CN113743890A - Efficient compiling and maintaining method for airplane system installation operation instruction book - Google Patents
Efficient compiling and maintaining method for airplane system installation operation instruction book Download PDFInfo
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Abstract
The invention discloses a method for efficiently compiling and maintaining an installation operation instruction book of an aircraft system, which comprises the following steps: 1) forming a standardized operation library; 2) forming an association rule base of the standard operation unit and the material information based on the material information; 3) forming an auxiliary information base which is simultaneously associated with the standard operation unit and the material information by taking the material information as a basis; 4) grouping core materials to form a material bag; 5) and collecting various information to generate an aircraft system operation instruction book. According to the invention, a large amount of engineering experience is summarized, refined and converted into corresponding material feature codes, standard operation and auxiliary information association rules, effective multiplexing of the engineering experience, the standard operation and the auxiliary information is realized through a single information source, description/expression of unified information is achieved, the compiling consistency and the information transmission efficiency are improved, and the compiling of an aircraft system operation instruction book and batch maintenance can be efficiently completed.
Description
Technical Field
The invention relates to the technical field of complex mechanical system assembly, in particular to an efficient compiling and maintaining method of an aircraft system installation operation instruction book.
Background
In the final assembly stage, the airplane mainly works as follows: and arranging a large number of system accessories such as wire harnesses, pipelines, electric finished products and the like in a limited space, and carrying out system functional tests. The airplane general assembly stage work is mainly operated manually due to the operation complex environment. During operation, a great deal of operation information and auxiliary information need to be provided for operators to support implementation of specific operation work of the operators, and an aircraft system installation operation instruction is an operation object and relevant operation and auxiliary information carriers thereof.
The aircraft system installation and operation instruction book generally consists of a series of operation and auxiliary information, and the information comprises information of multiple dimensions such as materials/materials, operation method descriptions, measurement requirements, skill requirements, instrument requirements and the like. The existing weaving mode is as follows: a programmer refers to design technical requirements, three-dimensional digital models, related engineering requirements and specifications, combines engineering experience and judgment, and combines and describes related information in different channels, different carriers and experience according to personal language habits to form an operation guidance information set, namely an airplane system installation operation guide book.
The aircraft system installation operation instruction formed by the existing compiling method has the following main problems: 1) a large amount of engineering experience is required in the compiling process, so that the compiling quality stability is poor and the efficiency is low; 2) information expression is not standardized, and description/expression of different people in the same information is not uniform, so that operation and auxiliary information are difficult to quickly and accurately understand; 3) information is scattered and mixed, a clear association relation is not established, information needs to be collected manually, and the information is difficult to be effectively recycled and maintained in batches, so that the installation operation instruction book of the aircraft system cannot be standardized and rapidly compiled and maintained.
Disclosure of Invention
The invention aims to solve the problems that the stability of compiling quality is poor, the efficiency is low, the uniformity of information is poor, the reutilization and the batch maintenance are difficult and the standardized and rapid compiling and maintaining can not be realized due to the fact that the height of engineering experience is depended on, the information expression is not standardized and the incidence relation between information is not clear in the compiling process of the existing aircraft system installation operation guide book, and provides a method for supporting the rapid reutilization and the batch maintenance of standardized information and realizing the standardized and rapid compiling and maintaining of the aircraft system installation operation guide book by standardizing operation and auxiliary information and establishing the association rule among material feature codes, the standard operation and the auxiliary information.
The invention is realized by the following technical scheme: an efficient compiling and maintaining method for an aircraft system installation operation instruction comprises the following steps:
(1) dividing the same type of operation of the aircraft system into coherent standard operation units with logical relationship, and collecting and arranging the standard operation units according to the logical rules of the operation flow to form a standardized operation library;
(2) confirming standard operation unit information required by the material based on the material information, associating the material information with the corresponding standard operation unit, and arranging according to the arrangement rule of the standard tapered operation library to form an association rule library of the standard operation unit and the material information;
(3) confirming auxiliary information required by the material under certain standard operation unit information by taking the material information as a basis, and associating the material information, the corresponding standard operation unit and the corresponding auxiliary information to form an auxiliary information base simultaneously associated with the standard operation unit and the material information;
(4) grouping core materials, surrounding the core materials, and listing auxiliary zero accessory relevance of the core materials to form a material package;
(5) and collecting various information to generate an aircraft system operation instruction book based on the standardized operation library, the association rule library of the standard operation unit and the material information, the auxiliary information library which is simultaneously associated with the standard operation unit and the material information, and the material bag.
The principle of the technical scheme is that standard operation is constructed to form a standard operation unit of the airplane system; establishing association rules of the standard operation and the material feature codes to form a contrast index relationship between the standard operation and the material feature codes; constructing auxiliary information associated with the standard operation/material characteristic code to form a plurality of dimensionality auxiliary information specific contents corresponding to the standard operation/material characteristic code; collecting the standard operation and the auxiliary information according to the material coding information provided by the material packet; and finally, arranging according to the standard operation logic sequence to form an aircraft system operation instruction book. According to the method for compiling the aircraft system operation instruction book based on the material feature codes, the operation object, the standard operation and the auxiliary information are clearly associated and defined through the association rules among the material feature codes, the standard operation and the auxiliary information, so that the aircraft system operation instruction book is efficiently compiled and maintained through the quick and effective multiplexing and simplification of information sources.
To better implement the method of the invention, further, the standard operation unit is composed of a series of consecutive standard actions, and can complete a certain part of work in a task.
To better implement the method of the present invention, further, the material information is at least one of a material code, a three-dimensional material digital model, and a material name.
In order to better implement the method of the present invention, further, the material code is a group of numbers formed according to engineering rules and composed of letters and numbers, and specifically includes a material feature code, and the material feature code is a field in the material code which uniquely represents a category or typical process features to which the material belongs.
In order to better implement the method of the present invention, the auxiliary information contained in the auxiliary information base is specifically specific information of at least one dimension of materials, operating method descriptions, measurement requirements, skill requirements, and mechanical information required by the materials corresponding to each standard operation.
In order to better implement the method of the present invention, further, the material bag in the step (4) is an information set composed of at least two groups of information in material sequence, material code, material name, quantity, and material assembly drawing number.
In order to better implement the method of the present invention, further, the core material in the step (4) is at least one of a part, a wire harness, a mechanical finished product and an electrical finished product in the material, which determines the order before and after assembly.
In order to better implement the method of the present invention, further, in step (5), the specific process of generating the aircraft system operation instruction book is as follows:
(5.1) obtaining material information of all materials in the material bag through the material bag;
(5.2) forming a specific standard operation unit and a material information base in the aircraft system operation guide book by combining the association rule base according to the material information obtained in the step (5.1);
(5.3) screening out an operation method description and specific auxiliary information of at least one dimension of measurement requirements, skill requirements and instrument information from the auxiliary information base by inputting the standard operation unit and the material information base acquired in the step (5.2), and realizing the expansion of the auxiliary information based on the standard operation unit and the material information base;
and (5.4) sequentially arranging according to the standard operation logic sequence in the standard operation units and the material information base to form an operation sequence, sequentially connecting each standard operation unit and the auxiliary information thereof in series to obtain each item of specific auxiliary information, and further forming an aircraft system operation instruction book.
Compared with the prior art, the invention has the following advantages and beneficial effects:
(1) according to the invention, a large amount of engineering experience is summarized and refined, and is converted into corresponding material feature codes, standard operation and auxiliary information association rules, so that the dependence on the engineering experience in the establishment of an aircraft system operation instruction book is reduced, and the stability and efficiency of the establishment quality are improved;
(2) the invention realizes the effective reuse of engineering experience, standard operation and auxiliary information by simplifying the information source, achieves the description/expression of unified information, and improves the compiling consistency and the information transmission efficiency;
(3) by simplifying the information source, the effective reuse of engineering experience, standard operation and auxiliary information is realized, and the compiling of the operation instruction book of the airplane system and the batch maintenance can be efficiently completed.
Detailed Description
In the embodiment of the present invention, a pipeline of a certain system on an aircraft is taken as an example to clearly and completely describe the technical solution in the embodiment of the present invention, and obviously, the described embodiment is only a part of the embodiment of the present invention, but not all embodiments, and specific contents of each information base of different products and different projects will be different.
Example 1:
the embodiment provides an efficient compiling and maintaining method for an aircraft system installation operation instruction book, which comprises five parts, namely standard operation construction, standard operation and material characteristic code association rule construction, auxiliary information construction associated with the standard operation/material characteristic code, material bag construction and aircraft system operation instruction book generation.
The standard operation construction is a process of dividing the same type of operation of an aircraft system into a series of standardized consecutive operation units with logical relationship according to a certain engineering principle, wherein the formed standardized operation units are standard operations which are collected into a standardized operation library;
the standard operation is composed of a series of continuous standard actions and can complete a certain part of work in a task;
the same type of operation of the aircraft system is different systems, but the operation is similar, and the whole operation process from material acquisition to operation completion and qualified quality inspection consists of a series of standard operations with logical relations;
the standard operation and material characteristic code association rule construction is based on information such as material codes, three-dimensional digital models or material names, the type of materials is judged, typical process characteristics are determined, the process of standard operation required by the materials is confirmed, the standard operation and material characteristic code association rules are uniformly identified, summarized and defined, and the association rules are arranged according to the established logic sequence of the standard operation, so that a standard operation and material characteristic code association rule base can be formed;
the association rule between the standard operation and the material feature code is substantially a comparison index relation between the standard operation and the material feature code;
the material feature code is a field which only represents the class or typical process feature of the material in the material code;
the material codes are a group of numbers formed according to engineering rules and composed of letters and numbers, such as AT221T0 LK-001;
the construction of the auxiliary information associated with the standard operation/material characteristic code is based on information such as material codes, three-dimensional digital models or material names, the class of materials is judged, typical process characteristics are determined, the process of specific auxiliary information required by the materials under certain standard operation is further confirmed, and the auxiliary information is uniformly identified, summarized and defined as various auxiliary information associated with the standard operation/material characteristic code to form various auxiliary information bases, including specific information bases with multiple dimensions such as materials, operation method descriptions, measurement requirements, skill requirements and instruments;
the auxiliary information associated with the standard operation/material feature code is a contrast index relation between each item of auxiliary information and the combined information of two fields of the standard operation/material feature code;
the auxiliary information is the specific information of multiple dimensions such as materials/materials, operation method descriptions, measurement requirements, skill requirements, instruments and the like required by the materials corresponding to each standard operation;
the operation method description information is detailed description/requirement information for further decomposing actions of standard operations;
the measurement requirement information is information which is required to be fed back through actual measurement after corresponding standard operation is completed, and comprises information such as measurement instruction, actual measurement data and the like;
the skill requirement information is the technical capability requirement required for completing corresponding standard operation, and comprises information such as work type, skill level, certificate of acceptance and the like;
the instrument information is information such as auxiliary tools, tools and equipment required for completing corresponding standard operation, and comprises information such as serial numbers, names, quantities and operation descriptions of instruments;
the material package construction is a process of distributing a group of materials of the aircraft system to a certain aircraft system installation operation instruction book according to a certain engineering principle: surrounding the core material, listing the auxiliary zero accessory relevance of the core material;
the material bag is an information set consisting of information such as material sequence, material codes, material names, quantity, material assembly drawing numbers and the like;
the core material is a part/wire harness/mechanical finished product/electrical finished product and the like which determine the sequence before and after assembly in the material;
the material assembly drawing number is a group of unique numbers consisting of letters and numbers formed according to engineering rules, is a three-dimensional digital model unit formed in the design process of the airplane, and comprises single or multiple core materials, auxiliary zero accessories of the core materials, part of design requirement description information and the like;
and finally, automatically generating an aircraft system operation instruction book based on the standard operation and material characteristic code association rule base, the auxiliary information base and the material bag, and collecting various information to form the aircraft system operation instruction book, wherein the specific method comprises the following steps:
1) acquiring a material code:
constructing a formed material bag through the material bag, and acquiring all material codes of the task;
2) obtaining standard operation and corresponding material/material information:
taking the material code formed in the step 1) as input, traversing the material feature code in the standard operation and material feature code association rule base, screening out the standard operation of which the material code accords with the material feature code, and associating the material code of which the material code accords with the material feature code with the corresponding standard operation to form specific standard operation and material/material information in the aircraft system operation instruction book, namely a standard operation/material code information base;
3) obtaining operating method description information
Taking the standard operation/material coding information set formed in the step 2) as input, traversing the standard operation/material feature codes in the operation method description information base, screening out corresponding operation method description information of which the standard operation/material codes conform to the standard operation/material feature codes, and associating the operation method description information with the corresponding standard operation/material codes to form specific operation method description information in the aircraft system installation operation instruction book;
4) obtaining measurement requirements, skill requirements and other ancillary information such as instruments
Repeating the step 3), and only replacing the operation method description information base in the step 3) with other auxiliary information bases such as corresponding measurement requirements, skill requirements and instruments, and the like to form specific other auxiliary information in the aircraft system operation guide book; other auxiliary information bases can be established based on the standard operation/material feature codes according to actual engineering requirements, and information expansion is achieved;
5) information is collected to form an aircraft system operation instruction information set
And (3) sequentially arranging according to a standard operation logic sequence in a standard operation and material feature code association rule base to form an operation sequence, and sequentially connecting each standard operation and auxiliary information thereof in series by combining each item of specific auxiliary information formed in the steps 2) -4) to form an aircraft system operation instruction book.
Example 2:
the embodiment provides a specific operation example for the efficient compiling and maintaining method of the aircraft system installation operation instruction book provided by the embodiment, and the specific operation example comprises the following steps:
first step S11: constructing standard operation;
the method comprises the following steps that engineering technicians divide the whole process of pipeline operation of a certain system of an airplane into a plurality of standardized operation units with logical relations according to a certain engineering principle and by combining engineering experience, standard pipeline operation of the certain system in the embodiment forms a standard operation library shown in the specification, and the standard operation library is listed in sequence according to the mutual operation logical relations, wherein the sequence number represents a standard operation sequence;
TABLE 1 Standard operation library
| Serial number | Standard operation |
| 1 | Material receiving |
| 2 | Pipeline installation |
| 3 | Lap resistance measurement |
| 4 | Safety anti-loose device |
| 5 | Quality inspection |
| … | … |
Second step S12: building a standard operation and material feature code association rule;
judging the class of the material according to information such as a material feature code, a material three-dimensional digital model, a material name and the like, determining typical process features of the material, confirming a process of standard operation required by the material, uniformly identifying, summarizing and defining the standard operation and the material feature code association rule, and forming a comparison index relation between the standard operation and the material feature code, wherein a 'material feature code' field consists of partial material coding fields and default symbols ', and only the default symbols' indicate that the standard operation is applicable to all material codes;
TABLE 2 Association rule base of standard operation and material feature code
Third step S13: constructing auxiliary information associated with the standard operation/material feature code;
carrying out classification compilation on reference information and engineering experience such as design technical requirements, three-dimensional digital models, related engineering requirements and specifications and the like according to multiple dimensions such as operation method description, measurement, skills, instruments and the like; the method comprises the steps of judging the category of a material according to information such as material codes, three-dimensional digital models or material names, determining typical process characteristics of the material, confirming the process of specific auxiliary information required by the material under certain standard operation, uniformly identifying, summarizing and defining the process as various auxiliary information associated with standard operation/material characteristic codes, and forming various auxiliary information bases comprising specific information bases with multiple dimensions such as materials, operation method descriptions, measurement requirements, skill requirements and instruments;
the following table 3 shows the operation method description information base:
TABLE 3 operating method description information base
The following table 4 shows the measurement requirement information base:
TABLE 4 measurement request information base
The skill requirement information base is shown in table 5 below:
TABLE 5 skill requirement information Bank
The instrument information library is shown in table 6 below:
TABLE 6 Instrument information base
Note that: in tables 3 to 6, except that "standard operation" and "material feature code" are mandatory fields, other column information is automatically divided according to actual engineering, and only the column information is not limited.
Fourth step S14: constructing a material bag;
according to the principle of the airplane engineering, a group of materials of an airplane system are distributed into an airplane system operation instruction book, the core materials are surrounded, zero accessory relevance is assisted, the material packages are information sets formed by information such as material sequence, material codes, material names, quantity, material assembly drawing numbers and the like, in order to explain that the method effectively reuses the information, 2 material packages are established in the step and are named as a material package AT-221-01 and a material package AT-221-02 respectively;
the material package AT-221-01 is shown in Table 7 below:
TABLE 7 Material packet AT-221-01
The material bag AT-221-02 is shown in the following table 8:
TABLE 8 Material bags AT-221-02
Fifth step S15: generating an aircraft system operation instruction;
1) acquiring a material code:
acquiring all material codes of the task through material packages AT-221-01 and AT-221-02 formed in the fourth step S14;
the material bag AT-221-01 comprises material codes: AT221T0LK-002, AT221T0LP-002 and HB 4-4-32;
the material bag AT-221-02 comprises material codes: AT221T0LL-002, AT22110LL-002, HB4-4-32 and AT422LBF 34;
2) obtaining standard operation and corresponding material/material information:
taking the material code formed in the step 1) as input, traversing the material feature code in the table 2 standard operation and material feature code association rule base, and screening out the standard operation of which the material code meets the material feature code; and associating the material codes meeting the material characteristic codes with corresponding standard operations to form material/material information, namely a standard operation/material code information base, which is specifically exemplified as follows:
material bag AT-221-01:
AT221T0LK-002, AT221T0LP-002 and HB4-4-32 are used as input, respectively traversing ' material feature codes ' in a table 2 standard operation and material feature code association rule base ', screening out standard operations, filling material codes of which the material codes accord with the material feature codes into corresponding standard operations, and forming a standard operation/material code information base as the following table 9:
TABLE 9 Material packet AT-221-01 Standard operation/Material coding information base
Material bag AT-221-02:
AT221T0LL-002, AT22110LL-002, HB4-4-32 and AT422LBF34 are used as input, respectively traverse the material feature codes in the standard operation and material feature code association rule base of table 2 to screen out the standard operation, and fill the material codes of the material code and material feature code into the corresponding standard operation to form the standard operation/material code information base as the following table 10:
TABLE 10 Material packet AT-221-02 Standard operation/Material coding information base
3) Obtaining operating method description information
Taking the standard operation/material coding information base formed in the step 2) as input, traversing the standard operation/material feature codes in the operation method description information base in the table 3, screening out corresponding operation method description information of which the standard operation/material codes conform to the standard operation/material feature codes, and associating the operation method description information with the corresponding standard operation/material codes to form specific operation method description information in an airplane system operation instruction book, wherein the specific example is as follows:
material bag AT-221-01:
by taking the 'material bag AT-221-01 standard operation/material coding information base of table 9 as input, traversing the' standard operation/material characteristic code 'in the' operation method description information base of table 3, screening out the corresponding operation method description information of 'standard operation/material coding' conforming to the 'standard operation/material characteristic code', and associating the operation method description information with the corresponding standard operation/material coding to form the operation method description information as the following table 11:
TABLE 11 material packet AT-221-01 operating method instruction information
Material bag AT-221-02:
by taking the 'material bag AT-221-02 standard operation/material coding information base of table 10 as input, traversing the' standard operation/material characteristic code 'in the' operation method description information base of table 3, screening out the corresponding operation method description information of 'standard operation/material coding' conforming to the 'standard operation/material characteristic code', and associating the operation method description information with the corresponding standard operation/material coding to form the operation method description information as the following table 12:
TABLE 12 material packet AT-221-02 operating method instruction information
4) Obtaining measurement requirements, skill requirements and other ancillary information such as instruments
And repeating the step 3), replacing the operation method description information base in the step 3) with other auxiliary information bases such as corresponding measurement requirements, skill requirements, instruments and the like, namely forming other specific auxiliary information in an operation instruction book of a certain aircraft system, and creating other auxiliary information bases based on standard operation/material feature codes according to actual engineering requirements to realize information expansion. Specific examples are as follows:
material bag AT-221-01:
by taking a standard operation/material coding information base AT-221-01 of a material bag in a table 9 as input, traversing a standard operation/material characteristic code in a measurement information base in a table 4, screening out corresponding measurement requirement information of which the standard operation/material code accords with the standard operation/material characteristic code, and associating the measurement requirement information with the corresponding standard operation/material code to form measurement removal information as shown in the following table 13:
TABLE 13 Material bag AT-221-01 measurement request information
By taking a 'material bag AT-221-01 standard operation/material coding information base' in a table 9 as input, traversing 'standard operation/material characteristic codes' in a 'skill information base' in a table 5, screening out corresponding skill requirement information of 'standard operation/material coding' conforming to 'standard operation/material characteristic codes', and associating the skill requirement information with the corresponding standard operation/material coding to form the skill requirement information as shown in the following table 15:
TABLE 15 material packet AT-221-01 skill requirement information
Using a standard operation/material coding information base AT-221-01 of a material package in a table 9 as input, traversing a standard operation/material feature code in an instrument information base in a table 6, screening out corresponding instrument information of which the standard operation/material code accords with the standard operation/material feature code, and associating the instrument information with the corresponding standard operation/material code to form the instrument information as shown in the following table 17:
TABLE 17 materiel bag AT-221-01 Instrument information
Material bag AT-221-02:
by taking the 'material bag AT-221-02 standard operation/material coding information base' of the table 10 as input, traversing the 'standard operation/material characteristic code' in the 'measurement information base' of the table 4, screening out the corresponding measurement requirement information of which the 'standard operation/material code' meets the 'standard operation/material characteristic code', and associating the measurement requirement information with the corresponding standard operation/material code to form the measurement requirement information as the following table 14:
TABLE 14 measurement request information for material bags AT-221-02
By taking a table 10 material bag AT-221-02 standard operation/material coding information base as input, traversing standard operation/material characteristic codes in a table 5 skill information base, screening out corresponding skill requirement information of which the standard operation/material codes meet the standard operation/material characteristic codes, and associating the skill requirement information with the corresponding standard operation/material codes to form the following table 16:
TABLE 16 material packet AT-221-02 skill requirement information
By taking the 'material bag AT-221-02 standard operation/material coding information base' of table 10 as input, traversing the 'standard operation/material feature code' in the 'instrument information base' of table 6, screening out the corresponding instrument information of which the 'standard operation/material code' meets the 'standard operation/material feature code', and associating the instrument information with the corresponding standard operation/material code to form the instrument information as shown in the following table 18:
TABLE 18 materiel package AT-221-02 apparatus information
5) Information is collected to form an aircraft system operation instruction information set
And taking a standard operation/material coding information base as an index, sequentially collecting each item of specific auxiliary information formed in the steps 2) to 4), and then forming an aircraft system operation instruction book, wherein specific examples are as follows:
material bag AT-221-01: taking a standard operation/material coding information base of a material bag AT-221-01 in the table 9 as an index, sequentially arranging all auxiliary information to form an operation sequence, combining each item of specific auxiliary information formed in the steps 2-4), sequentially connecting all standard operations and the auxiliary information in series to form an operation instruction of the material bag AT-221-01, as shown in the following table 19:
TABLE 19 material packet AT-221-01 operating instruction information set
Material bag AT-221-02: taking a standard operation/material coding information base of the material package AT-221-02 in the table 10 as an index, sequentially arranging all auxiliary information to form an operation sequence, combining each item of specific auxiliary information formed in the step 2) -4), sequentially connecting all standard operations and the auxiliary information in series to form an operation instruction book of the material package AT-221-02, as shown in the following table 20:
TABLE 20 Material packet AT-221-01 operating instruction information set
While embodiments of the invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.
Claims (8)
1. An efficient compiling and maintaining method for an aircraft system installation operation instruction is characterized by comprising the following steps:
(1) dividing the same type of operation of the aircraft system into coherent standard operation units with logical relationship, and collecting and arranging the standard operation units according to the logical rules of the operation flow to form a standardized operation library;
(2) confirming standard operation unit information required by the material based on the material information, associating the material information with the corresponding standard operation unit, and arranging according to the arrangement rule of the standard tapered operation library to form an association rule library of the standard operation unit and the material information;
(3) confirming auxiliary information required by the material under certain standard operation unit information by taking the material information as a basis, and associating the material information, the corresponding standard operation unit and the corresponding auxiliary information to form an auxiliary information base simultaneously associated with the standard operation unit and the material information;
(4) grouping core materials, surrounding the core materials, and listing auxiliary zero accessory relevance of the core materials to form a material bag;
(5) and collecting various information to generate an aircraft system operation instruction book based on the standardized operation library, the association rule library of the standard operation unit and the material information, the auxiliary information library which is simultaneously associated with the standard operation unit and the material information, and the material bag.
2. The method of claim 1, wherein the standard operating unit comprises a series of consecutive standard actions that can perform a portion of a task.
3. The method for efficient compiling and maintaining of the aircraft system installation operation instruction book according to claim 1 or 2, wherein the material information is at least one of a material code, a three-dimensional digital model of the material, and a material name.
4. The method for efficient compiling and maintaining of the aircraft system installation operation instruction book according to claim 3, wherein the material code is a group of numbers formed by engineering rules and composed of letters and numbers, and specifically comprises a material feature code, and the material feature code is a field in the material code which uniquely represents the class or typical process features of the material.
5. The method for efficiently compiling and maintaining the installation and operation instruction manual of the aircraft system according to claim 4, wherein the auxiliary information included in the auxiliary information base is specific information of at least one dimension of materials, operation method descriptions, measurement requirements, skill requirements and instrument information required by the materials to complete each standard operation.
6. The method for efficient compiling and maintaining of the aircraft system installation operation instruction book according to claim 5, wherein the material bags in the step (4) are information sets consisting of at least two groups of information of material sequence, material code, material name, quantity and material assembly drawing number.
7. The method for efficient compiling and maintaining of aircraft system installation operation instructions according to claim 6, wherein the core material in the step (4) is at least one of a part, a wiring harness, a mechanical finished product and an electrical finished product in the material, which determines the sequence of assembly.
8. The method for efficiently compiling and maintaining the aircraft system installation operation instruction book according to claim 7, wherein in the step (5), the specific process of generating the aircraft system operation instruction book is as follows:
(5.1) obtaining material information of all materials in the material bag through the material bag;
(5.2) forming a specific standard operation unit and a material information base in the aircraft system operation instruction book by combining the association rule base according to the material information obtained in the step (5.1);
(5.3) the standard operation unit and the material information base acquired in the step (5.2) are not input, an operation method description and specific auxiliary information of at least one dimension of measurement requirements, skill requirements and instrument information are screened from the auxiliary information base, and the expansion of the auxiliary information is realized based on the standard operation unit and the material information base;
and (5.4) sequentially arranging according to the standard operation logic sequence in the standard operation units and the material information base to form an operation sequence, and sequentially connecting each standard operation unit and the auxiliary information thereof in series to form an aircraft system operation instruction book.
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