CN114030633A - Automatic acquisition method for airplane wheel chock loading and unloading time - Google Patents

Automatic acquisition method for airplane wheel chock loading and unloading time Download PDF

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Publication number
CN114030633A
CN114030633A CN202111503901.9A CN202111503901A CN114030633A CN 114030633 A CN114030633 A CN 114030633A CN 202111503901 A CN202111503901 A CN 202111503901A CN 114030633 A CN114030633 A CN 114030633A
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module
data
state
wheel chock
electronic
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张�浩
宣彤
郑洪峰
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Variflight Technology Co ltd
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Variflight Technology Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/12Ground or aircraft-carrier-deck installations for anchoring aircraft
    • B64F1/16Pickets or ground anchors; Wheel chocks
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F16/00Information retrieval; Database structures therefor; File system structures therefor
    • G06F16/20Information retrieval; Database structures therefor; File system structures therefor of structured data, e.g. relational data
    • G06F16/25Integrating or interfacing systems involving database management systems
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F18/00Pattern recognition
    • G06F18/20Analysing
    • G06F18/24Classification techniques
    • G06F18/241Classification techniques relating to the classification model, e.g. parametric or non-parametric approaches

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Data Mining & Analysis (AREA)
  • Physics & Mathematics (AREA)
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  • General Engineering & Computer Science (AREA)
  • Bioinformatics & Cheminformatics (AREA)
  • Evolutionary Computation (AREA)
  • Evolutionary Biology (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Bioinformatics & Computational Biology (AREA)
  • Artificial Intelligence (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Traffic Control Systems (AREA)

Abstract

The invention relates to parking apron data acquisition, in particular to an automatic acquisition method for the time of loading and unloading a wheel gear of an airplane.A first detection module in an electronic wheel gear is awakened when the electronic wheel gear moves, the first detection module is matched with a second detection module in a base station to carry out state detection on the electronic wheel gear, the base station uploads the detection data of the second detection module to a server, and the server judges the state of the electronic wheel gear based on the detection data through a state identification module and sends the obtained time of loading and unloading the wheel gear to other systems; the technical scheme provided by the invention can effectively overcome the defects of insufficient stability and reliability and lower accuracy of data acquisition in the prior art.

Description

Automatic acquisition method for airplane wheel chock loading and unloading time
Technical Field
The invention relates to parking apron data acquisition, in particular to an automatic acquisition method for the time of loading and unloading wheel blocks of an airplane.
Background
According to the 88 th order issued by the general office of civil aviation in 2013, namely the regulation in the statistical approach for the normal flight of civil aviation, the time for the airplane to get on and off the wheel gear needs to be accurately recorded when the normality of the flight is checked.
The parking apron operation flow requires that the front and the rear wheel blocks of the airplane wheels are removed before the airplane takes off, the wheel blocks are placed in the front and the rear of the airplane wheels after landing, and the removal and placement conditions are timely notified to a navigation control center and other dispatching departments. At present, there are electronic wheel blocks based on RFID: the trigger switch is used for sensing whether the pull rope of the wheel chock is straightened and stressed, and the time collection of the upper wheel chock and the lower wheel chock is realized by combining the RFID technology.
However, in the process of collecting the time of the upper wheel chock and the lower wheel chock in the prior art, the problem of instability and reliability is caused due to the fact that the mechanical trigger switch is relied on to act, and the accuracy of the collected time data of the upper wheel chock and the lower wheel chock of the airplane is low.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects in the prior art, the invention provides the automatic acquisition method for the moments of loading and unloading the wheel chock of the airplane, which can effectively overcome the defects of insufficient stability and reliability and low accuracy of data acquisition in the prior art.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme:
an automatic acquisition method for the moment of loading and unloading a wheel chock of an airplane comprises the following steps:
s1, when the electronic wheel block moves, waking up an internal first detection module, and matching the first detection module with a second detection module in the base station to detect the state of the electronic wheel block;
s2, the base station uploads the detection data of the second detection module to the server;
and S3, the server judges the state of the electronic wheel gear based on the detection data through the state identification module, and sends the obtained wheel gear up-down time to other systems.
Preferably, the step S3, the determining, by the state identification module, the electronic gear state based on the detection data includes:
when the electronic wheel chock is in a lower wheel chock state, the state identification module continuously judges that the distance/angle between the electronic wheel chock and the base station is positioned at the airplane wheel twice, and after the electronic wheel chock stops moving for a period of time, the state identification module judges that the electronic wheel chock is in an upper wheel chock state;
when the electronic wheel chock is in an upper wheel chock state and the state identification module continuously judges that the distance/angle between the electronic wheel chock and the base station is away from the airplane wheel twice, the state identification module judges that the electronic wheel chock is in a lower wheel chock state.
Preferably, the server comprises a database, a state identification module and a data interface;
the database is used for storing the uploading data of the base station;
the state identification module judges whether the electronic wheel gear is in an upper wheel gear/lower wheel gear state based on the uploaded data of the base station and records the time of the upper wheel gear and the lower wheel gear;
and the data interface is in butt joint with other systems and sends the obtained wheel gear loading and unloading time to other systems.
Preferably, the electronic wheel chock comprises an IMU module, a first detection module and a data transmission module;
the IMU module is used for detecting whether the electronic wheel block is in a motion state or not and giving a sleep prompt/awakening prompt to the first detection module;
the first detection module is in data communication with the second detection module at fixed time intervals and is used for detecting the state of the electronic gear;
and the data sending module is used for sending the IMU data and the identity ID to the base station.
Preferably, when the electronic wheel chock stops moving, the first detection module enters a sleep mode under the prompt of the IMU module; when the electronic wheel chock moves, the first detection module wakes up under the prompt of the IMU module and enters a working mode.
Preferably, the base station includes a second detection module, a data receiving module and a data uploading module;
the second detection module is in data communication with the first detection module at fixed time intervals and is used for carrying out state detection on the electronic gear;
the data receiving module is used for receiving IMU data and identity ID sent by the electronic gear;
and the data uploading module uploads the detection data, the IMU data and the identity ID of the second detection module to the server.
Preferably, the first detection module and the second detection module perform data communication at regular intervals by using one or more of an RFID tag identification technology, an NFC tag identification technology, a bluetooth angle measurement technology, and a UWB ranging technology.
Preferably, the data uploading module uploads data to the server by adopting one or more of Wi-Fi, ethernet, LoRa, NB-IoT, 4G and 5G.
(III) advantageous effects
Compared with the prior art, the automatic acquisition method for the time of loading and unloading the wheel chock of the airplane provided by the invention has the following beneficial effects:
1) the IMU module is used for detecting whether the electronic wheel chock is in a motion state or not, and a dormancy prompt/awakening prompt is given to the first detection module, so that the starting of the system is independent of a mechanical device, and the stability and reliability of time collection of the upper wheel chock and the lower wheel chock are ensured;
2) in the process that the state identification module judges the state of the electronic wheel block based on the detection data of the second detection module, the IMU module provides the motion data of the electronic wheel block, so that the accuracy of data acquisition is effectively improved;
3) the state recognition module judges the state of the electronic wheel block by judging the distance/angle between the electronic wheel block and the base station, and the accuracy of data acquisition can be further improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It is obvious that the drawings in the following description are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be derived from them without inventive effort.
FIG. 1 is a schematic diagram of the system of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention. It is to be understood that the embodiments described are only a few embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
An automatic acquisition method for the moment of loading and unloading a wheel chock of an airplane comprises the following steps:
s1, when the electronic wheel block moves, waking up an internal first detection module, and matching the first detection module with a second detection module in the base station to detect the state of the electronic wheel block;
s2, the base station uploads the detection data of the second detection module to the server;
and S3, the server judges the state of the electronic wheel gear based on the detection data through the state identification module, and sends the obtained wheel gear up-down time to other systems.
In the technical scheme of the application, the whole system mainly comprises an electronic wheel block, a base station and a server, and as shown in fig. 1, the system structure of each part is as follows:
the electronic wheel chock comprises an IMU module, a first detection module and a data sending module;
the IMU module is used for detecting whether the electronic wheel block is in a motion state or not and giving a sleep prompt/awakening prompt to the first detection module;
the first detection module is in data communication with the second detection module at fixed time intervals and is used for detecting the state of the electronic gear;
and the data sending module is used for sending the IMU data and the identity ID to the base station.
The base station comprises a second detection module, a data receiving module and a data uploading module;
the second detection module is in data communication with the first detection module at fixed time intervals and is used for carrying out state detection on the electronic gear;
the data receiving module is used for receiving IMU data and identity ID sent by the electronic gear;
and the data uploading module uploads the detection data, the IMU data and the identity ID of the second detection module to the server.
The server comprises a database, a state identification module and a data interface;
the database is used for storing the uploading data of the base station;
the state identification module judges whether the electronic wheel gear is in an upper wheel gear/lower wheel gear state based on the uploaded data of the base station and records the time of the upper wheel gear and the lower wheel gear;
and the data interface is in butt joint with other systems and sends the obtained wheel gear loading and unloading time to other systems.
When the electronic wheel chock stops moving (is static), the first detection module enters a sleep mode under the prompt of the IMU module; when the electronic wheel chock moves, the first detection module wakes up under the prompt of the IMU module and enters a working mode.
After the first detection module enters the working mode, data communication is carried out between the first detection module and the second detection module at fixed time intervals, and the first detection module is used for carrying out state detection on the electronic gear. And the first detection module and the second detection module carry out data communication at fixed intervals through one or more of an RFID (radio frequency identification) tag identification technology, an NFC (near field communication) tag identification technology, a Bluetooth angle measurement technology and an UWB (ultra-wide band) distance measurement technology.
The base station receives the IMU data and the identity ID sent by the electronic gear through the data receiving module, and uploads the IMU data and the identity ID to the server together with the detection data of the second detection module by using the data uploading module. The data uploading module uploads data to the server by adopting one or more of Wi-Fi, Ethernet, LoRa, NB-IoT, 4G and 5G.
The server stores the uploading data of the base station into a database, and meanwhile, the state recognition module judges whether the electronic wheel block is in an upper wheel block/lower wheel block state based on the uploading data of the base station, records the time of loading and unloading the wheel block, and sends the obtained time of loading and unloading the wheel block to other systems through a data interface.
In the technical scheme, the state recognition module judges the state of the electronic wheel block by judging the distance/angle between the electronic wheel block and the base station, and the accuracy of data acquisition can be further improved. The method comprises the following specific steps:
the electronic wheel chock state is judged by judging the distance/angle between the electronic wheel chock and the base station:
when the electronic wheel chock is in a lower wheel chock state, the state identification module continuously judges twice that the distance/angle between the electronic wheel chock and the base station is positioned at the airplane wheel, and after the electronic wheel chock stops moving for a period of time (generally 10s), the state identification module judges that the electronic wheel chock is in an upper wheel chock state;
when the electronic wheel chock is in an upper wheel chock state and the state identification module continuously judges that the distance/angle between the electronic wheel chock and the base station is away from the airplane wheel twice, the state identification module judges that the electronic wheel chock is in a lower wheel chock state.
When the electronic wheel chock stops moving, the first detection module enters a sleep mode under the prompt of the IMU module, and the data communication process between the first detection module and the second detection module stops.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the corresponding technical solutions.

Claims (8)

1. An automatic acquisition method for the moment of loading and unloading a wheel chock of an airplane is characterized by comprising the following steps of: the method comprises the following steps:
s1, when the electronic wheel block moves, waking up an internal first detection module, and matching the first detection module with a second detection module in the base station to detect the state of the electronic wheel block;
s2, the base station uploads the detection data of the second detection module to the server;
and S3, the server judges the state of the electronic wheel gear based on the detection data through the state identification module, and sends the obtained wheel gear up-down time to other systems.
2. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 1, is characterized in that: the server passes through the state identification module in S3 and judges electron wheel gear state based on the detected data, includes:
when the electronic wheel chock is in a lower wheel chock state, the state identification module continuously judges that the distance/angle between the electronic wheel chock and the base station is positioned at the airplane wheel twice, and after the electronic wheel chock stops moving for a period of time, the state identification module judges that the electronic wheel chock is in an upper wheel chock state;
when the electronic wheel chock is in an upper wheel chock state and the state identification module continuously judges that the distance/angle between the electronic wheel chock and the base station is away from the airplane wheel twice, the state identification module judges that the electronic wheel chock is in a lower wheel chock state.
3. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 2, is characterized in that: the server comprises a database, a state identification module and a data interface;
the database is used for storing the uploading data of the base station;
the state identification module judges whether the electronic wheel gear is in an upper wheel gear/lower wheel gear state based on the uploaded data of the base station and records the time of the upper wheel gear and the lower wheel gear;
and the data interface is in butt joint with other systems and sends the obtained wheel gear loading and unloading time to other systems.
4. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 1, is characterized in that: the electronic wheel chock comprises an IMU module, a first detection module and a data sending module;
the IMU module is used for detecting whether the electronic wheel block is in a motion state or not and giving a sleep prompt/awakening prompt to the first detection module;
the first detection module is in data communication with the second detection module at fixed time intervals and is used for detecting the state of the electronic gear;
and the data sending module is used for sending the IMU data and the identity ID to the base station.
5. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 4, is characterized in that: when the electronic wheel chock stops moving, the first detection module enters a sleep mode under the prompt of the IMU module; when the electronic wheel chock moves, the first detection module wakes up under the prompt of the IMU module and enters a working mode.
6. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 1, is characterized in that: the base station comprises a second detection module, a data receiving module and a data uploading module;
the second detection module is in data communication with the first detection module at fixed time intervals and is used for carrying out state detection on the electronic gear;
the data receiving module is used for receiving IMU data and identity ID sent by the electronic gear;
and the data uploading module uploads the detection data, the IMU data and the identity ID of the second detection module to the server.
7. The method for automatically acquiring the time of loading and unloading the wheel chock of the airplane as claimed in claim 4 or 6, wherein: and the first detection module and the second detection module carry out data communication at fixed intervals through one or more of an RFID (radio frequency identification) tag identification technology, an NFC (near field communication) tag identification technology, a Bluetooth angle measurement technology and an UWB (ultra-wide band) distance measurement technology.
8. The method for automatically acquiring the moment when the aircraft goes up and down the wheel chock according to claim 6, is characterized in that: the data uploading module uploads data to the server by adopting one or more of Wi-Fi, Ethernet, LoRa, NB-IoT, 4G and 5G.
CN202111503901.9A 2021-12-09 2021-12-09 Automatic acquisition method for airplane wheel chock loading and unloading time Pending CN114030633A (en)

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109693805A (en) * 2018-11-14 2019-04-30 北京普联恒创科技有限公司 A kind of airplane chock and its management method, device, server-side, server and system
CN110015441A (en) * 2019-05-15 2019-07-16 成都耀塔科技有限公司 A kind of monitoring of airplane parking area electronics catch state and report method
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
CN110626517A (en) * 2018-06-21 2019-12-31 孙伟 Intelligent device and intelligent system for aircraft wheel block and automatic data acquisition method
CN110751748A (en) * 2018-12-24 2020-02-04 上海民航华东凯亚***集成有限公司 Intelligent wheel file, intelligent wheel file system and method for determining time of getting on and off wheel file of flight
CN210634772U (en) * 2018-06-21 2020-05-29 孙伟 Aircraft wheel chock
CN211108052U (en) * 2019-10-10 2020-07-28 武汉海巍感知科技有限公司 Airplane wheel chock and airplane wheel chock management system
CN112649894A (en) * 2019-10-10 2021-04-13 阿里巴巴集团控股有限公司 Detection system, method and device, intelligent wheel chock and wheel chock detection system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110626517A (en) * 2018-06-21 2019-12-31 孙伟 Intelligent device and intelligent system for aircraft wheel block and automatic data acquisition method
CN210634772U (en) * 2018-06-21 2020-05-29 孙伟 Aircraft wheel chock
CN109693805A (en) * 2018-11-14 2019-04-30 北京普联恒创科技有限公司 A kind of airplane chock and its management method, device, server-side, server and system
CN110751748A (en) * 2018-12-24 2020-02-04 上海民航华东凯亚***集成有限公司 Intelligent wheel file, intelligent wheel file system and method for determining time of getting on and off wheel file of flight
CN110015441A (en) * 2019-05-15 2019-07-16 成都耀塔科技有限公司 A kind of monitoring of airplane parking area electronics catch state and report method
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
CN211108052U (en) * 2019-10-10 2020-07-28 武汉海巍感知科技有限公司 Airplane wheel chock and airplane wheel chock management system
CN112649894A (en) * 2019-10-10 2021-04-13 阿里巴巴集团控股有限公司 Detection system, method and device, intelligent wheel chock and wheel chock detection system

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