PDFInfo
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- CN109649674B CN109649674B CN201811543844.5A CN201811543844A CN109649674B CN 109649674 B CN109649674 B CN 109649674B CN 201811543844 A CN201811543844 A CN 201811543844A CN 109649674 B CN109649674 B CN 109649674B
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- 238000000034 method Methods 0.000 title claims abstract description 13
- 238000004891 communication Methods 0.000 claims description 18
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- 238000005516 engineering process Methods 0.000 description 5
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- 230000000694 effects Effects 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
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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
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
- B64F1/16—Pickets or ground anchors; Wheel chocks
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- Engineering & Computer Science (AREA)
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- Aviation & Aerospace Engineering (AREA)
- Time Recorders, Dirve Recorders, Access Control (AREA)
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Abstract
The invention discloses a system for automatically recording the time of loading and unloading a wheel gear, which comprises a wheel position label arranged on the ground of an airport and positioned at the position of an airplane tire in a parking place, an airplane electronic wheel gear used for triggering when a wheel gear pull rope is straightened and stressed, identifying the wheel position label, reporting the reported information containing the triggering time and a radio frequency identification result, and a server used for receiving the reported information of the airplane electronic wheel gear, generating the time of loading and unloading the wheel gear according to the triggering time and the radio frequency identification result and recording the time of loading and unloading the wheel gear. The invention also discloses a method for automatically recording the time of loading and unloading the wheel gear based on the system for automatically recording the time of loading and unloading the wheel gear.
Description
Technical Field
The invention relates to a system and a method for automatically recording the time of loading and unloading a wheel chock, belonging to the technical field of aviation information.
Background
According to the regulation in the 88 th order issued by the general office of civil aviation as early as 2013, namely the 'civil aviation flight normal statistical approach', the time for the airplane to get on and off the wheel gear needs to be accurately recorded when the flight normality is checked. The key time node is always recorded manually, and the data has the problems of low timeliness, low accuracy, high loss rate and the like due to the fact that manual operation is inevitably influenced by factors of operation proficiency, detail habits, operation negligence and the like of different operators. Therefore, a technical scheme combining the modern internet of things technology is needed to be provided so as to realize the automatic recording of the time of the upper wheel chock and the lower wheel chock of the airplane, and therefore the three important problems of timeliness, accuracy and loss rate of the time recording of the upper wheel chock and the lower wheel chock of the airplane are solved.
Disclosure of Invention
The invention provides a system and a method for automatically recording the time of loading and unloading a wheel chock aiming at the defects of the prior art, and aims to solve the three important problems of timeliness, accuracy and deficiency rate of the time recording of the loading and unloading of the wheel chock of an airplane.
In order to solve the problems, the technical scheme adopted by the invention is as follows:
a system for automatically recording wheel chock getting on and off times, comprising:
a wheel position tag which is arranged on the ground of the airport and is positioned at the position of a tire of the airplane in the parking space,
an airplane electronic wheel block which is used for triggering when a wheel block pull rope is straightened and stressed, identifying the position label of an airplane wheel and reporting the reporting information containing the triggering time and the radio frequency identification result,
and the server is used for receiving the reported information of the electronic wheel gear of the airplane, generating the time for getting on and off the wheel gear according to the triggering time and the radio frequency identification result and recording the time for getting on and off the wheel gear.
As an improvement of the above technical solution, the electronic wheel chock for an aircraft includes:
a trigger switch used for sensing whether the wheel block pull rope of the electronic wheel block of the airplane is straightened and stressed,
a micro control unit for receiving the signal sent by the trigger switch,
a tag identification module for identifying a wheel position tag located on the airport ground, and the tag identification module is controlled by the micro control unit,
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module,
and the reporting communication module is used for reporting the reporting information.
The signal identification scheme between the wheel position tag and the tag identification module may be an RFID tag identification technology, an NFC tag identification technology, a bluetooth tag identification technology, a tag identification technology based on a 433m wireless module, and the like.
As an improvement of the above technical solution, the reporting communication module is a communication device based on a narrowband internet of things.
As an improvement of the above technical solution, the electronic wheel chock of the aircraft further includes a first power supply circuit for supplying power to the tag identification module, and a second power supply circuit for supplying power to the micro control unit and the reporting communication module.
As an improvement of the above technical solution, the electronic wheel chock of the aircraft further includes a storage battery module for supplying power to the first power supply circuit and the second power supply circuit, and a charging circuit connected to the storage battery module.
The invention also provides a method for automatically recording the time of loading and unloading the wheel chock, which comprises the following steps:
s1: set up the wheel position label at airport subaerial and lie in parking stall aircraft tire position department, adopt aircraft electron wheel fender, just aircraft electron wheel fender includes:
a trigger switch used for sensing whether the wheel block pull rope of the electronic wheel block of the airplane is straightened and stressed,
a micro control unit for receiving the signal sent by the trigger switch,
a tag identification module for identifying a wheel position tag located on the airport ground, and the tag identification module is controlled by the micro control unit,
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module,
a reporting communication module for reporting the reporting information;
s2: when the wheel chock pull rope is straightened and stressed to lift the airplane electronic wheel chock, the trigger switch is triggered, and the trigger switch sends a signal to the micro control unit;
s3: after receiving the signal sent by the trigger switch, the micro control unit records the time for receiving the signal and controls the label identification module to identify the position label of the airplane wheel;
s4: the micro control unit generates reporting information containing the trigger time of the trigger switch and the identification result of the label identification module;
s5: the micro control unit controls the reporting communication module to report the reporting information to a server;
s6: and the server generates the time of the upper wheel block and the lower wheel block according to the trigger time of the trigger switch and the identification result of the label identification module, and records the generated time of the upper wheel block and the lower wheel block.
Compared with the prior art, the invention has the following implementation effects:
the system and the method for automatically recording the time of the upper wheel chock and the lower wheel chock of the airplane can automatically report and record the time of the upper wheel chock and the lower wheel chock of the airplane, thereby overcoming the adverse effects of the manual recording of the time of the upper wheel chock and the lower wheel chock of the airplane caused by the factors of the operation proficiency, the detail habits, the operation negligence and the like of different operators, and solving the three important problems of timeliness, accuracy and missing rate of the time recording of the upper wheel chock and the lower wheel chock of the airplane.
Drawings
Fig. 1 is a schematic structural principle diagram of an electronic wheel chock of an aircraft according to the present invention.
Detailed Description
The present invention will be described with reference to specific examples.
Fig. 1 is a schematic structural diagram of an electronic wheel chock of an aircraft according to this embodiment.
The system for automatically recording the time of getting on and off the wheel chock provided by the embodiment comprises:
a wheel position tag which is arranged on the ground of the airport and is positioned at the position of a tire of the airplane in the parking space,
an airplane electronic wheel block which is used for triggering when a wheel block pull rope is straightened and stressed, identifying the position label of an airplane wheel and reporting the reporting information containing the triggering time and the radio frequency identification result,
and the server is used for receiving the reported information of the electronic wheel gear of the airplane, generating the time for getting on and off the wheel gear according to the triggering time and the radio frequency identification result and recording the time for getting on and off the wheel gear.
Specifically, the aircraft electronic wheel chock includes:
the trigger switch is used for sensing whether a wheel chock pull rope of an electronic wheel chock of an airplane is straightened and stressed; the trigger switch is not difficult to understand for the person skilled in the art and many embodiments can easily be imagined, for example: the trigger switch is arranged at the joint of the wheel chock pull rope and the wheel chock body, and the pulling force of the wheel chock pull rope on the wheel chock body is sensed; or the trigger switch is used as a connecting buckle of the wheel block pull rope to directly sense the pulling force borne by the wheel block pull rope;
the micro control unit is used for receiving a signal sent by the trigger switch;
a tag identification module for identifying a tag of a wheel position located on the ground of an airport, and the tag identification module is controlled by the micro control unit;
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module;
a reporting communication module for reporting the reporting information; specifically, the reporting communication module is a communication device based on a narrowband internet of things;
the tag identification module is used for receiving the tag identification information sent by the tag identification module and reporting the tag identification information to the reporting communication module;
the charging circuit is used for charging the power supply circuit I and the power supply circuit II; preferably, the battery module may be a lithium titanate battery.
The working method of the above system for automatically recording the time of loading and unloading the wheel chock can refer to the following method for automatically recording the time of loading and unloading the wheel chock, which includes the following steps:
s1: set up the wheel position label at airport subaerial and lie in parking stall aircraft tire position department, adopt aircraft electron wheel fender, just aircraft electron wheel fender includes:
a trigger switch used for sensing whether the wheel block pull rope of the electronic wheel block of the airplane is straightened and stressed,
a micro control unit for receiving the signal sent by the trigger switch,
a tag identification module for identifying a wheel position tag located on the airport ground, and the tag identification module is controlled by the micro control unit,
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module,
and the reporting communication module is used for reporting the reporting information.
S2: when the wheel chock pull rope is straightened and stressed to lift the airplane electronic wheel chock, the trigger switch is triggered, and the trigger switch sends a signal to the micro control unit;
specifically, when the wheel chock pull rope is pulled straight and stressed to lift the electronic wheel chock of the airplane, the trigger switch sends a first signal to the micro control unit; when the electronic wheel chock of the airplane is put down to enable the stress state of the wheel chock pull rope to disappear, the trigger switch sends a second signal to the micro control unit.
S3: after receiving the signal sent by the trigger switch, the micro control unit records the time for receiving the signal and controls the label identification module to identify the position label of the airplane wheel;
specifically, the micro control unit records a first trigger time and a second trigger time corresponding to the first signal and the second signal, and performs first wheel position label identification and second wheel position label identification corresponding to the first signal and the second signal.
S4: the micro control unit generates reporting information containing the trigger time of the trigger switch and the identification result of the label identification module;
specifically, the micro control unit generates first reporting information corresponding to the first trigger time and the first wheel position tag identification result, and generates second reporting information corresponding to the second trigger time and the second wheel position tag identification result.
S5: and the micro control unit controls the reporting communication module to report the reporting information to a server.
S6: the server generates upper and lower wheel gear time according to the trigger time of the trigger switch and the identification result of the tag identification module, and records the generated upper and lower wheel gear time; specifically, the method comprises the following steps:
when the tag identification module does not identify the airplane wheel position tag in the first reported information, and when the tag identification module does not identify the airplane wheel position tag in the second reported information, the time for getting on and off the wheel gear is not generated; at this time, the electronic wheel chock of the airplane is only transported between different storage positions or transportation tools and is not put into use.
When the tag identification module does not identify the airplane wheel position tag in the first reported information, and when the tag identification module identifies the airplane wheel position tag A in the second reported information, generating the gear-in time corresponding to the airplane wheel position tag A; at the moment, the airplane electronic wheel chock is transported to the tire of the airplane from a storage position or a transportation tool to be used.
When the information is reported for the first time, the tag identification module identifies the airplane wheel position tag A, and when the information is reported for the second time, the tag identification module does not identify the airplane wheel position tag, and the wheel gear descending time corresponding to the airplane wheel position tag A is generated; in this case, the electronic wheel chock is transported from the tire of the airplane to a storage location or a transportation tool after use.
When the information is reported for the first time, the tag identification module identifies a wheel position tag A, and when the information is reported for the second time, the tag identification module identifies a wheel position tag B, and then the lower wheel-shift time corresponding to the wheel position tag A and the upper wheel-shift time corresponding to the wheel position tag B are generated; at this time, the airplane electronic wheel chock is carried from one airplane tire to another airplane tire.
The foregoing is a detailed description of the invention with reference to specific embodiments, and the practice of the invention is not to be construed as limited thereto. For those skilled in the art to which the invention pertains, several simple deductions or substitutions can be made without departing from the spirit of the invention, and all shall be considered as belonging to the protection scope of the invention.
Claims (8)
1. The utility model provides a system for automatic record upper and lower wheel chock time, characterized by includes:
a wheel position tag which is arranged on the ground of the airport and is positioned at the position of a tire of the airplane in the parking space,
an airplane electronic wheel block which is used for triggering when a wheel block pull rope is straightened and stressed, identifying the position label of an airplane wheel and reporting the reporting information containing the triggering time and the radio frequency identification result,
and the server is used for receiving the reported information of the electronic wheel gear of the airplane, generating the time for getting on and off the wheel gear according to the triggering time and the radio frequency identification result and recording the time for getting on and off the wheel gear.
2. The system for automatically recording the time for loading and unloading a wheel chock of claim 1, wherein the electronic wheel chock of the airplane comprises:
a trigger switch used for sensing whether the wheel block pull rope of the electronic wheel block of the airplane is straightened and stressed,
a micro control unit for receiving the signal sent by the trigger switch,
a tag identification module for identifying a wheel position tag located on the airport ground, and the tag identification module is controlled by the micro control unit,
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module,
and the reporting communication module is used for reporting the reporting information.
3. The system for automatically recording the time for getting on and off the wheel chock as claimed in claim 2, wherein the reporting communication module is a communication device based on a narrow-band internet of things.
4. The system for automatically recording the time for loading and unloading the wheel chock as claimed in claim 2, wherein the electronic wheel chock of the airplane further comprises a first power supply circuit for supplying power to the tag identification module and a second power supply circuit for supplying power to the micro control unit and the reporting communication module.
5. The system for automatically recording the time for loading and unloading the wheel chock of claim 4, wherein the electronic wheel chock of the airplane further comprises a storage battery module for supplying power to the first power supply circuit and the second power supply circuit, and a charging circuit connected with the storage battery module.
6. A method for automatically recording the time of loading and unloading a wheel chock is characterized by comprising the following steps:
s1: set up the wheel position label at airport subaerial and lie in parking stall aircraft tire position department, adopt aircraft electron wheel fender, just aircraft electron wheel fender includes:
a trigger switch used for sensing whether the wheel block pull rope of the electronic wheel block of the airplane is straightened and stressed,
a micro control unit for receiving the signal sent by the trigger switch,
a tag identification module for identifying a wheel position tag located on the airport ground, and the tag identification module is controlled by the micro control unit,
the micro control unit is also used for generating reporting information containing the trigger time of the trigger switch and the identification result of the label identification module,
a reporting communication module for reporting the reporting information;
s2: when the wheel chock pull rope is straightened and stressed to lift the airplane electronic wheel chock, the trigger switch is triggered, and the trigger switch sends a signal to the micro control unit;
s3: after receiving the signal sent by the trigger switch, the micro control unit records the time for receiving the signal and controls the label identification module to identify the position label of the airplane wheel;
s4: the micro control unit generates reporting information containing the trigger time of the trigger switch and the identification result of the label identification module;
s5: the micro control unit controls the reporting communication module to report the reporting information to a server;
s6: and the server generates the time of the upper wheel block and the lower wheel block according to the trigger time of the trigger switch and the identification result of the label identification module, and records the generated time of the upper wheel block and the lower wheel block.
7. The method as claimed in claim 6, wherein in step S2, when the pull rope of the wheel chock is pulled straight to lift the electronic wheel chock of the airplane, the trigger switch sends a first signal to the micro control unit; when the electronic wheel chock of the airplane is put down to enable the stress state of the wheel chock pull rope to disappear, the trigger switch sends a second signal to the micro control unit;
in step S3, the micro control unit records a first trigger time and a second trigger time corresponding to the first signal and the second signal, and performs first wheel position tag identification and second wheel position tag identification corresponding to the first signal and the second signal;
in step S4, the mcu generates first reporting information corresponding to the first trigger time and the first wheel position tag identification result, and generates second reporting information corresponding to the second trigger time and the second wheel position tag identification result.
8. The method for automatically recording the time for getting on and off the wheel chock of claim 7, wherein in step S6:
when the tag identification module does not identify the airplane wheel position tag in the first reported information, and when the tag identification module does not identify the airplane wheel position tag in the second reported information, the time for getting on and off the wheel gear is not generated;
when the tag identification module does not identify the airplane wheel position tag in the first reported information, and when the tag identification module identifies the airplane wheel position tag A in the second reported information, generating the gear-in time corresponding to the airplane wheel position tag A;
when the information is reported for the first time, the tag identification module identifies the airplane wheel position tag A, and when the information is reported for the second time, the tag identification module does not identify the airplane wheel position tag, and the wheel gear descending time corresponding to the airplane wheel position tag A is generated;
when the information is reported for the first time, the tag identification module identifies the wheel position tag A, and when the information is reported for the second time, the tag identification module identifies the wheel position tag B, and then the wheel-down time corresponding to the wheel position tag A and the wheel-up time corresponding to the wheel position tag B are generated.
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| CN201811543844.5A CN109649674B (en) | 2018-12-17 | 2018-12-17 | System and method for automatically recording time of loading and unloading wheel chock |
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| CN201811543844.5A CN109649674B (en) | 2018-12-17 | 2018-12-17 | System and method for automatically recording time of loading and unloading wheel chock |
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Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110015441B (en) * | 2019-05-15 | 2024-06-04 | 成都耀塔科技有限公司 | Method for monitoring and reporting electronic wheel guard state of parking apron |
| WO2020227948A1 (en) * | 2019-05-15 | 2020-11-19 | 成都耀塔科技有限公司 | Method for monitoring and reporting state of electronic chock of parking apron |
| CN110097659A (en) * | 2019-05-16 | 2019-08-06 | 深圳市捷赛机电有限公司 | Catch, the time recording method for removing catch and Related product on a kind of aircraft |
| CN111696391A (en) * | 2020-06-10 | 2020-09-22 | 刘易聪 | Method and system for automatically identifying wheel gear operation through wheel gear state in area |
| CN111806715A (en) * | 2020-08-25 | 2020-10-23 | 青岛民航凯亚系统集成有限公司 | Wheel chock system based on sensor and RFID technology and wheel chock data generation method |
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