CN109649673A - A kind of airplane chock reporting the upper and lower block time automatically and its working method - Google Patents
A kind of airplane chock reporting the upper and lower block time automatically and its working method Download PDFInfo
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- CN109649673A CN109649673A CN201811543838.XA CN201811543838A CN109649673A CN 109649673 A CN109649673 A CN 109649673A CN 201811543838 A CN201811543838 A CN 201811543838A CN 109649673 A CN109649673 A CN 109649673A
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- 238000000034 method Methods 0.000 title claims abstract description 13
- 238000004891 communication Methods 0.000 claims abstract description 16
- 230000001960 triggered effect Effects 0.000 claims abstract description 7
- 230000002123 temporal effect Effects 0.000 claims description 7
- 230000005611 electricity Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 description 5
- 230000032258 transport Effects 0.000 description 3
- 235000013399 edible fruits Nutrition 0.000 description 2
- 238000012797 qualification Methods 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical group [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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- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
Classifications
-
- 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)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention discloses the airplane chocks that one kind reports the upper and lower block time automatically, whether it is straightened the trigger switch of stress including the catch drawstring for incuding airplane chock, for receiving the micro-control unit for the signal that the trigger switch issues, the tag recognition module of the wheel location tags in aircraft gate at aero tyre position is set on airport ground and is located at for identification, and the tag recognition module is by the micro-control unit controls, the micro-control unit is also used to generate block time information up and down according to the trigger switch triggered time and the tag recognition module recognition result, for reporting the block time information up and down to report communication module.The invention also discloses the working methods of above-mentioned airplane chock, the present invention can be realized reporting automatically for aircraft upper and lower block time, in order to which server automatically records, solve the existing timeliness of the upper and lower block time record of aircraft, accuracy, the big major issue of miss rate three.
Description
Technical field
The present invention relates to airplane chocks and its working method that one kind reports the upper and lower block time automatically, belong to aviation information
Technical field.
Background technique
It is " commercial air flights normal statistics method " according to the 88th command that China Administration of Civil Aviation promulgated early in 2013
In regulation, need accurately to record the time of the upper and lower catch of aircraft when examining View of Flight On-time Performance.This is crucial all the time
Timing node relies on manual type to be recorded always, since manual work will receive different work personnel's operation with being difficult to avoid that
The influence of qualification, details habit and negligence of operation etc. factor leads to this data there are timeliness low, accuracy
Low, the problems such as miss rate is high.Therefore, it is necessary to a kind of technical solution of combination modern times technology of Internet of things be provided, to realize aircraft
The upper and lower block time automatically records, to solve the existing timeliness of the upper and lower block time record of aircraft, accuracy, lack
The big major issue of mistake rate three.
Summary of the invention
The present invention is exactly in view of the deficienciess of the prior art, providing a kind of aircraft wheel for reporting the upper and lower block time automatically
Gear and its working method, to solve the existing timeliness of the upper and lower block time record of aircraft, accuracy, the weight greatly of miss rate three
Want problem.
To solve the above problems, the technical solution used in the present invention is as follows:
A kind of airplane chock reporting the upper and lower block time automatically, comprising:
Whether the catch drawstring for incuding airplane chock is straightened the trigger switch of stress,
For receiving the micro-control unit for the signal that the trigger switch issues,
It is set on airport ground for identification and is located at the wheel location tags in aircraft gate at aero tyre position
Tag recognition module, and the tag recognition module is by the micro-control unit controls,
The micro-control unit was also used to according to the trigger switch triggered time and tag recognition module identification knot
Fruit generates block time information up and down,
For reporting the block time information up and down to report communication module.
Signal identification scheme between the wheel location tags and the tag recognition module can be RFID label tag knowledge
Other technology, NFC label identification technology, Bluetooth label identification technology and tag identification technologies based on 433m wireless module etc..
As an improvement of the above technical solution, described to report communication module for the communication apparatus based on narrowband Internet of Things.
As an improvement of the above technical solution, further include for the power supply circuit one for the tag recognition module for power supply,
For for the micro-control unit and it is described report communication module power power supply circuit two.
It as an improvement of the above technical solution, further include for powering for the power supply circuit one and the power supply circuit two
Battery module, and the charging circuit of the connection battery module.
Above-mentioned one kind reports the working method of the airplane chock in upper and lower block time automatically, comprising the following steps:
S1: triggering the trigger switch after catch drawstring is straightened stress to lift airplane chock, and the triggering is opened
It closes to the micro-control unit and issues signal；
S2: after the micro-control unit receives the signal that the trigger switch issues, record receives the time of signal, and
The tag recognition module is controlled to identify wheel location tags；
S3: the micro-control unit is raw according to the trigger switch triggered time and the tag recognition module recognition result
At upper and lower block time information；
S4: report communication module by the block time information reporting up and down to service described in the micro-control unit controls
Device is recorded.
As an improvement of the above technical solution, in step S1, when catch drawstring is straightened stress to lift airplane chock,
The trigger switch issues first time signal to the micro-control unit；Catch drawstring stress is set to disappear when airplane chock is put down
When mistake, the trigger switch issues second of signal to the micro-control unit.
As an improvement of the above technical solution, in step S3:
When the micro-control unit receives first time signal, the tag recognition module is unidentified to be marked to wheel position
Label, and when the micro-control unit receives second of signal, the tag recognition module does not recognize wheel location tags yet,
Block time information up and down is not generated then；
When the micro-control unit receives first time signal, the tag recognition module is unidentified to be marked to wheel position
Label, and when the micro-control unit receives second of signal, the tag recognition module recognizes wheel location tags A, then
Generate the corresponding information of upper block time of wheel location tags A；
When the micro-control unit receives first time signal, the tag recognition module recognizes wheel location tags A,
And when the micro-control unit receives second of signal, the tag recognition module is unidentified to arrive wheel location tags, then gives birth to
At the corresponding lower catch temporal information of wheel location tags A；
When the micro-control unit receives first time signal, the tag recognition module recognizes wheel location tags A,
And when the micro-control unit receives second of signal, the tag recognition module recognizes wheel location tags B, then generates
The corresponding lower catch temporal information of wheel location tags A and the corresponding information of upper block time of wheel location tags B.
Compared with prior art, implementation result of the invention is as follows by the present invention:
One kind of the present invention reports the airplane chock and its working method in upper and lower block time automatically, can be realized winged
Reporting automatically for machine upper and lower block time, in order to which server automatically records, takes turns above and below to overcome manual record aircraft
The time is kept off by the adverse effect of different work personnel's operation qualification, details habit and negligence of operation etc. factor, is solved
The existing timeliness of the upper and lower block time record of aircraft, accuracy, the big major issue of miss rate three.
Detailed description of the invention
Fig. 1 is the principle schematic diagram for the airplane chock that one kind of the present invention reports the upper and lower block time automatically.
Specific embodiment
Illustrate the contents of the present invention below in conjunction with specific embodiments.
As shown in Figure 1, reporting the structure of the airplane chock in upper and lower block time automatically for one kind provided by the present embodiment
Schematic illustration.
One kind provided by the present embodiment reports the airplane chock in upper and lower block time automatically, comprising:
Whether the catch drawstring for incuding airplane chock is straightened the trigger switch of stress；It is well known, airplane chock packet
Include catch ontology and the catch drawstring for lifting the catch ontology；The trigger switch is to those skilled in the art
It can be appreciated that many specific embodiments can be easily associated, and such as: by the catch drawstring and the catch sheet
It is connected between body by the trigger switch, the trigger switch incudes the catch drawstring to the pulling force of the catch ontology；
Or using the trigger switch as a connection buckle of the catch drawstring, the trigger switch directly incudes the catch and draws
The pulling force for receiving of restricting；
For receiving the micro-control unit for the signal that the trigger switch issues；
It is set on airport ground for identification and is located at the wheel location tags in aircraft gate at aero tyre position
Tag recognition module, and the tag recognition module is by the micro-control unit controls；
The micro-control unit was also used to according to the trigger switch triggered time and tag recognition module identification knot
Fruit generates block time information up and down；
For reporting the block time information up and down to report communication module；Specifically, described to report the communication module to be
Communication apparatus based on narrowband Internet of Things；
It further include being used for for the power supply circuit one for the tag recognition module for power supply as the micro-control unit and institute
State the power supply circuit two for reporting communication module to power；
It further include for the battery module for the power supply circuit one and the power supply of the power supply circuit two, and connection institute
State the charging circuit of battery module；Preferably, the battery module is lithium titanate battery.
Above-mentioned one kind reports the working method of the airplane chock in upper and lower block time automatically, comprising the following steps:
S1: triggering the trigger switch after catch drawstring is straightened stress to lift airplane chock, and the triggering is opened
It closes to the micro-control unit and issues signal；
Specifically, when catch drawstring is straightened stress to lift airplane chock, the trigger switch is to the microcontroller
Unit issues first time signal；When airplane chock is put down, and catch drawstring stress is made to disappear, the trigger switch is to described
Micro-control unit issues second of signal.
S2: after the micro-control unit receives the signal that the trigger switch issues, record receives the time of signal, and
The tag recognition module is controlled to identify wheel location tags.
S3: the micro-control unit is raw according to the trigger switch triggered time and the tag recognition module recognition result
At upper and lower block time information；Specifically:
When the micro-control unit receives first time signal, the tag recognition module is unidentified to be marked to wheel position
Label, and when the micro-control unit receives second of signal, the tag recognition module does not recognize wheel location tags yet,
Block time information up and down is not generated then；At this point, airplane chock is only removed between different storage locations or means of transport
Fortune, does not come into operation.
When the micro-control unit receives first time signal, the tag recognition module is unidentified to be marked to wheel position
Label, and when the micro-control unit receives second of signal, the tag recognition module recognizes wheel location tags A, then
Generate the corresponding information of upper block time of wheel location tags A；At this point, airplane chock is removed on tool from storage location or transport
It is transported at aero tyre and comes into operation.
When the micro-control unit receives first time signal, the tag recognition module recognizes wheel location tags A,
And when the micro-control unit receives second of signal, the tag recognition module is unidentified to arrive wheel location tags, then gives birth to
At the corresponding lower catch temporal information of wheel location tags A；At this point, airplane chock is that use is carried to from aero tyre later
Storage location transports on tool.
When the micro-control unit receives first time signal, the tag recognition module recognizes wheel location tags A,
And when the micro-control unit receives second of signal, the tag recognition module recognizes wheel location tags B, then generates
The corresponding lower catch temporal information of wheel location tags A and the corresponding information of upper block time of wheel location tags B；At this point, flying
Wheel gear is carried at another aero tyre from an aero tyre.
S4: report communication module by the block time information reporting up and down to service described in the micro-control unit controls
Device is recorded.
The foregoing is a detailed description of the present invention in conjunction with specific embodiments, and it cannot be said that the present invention is specifically real
It applies and is only limitted to these explanations.For those skilled in the art to which the present invention belongs, before not departing from present inventive concept
It puts, a number of simple deductions or replacements can also be made, all shall be regarded as belonging to the scope of protection of the invention.
Claims (7)
1. the airplane chock that one kind reports the upper and lower block time automatically, characterized in that include:
Whether the catch drawstring for incuding airplane chock is straightened the trigger switch of stress,
For receiving the micro-control unit for the signal that the trigger switch issues,
The label of the wheel location tags in aircraft gate at aero tyre position is set on airport ground and is located at for identification
Identification module, and the tag recognition module is by the micro-control unit controls,
The micro-control unit is also used to raw according to the trigger switch triggered time and the tag recognition module recognition result
At upper and lower block time information,
For reporting the block time information up and down to report communication module.
2. the airplane chock that one kind according to claim 1 reports the upper and lower block time automatically, characterized in that described to report
Communication module is the communication apparatus based on narrowband Internet of Things.
3. the airplane chock that one kind according to claim 1 reports the upper and lower block time automatically, characterized in that further include using
In the power supply circuit one for the tag recognition module for power supply, for for the micro-control unit and described communication module being reported to supply
The power supply circuit two of electricity.
4. the airplane chock that one kind according to claim 4 reports the upper and lower block time automatically, characterized in that further include using
In the battery module for the power supply circuit one and the power supply of the power supply circuit two, and connect filling for the battery module
Circuit.
5. the work side that one kind according to any one of claims 1-4 reports the airplane chock in upper and lower block time automatically
Method, characterized in that the following steps are included:
S1: triggering the trigger switch after catch drawstring is straightened stress to lift airplane chock, the trigger switch to
The micro-control unit issues signal；
S2: after the micro-control unit receives the signal that the trigger switch issues, record receives the time of signal, and controls
The tag recognition module identifies wheel location tags；
S3: the micro-control unit is generated according to the trigger switch triggered time and the tag recognition module recognition result
Lower catch temporal information；
S4: reported described in the micro-control unit controls communication module will it is described up and down block time information reporting to server into
Row record.
6. one kind according to claim 5 reports the working method of the airplane chock in upper and lower block time, feature automatically
It is that in step S1, when catch drawstring is straightened stress to lift airplane chock, the trigger switch is to the micro-control unit
Issue first time signal；When airplane chock is put down, and catch drawstring stress is made to disappear, the trigger switch is to the micro-control
Unit processed issues second of signal.
7. one kind according to claim 6 reports the working method of the airplane chock in upper and lower block time, feature automatically
It is, in step S3:
When the micro-control unit receives first time signal, the tag recognition module is unidentified to wheel location tags, and
When the micro-control unit receives second of signal, the tag recognition module does not recognize wheel location tags yet, then not
Generate block time information up and down；
When the micro-control unit receives first time signal, the tag recognition module is unidentified to wheel location tags, and
When the micro-control unit receives second of signal, the tag recognition module recognizes wheel location tags A, then generates machine
Take turns the corresponding information of upper block time of location tags A；
When the micro-control unit receives first time signal, the tag recognition module recognizes wheel location tags A, and works as
When the micro-control unit receives second of signal, the tag recognition module is unidentified to arrive wheel location tags, then generates machine
Take turns the corresponding lower catch temporal information of location tags A；When the micro-control unit receives first time signal, the tag recognition
Module recognizes wheel location tags A, and when the micro-control unit receives second of signal, the tag recognition module is known
It is clipped to wheel location tags B, then generates the corresponding lower catch temporal information of wheel location tags A and wheel location tags B is corresponding
Information of upper block time.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811543838.XA CN109649673B (en) | 2018-12-17 | 2018-12-17 | Airplane wheel chock capable of automatically reporting wheel chock loading and unloading time and working method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811543838.XA CN109649673B (en) | 2018-12-17 | 2018-12-17 | Airplane wheel chock capable of automatically reporting wheel chock loading and unloading time and working method thereof |
Publications (2)
| Publication Number | Publication Date |
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| CN109649673A true CN109649673A (en) | 2019-04-19 |
| CN109649673B CN109649673B (en) | 2021-05-04 |
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| CN201811543838.XA Active CN109649673B (en) | 2018-12-17 | 2018-12-17 | Airplane wheel chock capable of automatically reporting wheel chock loading and unloading time and working method thereof |
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Cited By (5)
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| 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 |
| 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 |
| 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 |
| CN112078818A (en) * | 2019-06-12 | 2020-12-15 | 北京凯乐比兴科技有限公司 | Airplane wheel gear positioning system and method |
| 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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| Publication number | Publication date |
|---|---|
| CN109649673B (en) | 2021-05-04 |
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