CN114757157A - Method, apparatus, device and medium for generating aircraft work package - Google Patents

Method, apparatus, device and medium for generating aircraft work package Download PDF

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CN114757157A
CN114757157A CN202210676898.9A CN202210676898A CN114757157A CN 114757157 A CN114757157 A CN 114757157A CN 202210676898 A CN202210676898 A CN 202210676898A CN 114757157 A CN114757157 A CN 114757157A
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work
aircraft
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CN114757157B (en
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杨宾
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Beijing Hantuan Technology Co ltd
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Beijing Hantuan Technology Co ltd
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    • G06F40/00Handling natural language data
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    • G06F40/166Editing, e.g. inserting or deleting
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
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    • G06Q10/20Administration of product repair or maintenance

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Abstract

Embodiments of the present disclosure disclose methods, apparatus, electronic devices, and computer-readable media for generating an aircraft work package. One embodiment of the method comprises: acquiring target aircraft maintenance manual information; determining a target tool kit from the model tool kit according to the target maintenance manual information; selecting a first single aircraft card from a target work package according to the target aircraft information; generating a second single machine work card according to the target maintenance manual; and generating a target aircraft work package according to the first stand-alone work card and the second stand-alone work card. The implementation method enables the generated work package to better meet the needs of maintenance personnel, improves the working efficiency and the use experience of users, and reduces the possibility of errors.

Description

Method, apparatus, device and medium for generating aircraft work package
Technical Field
Embodiments of the present disclosure relate to the field of computer technology, and in particular, to a method, an apparatus, an electronic device, and a computer-readable medium for generating an aircraft work package.
Background
The aircraft maintenance manual is a very important work guiding material in the maintenance process and is also a main basis for aircraft maintenance operation. The aircraft service manual provides the maintenance content, the maintenance range and the aviation material resource requirement in the operation process.
The traditional aircraft maintenance worker card can only refer to an aircraft maintenance manual for repeated manual input and make modification adjustment or directly input maintenance numbers in the aircraft maintenance manual in a card editing stage, in addition, the effect difference between preview effect and the actual maintenance of executive personnel is large, and when other worker card numbers are referred in the content of the worker card, the corresponding numbers need to be manually searched in the whole aircraft maintenance manual, and printing and checking are carried out. The work content is extremely cumbersome and inefficient for the maintenance personnel, and in the case of aircraft, there are considerable safety risks and extremely expensive work costs in the event of a fault.
Disclosure of Invention
This summary is provided to introduce a selection of concepts in a simplified form that are further described below in the detailed description. This summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter.
Some embodiments of the present disclosure propose methods, apparatuses, electronic devices and computer readable media for generating an aircraft work package to solve the technical problems mentioned in the background section above.
In a first aspect, some embodiments of the present disclosure provide a method for generating an aircraft work package, the method comprising: acquiring target aircraft maintenance manual information, wherein the target aircraft maintenance manual information comprises a target maintenance manual, target aircraft information and target maintenance manual information; determining a target tool kit from the model tool kit according to the target maintenance manual information; selecting a first single machine work card from the target work packet according to the target aircraft information; generating a second single machine work card according to the target maintenance manual; and generating a target aircraft work package according to the first single machine work card and the second single machine work card.
In a second aspect, some embodiments of the present disclosure provide an apparatus for generating an aircraft bag, the apparatus comprising: an acquisition unit configured to acquire target aircraft service manual information, wherein the target aircraft service manual information includes a target service manual, target aircraft information, and target service manual information; a determination unit configured to determine a target tool pack from the model tool pack according to the target service manual information; the selecting unit is configured to select a first stand-alone work card from the target work package according to the target aircraft information; a first generating unit configured to generate a second stand-alone work card according to the target service manual; and a second generating unit configured to generate a target aircraft work package according to the first standalone work card and the second standalone work card.
In a third aspect, an embodiment of the present application provides an electronic device, where the network device includes: one or more processors; storage means for storing one or more programs; when executed by one or more processors, cause the one or more processors to implement a method as described in any implementation of the first aspect.
In a fourth aspect, the present application provides a computer-readable medium, on which a computer program is stored, which, when executed by a processor, implements the method as described in any implementation manner of the first aspect.
One of the above various embodiments of the present disclosure has the following beneficial effects: firstly, obtaining target aircraft maintenance manual information, then determining a target work package from a model work package, then selecting a first stand-alone work card from the target work package, then generating a second stand-alone work card according to the target maintenance manual, and finally generating the target aircraft work package according to the first stand-alone work card and the second stand-alone work card. Therefore, the generated work package can better meet the needs of maintenance personnel, the working efficiency and the use experience of a user are improved, and the possibility of errors is reduced.
Drawings
The above and other features, advantages, and aspects of embodiments of the present disclosure will become more apparent by referring to the following detailed description when taken in conjunction with the accompanying drawings. Throughout the drawings, the same or similar reference numbers refer to the same or similar elements. It should be understood that the drawings are schematic and that elements and components are not necessarily drawn to scale.
FIG. 1 is a schematic illustration of one application scenario for a method of generating an aircraft work package, in accordance with some embodiments of the present disclosure;
FIG. 2 is a flow diagram of some embodiments of a method for generating an aircraft kit according to the present disclosure;
FIG. 3 is a schematic block diagram of some embodiments of an apparatus for generating an aircraft bag according to the present disclosure;
FIG. 4 is a schematic block diagram of an electronic device suitable for use in implementing some embodiments of the present disclosure.
Detailed Description
Embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While certain embodiments of the present disclosure are shown in the drawings, it is to be understood that the disclosure may be embodied in various forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided for a more thorough and complete understanding of the present disclosure. It should be understood that the drawings and embodiments of the disclosure are for illustration purposes only and are not intended to limit the scope of the disclosure.
It should be noted that, for convenience of description, only the portions related to the present invention are shown in the drawings. The embodiments and features of the embodiments in the present disclosure may be combined with each other without conflict.
It should be noted that the terms "first", "second", and the like in the present disclosure are only used for distinguishing different devices, modules or units, and are not used for limiting the order or interdependence of the functions performed by the devices, modules or units.
It is noted that references to "a" or "an" in this disclosure are intended to be illustrative rather than limiting, and that those skilled in the art will appreciate that references to "one or more" are intended to be exemplary and not limiting unless the context clearly indicates otherwise.
The names of messages or information exchanged between devices in the embodiments of the present disclosure are for illustrative purposes only, and are not intended to limit the scope of the messages or information.
The present disclosure will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Fig. 1 is a schematic illustration of one application scenario of a method for generating an aircraft work package, in accordance with some embodiments of the present disclosure.
As shown in fig. 1, the executive body server 101 may obtain target aircraft service manual information 102, specifically, the target aircraft service manual information 102 includes a target service manual 103, target aircraft information 105, and target service manual information 107. Thereafter, an object kit 106 is identified from the model kit 104 based on the object service manual information 103. Then, a first standalone tooling card 109 is selected from the target package 106 according to the target aircraft information 105. Next, a second stand-alone work card 108 is generated based on the target service manual 107. Finally, a target aircraft package 110 is generated from the first standalone service card 109 and the second standalone service card 108.
It is understood that the method for generating the aircraft work package may be executed by a terminal device, or may also be executed by the server 101, and an execution subject of the method may also include a device formed by integrating the terminal device and the server 101 through a network, or may also be executed by various software programs. The terminal device may be various electronic devices with information processing capability, including but not limited to a smart phone, a tablet computer, an e-book reader, a laptop portable computer, a desktop computer, and the like. The execution body may also be embodied as the server 101, software, or the like. When the execution subject is software, the software can be installed in the electronic device listed above. It may be implemented, for example, as multiple software or software modules to provide distributed services, or as a single software or software module. And is not particularly limited herein.
It should be understood that the number of servers in fig. 1 is merely illustrative. There may be any number of servers, as desired for implementation.
With continued reference to fig. 2, a flow 200 of some embodiments of a method of generating an aircraft crew according to the present disclosure is shown. The method for generating the aircraft work package comprises the following steps:
Step 201, obtaining the information of the target aircraft maintenance manual.
In some embodiments, the executing agent (e.g., the server shown in fig. 1) of the method for generating an aircraft kit may obtain the target aircraft service manual information via a wired connection or a wireless connection. It should be noted that the wireless connection means may include, but is not limited to, a 3G/4G connection, a WiFi connection, a bluetooth connection, a WiMAX connection, a Zigbee connection, a uwb (ultra wideband) connection, and other wireless connection means now known or developed in the future.
Specifically, the target aircraft manual information includes a target service manual, target aircraft information, and target service manual information. Here, the target service manual generally refers to a manual for instructing how to perform service on the target aircraft. The target aircraft information is generally information of the target aircraft, and includes a model, a shipment time, a manufacturing company, and the like. The target service manual information is generally information of the target service manual. The target service manual information may be, for example, a model corresponding to the target service manual, a change record, or the like. Here, the target aircraft is generally an aircraft designated by a user.
In some optional implementation manners of some embodiments, the executing body may further detect whether a target kit exists in the model kit according to the target aircraft information. As an example, the execution subject may search whether or not a target package exists in the model packages using model information in the target aircraft information.
And responding to the condition that the target tool pack is not detected in the machine tool pack, and performing structured splitting on the target maintenance manual to obtain at least one tool card. Specifically, the structural splitting generally refers to a manner of splitting the target service manual according to types. As an example, the type of the above-described split may be a part type, a part position type, or the like.
And generating a target work package according to the at least one work card, and adding the target work package into the model work package. As an example, the execution subject may merge the at least one work card into one set as a target work package, and add the target work package to a model work package set of a local database.
In some optional implementations of some embodiments, the execution subject may classify the target service manual according to at least one dimension, and obtain at least one target service manual dimension data. By way of example, the at least one dimension may be a part location dimension, a part category dimension, and the like.
And performing cross-taking union on the dimensional data of the at least one target maintenance manual to obtain a daughter card list. Specifically, the executing entity may use the collected dimensional data of the target service manual as a daughter card, and generate a daughter card list.
And filtering the daughter card list, and adding a label and a work card identifier to each daughter card in the daughter card list to obtain at least one work card. By way of example, the executive body may filter out some daughter cards that are not suitable for the target aircraft through the target aircraft information, and add the labels and work card identifications of the above dimensions to the remaining daughter cards. Specifically, the work card identifier generally refers to a serial number used for characterizing the work card. As an example, the work card identification of the work card applicable to the a123 part may be a 123. As yet another example, the work card identification for a work card applicable to parts of the A3 region B2 sub-region D3 parts category may be A3B2D 3.
The daughter card list is filtered to screen out the items of the maintenance manual which are not suitable for part of parts due to the fact that the version of the maintenance manual is not updated timely, and convenience is provided for maintenance personnel.
And step 202, determining a target tool kit from the model tool kit according to the target maintenance manual information.
In some embodiments, based on the target service manual information obtained in step 201, the execution subject (e.g., the server shown in fig. 1) may determine the target kit from the model kit according to the target service manual information. As an example, the execution body may select a model kit suitable for the a model from the model kits as a target kit by using information that a service manual is suitable for the a model in the service manual information.
Here, the above-mentioned model kit generally refers to a set consisting of a plurality of model cards. The model workbook is a fragment of a service manual applicable to a model. As an example, the model workbook may be a service manual fragment applicable to the a-field of the a-model. As yet another example, the model workbook may also be a section of a service manual for model a, b.
And 203, selecting a first single machine work card from the target work package according to the target aircraft information.
In some embodiments, the executive body may select a first standalone tooling card from the target kit according to target aircraft information. Specifically, the execution agent may determine, as the first standalone service card, the target aircraft and a part of the standalone service cards applicable to the target package by using the target aircraft information. As an example, the a component information in the target aircraft information may be used to determine that the same or similar work cards that may be applicable to the a component exist in the target package as the first standalone work card.
As an example, the above-mentioned stand-alone work card may be a work card applicable only to a aircraft among a model aircraft. Specifically, since there are a plurality of aircraft in each model, and since the plurality of aircraft are produced by different manufacturers although the models are the same and production techniques are different from each other, there are many individual differences even for the same model of aircraft.
And step 204, generating a second single machine work card according to the target maintenance manual.
In some embodiments, the execution agent may generate a second standalone work card according to the target service manual. As an example, the execution subject may determine that there is no component a of the corresponding first standalone service card in the target aircraft, and the execution subject may search the target service manual for a part of the service manual applicable to the component a as the second standalone service card. As another example, the execution main body may disassemble all contents of the target service manual to obtain a second standalone service card.
And step 205, generating a target aircraft work package according to the first stand-alone work card and the second stand-alone work card.
In some embodiments, the execution agent may generate the target aircraft package from the first standalone work card and the second standalone work card. As an example, the execution subject may combine the second standalone tool card and the first standalone tool card into a target aircraft package. As another example, the execution subject may further merge the first standalone work card and the second standalone work card into a work card set, and remove the same or similar work cards from the work card set to obtain the target aircraft work package.
In some optional implementations of some embodiments, the execution subject may further display a first presentation interface, where the first presentation interface includes a package selection control. Here, the above-mentioned tool pack selection control is used for selecting a tool pack.
And responding to the detected selection operation of the user for the work package selection control, and displaying a second display interface according to the selection operation, wherein the second display interface comprises the user selection work package. Herein, the user selection tool pack generally refers to a tool pack selected by a user on the first presentation interface.
And in response to the detection of the editing operation of the user on the user selection work package, editing the work card in the user selection work package according to the editing operation. By way of example, the editing operation may be deleting the work card, modifying the content of the work card, modifying the tag in the work card, and the like.
And generating a work card editing log according to the editing operation, and taking the edited user selection work package and the work card editing log as a target aircraft work package. Here, the editing log generally refers to a record of modification or deletion of the work card by the user. The edit log may include, as examples, a person for modification, time for modification, content for modification, and the like. Specifically, the execution agent may associate or bind the work card edit log with a work card corresponding to the work card edit log, and then use the set of work cards (user selection kit) as a target aircraft kit.
Therefore, when parts are replaced, the user can freely modify the work card, and maintenance personnel can clearly see the differential comparison of work card version replacement.
In some optional implementations of some embodiments, the executing subject may further send the target aircraft bundle and the target prompt content to the target device in response to not detecting that the electronic signature of the target user exists in the target aircraft bundle. Specifically, the electronic signature is generally an electronic signature obtained by checking a target aircraft work package by a user.
And in response to detecting that the electronic signature of the target user exists in the target aircraft work package, determining the target work card from the target aircraft work package with the electronic signature. Specifically, the target work card is generally a work card selected by a user. As an example, a service person is responsible for servicing a part a, which may be a target work card. As yet another example, the customer may desire B part information and may have a B part work card as the target work card.
And determining target equipment according to the target work card, and sending the target work card to the target equipment. The execution main body can determine the device corresponding to the target work card as the target device. As an example, the target device corresponding to the part a work card is a device of a serviceman responsible for servicing the part a.
One of the above various embodiments of the present disclosure has the following beneficial effects: firstly, obtaining target aircraft maintenance manual information, then determining a target work package from a model work package, then selecting a first stand-alone work card from the target work package, then generating a second stand-alone work card according to the target maintenance manual, and finally generating the target aircraft work package according to the first stand-alone work card and the second stand-alone work card. Therefore, the generated work package can better meet the needs of maintenance personnel, the working efficiency and the use experience of a user are improved, and the possibility of errors is reduced.
With further reference to fig. 3, as an implementation of the methods illustrated in the above figures, the present disclosure provides some embodiments of a device for generating an aircraft work package, which correspond to those of the method embodiments illustrated in fig. 2, which may be particularly applicable in various electronic devices.
As shown in fig. 3, the generating an aircraft tooling device 300 of some embodiments includes: an acquisition unit 301, a determination unit 302, a selection unit 303, a first generation unit 304, and a second generation unit 305. The acquiring unit 301 is configured to acquire target aircraft maintenance manual information, where the target aircraft maintenance manual information includes a target maintenance manual, target aircraft information, and target maintenance manual information; a determination unit 302 configured to determine a target tool pack from the model tool pack according to the target service manual information; a selecting unit 303 configured to select a first standalone tooling card from the target package according to the target aircraft information; a first generating unit 304 configured to generate a second stand-alone work card according to the target service manual; and a second generating unit 305 configured to generate a target aircraft package according to the first standalone tooling card and the second standalone tooling card.
In an optional implementation manner of some embodiments, the apparatus further includes an adding unit configured to: detecting whether a target work packet exists in the model work packet or not according to the target aircraft information; responding to the situation that the target tool pack is not detected in the machine tool pack, and carrying out structured splitting on the target maintenance manual to obtain at least one tool card; and generating a target work packet according to the at least one work card, and adding the target work packet into the model work packet.
In an optional implementation manner of some embodiments, the adding unit is further configured to: classifying the target maintenance manuals according to at least one dimension to obtain at least one target maintenance manual dimension data; performing cross-taking union on the dimensional data of the at least one target maintenance manual to obtain a daughter card list; and filtering the daughter card list, and adding a label and a work card identifier to each daughter card in the daughter card list to obtain at least one work card.
In an optional implementation manner of some embodiments, the apparatus further includes a display unit configured to: displaying a first display interface, wherein the first display interface comprises a work package selection control; responding to the detected selection operation of the user for the work package selection control, and displaying a second display interface according to the selection operation, wherein the second display interface comprises a user selection work package; in response to the fact that the editing operation of the user for the user selection work package is detected, editing the work cards in the user selection work package according to the editing operation; and generating a work card editing log according to the editing operation, and taking the edited user selection work package and the work card editing log as a target aircraft work package.
In an optional implementation manner of some embodiments, the apparatus further includes a sending unit configured to: in response to the fact that the electronic signature of the target user is not detected to exist in the target aircraft work package, the target aircraft work package and the target prompt content are sent to the target device; in response to detecting that the electronic signature of the target user exists in the target aircraft work package, determining a target work card from the target aircraft work package with the electronic signature; and determining target equipment according to the target work card, and sending the target work card to the target equipment.
It will be understood that the units described in the apparatus 300 correspond to the various steps in the method described with reference to fig. 2. Thus, the operations, features and resulting advantages described above with respect to the method are also applicable to the apparatus 300 and the units included therein, and are not described herein again.
One of the above-described various embodiments of the present disclosure has the following advantageous effects: firstly, obtaining target aircraft maintenance manual information, then determining a target work package from a model work package, then selecting a first stand-alone work card from the target work package, then generating a second stand-alone work card according to the target maintenance manual, and finally generating the target aircraft work package according to the first stand-alone work card and the second stand-alone work card. Therefore, the generated work package can better meet the needs of maintenance personnel, the working efficiency and the use experience of a user are improved, and the possibility of errors is reduced.
Referring now to fig. 4, a block diagram of an electronic device (e.g., server in fig. 1) 400 suitable for use in implementing some embodiments of the present disclosure is shown. The electronic device shown in fig. 4 is only an example, and should not bring any limitation to the functions and the scope of use of the embodiments of the present disclosure.
As shown in fig. 4, electronic device 400 may include a processing device (e.g., central processing unit, graphics processor, etc.) 401 that may perform various appropriate actions and processes in accordance with a program stored in a Read Only Memory (ROM) 402 or a program loaded from a storage device 408 into a Random Access Memory (RAM) 403. In the RAM 403, various programs and data necessary for the operation of the electronic apparatus 400 are also stored. The processing device 401, the ROM 402, and the RAM 403 are connected to each other via a bus 404. An input/output (I/O) interface 405 is also connected to bus 404.
Generally, the following devices may be connected to the I/O interface 405: input devices 406 including, for example, a touch screen, touch pad, keyboard, mouse, camera, microphone, accelerometer, gyroscope, etc.; an output device 407 including, for example, a Liquid Crystal Display (LCD), a speaker, a vibrator, and the like; storage 408 including, for example, tape, hard disk, etc.; and a communication device 409. The communication means 409 may allow the electronic device 400 to communicate wirelessly or by wire with other devices to exchange data. While fig. 4 illustrates an electronic device 400 having various means, it is to be understood that not all illustrated means are required to be implemented or provided. More or fewer devices may alternatively be implemented or provided. Each block shown in fig. 4 may represent one device or may represent multiple devices as desired.
In particular, according to some embodiments of the present disclosure, the processes described above with reference to the flow diagrams may be implemented as computer software programs. For example, some embodiments of the present disclosure include a computer program product comprising a computer program embodied on a computer-readable medium, the computer program comprising program code for performing the method illustrated by the flow chart. In some such embodiments, the computer program may be downloaded and installed from a network through communications device 409, or installed from storage device 408, or installed from ROM 402. The computer program, when executed by the processing device 401, performs the above-described functions defined in the methods of some embodiments of the present disclosure.
It should be noted that the computer readable medium described above in some embodiments of the present disclosure may be a computer readable signal medium or a computer readable storage medium or any combination of the two. A computer readable storage medium may be, for example, but not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any combination of the foregoing. More specific examples of the computer readable storage medium may include, but are not limited to: an electrical connection having one or more wires, a portable computer diskette, a hard disk, a Random Access Memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing. In some embodiments of the disclosure, a computer readable storage medium may be any tangible medium that can contain, or store a program for use by or in connection with an instruction execution system, apparatus, or device. In some embodiments of the present disclosure, however, a computer readable signal medium may include a propagated data signal with computer readable program code embodied therein, for example, in baseband or as part of a carrier wave. Such a propagated data signal may take many forms, including, but not limited to, electro-magnetic, optical, or any suitable combination thereof. A computer readable signal medium may also be any computer readable medium that is not a computer readable storage medium and that can communicate, propagate, or transport a program for use by or in connection with an instruction execution system, apparatus, or device. Program code embodied on a computer readable medium may be transmitted using any appropriate medium, including but not limited to: electrical wires, optical cables, RF (radio frequency), etc., or any suitable combination of the foregoing.
In some embodiments, the clients, servers may communicate using any currently known or future developed network Protocol, such as HTTP (HyperText Transfer Protocol), and may be interconnected with any form or medium of digital data communication (e.g., a communication network). Examples of communication networks include a local area network ("LAN"), a wide area network ("WAN"), the Internet (e.g., the Internet), and peer-to-peer networks (e.g., ad hoc peer-to-peer networks), as well as any currently known or future developed network.
The computer readable medium may be embodied in the electronic device; or may be separate and not incorporated into the electronic device. The computer readable medium carries one or more programs which, when executed by the electronic device, cause the electronic device to: acquiring target aircraft maintenance manual information, wherein the target aircraft maintenance manual information comprises a target maintenance manual, target aircraft information and target maintenance manual information; determining a target tool kit from the model tool kit according to the target maintenance manual information; selecting a first stand-alone work card from the target work package according to the target aircraft information; generating a second single machine work card according to the target maintenance manual; and generating a target aircraft work package according to the first stand-alone work card and the second stand-alone work card.
Computer program code for carrying out operations for embodiments of the present disclosure may be written in any combination of one or more programming languages, including an object oriented programming language such as Java, Smalltalk, C + +, and conventional procedural programming languages, such as the "C" programming language or similar programming languages. The program code may execute entirely on the user's computer, partly on the user's computer, as a stand-alone software package, partly on the user's computer and partly on a remote computer or entirely on the remote computer or server. In the case of a remote computer, the remote computer may be connected to the user's computer through any type of network, including a Local Area Network (LAN) or a Wide Area Network (WAN), or the connection may be made to an external computer (for example, through the Internet using an Internet service provider).
The flowchart and block diagrams in the figures illustrate the architecture, functionality, and operation of possible implementations of systems, methods and computer program products according to various embodiments of the present disclosure. In this regard, each block in the flowchart or block diagrams may represent a module, segment, or portion of code, which comprises one or more executable instructions for implementing the specified logical function(s). It should also be noted that, in some alternative implementations, the functions noted in the block may occur out of the order noted in the figures. For example, two blocks shown in succession may, in fact, be executed substantially concurrently, or the blocks may sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each block of the block diagrams and/or flowchart illustration, and combinations of blocks in the block diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems which perform the specified functions or acts, or combinations of special purpose hardware and computer instructions.
The units described in some embodiments of the present disclosure may be implemented by software or hardware. The described units may also be provided in a processor, and may be described as: a processor includes an acquisition unit, a determination unit, a selection unit, a first generation unit, and a second generation unit. Where the names of the units do not in some cases constitute a limitation on the units themselves, the receiving unit may also be described as a "unit for obtaining target aircraft service manual information", for example.
The functions described herein above may be performed, at least in part, by one or more hardware logic components. For example, without limitation, exemplary types of hardware logic components that may be used include: field Programmable Gate Arrays (FPGAs), Application Specific Integrated Circuits (ASICs), Application Specific Standard Products (ASSPs), systems on a chip (SOCs), Complex Programmable Logic Devices (CPLDs), and the like.
The foregoing description is only exemplary of the preferred embodiments of the disclosure and is illustrative of the principles of the technology employed. It will be appreciated by those skilled in the art that the scope of the invention in the embodiments of the present disclosure is not limited to the specific combination of the above-mentioned features, but also encompasses other embodiments in which any combination of the above-mentioned features or their equivalents is made without departing from the inventive concept as defined above. For example, the above features and (but not limited to) technical features with similar functions disclosed in the embodiments of the present disclosure are mutually replaced to form the technical solution.

Claims (8)

1. A method for generating an aircraft toolkit, comprising:
acquiring target aircraft maintenance manual information, wherein the target aircraft maintenance manual information comprises a target maintenance manual, target aircraft information and target maintenance manual information;
determining a target tool kit from a model tool kit according to the target maintenance manual information;
selecting a first single machine work card from the target work package according to the target aircraft information;
generating a second single machine work card according to the target maintenance manual;
and generating a target aircraft work package according to the first single machine work card and the second single machine work card.
2. The method of claim 1, wherein prior to said determining a target kit from a model kit according to said target manual service information, said method further comprises:
detecting whether a target work packet exists in the model work packet or not according to the target aircraft information;
responding to the situation that the target work package is not detected in the machine type work package, and performing structural splitting on the target maintenance manual to obtain at least one work card;
and generating a target work package according to the at least one work card, and adding the target work package into the machine type work package.
3. The method of claim 2, wherein said structurally splitting the target service manual comprises:
classifying the target maintenance manual according to at least one dimension to obtain at least one target maintenance manual dimension data;
performing cross-taking union on the at least one target maintenance manual dimensional data to obtain a daughter card list;
and filtering the daughter card list, and adding a label and a work card identifier for each daughter card in the daughter card list to obtain at least one work card.
4. The method of claim 1, wherein the method further comprises:
displaying a first presentation interface, wherein the first presentation interface comprises a package selection control;
in response to detecting a selection operation of a user for the work package selection control, displaying a second display interface according to the selection operation, wherein the second display interface comprises a user selection work package;
in response to the fact that the editing operation of the user for the user selection work package is detected, editing the work cards in the user selection work package according to the editing operation;
and generating a work card editing log according to the editing operation, and taking the edited user selection work package and the work card editing log as a target aircraft work package.
5. The method of claim 1, wherein the method further comprises:
in response to not detecting the presence of the electronic signature of the target user in the target aircraft work package, sending the target aircraft work package and target prompt content to a target device;
in response to detecting that the electronic signature of the target user exists in the target aircraft work package, determining a target work card from the target aircraft work package with the electronic signature;
and determining target equipment according to the target work card, and sending the target work card to the target equipment.
6. An apparatus for generating an aircraft kit, comprising:
an acquisition unit configured to acquire target aircraft service manual information, wherein the target aircraft service manual information includes a target service manual, target aircraft information, and target service manual information;
a determination unit configured to determine a target tool pack from a model tool pack according to the target service manual information;
the selecting unit is configured to select a first stand-alone work card from the target work package according to the target aircraft information;
a first generating unit configured to generate a second stand-alone work card according to the target service manual;
A second generation unit configured to generate a target aircraft package according to the first and second standalone industrial cards.
7. An electronic device, comprising:
one or more processors;
a storage device having one or more programs stored thereon,
when executed by the one or more processors, cause the one or more processors to implement the method of any one of claims 1-5.
8. A computer-readable medium, on which a computer program is stored, wherein the program, when executed by a processor, implements the method of any one of claims 1-5.
CN202210676898.9A 2022-06-16 2022-06-16 Method, apparatus, device and medium for generating an aircraft kit Active CN114757157B (en)

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