Method and device for generating conductor number of airplane and matching conductor number with connector hole number, computer equipment and medium

Abstract

The embodiment of the invention provides a method and device for generating a wire number of an airplane and matching the wire number with a connector hole number, computer equipment and a medium, and the method comprises the following steps: obtaining all airborne equipment of a flight control system, and according to the attributes of all the airborne equipment and a wire connected with the airborne equipment, determining the wire number of the airplane according to the attributes of all the airborne equipment and the wire connected with the airborne equipment; determining a sleeve number of the wire, a wire mark, a wire serial number corresponding to the wire mark, a wire distinguishing number, a wire gauge, a function code, an electromagnetic compatibility code and a wire attribute; on the basis of a wire numbering rule, a wire number is generated through a sleeve number, a wire mark, a wire serial number, a wire distinguishing number, a wire gauge, a function code, an electromagnetic compatibility code and a wire attribute; and analyzing the wire serial number, determining the corresponding airborne equipment through the sleeve number, and matching the wire serial number with the connector hole number of the airborne equipment through the wire serial number. According to the scheme, the wires can be quickly numbered, and the efficiency of wire harness processing and system line troubleshooting is improved.

Description

Technical Field

[0001] This invention relates to the field of aircraft flight control system technology, and in particular to a method, apparatus, computer equipment, and medium for generating aircraft wire numbers and matching them with connector hole numbers. Background Technology

[0002] The flight control system is one of the core systems of modern aircraft, responsible for processing signals from the pilot, sensors, and other systems to control the aircraft's attitude and trajectory. Wiring harnesses, as the connecting links between various components in the flight control system, are responsible for transmitting signals and power. Their design directly affects the system's performance, reliability, and safety. However, the complexity of flight control systems also brings problems such as a large number of wiring harnesses and connectors, which not only increases the difficulty of system design and manufacturing but may also lead to assembly errors and increased maintenance costs. Summary of the Invention

[0003] In view of this, embodiments of the present invention provide a method for generating aircraft wire numbers and matching them with connector hole numbers, to solve the technical problems of assembly errors and high maintenance costs caused by chaotic wire numbering in the prior art. The method includes: Obtain all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment; Based on the conductor numbering rules, a conductor number is generated using the set number, the wire mark, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The wire number is parsed, and the set number and wire serial number are extracted from the wire number. The corresponding airborne equipment is determined by the set number, and the wire number is matched with the connector hole number of the airborne equipment by the wire serial number.

[0004] This invention also provides a device for generating aircraft wire numbers and matching them with connector hole numbers, to solve the technical problems of assembly errors and high maintenance costs caused by chaotic wire numbering in the prior art. The device includes: The wire parameter acquisition module is used to acquire all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment. The conductor numbering generation module is used to generate conductor numbers based on conductor numbering rules, using the set number, the wire mark, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The hole number matching module is used to parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number.

[0005] This invention also provides a computer device, including a memory, a processor, and a computer program stored in the memory and executable on the processor. When the processor executes the computer program, it implements the method for generating wire numbers for any of the above-mentioned aircraft and matching them with connector hole numbers, thereby solving the technical problems of assembly errors and high maintenance costs caused by chaotic wire numbers in the prior art.

[0006] This invention also provides a computer-readable storage medium storing a computer program that performs the above-described method for generating wire numbers for any aircraft and matching them with connector hole numbers, in order to solve the technical problems of assembly errors and high maintenance costs caused by chaotic wire numbers in the prior art.

[0007] Compared with the prior art, the beneficial effects that at least one technical solution adopted in the embodiments of this specification can achieve include at least: The numbering generation method of this invention can quickly number wires, improving the efficiency of wire harness processing and system circuit fault diagnosis. Attached Figure Description

[0008] To more clearly illustrate the technical solutions of the embodiments of this application, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0009] Figure 1 This is a flowchart of a method for generating aircraft wire numbers and matching them with connector hole numbers, provided by an embodiment of the present invention; Figure 2 This is a diagram showing the installation locations of the main flight control system equipment on the aircraft. Figure 3 This is a connection diagram of the airborne equipment of the flight control system; Figure 4 This is a diagram showing the correspondence between wire numbers and connector hole numbers provided in an embodiment of the present invention; Figure 5This is a structural block diagram of a computer device provided in an embodiment of the present invention; Figure 6 This is a structural block diagram of a device for generating aircraft wire numbers and matching them with connector hole numbers, provided in an embodiment of the present invention. Detailed Implementation

[0010] The embodiments of this application will now be described in detail with reference to the accompanying drawings.

[0011] The following specific examples illustrate the implementation of this application. Those skilled in the art can easily understand other advantages and effects of this application from the content disclosed in this specification. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of them. This application can also be implemented or applied through other different specific embodiments, and the details in this specification can also be modified or changed based on different viewpoints and applications without departing from the spirit of this application. It should be noted that, in the absence of conflict, the following embodiments and features in the embodiments can be combined with each other. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0012] To address existing problems, this invention proposes a wire numbering rule based on equipment installation location and system function, as well as a method for matching wire numbers with connector hole numbers. Practical application has verified that this reduces changes to design drawings and process documents, saves on wire harness manufacturing costs, shortens system development cycles, significantly improves the efficiency of wire harness processing and system circuit fault diagnosis, and provides new ideas for wire harness design in other systems.

[0013] In this embodiment of the invention, a method for generating aircraft wire numbers and matching them with connector hole numbers is provided, such as... Figure 1 As shown, the method includes: Step S101: Obtain all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes according to the attributes of all the airborne equipment and the wires connecting the airborne equipment; Step S102: Based on the wire numbering rules, generate a wire number using the set number, the wire mark, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes; Step S103: Parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number.

[0014] In specific implementation, the following steps are used to determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire classification number, wire gauge, function code, electromagnetic compatibility code, and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment: Identical airborne equipment is grouped into equipment groups, and the airborne equipment in each equipment group is numbered sequentially, with the generated numbers serving as a set number. The correspondence between the airborne equipment and wire markings in the flight control system is determined, and the corresponding wire markings for each airborne equipment are determined based on this correspondence. The connection relationships between the airborne equipment are obtained, and the wire serial number corresponding to each wire marking is determined according to the connection relationships based on the wire markings of the airborne equipment. The airborne equipment includes a computing device group, an execution sensing mechanism, operating components, a power distribution system, an external interconnection system, a system detection port, and an internal flight control subsystem. Wire identification numbers are determined. Based on the current carrying capacity and voltage drop requirements of the conductor, the wire gauge is determined through electrical calculations. A functional code-wire function correspondence is established, and the function code is determined based on the function of the conductor through this correspondence. The electromagnetic compatibility code is determined based on the transmission signal characteristics of the conductor through isolation design specifications. The wire attributes are determined based on the physical characteristics of the conductor through a correspondence table between physical characteristics and wire attributes.

[0015] In specific implementation, the following steps are used to determine the wire serial number corresponding to the wire mark based on the connection relationship using the wire mark on the airborne equipment: Based on the connection relationships between the airborne devices, the wire serial numbers are divided into multiple functional zones, and wire serial numbers are assigned to the wires according to the functional zones: the wires from the computing device group to the actuating sensing mechanism are divided into one functional zone; the wires from the operating component to the computing device group are divided into one functional zone; the wires between the computer devices in the computing device group are divided into one functional zone; the wires from the power distribution system to the computing device group, the power distribution system to the operating component, and the power distribution system to the actuating sensing mechanism are divided into one functional zone; the wires from the external interconnection system to the computing device group are divided into one functional zone; and the wires from the system detection port to the computing device group are divided into one functional zone.

[0016] In practice, the following steps are used to determine the wire identification number: When multiple conductors are connected in parallel or series to form a parallel conductor group or a series conductor group, the starting letter is used as the wire identification number of the first conductor in the parallel conductor group or the series conductor group. Following the conductor connection order, when a conductor is subsequently added to the parallel conductor group or the series conductor group, subsequent letters are sequentially assigned as the corresponding wire identification number. Each wire identification number remains unique within its respective parallel conductor group or the series conductor group. When a single conductor passes through a transfer point during transmission and its function remains unchanged, after the transfer point, a subsequent letter is assigned as the new wire identification number corresponding to the single conductor. Each wire identification number remains unique within the transfer path and within the conductor group or transfer path to which it belongs.

[0017] In specific implementation, the wire-based numbering rule is implemented through the following steps: a wire number is generated using the set number, the wire marking, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The wire number is generated by combining the set number, the wire mark, the wire serial number corresponding to the wire mark, the identification number, the wire gauge, the separator, the function code, the electromagnetic compatibility code, and the wire attribute in sequence; the separator is a fixed character.

[0018] In specific implementation, the following steps are used to parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number: Parse the wire number and extract the set number and wire serial number from the wire number; determine the corresponding airborne equipment based on the set number and locate the target connector on the airborne equipment; obtain the set of connector hole numbers of the target connector; establish the correspondence between the wire serial number and the connector hole number, so that each wire serial number corresponds one-to-one with the connector hole number.

[0019] Specifically, the one-to-one correspondence between wire serial numbers and connector hole numbers is as follows: when the wire serial numbers in the wire numbering are consecutive, the corresponding connector hole numbers are also consecutive, forming a sequential mapping relationship between the wire serial numbers and connector hole numbers.

[0020] In practice, the fault response is achieved through the following steps: When a fault occurs, a fault information is received, which includes the wire number of the faulty wire; the wire number is parsed to obtain the set number, the wire mark, and the wire serial number; the airborne equipment is located based on the set number and the wire mark, and the connector hole number of the faulty wire on the target connector is located based on the wire serial number; the airborne equipment and the connector hole number are saved as fault location information.

[0021] In one embodiment of the present invention, the wires are numbered in the form of “set number + wire mark + wire serial number of wire mark + wire identification number + wire gauge + separator + function code + electromagnetic compatibility code + wire attribute”, that is, in the form of ×△△××× △××-△×△△, where × is 1 digit and △ is 2 digits.

[0022] Specifically, when two or more identical airborne devices are installed on the same aircraft and their wiring needs to be distinguished, a serial number is used to differentiate them. The serial number is numbered consecutively from 1 based on the number of airborne devices (electronic systems or other equipment) installed on the aircraft. The first set is 1, the second set is 2, and if there is only one set, the serial number is omitted. Both the airborne equipment and the mission system equipment are numbered consecutively, with the airborne equipment listed first, followed by the mission system equipment.

[0023] Specifically, the wire markings are two digits. A correspondence table between airborne equipment and wire markings is constructed. When new airborne equipment is added, the new airborne equipment shall be designated in subsequent designs using the system (using the first letters of the full name of the system in Chinese Pinyin) or the equipment model (the first letters of the full name of the equipment in Chinese Pinyin for domestic equipment, and the abbreviation of the equipment for imported equipment) letter codes, which shall not be duplicated with the wire markings in the correspondence table.

[0024] Specifically, the wire serial numbers are sequentially numbered from 001 to 899 within the system, while wire numbers from 900 to 999 are provided for use by aircraft users.

[0025] The wire serial numbers (001~899) are assigned according to the equipment installation location and system function, as follows: (001~199): Used to calculate the wire numbers between the calculation device and the actuator; (201-299): Wire numbers used between the computing device and the operating component, where the operating component is installed in front of the computing device (e.g., ...). Figure 2 , Figure 3 (as shown) (301~399): Used to calculate internal cross-linking of equipment (e.g.) Figure 2 , Figure 3 (as shown) (501~599): Used for system power distribution conductor numbering (e.g.) Figure 2 , Figure 3 (as shown) (601~699): Used for the numbering of external cross-linking conductors in the system (e.g., ... Figure 2 , Figure 3 (as shown) (701~799): Numbers used for system testing interface wires (e.g.) Figure 2 , Figure 3 (as shown) (801~899): Used for wiring numbers of internal small systems within the flight control system, or for wiring numbers between operating components and actuators (e.g., ...). Figure 2 , Figure 3 (as shown) By combining the set number (0-9) and the wire serial number (001-899), the wires between each computing device are numbered, and the data is distinguished by which computing device sent it.

[0026] When designing schematic diagrams and power supply diagrams, wire numbers can be quickly generated based on the wire numbering method of this invention. Especially when the system interconnection relationship changes or the number of interfaces between system devices increases, it ensures that the interface wire numbers of a device are continuous, thereby enabling rapid identification of the number of interfaces of that device. During wire harness manufacturing, the number of wires can be quickly identified by wire numbers, and the continuous wire numbers are less likely to be lost. During fault diagnosis, the function of the wire and the device it is connected to can be quickly located by identifying the wire number, and the drawings can be quickly found to assist in fault diagnosis.

[0027] Color-coded letters are used only for identifying double-twisted or multi-twisted cables with the same sheath. In aircraft cables (two or more wires forming a sheathed shielded or twisted cable), each wire is identified by the color of its insulation. Each wire within these cables should use the same marking, followed by a different color code after the electromagnetic compatibility (EMC) code. The wire attributes are listed in the order of white, red, blue, yellow, and green to identify each wire in the cable. The wire attribute immediately follows the EMC code.

[0028] In one embodiment of the present invention, the method for matching wire numbers with connector hole numbers is as follows: the computing device is determined by the serial number; the connector hole number on the connector is obtained; the serial number of the marked wire corresponds to the connector hole number of the corresponding computing device.

[0029] like Figure 4 As shown, the wire numbers correspond one-to-one with the connector hole numbers.

[0030] This method facilitates wire termination, prevents wires from being inserted into the wrong holes, and prevents wire loss during cable processing. During troubleshooting, for cable bundles containing a large number of wires, if the wire numbers cannot be used to locate the wires, the hole numbers on the connectors can be used to find the wires, aiding in troubleshooting.

[0031] In this embodiment, a computer device is provided, such as... Figure 5 As shown, it includes a memory 501, a processor 502, and a computer program stored in the memory and executable on the processor. When the processor executes the computer program, it implements the method for generating wire numbers for any of the above-mentioned aircraft and matching them with connector hole numbers.

[0032] Specifically, the computer device can be a computer terminal, a server, or a similar computing device.

[0033] In this embodiment, a computer-readable storage medium is provided, which stores a computer program that performs the above-described method for generating wire numbers for any of the aircraft and matching them with connector hole numbers.

[0034] Specifically, computer-readable storage media include both permanent and non-permanent, removable and non-removable media, which can store information using any method or technology. Information can be computer-readable instructions, data structures, modules of programs, or other data. Examples of computer-readable storage media include, but are not limited to, phase-change memory (PRAM), static random access memory (SRAM), dynamic random access memory (DRAM), other types of random access memory (RAM), read-only memory (ROM), electrically erasable programmable read-only memory (EEPROM), flash memory or other memory technologies, CD-ROM, digital versatile optical disc (DVD) or other optical storage, magnetic tape, magnetic disk storage or other magnetic storage devices, or any other non-transferable medium that can be used to store information accessible by a computing device. As defined herein, computer-readable storage media do not include transient media, such as modulated data signals and carrier waves.

[0035] Based on the same inventive concept, this invention also provides an apparatus for generating aircraft wire numbers and matching them with connector hole numbers, as described in the following embodiments. Since the principle of the apparatus for generating aircraft wire numbers and matching them with connector hole numbers is similar to that of the method for generating aircraft wire numbers and matching them with connector hole numbers, the implementation of the apparatus for generating aircraft wire numbers and matching them with connector hole numbers can refer to the implementation of the method for generating aircraft wire numbers and matching them with connector hole numbers; repeated details will not be elaborated further. As used below, the terms "unit" or "module" can refer to a combination of software and / or hardware that performs a predetermined function. Although the apparatus described in the following embodiments is preferably implemented in software, hardware implementation, or a combination of software and hardware, is also possible and contemplated.

[0036] Figure 6This is a structural block diagram of a device for generating aircraft wire numbers and matching them with connector hole numbers, according to an embodiment of the present invention. Figure 6 As shown, it includes: a conductor parameter acquisition module 601, a conductor number generation module 602, and a hole number matching module 603. The structure is described below.

[0037] The wire parameter acquisition module 601 is used to acquire all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment. The conductor numbering generation module 602 is used to generate conductor numbers based on the conductor numbering rules, using the set number, the wire mark, the wire serial number, the wire differentiation number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The hole number matching module 603 is used to parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number.

[0038] In one embodiment, the wire parameter acquisition module includes: A serial number generation unit is used to group identical airborne equipment into a group of equipment, sequentially number the airborne equipment in each group of equipment, and use the generated number as a serial number. A wire marker generation unit is used to determine the correspondence between the airborne equipment in the flight control system and the wire markers, and to determine the wire markers corresponding to the airborne equipment through the correspondence. The wire serial number generation unit is used to obtain the connection relationship between the airborne equipment and determine the wire serial number corresponding to the wire mark according to the connection relationship based on the wire mark of the airborne equipment. The airborne equipment includes a computing device group, an execution sensing mechanism, an operating component, a power distribution system, an external cross-linking system, a system detection port, and a flight control internal subsystem. The wire identification number generation unit is used to determine the wire identification number; The wire gauge generation unit is used to determine the wire gauge through electrical calculations based on the current that the conductor needs to carry and the voltage drop requirements of the line. A function code generation unit is used to establish a function code and a function correspondence between the wires, and to determine the function code based on the function of the wires through the function correspondence. The electromagnetic compatibility code generation unit is used to determine the electromagnetic compatibility code based on the transmission signal characteristics of the conductor and the isolation design specifications. The wire attribute generation unit is used to determine the wire attributes based on the physical characteristics of the conductor and through a correspondence table between physical characteristics and wire attributes.

[0039] In one embodiment, the wire serial number generation unit is further configured to divide the wire serial number into multiple functional zones based on the connection relationships between the airborne devices, and assign wire serial numbers to the wires according to the functional zones: dividing the wires from the computing device group to the actuating sensing mechanism into one functional zone; dividing the wires from the operating component to the computing device group into one functional zone; dividing the wires between the computer devices in the computing device group into one functional zone; dividing the wires from the power distribution system to the computing device group, the power distribution system to the operating component, and the power distribution system to the actuating sensing mechanism into one functional zone; dividing the wires from the external interconnection system to the computing device group into one functional zone; and dividing the wires from the system detection port to the computing device group into one functional zone.

[0040] In one embodiment, the wire identification number generation unit is further configured to: when there are multiple wires connected in parallel or series to form a parallel wire group or a series wire group, assign a starting letter as the wire identification number of the first wire in the parallel wire group or the series wire group; according to the wire connection order, when a wire is subsequently added to the parallel wire group or the series wire group, sequentially assign subsequent letters as the corresponding wire identification number, wherein each wire identification number remains unique within its respective parallel wire group or the series wire group; when a single wire passes through a transfer point during transmission and its function remains unchanged, assign subsequent letters as a new wire identification number for the single wire after the transfer point, wherein each wire identification number remains unique within the transfer path; and each wire identification number remains unique within the wire group or transfer path to which the wire identification number belongs.

[0041] In one embodiment, the wire number generation module includes: The conductor number generation unit is used to combine the set number, the wire mark, the wire serial number corresponding to the wire mark, the differentiation number, the wire gauge, the separator, the function code, the electromagnetic compatibility code, and the wire attributes in sequence to generate a conductor number; A delimiter definition unit is used when the delimiter is a fixed character.

[0042] In one embodiment, the hole number matching module includes: An information extraction unit is used to parse the wire number and extract the set number and wire serial number from the wire number; A positioning connector unit is used to determine the corresponding airborne equipment based on the kit number and to position the target connector on the airborne equipment. A connector hole number set acquisition unit is used to acquire the connector hole number set of the target connector; The matching unit is used to establish the correspondence between the wire serial number and the connector hole number, so that each wire serial number corresponds one-to-one with the connector hole number.

[0043] In one embodiment, the above-mentioned device further includes a fault handling module; In one embodiment, the fault handling module includes: An information acquisition unit is used to receive fault information when a fault occurs, wherein the fault information includes the wire number of the faulty wire. A wire number parsing unit is used to parse the wire number and obtain the set number, the wire mark, and the wire serial number from the wire number; The connector hole number locator is used to locate the airborne equipment based on the kit number and the wire marking, and to locate the connector hole number of the faulty wire on the target connector based on the wire serial number. An information storage unit is used to store the airborne equipment and the connector hole number as fault location information.

[0044] The embodiments of the present invention achieve the following technical effects: Based on the challenges in identifying difficulties in the production, manufacturing, use, and maintenance of aircraft wiring harnesses, this paper proposes a wiring harness design method for flight control systems with a large number of wiring harnesses. This method is based on wire numbering rules according to equipment installation location and system function, and matches wire numbers with connector hole numbers. It solves the problems of low efficiency caused by the large number of wires in the manufacturing process of aircraft flight control systems, as well as the difficulty in quickly locating wires during troubleshooting and maintenance. Practical application has verified that this method reduces changes to design drawings and process documents, saves wiring harness manufacturing costs, shortens the system development cycle, significantly improves the efficiency of troubleshooting system circuit faults, and provides new ideas for the design of wiring harnesses in other systems.

[0045] Obviously, those skilled in the art should understand that the modules or steps of the above-described embodiments of the present invention can be implemented using general-purpose computing devices. They can be centralized on a single computing device or distributed across a network of multiple computing devices. Optionally, they can be implemented using computer-executable program code, thereby storing them in a storage device for execution by a computing device. In some cases, the steps shown or described can be performed in a different order than those presented here, or they can be fabricated as separate integrated circuit modules, or multiple modules or steps can be fabricated as a single integrated circuit module. Thus, the embodiments of the present invention are not limited to any particular hardware and software combination.

[0046] The above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, various modifications and variations can be made to the embodiments of the present invention. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A method for generating aircraft wire numbers and matching them with connector hole numbers, characterized in that, include: Obtain all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment; Based on the conductor numbering rules, a conductor number is generated using the set number, the wire mark, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The wire number is parsed, and the set number and wire serial number are extracted from the wire number. The corresponding airborne equipment is determined by the set number, and the wire number is matched with the connector hole number of the airborne equipment by the wire serial number.

2. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in claim 1, characterized in that, Based on the attributes of all the airborne equipment and the wires connecting the airborne equipment, determine the wire's set number, wire marking, wire serial number corresponding to the wire marking, wire classification number, wire gauge, function code, electromagnetic compatibility code, and wire attributes, including: Identical airborne equipment is grouped into a single equipment group, and the airborne equipment in each equipment group is numbered sequentially. The generated number is then used as a set number. Determine the correspondence between the airborne equipment and the wire markers in the flight control system, and determine the wire markers corresponding to the airborne equipment through the correspondence; The connection relationship between the airborne devices is obtained, and the wire serial number corresponding to the wire mark is determined according to the connection relationship through the wire mark of the airborne device. The airborne device includes a computing device group, an execution sensing mechanism, an operating component, a power distribution system, an external communication system, a system detection port, and a flight control internal subsystem. Determine the wire identification number; The wire gauge is determined through electrical calculations based on the current that the conductor needs to carry and the voltage drop requirements of the line. Establish a functional correspondence between function codes and wires, and determine the function codes based on the function correspondence of the wires. Based on the signal transmission characteristics of the conductor, the electromagnetic compatibility code is determined through isolation design specifications; Based on the physical characteristics of the conductor, the wire properties are determined using a table that maps physical characteristics to wire properties.

3. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in claim 2, characterized in that, Determining the wire serial number corresponding to the wire marker based on the connection relationship using the wire marker on the airborne equipment includes: Based on the connection relationships between the airborne equipment, the wire serial number is divided into multiple functional zones, and wire serial numbers are assigned to the conductors according to the functional zones: The wires connecting the computing device group to the sensing mechanism are divided into a functional area; The wires connecting the operating components to the computing device group are divided into a functional area; The wires connecting the computer devices in the computing device group are divided into a functional area; The wires connecting the power distribution system to the computing device group, the power distribution system to the operating component, and the power distribution system to the actuating sensing mechanism are divided into a functional area; The wires connecting the external interconnection system to the computing device group are divided into a functional area; The wire from the system detection port to the computing device group is divided into a functional area.

4. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in claim 2, characterized in that, Determine the wire zone number, including: When there are multiple conductors connected in parallel or in series to form a parallel conductor group or a series conductor group, the starting letter is used as the wire identification number of the first conductor in the parallel conductor group or series conductor group. According to the wire connection sequence, when a wire is added to the parallel wire group or the series wire group, the subsequent letters are sequentially assigned as the corresponding wire identification number. Each wire identification number is unique in the parallel wire group or the series wire group to which it belongs. When a single wire passes through a transfer point during transmission and its function remains unchanged, after the transfer point, a subsequent letter is assigned to the single wire as a new wire identification number corresponding to the single wire, wherein each wire identification number remains unique in the transfer path. Each of the aforementioned wire zone numbers remains unique within the conductor group or transition path to which the wire zone number belongs.

5. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in claim 1, characterized in that, Based on the conductor numbering rules, a conductor number is generated using the set number, the wire marking, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes, including: The wire number is generated by combining the set number, the wire mark, the wire serial number corresponding to the wire mark, the identification number, the wire gauge, the separator, the function code, the electromagnetic compatibility code, and the wire attributes in sequence. The separator is a fixed character.

6. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in claim 1, characterized in that, Parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number, including: Parse the wire number and extract the set number and wire serial number from the wire number; Based on the serial number, the corresponding airborne equipment is determined, and the target connector on the airborne equipment is located. Obtain the set of connector hole numbers for the target connector; Establish a correspondence between the wire serial number and the connector hole number, so that each wire serial number corresponds one-to-one with the connector hole number.

7. The method for generating aircraft wire numbers and matching them with connector hole numbers as described in any one of claims 1 to 6, further comprising: When a fault occurs, receive fault information, which includes the wire number of the faulty wire; Parse the wire number to obtain the set number, the wire mark, and the wire serial number from the wire number; The airborne equipment is located based on the set number and the wire marking, and the connector hole number of the faulty wire on the target connector is located based on the wire serial number. The airborne equipment and the connector hole number are saved as fault location information.

8. A device for generating aircraft wire numbers and matching them with connector hole numbers, characterized in that, include: The wire parameter acquisition module is used to acquire all airborne equipment of the flight control system, and determine the wire set number, wire mark, wire serial number corresponding to the wire mark, wire identification number, wire gauge, function code, electromagnetic compatibility code and wire attributes based on the attributes of all the airborne equipment and the wires connecting the airborne equipment. The conductor numbering generation module is used to generate conductor numbers based on conductor numbering rules, using the set number, the wire mark, the wire serial number, the wire identification number, the wire gauge, the function code, the electromagnetic compatibility code, and the wire attributes. The hole number matching module is used to parse the wire number, extract the set number and wire serial number from the wire number, determine the corresponding airborne equipment through the set number, and match the wire number with the connector hole number of the airborne equipment through the wire serial number.

9. A computer device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, characterized in that, When the processor executes the computer program, it implements the method for generating wire numbers for the aircraft and matching them with connector hole numbers as described in any one of claims 1 to 7.

10. A computer-readable storage medium, characterized in that, The computer-readable storage medium stores a computer program that performs a method for generating wire numbering of an aircraft and matching it with connector hole numbers according to any one of claims 1 to 7.

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