CN106021380A - Method and device for compiling aircraft technical publication based on maintenance engineering analysis data - Google Patents

Method and device for compiling aircraft technical publication based on maintenance engineering analysis data Download PDF

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Publication number
CN106021380A
CN106021380A CN201610311624.4A CN201610311624A CN106021380A CN 106021380 A CN106021380 A CN 106021380A CN 201610311624 A CN201610311624 A CN 201610311624A CN 106021380 A CN106021380 A CN 106021380A
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data
data message
engineering analysis
maintenance engineering
analysis data
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彭和平
黄伟
沈萍
乔万鑫
马文帅
李伟
孙玛丽
王会丽
闫瑾
韩皓
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Commercial Aircraft Corp of China Ltd
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Commercial Aircraft Corp of China Ltd
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Priority to CN201610311624.4A priority Critical patent/CN106021380A/en
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    • 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
    • G06F16/258Data format conversion from or to a database

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  • Engineering & Computer Science (AREA)
  • Databases & Information Systems (AREA)
  • Theoretical Computer Science (AREA)
  • Data Mining & Analysis (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention provides a method and a device for compiling an aircraft technical publication based on maintenance engineering analysis data. The aircraft technical publication comprises a plurality of data modules. The method comprises the following steps of analyzing the maintenance engineering analysis data to obtain first data information; establishing a mapping relation between the first data information and second data information in the data modules; and converting the first data information into the second data information according to the conversion specification and the mapping relation. The invention also provides a device for compiling the aircraft technical publication based on the maintenance engineering analysis data. By adoption of the method and the device, the compiling efficiency and the content accuracy rate of the technical publication are improved.

Description

Method and device based on maintenance engineering analysis data organization aircraft technology publication
Technical field
The disclosure relates generally to the establishment field of aircraft publication.Particularly, relate to a kind of based on The method of maintenance engineering analysis data organization aircraft technology publication and device thereof.
Background technology
Civil aircraft technical publications is the important component part of civil aircraft customer service, is to protect Barrier aircraft safety runs, the basis of continuing airworthiness, the operation of modern civil aircraft and maintenance requirement Within the aircraft life. cycle cycle, keep property prevailing for the time being in force and and the aircraft thereof of technical publications content The concordance of configuration states, this core being both by technical publications management and difficult point, be also The basic demand of the civil aviaton's regulations must being fulfilled for.
In recent years, domestic civil aircraft manufacturer was by introducing S1000D standard and building corresponding skill Art publication establishment management system, considerably improves establishment and the management mode of technical publications, Technical publications content compilation efficiency increases, management process specification, and content degree of reusing is high. But, the source data problem of technical publications is the most effectively solved, and especially flies Machine servicing manual (AMM), maintenance project file (MPD), Fault Isolation Manual (FIM) Deng technical publications, it is in the acquisition of source data and utilizes aspect to lack effective approach and hands Section.
Maintenance engineering analysis data are the main source datas of establishment AMM, MPD, FIM, But most domestic civil aircraft model carries out maintenance engineering analysis work the most comprehensively at present, even if few Number model has carried out maintenance engineering analysis work, but maintenance engineering analysis data are published in technology Application in thing compilation process not deeply, is primarily present problems with:
1) the maintenance engineering analysis data effective application system in technical publications is lacked
Although minority civil aircraft model has carried out maintenance engineering analysis work, and achieves maintenance engineering The structuring of analytical data and standardization, but technical publications work out in and utilization not yet in effect Maintenance engineering analysis data, do not set up effective application system, lack maintenance engineering analysis data To the data mapping relations of technical publications with change the mechanism.
2) the life-cycle follow-up mechanism of maintenance engineering analysis data is lacked
The change of maintenance engineering analysis data inevitably results in the change of correlation technique publication, because of The version of maintenance engineering analysis data is effectively followed the tracks of by this, is to ensure that correlation technique publication The important foundation of real-time update.But the work of the technical publications of current domestic main manufacturer is generally Only focus on writing of content, in being not set up life cycle management, maintenance engineering analysis data are carried out The standardization working procedure that record, change are followed the tracks of, the content sources causing Relevant Publications cannot Review, it is judged that technical publications change scope can only rely on experience, both labor intensive, the most easily Produce omission, mistake.This situation has been not suitable with the development of modern civil aircraft customer service Requirement, does not meets the demand of civil aircraft client yet, eventually affects the competitiveness of model.
3) data conversion tools of lack of wisdom realizes maintenance engineering analysis data and goes out to technology The automatic conversion of version thing
Structuring and standardized maintenance engineering analysis data are intelligentized automatic crossover tool Exploitation is had laid a good foundation, but current domestic main manufacturer does not build automatic data Crossover tool, still relies primarily on and manually goes acquisition, copy maintenance engineering analysis data to carry out phase Pass publication establishment, inefficiency, error-prone.
Change the mechanism to the data of technical publications by setting up maintenance engineering analysis data, and open Send out data conversion tools corresponding, can effectively solve problem above, major tuneup maintenance engineering Analytical data application present situation in technical publications, improves the technology such as AMM, MPD and publishes The establishment efficiency of thing and content accuracy rate, have great importance.
Summary of the invention
To this end, the first aspect of the disclosure provides a kind of based on maintenance engineering analysis data organization The method of aircraft technology publication, wherein said aircraft technology publication includes multiple data mould Block, including step: resolve maintenance engineering analysis data to obtain the first data message;Set up institute State the mapping relations of the first data message and the second data message in described data module;According to Transition specification and described mapping relations, be converted to described second data described first data message Information.
In one embodiment, further comprise the steps of: on described second data message, add mark Information, wherein said markup information is used for indicating described second data message and described first data Information is associated.
In one embodiment, further comprise the steps of: whether confirmation the first data message changes, When described first data message changes, point out and described second data message is implemented more Newly.
In one embodiment, maintenance engineering analysis data are being resolved to obtain the first data message Also include before step: described maintenance engineering analysis data are converted to structural data.
The second aspect of the disclosure provides a kind of based on maintenance engineering analysis data organization aircraft The device of technical publications, wherein said aircraft technology publication includes multiple data module, institute Stating device to include: resolution unit, it is used for resolving maintenance engineering analysis data to obtain the first number It is believed that breath;Map unit, it is used for setting up in described first data message and described data module The mapping relations of the second data message;Converting unit, it is for according to transition specification and described Mapping relations, are converted to described second data message described first data message.
In one embodiment, also including: mark unit, it is at described second data letter Add markup information on breath, wherein said markup information be used for indicating described second data message with Described first data message is associated.
In one embodiment, also including: confirmation unit, it is for confirming the first data message Whether change;Tip element, it is for when described first data message changes, Point out and implement to update to described second data message.
In one embodiment, also including: processing unit, it is for dividing described maintenance engineering Analysis data are converted to structural data.
Published based on maintenance engineering analysis data organization aircraft technology by disclosed in this invention Major tuneup maintenance engineering analysis data are existed by the method and device of thing in the application of customer service company Application present situation in technical publications, improves the establishment effect of the technical publications such as AMM, MPD Rate and content accuracy rate, specifically, its application advantage is as follows:
1) based on maintenance engineering analysis data organization technical publications, both specify that in AMM Maintenance procedure part, the Data Source of MPD, FIM, it helps improve these technology and publish The quality of thing.
2) the maintenance engineering analysis data directly application in technical publications is worked out, to maintenance Structure and the content integrity of engineering analysis data serve facilitation, are conducive to advancing civil aircraft In development, maintenance engineering analysis work carries out.
3) by being automatically converted to meet S1000D by structurized maintenance engineering analysis data The data module of 4.1 standards, substantially increases maintenance procedure part, MPD, FIM in AMM The establishment efficiency of these several handbooks and content accuracy rate.
4) maintenance engineering analysis data conversion tools achieves and the maintenance engineering analysis system integration, With the data of online retrieving maintenance engineering analysis system, and phase can be completed according to set transformational rule The data conversion answered, is automatically performed SDI mark simultaneously, both ensure that technical publications Content and the concordance of maintenance engineering analysis data, also improve annotating efficiency and the standard of source data Really rate.
Accompanying drawing explanation
By reading retouching in detail with reference to made non-limiting example is made of the following drawings Stating, the other features, objects and advantages of the disclosure will become more apparent:
Fig. 1 shows compiling based on maintenance engineering analysis data of an embodiment according to the disclosure The method flow diagram of aircraft technology publication processed;
Fig. 2 shows the first data message and second data of an embodiment according to the disclosure The mapping relations table of information;And
Fig. 3 shows compiling based on maintenance engineering analysis data of an embodiment according to the disclosure The apparatus module figure of aircraft technology publication processed.
Detailed description of the invention
In the specific descriptions of following preferred embodiment, by with reference to constituting a disclosure part Appended accompanying drawing.Appended accompanying drawing has been illustrated by way of example the spy being capable of the disclosure Fixed embodiment.The embodiment of example is not intended as the limit all embodiments according to the disclosure. It is appreciated that on the premise of without departing from the scope of the present disclosure, it is possible to use other embodiments, Structural or the amendment of logicality can also be carried out.Therefore, following specific descriptions not limit Property processed, and the scope of the present disclosure is defined by the claims appended hereto.Although additionally, explanation Book describes the step of method in a particular order, but this does not requires that or implies necessary Perform these operations according to this particular order, or have to carry out the most shown operation ability Realizing desired result, on the contrary, the step of description can change execution sequence.Additionally or standby Multiple steps are merged into a step and are performed by selection of land, it is convenient to omit some step, and/or will One step is decomposed into multiple step and performs.
The mentality of designing of the present invention is: carrys out establishment technique based on maintenance engineering analysis data and publishes Thing, and set up the mapping relations of maintenance engineering analysis data and technical publications and change the mechanism, Thus when needs establishment aircraft technology publication, can be according to this mapping relations and changing the mechanism Automatically generate and the technical publications of maintenance engineering analysis data association, wherein can also set up Effective data tracking, when maintenance engineering analysis data change, can point out technology to go out Version thing implements corresponding renewal.Below in conjunction with Fig. 1 in the present invention based on maintenance engineering analysis number Illustrate according to the method for establishment aircraft technology publication.
In step s 102, maintenance engineering analysis data are converted to structural data.
Generally, maintenance engineering analysis data preserve with non-structured data mode, such as, The analytical data of the form record maintenance engineering described with word in word document.This kind of non- Structurized data are unfavorable for implementing data analysis, therefore, execute factually for the ease of logarithm Analyze, first have to these type of non-structured data to be converted to, such as with excel form or its The structurized data that the form of his form preserves.The data preserved with structurized data mode It is easier to extract and analyze, the enforcement of step S104 after being conducive to.
It is appreciated that this step S102 is optional step in the present invention, rather than indispensable step, This step can be omitted in some embodiments.
In step S104, resolve maintenance engineering analysis data to obtain the first data message.
Concrete, implement to resolve to maintenance engineering analysis data, and therefrom obtain establishment aircraft skill At least one data message (the hereinafter referred to as first data message) required for art publication.Example As, work out aircraft maintenance class technical publications time, this publication need record maintenance task, The information such as maintenance step, instrument title, number of tools, maintainer number, therefore can pass through Resolve maintenance engineering analysis data, with obtain with maintenance task, maintenance step, instrument title, The first relevant data messages such as number of tools, maintainer number make for establishment technique publication With.
In step s 106, the first data message and the second data letter in data module are set up The mapping relations of breath.
Generally, aircraft technology publication includes multiple data module, such as, program module, meter Drawing module, fault isolation routine data module etc., modules relates separately to the difference of publication Content.Each data module is respectively provided with at least one data message (the hereinafter referred to as second number It is believed that breath), generally these second data messages and the first data in maintenance engineering analysis data Information is correlated with.In the present invention, based on the first data message in maintenance engineering analysis data with Dependency or corresponding relation between the second data message in the data module of publication, set up two Mapping relations between person.
Fig. 2 shows the first data message and second data of an embodiment according to the disclosure The mapping relations table of information, in wherein maintenance engineering analysis data FMEA " inefficacy confirmation is arranged Execute " content that recorded of data item and the element in publication S1000D The content that "/dmodule/content/faultIsolation/commonInfo/para " is recorded is relative Should.Therefore according to this mapping relations table, when working out S1000D publication, element Content in "/dmodule/content/faultIsolation/commonInfo/para " is based on maintenance " inefficacy confirmation measure " data item in engineering analysis data FMEA.
In step S108, according to transition specification and described mapping relations, described first number It is believed that breath is converted to described second data message.
Concrete, according to the mapping relations obtained in step S106, and go out according to aircraft technology The transition specification of version thing, is converted into the first data message obtained in maintenance engineering analysis data The second data message in aircraft technology publication.Wherein this transition specification defines this second The form of expression of data message, such as, font format, putting in order of data.
In step s 110, described second data message adds markup information, Qi Zhongsuo State markup information for indicating described second data message to be associated with described first data message.
Concrete, described second data message adds markup information to set up the first data letter Breath and the real time correlation of the second data message, in order to when the first number in maintenance engineering analysis data It is believed that when breath changes, can be pointed out timely on this second data message.
In step S112, confirm whether the first data message becomes by this markup information Change, when described first data message changes, point out and described second data message is implemented Update.
Concrete, set one and confirm the cycle, and by this cycle to markup information examinations, To confirm whether this first data message changes, if be detected that change then in step S114 point out data changed and need the data to technical publications to implement to update.
In a specific embodiment renewal of these data be automatically implemented by system or By artificial enforcement.When automatically implementing, if the first data change, system is automatic According to transition specification and described mapping relations, the first new data message is converted to the second data Information.When manually implementing, this first new data message is converted to the second data message Process needs the confirmation through technical staff.
Being appreciated that step S110, S112, S114 are optional steps, in this programme, it is also Not necessarily.
Fig. 3 shows compiling based on maintenance engineering analysis data of an embodiment according to the disclosure Device 300 module map of aircraft technology publication processed, this device 300 includes: processing unit 302, Resolution unit 304, map unit 306, converting unit 308, mark unit 310, confirmation form Unit 312, Tip element 314, its annexation is as shown in Figure 3.Wherein processing unit 302, Mark unit 310, confirmation unit 312, Tip element 314 are optional, rather than necessary.
Processing unit 302 is configured to maintenance engineering analysis data and is converted to structural data.
Generally, maintenance engineering analysis data preserve with non-structured data mode, such as, The analytical data of the form record maintenance engineering described with word in word document.This kind of non- Structurized data are unfavorable for implementing data analysis, therefore, execute factually for the ease of logarithm Analyze, first have to these type of non-structured data to be converted to, such as with excel form or its The structurized data that the form of his form preserves.The data preserved with structurized data mode It is easier to extract and analyze, the parsing of the resolution unit 304 after being conducive to.Upon the transition, 302 structural datas of processing unit send to resolution unit 304.
Resolution unit 304 is configured to resolve maintenance engineering analysis data to obtain the first data letter Breath.
Concrete, maintenance engineering analysis data are implemented to resolve by resolution unit 304, and therefrom obtain Take at least one data message (the hereinafter referred to as first number required for establishment aircraft technology publication It is believed that breath).Such as, when working out the technical publications of aircraft maintenance class, this publication needs Record the information such as maintenance task, maintenance step, instrument title, number of tools, maintainer number, Therefore can by resolve maintenance engineering analysis data, with obtain with maintenance task, maintenance step, The first relevant data messages such as instrument title, number of tools, maintainer number are for establishment skill Art publication uses.Then, 304 the first data messages of resolution unit send to map unit 306。
Map unit 306 is configured to set up the first data message and the second number in data module It is believed that the mapping relations of breath.
Generally, aircraft technology publication includes multiple data module, such as, program module, meter Drawing module, fault isolation routine data module etc., modules relates separately to the difference of publication Content.Each data module is respectively provided with at least one data message (the hereinafter referred to as second number It is believed that breath), generally these second data messages and the first data in maintenance engineering analysis data Information is correlated with.In the present invention, map unit 306 is based in maintenance engineering analysis data Dependency or right between the second data message in the data module of one data message and publication Should be related to, set up mapping relations between the two.Then 306 the first data letters of map unit Breath and these mapping relations send to converting unit 308.
Fig. 2 shows the first data message and second data of an embodiment according to the disclosure The mapping relations table of information, in wherein maintenance engineering analysis data FMEA " inefficacy confirmation is arranged Execute " content that recorded of data item and the element in publication S1000D The content that "/dmodule/content/faultIsolation/commonInfo/para " is recorded is relative Should.Therefore according to this mapping relations table, when working out S1000D publication, element Content in "/dmodule/content/faultIsolation/commonInfo/para " is based on maintenance " inefficacy confirmation measure " data item in engineering analysis data FMEA.
Converting unit 308 is configured to according to transition specification and described mapping relations, described One data message is converted to described second data message, thus generates aircraft technology publication.
Concrete, according to the mapping relations obtained from map unit 306, and according to aircraft skill The transition specification of art publication, obtained in 308 maintenance engineering analysis data of converting unit One data message is converted into the second data message in aircraft technology publication.Wherein this conversion rule Model defines the form of expression of this second data message, such as, font format, the row of data Row order etc..
The most also include: mark unit 310, confirmation unit 312 and Tip element 314.
Mark unit 310 is configured on described second data message add markup information, its Described in markup information be used for indicating described second data message and described first data message phase Association.
Concrete, mark unit 310 adds markup information to build on described second data message Vertical first data message and the real time correlation of the second data message, in order to when maintenance engineering analysis number When the first data message according to changes, can obtain on this second data message in time Prompting.
Confirmation unit 312 is configured to this markup information and confirms whether the first data message is sent out Changing, when described first data message changes, Tip element 314 is pointed out described Second data message is implemented to update.
Concrete, confirmation unit 312 can set a confirmation cycle, and by this cycle to mark Note information examinations, to confirm whether this first data message changes, if be detected that Change, then Tip element 314 points out data to change and needed technical publications Data implement update.
In a specific embodiment renewal of these data be automatically implemented by system or By artificial enforcement.When automatically implementing, if the first data change, system is automatic According to transition specification and described mapping relations, the first new data message is converted to the second data Information.When manually implementing, this first new data message is converted to the second data message Process needs the confirmation through technical staff.
Although the device 300 of this example has been described above being illustrated, but described above One or more unit can merged, separate, rearrange, omit, remove and/or with appoint Where formula is implemented.Further, the unit of example and module can by hardware, software, Firmware and/or any of hardware, software and/or firmware are implemented in combination in.More generally, example Said units in any one can by one or more circuit, programmable processor, Special IC (ASIC), programmable logic device (PLD) and/or field-programmable Logic device (FPLD) etc. realizes.
It is obvious to a person skilled in the art that the disclosure is not limited to above-mentioned one exemplary embodiment Details, and in the case of without departing substantially from the spirit or essential attributes of the disclosure, it is possible to it His concrete form realizes embodiment of the disclosure.Therefore, in any case from the point of view of, all should be by reality Execute example and regard exemplary as, and be nonrestrictive.Additionally, it will be evident that " including " one Word is not excluded for other elements and step, and wording " one " is not excluded for plural number.Device right is wanted The multiple elements asking middle statement can also be realized by an element.The first, the second word such as grade is used Represent title, and be not offered as any specific order.

Claims (8)

1. a method based on maintenance engineering analysis data organization aircraft technology publication, wherein Described aircraft technology publication includes multiple data module, including step:
Resolve maintenance engineering analysis data to obtain the first data message;
Set up reflecting of described first data message and the second data message in described data module Penetrate relation;
According to transition specification and described mapping relations, described first data message is converted to described Second data message.
Method the most according to claim 1, wherein further comprises the steps of:
Adding markup information on described second data message, wherein said markup information is used for referring to Show that described second data message is associated with described first data message.
Method the most according to claim 1, wherein further comprises the steps of:
Confirm whether the first data message changes, when described first data message changes Time, point out and implement to update to described second data message.
Method the most according to claim 1, wherein resolve maintenance engineering analysis data with Also include before obtaining the first data message step:
Described maintenance engineering analysis data are converted to structural data.
5. a device based on maintenance engineering analysis data organization aircraft technology publication, wherein Described aircraft technology publication includes that multiple data module, described device include:
Resolution unit, it is used for resolving maintenance engineering analysis data to obtain the first data message;
Map unit, it is for setting up the in described first data message and described data module The mapping relations of two data messages;
Converting unit, it is for according to transition specification and described mapping relations, described first number It is believed that breath is converted to described second data message.
Device the most according to claim 5, the most also includes:
Mark unit, it is for adding markup information, Qi Zhongsuo on described second data message State markup information for indicating described second data message to be associated with described first data message.
Device the most according to claim 5, the most also includes:
Confirmation unit, it is for confirming whether the first data message changes;
Tip element, it is for when described first data message changes, and prompting is to described Second data message is implemented to update.
Device the most according to claim 5, the most also includes:
Processing unit, it is for being converted to structural data described maintenance engineering analysis data.
CN201610311624.4A 2016-05-12 2016-05-12 Method and device for compiling aircraft technical publication based on maintenance engineering analysis data Pending CN106021380A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111104712A (en) * 2019-12-04 2020-05-05 江西洪都航空工业集团有限责任公司 Method for calculating aircraft configuration effectiveness
CN112347736A (en) * 2020-12-01 2021-02-09 中国商用飞机有限责任公司 Method for converting structured data files relating to civil aviation regulations into word documents

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101216835A (en) * 2007-12-29 2008-07-09 北京大学 Data file conversion method and apparatus
CN101477526A (en) * 2008-12-31 2009-07-08 中兴通讯股份有限公司 Method and system for implementing statistical forms customization
CN101944118A (en) * 2010-09-21 2011-01-12 深圳市佳创视讯技术股份有限公司 Viewer behavior analysis system
CN103678522A (en) * 2013-11-28 2014-03-26 许继电气股份有限公司 Method for acquiring and converting data of metering system of intelligent transformer substation
CN103744949A (en) * 2013-12-31 2014-04-23 金蝶软件(中国)有限公司 Data integrating method and system
CN104657396A (en) * 2013-11-25 2015-05-27 腾讯科技(深圳)有限公司 Data migration method and device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101216835A (en) * 2007-12-29 2008-07-09 北京大学 Data file conversion method and apparatus
CN101477526A (en) * 2008-12-31 2009-07-08 中兴通讯股份有限公司 Method and system for implementing statistical forms customization
CN101944118A (en) * 2010-09-21 2011-01-12 深圳市佳创视讯技术股份有限公司 Viewer behavior analysis system
CN104657396A (en) * 2013-11-25 2015-05-27 腾讯科技(深圳)有限公司 Data migration method and device
CN103678522A (en) * 2013-11-28 2014-03-26 许继电气股份有限公司 Method for acquiring and converting data of metering system of intelligent transformer substation
CN103744949A (en) * 2013-12-31 2014-04-23 金蝶软件(中国)有限公司 Data integrating method and system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111104712A (en) * 2019-12-04 2020-05-05 江西洪都航空工业集团有限责任公司 Method for calculating aircraft configuration effectiveness
CN111104712B (en) * 2019-12-04 2022-12-23 江西洪都航空工业集团有限责任公司 Method for calculating aircraft configuration effectiveness
CN112347736A (en) * 2020-12-01 2021-02-09 中国商用飞机有限责任公司 Method for converting structured data files relating to civil aviation regulations into word documents

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Application publication date: 20161012