CN106960231A - Unmanned plane part management system - Google Patents
Unmanned plane part management system Download PDFInfo
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- CN106960231A CN106960231A CN201610016643.4A CN201610016643A CN106960231A CN 106960231 A CN106960231 A CN 106960231A CN 201610016643 A CN201610016643 A CN 201610016643A CN 106960231 A CN106960231 A CN 106960231A
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- Prior art keywords
- unmanned plane
- parts
- management system
- identification information
- part management
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06K—GRAPHICAL DATA READING; PRESENTATION OF DATA; RECORD CARRIERS; HANDLING RECORD CARRIERS
- G06K17/00—Methods or arrangements for effecting co-operative working between equipments covered by two or more of main groups G06K1/00 - G06K15/00, e.g. automatic card files incorporating conveying and reading operations
Abstract
The present invention relates to the technical field of logistics transportation, a kind of unmanned plane part management system is disclosed, for the reliability management of unmanned plane, including：Identify unit, the identification information for identifying and storing unmanned plane parts；Reading unit is identified, the identification information flown in its front and rear mark unit is held for reading unmanned plane；Unmanned plane dispatches system, holds winged for dispatching unmanned plane, and obtains identification information with the life parameter of accumulation unmanned plane parts；Communication module, for identification information to be transferred into unmanned plane scheduling system；The whole machine health state evaluation system of unmanned plane, for analyzing the reliability of unmanned plane according to the life parameter of unmanned plane parts, and feeds back to unmanned plane operation management personnel by the reliability state of unmanned plane.The embodiment of the present invention propose unmanned plane part management system, realize effective management to the unmanned plane parts in operation, it is ensured that unmanned plane it is safe and reliable, improve the security of unmanned plane, saved unmanned plane operation cost.
Description
Technical field
The present invention relates to the technical field of logistics transportation, more particularly to a kind of unmanned plane part management system.
Background technology
Unmanned mother aircraft, abbreviation unmanned plane, unmanned plane can be taken photo in the sky, resource investigation,
Patrol, the delivering project such as disaster relief supplies, its demand more and more higher in social life.With aspect
The universalness of control system and space technology, the UAV of all size progresses into commercial market,
Especially in freight logistics industry, unmanned plane is gradually utilized transport goods, and its application has broad prospects.
On unmanned plane each part, component, part or other equipment (engine of such as helicopter,
Mast, rotor blade, propeller hub, main legacy system gear, winged control etc.；Such as multi-rotor unmanned aerial vehicle
Battery, the mechanical, electrical tune of electricity, propeller, winged control, jointing etc.；The such as engine of fixed-wing unmanned plane
Or motor, transmission system gear, propeller, winged control etc.) all there are service life, each parts one
As be used as life-span basis for estimation with accumulative use time or number of times., it is necessary to this during unmanned plane operation
A little parts are managed, to understand the health status of every frame unmanned plane at any time, it is ensured that the reliability of unmanned plane.
At present, in manned aircraft field, its parts is managed using stamp, there is correspondence per airplane
Parts inventory, enumerates each parts code in detail.The parts design life-span one of manned aircraft
As above aircraft service life, its reliability determines by whole machine, periodic maintenance, periodic inspection or overhaul with
Ensure aircraft safety.In unmanned plane field, especially civilian or industrial application, unmanned plane parts
Management is also without a set of scientific method.And unmanned plane parts service life be generally lower than it is man-machine, by
In cost control, the unmanned plane parts design life-span is also restricted, and such as battery access times limitation, motor tires out
Use time limitation is counted, in addition, some parts for scrapping unmanned plane still may proceed to use so that unmanned plane
Operation has potential safety hazard.However, carrying out part management membership dues using having man-machine icotype to unmanned plane
Thing is laborious, and error is very easy to again, is not managed, unmanned plane security reliability can not ensure, therefore how
A kind of unmanned plane part management system is provided, the unmanned plane parts in operation are managed, to ensure
Unmanned plane is safe and reliable, is technical problem urgently to be resolved hurrily in the industry.
The content of the invention
It is an object of the invention to overcome above-mentioned the deficiencies in the prior art, there is provided a kind of unmanned plane parts pipe
Reason system, realizes effective management to the unmanned plane parts in operation, it is ensured that the safety of unmanned plane can
Lean on, improve the security of unmanned plane, saved unmanned plane operation cost.
In a first aspect, the embodiments of the invention provide a kind of unmanned plane part management system, for unmanned plane
Reliability management, the unmanned plane part management system includes：
Identify unit, the identification information for identifying and storing unmanned plane parts；
Reading unit is identified, the identification information flown in its front and rear mark unit is held for reading unmanned plane；
Unmanned plane dispatches system, holds winged for dispatching unmanned plane, and obtains the identification information to accumulate nobody
The life parameter of machine parts；
Communication module, system is dispatched for the identification information to be transferred into the unmanned plane；
The whole machine health state evaluation system of unmanned plane, for according to the life parameter of the unmanned plane parts point
The reliability of unmanned plane is analysed, and the reliability state of the unmanned plane is fed back into unmanned plane operation management personnel.
With reference in a first aspect, in the first possible implementation, the mark reading unit is hand-held movement
Formula code reader, or NFC module read equipment, or magnetic identification reads equipment, or radio frequency identification reads equipment.
With reference in a first aspect, in second of possible implementation, the mark reading unit is that can be read
NFC, magnetic identification and radio frequency identification signals Multifunctional label read equipment.
The first with reference to first aspect or combination first aspect is any into second of possible embodiment
One kind, in the third possible implementation, the mark unit includes the code device for encoding,
And for storing the mark of identification information, the mark is arranged on the unmanned plane and its parts.
With reference to the third possible implementation of first aspect, in the 4th kind of possible implementation, institute
Stating identification information includes any one of radio frequency code, position code and other unique identifiers.
The first with reference to first aspect or combination first aspect is any into second of possible embodiment
One kind, in the 5th kind of possible implementation, when the life parameter includes the use of unmanned plane parts
Between or access times, or use time and access times combination.
With reference to the 5th kind of possible implementation of first aspect, in the 6th kind of possible implementation, institute
Stating unmanned plane scheduling system includes the accumulated time module for accumulation unmanned plane parts use time, and
Number of times accumulation module for accumulation unmanned plane parts access times.
The first with reference to first aspect or combination first aspect is any into second of possible embodiment
One kind, in the 7th kind of possible implementation, the communication module is wireless communication module.
The first with reference to first aspect or combination first aspect is any into second of possible embodiment
One kind, in the 8th kind of possible implementation, the whole machine health state evaluation system of unmanned plane, which has, to be used
In the unmanned plane fail-safe analysis algorithm of analysis unmanned plane reliability.
The unmanned plane part management system proposed based on above-mentioned technical proposal, the embodiment of the present invention, by it
Mark unit is write and stores the identification information of unmanned plane parts, and identifying reading unit by it reads nobody
Machine holds the identification information flown in its front and rear mark unit, and identification information is transferred into its nothing by its communication module
Man-machine scheduling system, by the unmanned plane dispatch system call unmanned plane hold it is winged, while obtain identification information simultaneously
The life parameter of accumulation unmanned plane parts, by the whole machine health state evaluation system of its unmanned plane according to nobody
The life parameter of machine parts analyzes the reliability of the unmanned plane, and the reliability state of the unmanned plane is fed back
Unmanned plane operation management personnel are given, thus, effective management to the unmanned plane parts in operation is realized,
So that unmanned plane operation management personnel can timely and effectively understand the reliability state of unmanned plane, it is to avoid nobody
Potential safety hazard caused by machine and its part life state are unclear, it is ensured that it is safe and reliable that unmanned plane is runed,
Also save unmanned plane operation cost.
Brief description of the drawings
Fig. 1 is the system schematic for the unmanned plane part management system that the embodiment of the present invention is proposed.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with accompanying drawing and reality
Example is applied, the present invention will be described in further detail.It should be appreciated that specific embodiment described herein is only
Only to explain the present invention, it is not intended to limit the present invention.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, it can be straight
It is connected on another element or may be simultaneously present centering elements.When an element is known as " being connected to " separately
One element, it can be directly to another element or may be simultaneously present centering elements.
In addition, it should also be noted that, the orientation term such as left and right, upper and lower in the embodiment of the present invention,
Only it is relative concept or using the normal operating condition of product as reference each other, and should not be regarded as having
Restricted.The realization of the present invention is described in detail below in conjunction with specific embodiment.
As shown in figure 1, the embodiment of the present invention proposes a kind of unmanned plane part management system, the management system
The reliability management united for unmanned plane.Specifically, the unmanned plane part management system may include that mark is single
Member 1, mark reading unit 2, communication module 3, unmanned plane scheduling system 4 and the healthy shape of the whole machine of unmanned plane
State assessment system 5, wherein, mark unit 1 is used for the identification information for writing and storing unmanned plane parts；
Mark reading unit 2 holds the identification information flown in its front and rear mark unit 1 for reading unmanned plane, herein,
Unmanned plane is held fly before and after, refer to when unmanned plane takes off and during landing；The connection identifier of communication module 3 reads single
Member 2 and unmanned plane scheduling system 4, the communication module 3 are used to transmit the identification information of unmanned plane parts
System 4 is dispatched to unmanned plane；Here, unmanned plane scheduling system 4 is the total system of unmanned plane operation, can be obtained
The identification information of unmanned plane parts is taken and handles, with the life parameter of accumulation unmanned plane parts, meanwhile,
The unmanned plane scheduling system 4 can be additionally used in scheduling unmanned plane hold it is winged, herein, unmanned plane scheduling system 4 in,
The identification information of unmanned plane parts all can be stored in unmanned plane scheduling system 4 it is inner in the unmanned plane
The parameters such as specification, model are corresponded, this way it is ensured that the uniqueness of unmanned plane and parts；In addition,
The whole machine health state evaluation system 5 of unmanned plane is used to analyze this nobody according to the life parameter of unmanned plane parts
The reliability of machine, and the reliability state of the unmanned plane is fed back into unmanned plane operation management personnel, in order to
Unmanned plane operation management personal scheduling unmanned plane.
The unmanned plane part management system that the embodiment of the present invention is proposed, with following features：
The unmanned plane part management system that the embodiment of the present invention is proposed, is write and is deposited by its mark unit 1
The identification information of unmanned plane parts is stored up, winged front and rear its is held by its mark reading unmanned plane of reading unit 2 and marked
Know the identification information in unit 1, identification information is transferred to by its unmanned plane scheduling system by its communication module 3
System 4, by the unmanned plane dispatch system 4 dispatch unmanned plane hold it is winged, while obtaining identification information and accumulating nothing
The life parameter of man-machine parts, by the whole machine health state evaluation system 5 of its unmanned plane according to unmanned plane zero
The life parameter of part analyzes the reliability of the unmanned plane, and the reliability state of the unmanned plane is fed back into nothing
Man-machine operation management personnel, thus, realizing effective management to the unmanned plane parts in operation so that
Unmanned plane operation management personnel can timely and effectively understand the reliability state of unmanned plane, it is to avoid unmanned plane and
Potential safety hazard caused by its part life state is unclear, it is ensured that unmanned plane and the safety of unmanned plane operation can
Lean on, also save unmanned plane operation cost.
Further, in an embodiment of the present invention, above-mentioned mark reading unit 2 can be hand-held mobile
Code reader, or NFC module read equipment, or magnetic identification reads equipment, or radio frequency identification reads equipment.
Herein, mark reading unit 2 is preferably that NFC module reads equipment, certainly, according to actual conditions and specifically
Demand, in other embodiments of the invention, above-mentioned mark reading unit 2 can be also other reading equipment,
Unique restriction is not made herein.
Or, in another embodiment of the invention, above-mentioned mark reading unit 2 can also be Multifunctional label
Equipment is read, herein, the Multifunctional label reads device-readable and takes NFC, magnetic identification and radio frequency identification letter
Number.Certainly, according to actual conditions and real needs, in other embodiments of the invention, above-mentioned mark is read
It can be also other reading equipment to take unit 2, do not make unique restriction herein.
Further, in an embodiment of the present invention, above-mentioned mark unit 1 may include code device and mark
(being not drawn into accompanying drawing), wherein, code device is encoded with for staff to unmanned plane parts,
And by the code storage in mark, the mark is arranged on unmanned plane and its parts.Certainly, according to reality
Border situation and real needs, in other embodiments of the invention, above-mentioned mark unit 1 can be also other knots
Structure is constituted, and does not make unique restriction herein.
Further, in an embodiment of the present invention, above-mentioned identification information is preferably radio frequency code, here, work
Make personnel to encode unmanned plane parts by code device, so so that the unmanned plane parts have
There is relatively independent and unique coding, so so that unmanned plane parts possess uniqueness so that follow-up
Reading monitoring it is convenient and swift.Certainly, according to actual conditions and real needs, in other implementations of the present invention
In example, above-mentioned identification information can also be encoded for other types, such as position code by putting position,
Also such as other unique identifiers, do not make unique restriction herein.
In an embodiment of the present invention, above-mentioned life parameter includes the use time of unmanned plane parts or used
Number of times, or use time and access times combination, herein, life parameter is preferably making for unmanned plane parts
With time or access times.Above-mentioned unmanned plane scheduling system 4 obtains and handled the identification letter of unmanned plane parts
Breath, with the use time or access times of the life parameter of accumulation unmanned plane parts, i.e. accumulation unmanned plane.
Certainly, according to actual conditions and real needs, in other embodiments of the invention, above-mentioned life parameter is also
It can be other kinds of life-span basis for estimation parameter, not make unique restriction herein.
Further, in an embodiment of the present invention, above-mentioned communication module 3 is preferably wireless communication module,
The wireless communication module can be WIFI module or bluetooth module etc., that is, identify reading unit 2 and nothing
Communication mode between man-machine scheduling system 4 is preferably radio communication, the radio communication include WIFI transmission,
Bluetooth etc. transmission means.Certainly, according to actual conditions and real needs, in the other embodiment of the present invention
In, above-mentioned communication module 3 or wire communication module identify reading unit 2 and unmanned plane scheduling system
Realized and communicated by wired data transfer between system 4, do not make unique restriction herein.
Further, in an embodiment of the present invention, the whole machine health state evaluation system 5 of above-mentioned unmanned plane belongs to
The part in system 4 is dispatched in above-mentioned unmanned plane, and the whole machine health state evaluation system 5 of the unmanned plane has
There is a set of unmanned plane fail-safe analysis algorithm for being used to analyze unmanned plane reliability, that is to say, that work as unmanned plane
Scheduling system 4 is obtained and handled after the identification information of unmanned plane parts, the life-span of accumulation unmanned plane parts
Parameter, and the life parameter is transferred to the whole machine health state evaluation system 5 of unmanned plane, the assessment system is led to
Cross unmanned plane fail-safe analysis algorithm to be analyzed and assessed according to the life parameter of unmanned plane parts, assess
After the completion of, the reliability state of the unmanned plane is fed back into unmanned plane operation management personnel, in order to unmanned plane
Operation management personal scheduling unmanned plane.
The foregoing is only a specific embodiment of the invention, but protection scope of the present invention is not limited to
This, any one skilled in the art the invention discloses technical scope in, can readily occur in
Various equivalent modifications, replace and improve etc., these modification, replace and improve should all cover the present invention
Within protection domain.Therefore, protection scope of the present invention should be defined by scope of the claims.
Claims (9)
1. unmanned plane part management system, the reliability management for unmanned plane, it is characterised in that described
Unmanned plane part management system includes：
Identify unit, the identification information for identifying and storing unmanned plane parts；
Reading unit is identified, the identification information flown in its front and rear mark unit is held for reading unmanned plane；
Unmanned plane dispatches system, holds winged for dispatching unmanned plane, and obtains the identification information to accumulate nobody
The life parameter of machine parts；
Communication module, system is dispatched for the identification information to be transferred into the unmanned plane；
The whole machine health state evaluation system of unmanned plane, for according to the life parameter of the unmanned plane parts point
The reliability of unmanned plane is analysed, and the reliability state of the unmanned plane is fed back into unmanned plane operation management personnel.
2. unmanned plane part management system as claimed in claim 1, it is characterised in that the mark is read
Unit is taken for hand-held mobile code reader, or NFC module reads equipment, or magnetic identification reads equipment, or
Radio frequency identification reads equipment.
3. unmanned plane part management system as claimed in claim 1, it is characterised in that the mark is read
It is that the Multifunctional label that NFC, magnetic identification and radio frequency identification signals can be read reads equipment to take unit.
4. the unmanned plane part management system as described in any one of claims 1 to 3, it is characterised in that
The mark unit includes the code device for encoding, and for storing the mark of identification information, it is described
Mark is arranged on the unmanned plane and its parts.
5. unmanned plane part management system as claimed in claim 4, it is characterised in that the identification letter
Breath includes any one of radio frequency code, position code and other unique identifiers.
6. the unmanned plane part management system as described in any one of claims 1 to 3, it is characterised in that
The life parameter includes the use time or access times of unmanned plane parts, or use time and use time
Array is closed.
7. unmanned plane part management system as claimed in claim 6, it is characterised in that the unmanned plane
Scheduling system includes the accumulated time module for accumulation unmanned plane parts use time, and for accumulating
The number of times accumulation module of unmanned plane parts access times.
8. the unmanned plane part management system as described in any one of claims 1 to 3, it is characterised in that
The communication module is wireless communication module.
9. the unmanned plane part management system as described in any one of claims 1 to 3, it is characterised in that
The whole machine health state evaluation system of unmanned plane has the unmanned plane reliability for being used for analyzing unmanned plane reliability
Parser.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610016643.4A CN106960231A (en) | 2016-01-11 | 2016-01-11 | Unmanned plane part management system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610016643.4A CN106960231A (en) | 2016-01-11 | 2016-01-11 | Unmanned plane part management system |
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| CN106960231A true CN106960231A (en) | 2017-07-18 |
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| CN201610016643.4A Pending CN106960231A (en) | 2016-01-11 | 2016-01-11 | Unmanned plane part management system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110287742A (en) * | 2018-03-19 | 2019-09-27 | 江苏现代造船技术有限公司 | A kind of intelligent identifying system and method for individuals of hull structure |
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| CN104680350A (en) * | 2005-09-20 | 2015-06-03 | 波音公司 | System And Methods For Tracking Aircraft Components |
| CN105046463A (en) * | 2015-06-18 | 2015-11-11 | 顺丰科技有限公司 | Unmanned aerial vehicle freight flying method based on intelligent nacelle and the intelligent nacelle |
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2016
- 2016-01-11 CN CN201610016643.4A patent/CN106960231A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104680350A (en) * | 2005-09-20 | 2015-06-03 | 波音公司 | System And Methods For Tracking Aircraft Components |
| CN202351899U (en) * | 2011-07-21 | 2012-07-25 | 领科无线射频系统(上海)有限公司 | RFID-based automobile component tracing management system |
| CN105046463A (en) * | 2015-06-18 | 2015-11-11 | 顺丰科技有限公司 | Unmanned aerial vehicle freight flying method based on intelligent nacelle and the intelligent nacelle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110287742A (en) * | 2018-03-19 | 2019-09-27 | 江苏现代造船技术有限公司 | A kind of intelligent identifying system and method for individuals of hull structure |
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