Carbon footprint accounting method, device and equipment for airplane horizontal tail and medium

Abstract

The invention discloses a carbon footprint accounting method, device and equipment for an airplane horizontal tail and a medium. The method comprises the steps of determining total processing information corresponding to a target aircraft horizontal tail based on a preset design composition and a preset total process route corresponding to the target aircraft horizontal tail; generating a basic carbon emission list corresponding to the horizontal tail of the target aircraft based on the total processing information and preset process logic; determining basic carbon emission data corresponding to the target part process based on preset process basic information, and filling and processing the basic carbon emission data corresponding to the whole target part process in combination with a basic carbon emission list to generate a target part carbon footprint; and accounting and processing the target part carbon footprint based on preset mapping logic, and generating a full-flow carbon footprint corresponding to the target aircraft horizontal tail. According to the technical scheme of the invention, the method can achieve the accounting of the carbon footprint in the processing process of the horizontal tail of the airplane, reduces the complexity of the accounting of the carbon footprint, and improves the accuracy of the accounting of the carbon footprint.

Description

TECHNICAL FIELD

[0001] The present application relates to the field of aviation manufacturing technology, and in particular to a carbon footprint accounting method, device, equipment and medium for a horizontal tail of an airplane. BACKGROUND

[0002] With the rapid development of the aviation manufacturing field, the consumption of energy and materials also gradually increases, and a large amount of carbon emissions will also be generated. Therefore, it is urgent to implement effective energy-saving and emission-reducing strategies, rationally utilize resources, and optimize the production structure of aviation manufacturing enterprises. Currently, the development of energy-saving and emission-reducing strategies needs to be based on the carbon emission data of the research object, and carbon footprint accounting is the premise and basis for subsequent carbon diagnosis and carbon emission reduction.

[0003] The existing technology mainly accounts for the carbon footprint of a single part, that is, considers the composition of the part, and accumulates the carbon emissions generated by processing standard features into the carbon emissions generated by processing the part.

[0004] However, the method of the existing technology is relatively convenient for accounting for parts with relatively simple structures, but cannot meet the carbon footprint accounting of complex parts or assembled parts such as horizontal tails of airplanes. Therefore, how to account for the carbon footprint in the processing of the horizontal tail of the airplane, reduce the complexity of the carbon footprint accounting, and improve the accuracy of the carbon footprint accounting are the problems to be solved at present. SUMMARY

[0005] The present application provides a carbon footprint accounting method, device, equipment and medium for a horizontal tail of an airplane, which can solve the problems of high complexity and low accuracy of carbon footprint accounting in the processing of the horizontal tail of the airplane.

[0006] According to an aspect of the present application, a carbon footprint accounting method for a horizontal tail of an airplane is provided, comprising:

[0007] Based on the preset design composition and the preset total process route corresponding to the target horizontal tail of the airplane, the full-amount processing information corresponding to the target horizontal tail of the airplane is determined;

[0008] Based on the full-amount processing information and the preset process logic, a basic carbon emission inventory corresponding to the target horizontal tail of the airplane is generated; wherein the basic carbon emission inventory contains full-amount part processes corresponding to the target horizontal tail of the airplane;

[0009] Based on the preset process basic information, the basic carbon emission data corresponding to the target part process is determined, and the basic carbon emission data corresponding to the full-amount target part process is filled in combination with the basic carbon emission inventory to generate a target component carbon footprint;

[0010] The target aircraft tail plane corresponding whole-process carbon footprint is generated by accounting and processing the target component carbon footprint based on preset mapping logic, wherein the preset mapping logic is mapping logic between the aircraft tail plane manufacturing process and the design process.

[0011] According to another aspect of the present application, there is provided an aircraft tail plane carbon footprint accounting device, comprising:

[0012] An information determination module is configured to determine whole-amount processing information corresponding to the target aircraft tail plane based on preset design components and a preset total process route corresponding to the target aircraft tail plane.

[0013] An inventory generation module is configured to generate a basic carbon emission inventory corresponding to the target aircraft tail plane based on the whole-amount processing information and a preset process logic, wherein the basic carbon emission inventory comprises whole-amount component processes corresponding to the target aircraft tail plane.

[0014] A first generation module is configured to determine basic carbon emission data corresponding to the target component process based on preset process basic information, and fill in the basic carbon emission data corresponding to the whole-amount target component process based on the basic carbon emission inventory, to generate the target component carbon footprint.

[0015] A second generation module is configured to generate the target aircraft tail plane corresponding whole-process carbon footprint by accounting and processing the target component carbon footprint based on preset mapping logic, wherein the preset mapping logic is mapping logic between the aircraft tail plane manufacturing process and the design process.

[0016] According to another aspect of the present application, there is provided an electronic device, comprising:

[0017] at least one processor; and

[0018] a memory in communication with the at least one processor; wherein

[0019] The memory stores a computer program executable by the at least one processor, and the computer program is executed by the at least one processor to enable the at least one processor to execute the aircraft tail plane carbon footprint accounting method according to any one of the embodiments of the present application.

[0020] According to another aspect of the present application, there is provided a computer readable storage medium storing computer instructions for enabling a processor to implement the aircraft tail plane carbon footprint accounting method according to any one of the embodiments of the present application when executed by the processor.

[0021] According to another aspect of the present application, there is provided a computer program product comprising a computer program for implementing the aircraft tail plane carbon footprint accounting method according to any one of the embodiments of the present application when executed by a processor.

[0022] The technical scheme of the embodiment of the present application determines the full-amount processing information corresponding to the target aircraft tail plane through the preset design composition and the preset total process route corresponding to the target aircraft tail plane, and then generates the basic carbon emission inventory corresponding to the target aircraft tail plane based on the full-amount processing information and the preset process logic. Further, the basic carbon emission data corresponding to the target part process is determined based on the preset process basic information, and the basic carbon emission data corresponding to the full-amount target part process is filled and processed in combination with the basic carbon emission inventory to generate the target component carbon footprint. Finally, the target component carbon footprint is accounted and processed based on the preset mapping logic to generate the full-process carbon footprint corresponding to the target aircraft tail plane. The problem of high complexity and low accuracy of carbon footprint accounting in the aircraft tail plane processing process is solved, the carbon footprint in the aircraft tail plane processing process can be accounted, the complexity of carbon footprint accounting is reduced, and the accuracy of carbon footprint accounting is improved.

[0023] It should be understood that the content described in this part is not intended to identify the key or important features of the embodiments of the present application, nor is it intended to limit the scope of the present application. Other features of the present application will become apparent from the following description. BRIEF DESCRIPTION OF DRAWINGS

[0024] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed in the embodiment description will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application, and other drawings can be obtained by those skilled in the art without creative labor on the basis of these drawings.

[0025] Figure 1 is a flowchart of a carbon footprint accounting method of an aircraft tail plane according to an embodiment of the present application;

[0026] Figure 2 is a flowchart of a carbon footprint accounting method of an aircraft tail plane according to an embodiment of the present application;

[0027] Figure 3 is a process hierarchy structure diagram of an aircraft tail plane according to an embodiment of the present application;

[0028] Figure 4 is a structural schematic diagram of a carbon footprint accounting device of an aircraft tail plane according to an embodiment of the present application;

[0029] Figure 5 is a structural schematic diagram of an electronic device for implementing the carbon footprint accounting method of an aircraft tail plane according to an embodiment of the present application. DETAILED DESCRIPTION

[0030] In the following, the technical solutions in the embodiments of the present application will be described clearly and completely with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of embodiments of the present application, rather than all embodiments of the present application. Based on the embodiments in the present application, all other embodiments obtained by a person of ordinary skill in the art without creative work should fall within the protection scope of the present application.

[0031] It should be noted that the terms "first", "second", "target" and the like in the specification and claims of the present application and the above-described drawings are used to distinguish similar objects, and do not necessarily have to be used to describe a specific order or sequence. It should be understood that the data thus used can be interchanged under appropriate circumstances, so that the embodiments of the application described herein can be implemented in an order other than that illustrated or described herein. In addition, the terms "include" and "have" and any variations thereof are intended to cover non-exclusive inclusion, for example, a process, method, system, product or device that includes a series of steps or units does not have to be limited to those steps or units clearly listed, but can include other steps or units that are not clearly listed or inherent to these processes, methods, products or devices.

[0032] It should be noted that the acquisition, storage, use and processing of data in the technical solutions of the present application comply with the relevant provisions of national laws and regulations.

[0033] Embodiment one

[0034] Figure 1 A flowchart of a carbon footprint accounting method for an aircraft tail provided by the first embodiment of the present application. The present embodiment can be applicable to the case of accounting for the carbon footprint in the processing of an aircraft tail. The method can be executed by a carbon footprint accounting device for an aircraft tail, which can be realized in the form of hardware and / or software, and can be configured in an electronic device. As shown in the figure, the method comprises: Figure 1

[0035] S110, based on the preset design composition and the preset total process route corresponding to the target aircraft tail, determining the total processing information corresponding to the target aircraft tail.

[0036] ​The aircraft tail can refer to the horizontal tail mounted on both sides of the tail of the fuselage, which usually has the functions of longitudinal stability and pitch control. The target aircraft tail can refer to the aircraft tail that needs to be calculated for carbon footprint. The preset design composition can refer to the preset design structure of the aircraft tail. For example, the preset design composition can include the feature structure and geometric composition of the aircraft tail. Generally, the preset design composition is created by the research and development department, and can be directly obtained subsequently. The preset overall process route can refer to the preset process flow of the parts. For example, the preset overall process route can include the processing sequence of each part and the assembly sequence of each part.

[0037] The full-quantity machining information can refer to the machining information involved in the entire machining process of the target aircraft tail. In an optional embodiment, the full-quantity machining information can include: a station, a station, an assembly outline, an advance assembly outline, a component, and part machining information. The station can refer to the installation position of the part in the assembly process. The station can refer to an installation position with finer granularity than the station. Generally, a station can include multiple stations. The assembly outline (AO) can refer to a productive assembly process document prepared by the assembly process department to approve the assembly task of a specific product. The advance assembly outline (AAO) can refer to a productive assembly process document with finer granularity than the assembly outline. Generally, an assembly outline can include multiple advance assembly outlines. The component can refer to the single part information that constitutes the aircraft tail. For example, the component can include component number and component name. The part machining information can refer to the process information contained in the component machining link. For example, it can include machining product information, process parameters, tool information, and cutting fluid information.

[0038] It is worth noting that the machining process of the aircraft tail usually includes the part machining link and the assembly link. The part machining link includes the component and the part machining information, and the assembly link includes the station, the station, the assembly outline, and the advance assembly outline.

[0039] S120, generating a basic carbon emission inventory corresponding to the target aircraft tail based on the full-quantity machining information and the preset process logic; wherein the basic carbon emission inventory includes the full-quantity part process corresponding to the target aircraft tail.

[0040] The preset process logic can refer to the preset aircraft tail machining logic. For example, the preset process logic can be that the station is the top layer, the station is the second layer, the AO is the third layer, the AAO is the fourth layer, the component is the fifth layer, and the part machining information is the last layer.

[0041] The basic carbon emission list can refer to a carbon emission blank form corresponding to the target aircraft tail. Generally, the basic carbon emission list only contains a table header and a framework, and does not contain specific numerical values. For example, the basic carbon emission list can be a carbon-manufacture bill of material (C-MBOM).

[0042] Generally, the basic carbon emission list contains three carbon emission sources, namely, energy carbon, material carbon and process carbon. The energy carbon can refer to the carbon emission generated by energy consumption in the processing process. The material carbon can refer to the carbon generated by using water, gas or raw materials in the processing process. The process carbon can refer to the carbon generated when the waste generated after using consumables in the processing process is treated.

[0043] The part process can refer to a component machining process or a component assembly process. Generally, the component machining process can be determined by part machining information, and the component assembly process can be determined by an assembly outline and a prior assembly outline. In the embodiment of the present application, the component machining process can include eight typical processes, such as milling, turning, drilling, stamping, welding, quenching, normalizing and tempering. The component assembly process can include ten processes, such as positioning, hole making, deburring and cleaning, sealing, fastener installation, hole expansion, riveting, repair, disassembly and painting. The total part process can refer to all part processes in the aircraft tail processing process.

[0044] S130, determining the basic carbon emission data corresponding to the target part process based on the preset process basic information, and filling the basic carbon emission data corresponding to the total target part process in the basic carbon emission list to generate the target component carbon footprint.

[0045] The preset process basic information can refer to a preset process carbon emission list. The preset process basic information contains carbon emission data corresponding to each process. The target part process can refer to a specified query part process.

[0046] The basic carbon emission data can refer to carbon emission data corresponding to each target part process. Generally, the basic carbon emission data can include energy carbon emission data, material carbon emission data and process carbon emission data. The filling process can refer to the operation of filling the basic carbon emission data into the basic carbon emission list. The target component carbon footprint can refer to the total data generated after filling the basic carbon emission data corresponding to the total target part process into the basic carbon emission list.

[0047] S140, based on the preset mapping logic, accounting and processing the target component carbon footprint to generate a full-process carbon footprint corresponding to the target aircraft tail; wherein the preset mapping logic is a mapping logic between the aircraft tail manufacturing process and the design process.

[0048] The preset mapping logic can refer to a preset mapping logic between the aircraft tail manufacturing process and the design process. The process flow corresponding to the design process can be determined through the preset mapping logic. The full-process carbon footprint can refer to the total carbon emissions in the aircraft tail manufacturing process calculated according to the design process.

[0049] The technical scheme of the embodiment of the application determines the full-amount processing information corresponding to the target aircraft tail through the preset design composition and the preset total process route corresponding to the target aircraft tail, and then generates the basic carbon emission list corresponding to the target aircraft tail based on the full-amount processing information and the preset process logic. Further, the basic carbon emission data corresponding to the target part process is determined based on the preset process basic information, and the basic carbon emission data corresponding to the full-amount target part process is filled and processed in combination with the basic carbon emission list to generate the target component carbon footprint. Finally, the target component carbon footprint is accounted and processed based on the preset mapping logic to generate the full-process carbon footprint corresponding to the target aircraft tail. The problem of high complexity and low accuracy of carbon footprint accounting in the aircraft tail processing process is solved, the carbon footprint in the aircraft tail processing process can be accounted, the complexity of carbon footprint accounting is reduced, and the accuracy of carbon footprint accounting is improved.

[0050] Embodiment two

[0051] Figure 2 A flowchart of a carbon footprint accounting method of an aircraft tail according to the second embodiment of the application is provided. The present embodiment is based on the above-mentioned embodiment and is refined. In the present embodiment, the operation of generating the basic carbon emission list corresponding to the target aircraft tail based on the full-amount processing information and the preset process logic is refined, and can specifically include: determining the target process hierarchy corresponding to the target aircraft tail based on the preset process logic; sorting and processing the full-amount processing information based on the target process hierarchy to generate the basic carbon emission list corresponding to the target aircraft tail. As shown in FIG. 8, the method includes: Figure 2

[0052] S210, determining the full-amount processing information corresponding to the target aircraft tail based on the preset design composition and the preset total process route corresponding to the target aircraft tail.

[0053] Specifically, the full-amount processing information including the station, the station, the assembly outline, the preliminary assembly outline, the component assembly, and the part processing information involved in the entire processing process of the target aircraft tail is identified through the preset design composition and the preset total process route corresponding to the target aircraft tail.

[0054] S220, determining the target process hierarchy corresponding to the target aircraft tail based on the preset process logic.

[0055] ​The target process hierarchy can refer to a process tree structure corresponding to the target aircraft tail fin determined based on a preset process logic. Figure 3 An aircraft tail fin corresponding process hierarchy provided by the embodiment of the application is shown. Specifically, the target process hierarchy can mainly take AO as the core. Generally, the AOs are in assembly process relationship and do not form a nested structure. The workstation is the top layer, the station is the second layer, the AO is the third layer, the AAO is the fourth layer, the component is the fifth layer, and the part processing information (i.e., processing procedure) is the last layer. Generally, for the processing of an aircraft tail fin, the number of top layer workstations is 1, the number of stations under the workstation can be n, and each station can contain multiple AOs. For example, station 1 can contain i AOs, station 2 can contain j AOs, and station n can contain k AOs. The AO n,k under the nth station can represent the kth AO under the nth station. In addition, each AO can also contain multiple AAOs. For example, AO 1,1 may contain f AAOs, AO 2,1 may contain g AAOs, and AO n,1 may contain h AAOs. The AAO n,1,h under the first AO under the nth station can represent the hth AAO under the first AO under the nth station. In addition, each AAO can contain m components, and each component can contain s processing procedures.

[0056] It is worth noting that for the AOs with AAOs, the AAO nodes are regarded as lower nodes of the hanging AO nodes, i.e., in the same level as the component nodes of the hanging AO. When the component nodes of the AAO appear in the next layer of the AO node, the AO and the AAO form a nested structure.

[0057] S230, sorting the full amount of processing information based on the target process hierarchy to generate a basic carbon emission inventory corresponding to the target aircraft tail fin.

[0058] The sorting process can refer to the operation of logically sorting the full amount of processing information.

[0059] It is worth noting that in the embodiment of the application, while sorting the full amount of processing information according to the target process hierarchy, each process can also be numbered and modularized to facilitate the implementation of subsequent filling processing operations. Specifically, after determining the target process hierarchy corresponding to the target aircraft tail fin, the component processing procedure can be determined according to the part processing information, and the component assembly procedure can be determined according to the component and the corresponding assembly outline and the preceding assembly outline. Then, according to the target process hierarchy, each component processing procedure and component assembly procedure is numbered and modularized, and the full amount of processing information is sorted to generate a basic carbon emission inventory.

[0060] Exemplarily, in the full-quantity processing information corresponding to the target aircraft tail plane, the station is A, the station position is station position A1, the component is component No. A1.1, the part No. is part No. A1.1.1, and the part processing information is blanking, milling, deburring, trimming and inspection. Then, the component assembly process can be determined according to the part No. A1.1.1 and the corresponding assembly outline and the preceding assembly outline, the component processing process can be determined according to the part processing information, which is blanking, milling, deburring, trimming and inspection, and then, the component processing process and the component assembly process are numbered and modularized according to the target process hierarchy, for example, the blanking is numbered as process 1, the milling is numbered as process 2, the deburring and trimming are numbered as process 3, and the inspection is numbered as process 4. Finally, the full-quantity processing information is sorted according to the target process hierarchy, and the basic activity data items of material carbon, energy carbon and process carbon and the part carbon source data items during the processing are added, to generate the basic carbon emission list as shown in Table 1.

[0061] Table 1 Basic carbon emission list corresponding to target aircraft tail plane

[0062]

[0063] It is worth noting that if the full-quantity processing information contains multiple station positions or components, the station positions or components can be sequentially arranged according to the target process hierarchy, and if multiple station positions have the same number, a secondary station position can be established. Exemplarily, a secondary station position Ax can be established for station position A1 and station position A2.

[0064] S240, determining the target emission source and the target process parameter corresponding to the target part process based on the preset process basic information.

[0065] The target emission source can refer to the carbon emission production source corresponding to the target part process. Exemplarily, the target emission source can be energy carbon, material carbon and process carbon. The target process parameter can refer to the device working parameter or calculation coefficient corresponding to the target part process.

[0066] S250, determining the target accounting model corresponding to the target emission source, and determining the basic carbon emission data corresponding to the target part process based on the target accounting model and the target process parameter.

[0067] The target accounting model can refer to the accounting model of the target part process under the target emission source.

[0068] Specifically, in the part processing link, if the target part process is milling, the energy carbon includes machine tool cutting power consumption and peripheral auxiliary power consumption, and the target accounting model of the machine tool cutting power consumption is: E cutting +E spindle+E standby +E additional +E fluid +E gas wherein, E spindle = (k1·n+b)·t spindle , E standby = P standby ·t standby , E fluid = P fluid ·t fluid , The target process parameters include: cutting force influence index C F , cutting force calculation related indexes x F , y F , mu F , q F and w F , cutting force correction coefficient K F when milling condition changes, diameter d0 of the milling cutter, cutting time t cutting , cutting width a e , cutting depth a p , spindle frequency f z , spindle idle power coefficient k1 and b, spindle speed n, spindle working time t spindle , machine tool standby energy consumption P standby , standby time t standby , linear function calculation coefficient a0, quadratic function calculation coefficient a1, cutting consumption power P cutting , additional time t additional , cutting fluid consumption power P fluid , cutting fluid time t fluid , compressor rated power P rated , single working cycle gas production time t work , compressor single working cycle usage time t use , compressor working time t gas ; The target accounting model of peripheral auxiliary power consumption is: P public ·T p ·Ce electricity ×3.6×10 -6 , The target process parameters include: public energy consumption power P public , machine tool processing time T p , and local power grid carbon emission factor Ce electricity . The material carbon includes cutting fluid, and the corresponding target accounting model is: wherein, V fluid,replace = V fluid,original + V fluid,added N fluid , Cefluid =Ce fluid,production +Ce fluid,disposal The target process parameters include: initial cutting fluid volume V fluid,original , the volume of cutting fluid added each time V fluid,added , the number of times the cutting fluid is replenished during the cutting fluid replacement cycle N fluid , carbon emission coefficient of cutting fluid production Ce fluid,production And the carbon emission coefficient Ce of waste cutting fluid fluid,disposal The process carbon includes tool wear and waste chip treatment, among which the target calculation model of tool wear is: Target process parameters include: tool regrinding times n tool , carbon emission coefficient Ce when producing cutting tools tool,production , Carbon emission coefficient when dealing with worn tools, Ce tool,disposal , the carbon emissions generated by a single tool regrinding Ce tool,regringding , the mass of the new knife used is m tool The target calculation model for tool life T and waste disposal is: MRV total ρ material ×[(1-η recycling )×Ce material +η recycling E recycling ×Ce electricity ]×10 -9 , the target process parameters include: total material removal volume MRV of each process total , workpiece material density ρ material , chip recovery rate η recycling , carbon emission coefficient of workpiece material Ce material , Chip recovery energy consumption per unit mass E recycling and the carbon emission factor Ce of the local power grid electricity .

[0069] If the target part process is turning, then the energy carbon includes electricity, and the corresponding target accounting model is: CEF elec EC machine , where EC machine =P u ·t idle +P i ·t c Target process parameters include: Electricity carbon emission factor CEF elec , no-load power P u , input power P i , no-load time t idle and cutting time t c Material carbon includes cutting materials, cutting fluids and tool preparation. The target calculation model for cutting materials is: CEF m× M chip , wherein CEF m = EE ce × CEF ce , M chip = Q × t c × ρ / 10 6 . The target process parameters include: material energy-carrying energy equivalent EE ce , carbon emission factor CEF ce of standard coal, material removal rate Q and material density ρ; the target accounting model corresponding to the cutting fluid is: wherein CE oil = CEF oil × (CC+AC), CE wc = CEF wc × [(CC+AC) / δ]. The target process parameters include: initial cutting oil consumption CC, additional cutting oil consumption AC, cutting fluid concentration δ, cutting fluid replacement period T coolant , carbon emission CEF oil caused by cutting oil waste disposal, carbon emission CEF wc caused by cutting fluid waste disposal, idle time t idle ; the target accounting model corresponding to the tool preparation is: The target process parameters include: tool life T tool , tool carbon emission factor CEF tool and tool weight W tool ; the target accounting model corresponding to the process carbon containing waste chip disposal is: CEF chip × M chip , wherein CEF chip = CEF ce × EC ce . The target process parameters include: consumption of standard coal EC ce consumed per unit mass of waste chip and mass M chip of the waste chip.

[0070] If the target part process is drilling, the energy carbon contains electric energy, and the target accounting model corresponding thereto is: wherein p u = a+bn+cn 2 , p a = α·p m , The target process parameters include: power fitting coefficients a, b and c, spindle speed n, torque influence coefficient C T , workpiece diameter or tool outer diameter d0, hole diameter torque influence index z T , feed amount f, and feed amount torque influence index y T, drilling conditions change the torque correction coefficient k T , additional load loss coefficient α processing time t m and preparation time t p Material carbon includes cutting fluid, and the corresponding target calculation model is: Target process parameters include: Carbon emission factor C of cutting fluid production pe , processing cutting fluid carbon emission factor C de , cutting fluid replacement cycle C L And the cutting fluid volume V. Process carbon includes tool preparation, and the corresponding target calculation model is: T f m t β, where Target process parameters include: Tool production carbon emission factor T f , tool weight m t And the tool wear rate β. Among them, the tool durability, that is, the tool life is T.

[0071] If the target part process is stamping, and the energy carbon includes electrical energy, the corresponding target accounting model is: in, The target process parameters include: energy conversion coefficient η, sheet thickness t, punch stroke h, punch corner radius r p , die corner radius r d , stroke H, plate width b, friction coefficient μ and punch-die gap c. Among them, M Q is the bending moment caused by the internal stress of the sheet, and θ is the bending angle. Material carbon includes lost material and tool loss, among which the target calculation model corresponding to lost material is: CEF m ·M chip , among which, CEF m =EE m ·CEF ce , M chip =M output -M input The target process parameters include: material energy EE m , standard coal carbon emission factor CEF ce , rough M input And product M output The target calculation model corresponding to tool loss is: Target process parameters include: tool regrinding times n tool , carbon emission coefficient Ce when producing cutting tools tool,production , Carbon emission coefficient Ce when dealing with worn tools tool,disposal , the carbon emissions generated by a single tool regrinding Ce tool,regringding , the mass of the new knife used is m tool , cutting time tcutting and tool life T.

[0072] If the target part process is welding, the energy carbon includes laser, robot, cooling system, air compressor and wire feeding system. Among them, the target accounting model corresponding to the laser is: The target process parameters include: electric energy carbon emission coefficient CEF elec (i.e. CEF electricity ), laser idle state power P lws , laser idle state duration t lws , laser processing state power P lwo , laser processing state duration t lwo and energy conversion efficiency η. The target accounting model corresponding to the robot is: CEF elec ·(P rs ·t rs +P m ·t m ), and the target process parameters include: robot standby average power P rs , robot motion state average power P m , standby state duration t rs and motion state duration t m . The target accounting model corresponding to the cooling system is: CEF elec ·(P cs ·t cs +P con ·t con ), and the target process parameters include: cooling system standby average power P cs , cooling system running state average power P con , standby state duration t cs and running state average power t con . The target accounting model corresponding to the air compressor is: CEF elec ·P compressor ·t compressor , wherein, The target process parameters include: compressed air on time t compressor , gas density ρ ca , gas flow rate Q ca , heat capacity c p,ca , heat capacity ratio k, temperature T0 in the environment state, pressure p1 before compression and pressure p2 after compression. The target accounting model corresponding to the wire feeding system is: CEF elec ·P w ·t w , and the target process parameters include: wire feeding average power P w and wire feeding time t wThe material carbon includes cooling liquid, protective gas and welding wire. The cooling liquid corresponds to a target accounting model: wherein, The target process parameters include: inert protective gas carbon emission coefficient CEF cf , cooling system cooling liquid volume V f , cooling liquid density p f , cooling liquid specific heat capacity C f , temperature difference between actual temperature inside the laser and ambient temperature, volume V cf of consumed cooling liquid, cooling liquid replacement period T w and laser energy conversion efficiency lw . The target accounting model corresponding to the protective gas is: CEF Ar ·Q Ar ·t Ar , and the target process parameters include: inert protective gas carbon emission coefficient CEF Ar , inert gas flow rate Q Ar and argon gas opening time t Ar . The target accounting model corresponding to the welding wire is: CEF wire ·p w ·S·v w ·t lwo , and the target process parameters include: welding wire carbon emission coefficient CEF wire , welding wire density p w , welding wire cross-sectional area S and wire feeding speed v w .

[0073] If the target part process is quenching, the energy carbon includes electric energy under the actual parameter method and electric energy under the standard conversion method. The target accounting model corresponding to the electric energy under the actual parameter method is: EF electricity ·(Q 工蓄 +Q 辅助 +Q 散热 +Q 设蓄 +Q 其他 ), wherein Q 工蓄 =c 工 ·m 工 ·(t 介 -t 工 ), Q 辅助 =c 辅 ·m 辅 ·(t 介 -t 工 ), Q 设蓄 =m 炉衬1 ·c1·(t 介 -t 工 )+m 炉衬2 ·c2·(t 介 -t工 ), Target process parameters include: overall heat transfer coefficient α of furnace wall outer surface to air gap, carbon emission coefficient EF of electric energy electricity , medium temperature t 介 , workpiece temperature t 工 , specific heat capacity c 工 , workpiece mass m 工 , auxiliary component specific heat capacity c 辅 , auxiliary component mass m 辅 , average area F of equipment furnace lining structure, thickness s of furnace wall, thermal conductivity 1 λ1, thermal conductivity 2 λ2, overall heat transfer coefficient α to air 空 , mass m of furnace lining 1 炉衬1 , mass c1 of furnace lining 2, specific heat capacity c2 of furnace lining 2 material. The target accounting model corresponding to the electric energy under the standard conversion method is: EF electricity ·N b ·k1·k2·k3·k4·k5·m 工 , target process parameters include: conversion process coefficient k1, heating mode coefficient k2, production mode coefficient k3, workpiece material coefficient k4, loading coefficient k5 and standard process electric energy consumption N b .

[0074] If the target part process is normalizing, the energy carbon includes the electric energy under the actual parameter method and the electric energy under the standard conversion method. Among them, the target accounting model corresponding to the electric energy under the actual parameter method is: EF electricity ·(Q 工蓄 +Q 辅助 +Q 散热 +Q 设蓄 +Q 其他 ), wherein Q 工蓄 =c 工 ·m 工 ·(t 介 -t 工 ), Q 辅助 =c 辅 ·m 辅 ·(t 介 -t 工 ), Q 设蓄 =m 炉衬1 ·c1·(t 介 -t 工 )+m 炉衬2 ·c2·(t 介 -t 工 ), Target process parameters include: carbon emission coefficient EF of electric energy electricity , medium temperature t 介 , workpiece temperature t 工 , specific heat capacity c 工, workpiece mass m 工 , auxiliary component specific heat capacity c 辅 , auxiliary component mass m 辅 , average area F of the equipment furnace lining structure, thickness s of the furnace wall, thermal conductivity 1 λ1, thermal conductivity 2 λ2, total heat transfer coefficient α to air 空 , mass m of the furnace lining 1 炉衬1 , mass c1 of the furnace lining 2, specific heat capacity c2 of the furnace lining 2 material. The target accounting model corresponding to the electric energy under the standard conversion method is: EF electricity ·N b ·k1·k2·k3·k4·k5·m 工 , The target process parameters include: conversion process coefficient k1, heating mode coefficient k2, production mode coefficient k3, workpiece material coefficient k4, loading coefficient k5 and standard process electric energy consumption N b .

[0075] If the target part process is tempering, the energy carbon includes the electric energy under the actual parameter method and the electric energy under the standard conversion method. Among them, the target accounting model corresponding to the electric energy under the actual parameter method is: EF electricity ·(Q 工蓄 +Q 辅助 +Q 散热 +Q 设蓄 +Q 其他 ), wherein Q 工蓄 =c 工 ·m 工 ·(t 介 -t 工 ), Q 辅助 =c 辅 ·m 辅 ·(t 介 -t 工 ), Q 设蓄 =m 炉衬1 ·c1·(t 介 -t 工 )+m 炉衬2 ·c2·(t 介 -t 工 ), The target process parameters include: electric energy carbon emission coefficient EF electricity , medium temperature t 介 , workpiece temperature t 工 , specific heat capacity c 工 , workpiece mass m 工 , auxiliary component specific heat capacity c 辅 , auxiliary component mass m 辅 , average area F of the equipment furnace lining structure, thickness s of the furnace wall, thermal conductivity 1 λ1, thermal conductivity 2 λ2, total heat transfer coefficient α to air 空 , mass m of the furnace lining 1炉衬1 , the quality c1 of the furnace lining 2, the specific heat capacity c2 of the furnace lining 2 material. The target accounting model corresponding to the electric energy under the standard conversion method is: EF electricity ·N b ·k1·k2·k3·k4·k5·m 工 , the target process parameters include: the conversion process coefficient k1, the heating mode coefficient k2, the production mode coefficient k3, the workpiece material coefficient k4, the loading coefficient k5, and the standard process electric energy consumption N b .

[0076] In the assembly link, if the target part process is positioning, the carbon emission elements can be positioning man-hours and support facility electric energy consumption; if the target part process is hole making, the carbon emission elements can be drilling quantity, drilling man-hours, and air drill gas flow consumption; if the target part process is deburring and cleaning, the carbon emission elements can be dust collector operating power, cleaning agent consumption, and man-hours; if the target part process is sealing, the carbon emission elements can be sealing glue type, sealing glue consumption, and sealing man-hours; if the target part process is fastener installation, the carbon emission elements can be standard parts (such as bolt consumption) or fastening pneumatic tool compressed air consumption; if the target part process is reaming, the carbon emission elements can be reaming man-hours and reaming tool compressed air gas flow consumption; if the target part process is riveting, the carbon emission elements can be rivet model, riveting tool, riveting man-hours, and pneumatic riveter compressed air gas flow consumption; if the target part process is repair, the carbon emission elements can be repair tool, repair man-hours, and repair pneumatic equipment unit time compressed air gas flow consumption; if the target part process is disassembly, the carbon emission elements can be disassembly tool, disassembly man-hours, and disassembly tool energy consumption; if the target part process is painting, the carbon emission elements can be paint, paint consumption, and painting man-hours.

[0077] It is worth noting that the units of each target process parameter in the embodiment of the application can be uniformly set according to standard measurement units, and the embodiment of the application does not limit this.

[0078] S260, determining a data filling position corresponding to the target part process based on the basic carbon emission list.

[0079] The data filling position can refer to a data storage position corresponding to the target part process. For example, the data filling position can be determined by the name corresponding to the target part process and the basic structure of the basic carbon emission list.

[0080] S270, filling the basic carbon emission data corresponding to the target part process based on the data filling position to generate a basic component carbon footprint.

[0081] The basic component carbon footprint can refer to individual carbon emission data corresponding to each target part process.

[0082] S280, combine the total basic component carbon footprints to generate a target component carbon footprint.

[0083] Specifically, after generating the basic component carbon footprint corresponding to each target part process, all the basic component carbon footprints can be combined in sequence, and then the target component carbon footprint is generated.

[0084] S290, determine the target mapping logic between the manufacturing process and the design process of the target aircraft tail fin based on the preset mapping logic.

[0085] The target mapping logic can refer to the logical mapping relationship between the manufacturing process and the design process of the target aircraft tail fin. Generally, the logical structure of the manufacturing process and the design process of the target aircraft tail fin is different, so the manufacturing process and the design process need to be associated through the target mapping logic.

[0086] S2100, determine the selected carbon footprint in the target component carbon footprint and the accounting superposition logic between each selected carbon footprint based on the target mapping logic.

[0087] The selected carbon footprint can refer to the carbon footprint selected for accounting in the target component carbon footprint according to the target mapping logic. For example, the target component carbon footprint includes the total carbon emissions of each part process in the target aircraft tail fin manufacturing process under the three carbon emission sources of energy carbon, material carbon and process carbon, and then the target mapping logic can select the part process that needs to be accounted for. Finally, the total carbon emissions of the part process are selected as the selected carbon footprint, which provides an effective basis for subsequent operations.

[0088] The accounting superposition logic can refer to a pre-set carbon footprint superposition logic structure. For example, in the embodiment of the application, the accounting superposition logic can be sequential accumulation.

[0089] S2110, account for the selected carbon footprint based on the accounting superposition logic to generate a total process carbon footprint corresponding to the target aircraft tail fin.

[0090] Specifically, after determining the selected carbon footprint in the target component carbon footprint and the accounting superposition logic between each selected carbon footprint, each selected carbon footprint can be accounted for according to the accounting superposition logic, and then a total process carbon footprint corresponding to the target aircraft tail fin is generated.

[0091] In an optional embodiment, after the accounting processing of the candidate carbon footprints based on the accounting superposition logic generates the full-process carbon footprint corresponding to the target aircraft tail plane, it can further include: determining the occupation proportion corresponding to each of the candidate carbon footprints based on the full-process carbon footprint; sorting the occupation proportions corresponding to each of the candidate carbon footprints to determine the target candidate carbon footprint corresponding to the highest occupation proportion; and generating an evaluation result corresponding to the target candidate carbon footprint based on the highest occupation proportion. The occupation proportion can refer to the proportion coefficient of each individual candidate carbon footprint relative to the full-process carbon footprint. For example, the occupation proportion corresponding to each candidate carbon footprint can be determined by dividing the candidate carbon footprint by the full-process carbon footprint. The target candidate carbon footprint can refer to the candidate carbon footprint corresponding to the highest occupation proportion. In this way, by determining the target candidate carbon footprint and the highest occupation proportion, an evaluation result, such as the highest carbon emission of milling, can be generated for the manufacturing process of the target aircraft tail plane, providing a basis for improvement for subsequent manufacturing processes.

[0092] The technical scheme of the embodiment of the present application determines the full-amount machining information corresponding to the target aircraft tail plane based on the preset design composition and the preset total process route corresponding to the target aircraft tail plane, and then determines the target process hierarchy structure corresponding to the target aircraft tail plane based on the preset process logic, sorts the full-amount machining information based on the target process hierarchy structure, generates the basic carbon emission list corresponding to the target aircraft tail plane, further determines the target emission source and the target process parameter corresponding to the target part process based on the preset process basic information, determines the target accounting model corresponding to the target emission source, determines the basic carbon emission data corresponding to the target part process based on the target accounting model and the target process parameter, determines the data filling position corresponding to the target part process based on the basic carbon emission list, fills the basic carbon emission data corresponding to the target part process based on the data filling position, generates the basic component carbon footprint, combines the full-amount basic component carbon footprint, generates the target component carbon footprint, finally determines the target mapping logic between the manufacturing process and the design process corresponding to the target aircraft tail plane based on the preset mapping logic, determines the candidate carbon footprint in the target component carbon footprint and the accounting superposition logic between each of the candidate carbon footprints based on the target mapping logic, and generates the full-process carbon footprint corresponding to the target aircraft tail plane by accounting processing the candidate carbon footprint based on the accounting superposition logic. The technical scheme solves the problems of high complexity and low accuracy of carbon footprint accounting in the aircraft tail machining process, can account for the carbon footprint in the aircraft tail machining process, reduces the complexity of carbon footprint accounting, and improves the accuracy of carbon footprint accounting.

[0093] Embodiment Three

[0094] Figure 4 A structural schematic diagram of an aircraft tail carbon footprint accounting device provided by Embodiment Three of the present application is shown in FIG. 3. Figure 4As shown, the device comprises: an information determining module 310, a list generating module 320, a first generating module 330, and a second generating module 340;

[0095] The information determining module 310 is configured to determine full-amount processing information corresponding to the target aircraft tail fin based on preset design composition and a preset overall process route corresponding to the target aircraft tail fin.

[0096] The list generating module 320 is configured to generate a basic carbon emission list corresponding to the target aircraft tail fin based on the full-amount processing information and a preset process logic; wherein the basic carbon emission list comprises full-amount part processes corresponding to the target aircraft tail fin.

[0097] The first generating module 330 is configured to determine basic carbon emission data corresponding to a target part process based on preset process basic information, and fill in the basic carbon emission data corresponding to the full-amount target part process based on the basic carbon emission list to generate a target component carbon footprint.

[0098] The second generating module 340 is configured to account for the target component carbon footprint based on a preset mapping logic to generate a full-process carbon footprint corresponding to the target aircraft tail fin; wherein the preset mapping logic is a mapping logic between the aircraft tail fin manufacturing process and the design process.

[0099] The technical scheme of the embodiment of the present application determines the full-amount processing information corresponding to the target aircraft tail fin based on the preset design composition and the preset overall process route corresponding to the target aircraft tail fin, and then generates the basic carbon emission list corresponding to the target aircraft tail fin based on the full-amount processing information and the preset process logic, further determines the basic carbon emission data corresponding to the target part process based on the preset process basic information, fills in the basic carbon emission data corresponding to the full-amount target part process based on the basic carbon emission list to generate the target component carbon footprint, and finally accounts for the target component carbon footprint based on the preset mapping logic to generate the full-process carbon footprint corresponding to the target aircraft tail fin, thereby solving the problem of high complexity and low accuracy of carbon footprint accounting in the aircraft tail fin processing process, and enabling the carbon footprint in the aircraft tail fin processing process to be accounted for, reducing the complexity of carbon footprint accounting and improving the accuracy of carbon footprint accounting.

[0100] Optionally, the list generating module 320 can be specifically configured to:

[0101] determine a target process hierarchy corresponding to the target aircraft tail fin based on a preset process logic;

[0102] sort and process the full-amount processing information based on the target process hierarchy to generate the basic carbon emission list corresponding to the target aircraft tail fin.

[0103] Optionally, the first generating module 330 can be specifically configured to:

[0104] determine a target emission source and a target process parameter corresponding to the target part process based on the preset process basic information;

[0105] determine a target accounting model corresponding to the target emission source, and determine the basic carbon emission data corresponding to the target part process based on the target accounting model and the target process parameter.

[0106] Optionally, the first generation module 330 can be specifically used for:

[0107] determine a data filling position corresponding to the target part process based on the basic carbon emission inventory;

[0108] fill the basic carbon emission data corresponding to the target part process based on the data filling position, and generate a basic component carbon footprint;

[0109] combine the full-amount basic component carbon footprint to generate a target component carbon footprint.

[0110] Optionally, the second generation module 340 can be specifically used for:

[0111] determine a target mapping logic between the manufacturing process and the design process corresponding to the target aircraft tail based on a preset mapping logic;

[0112] determine a selected carbon footprint in the target component carbon footprint and an accounting superposition logic between each selected carbon footprint based on the target mapping logic;

[0113] account for the selected carbon footprint based on the accounting superposition logic to generate a full-process carbon footprint corresponding to the target aircraft tail.

[0114] Optionally, the aircraft tail carbon footprint accounting device can further include an evaluation result generation module, configured to determine an occupancy ratio corresponding to each selected carbon footprint based on the full-process carbon footprint after the selected carbon footprint is accounted for based on the accounting superposition logic to generate a full-process carbon footprint corresponding to the target aircraft tail; sort the occupancy ratios corresponding to each selected carbon footprint to determine a target selected carbon footprint corresponding to a highest occupancy ratio; and generate an evaluation result corresponding to the target selected carbon footprint based on the highest occupancy ratio.

[0115] Optionally, the full-amount processing information includes: a work station, a station, an assembly outline, a prior assembly outline, a component processing information, and a part processing information.

[0116] The aircraft tail carbon footprint accounting device provided in the embodiments of the present application can execute the aircraft tail carbon footprint accounting method provided in any of the embodiments of the present application, and has the corresponding function modules and beneficial effects of the execution method.

[0117] Embodiment Four

[0118] Figure 5 A structural diagram of an electronic device 410 that can be used to implement embodiments of the present application is shown. The electronic device is intended to represent various forms of digital computers, such as laptops, desktops, tablets, personal digital assistants, servers, blade servers, mainframes, and other appropriate computers. The electronic device can also represent various forms of mobile devices, such as personal digital assistants, cellular telephones, smartphones, wearable devices (e.g., headsets, glasses, watches, etc.), and other similar computing devices. The components shown here, their connections and relationships, and their functions, are meant to be examples only, and are not meant to limit implementations of the present application described and / or claimed in this document.

[0119] As shown in Figure 5 The electronic device 410 includes at least one processor 420, and a memory, such as a read-only memory (ROM) 430, a random access memory (RAM) 440, etc., connected to the at least one processor 420, where the memory stores computer programs executable by the at least one processor. The processor 420 can perform various appropriate actions and processes according to the computer programs stored in the read-only memory (ROM) 430 or loaded into the random access memory (RAM) 440 from the storage unit 490. In the RAM 440, various programs and data required for the operation of the electronic device 410 can also be stored. The processor 420, the ROM 430, and the RAM 440 are connected to each other through a bus 450. An input / output (I / O) interface 460 is also connected to the bus 450.

[0120] Various components in the electronic device 410 are connected to the I / O interface 460, including an input unit 470, such as a keyboard, a mouse, etc., an output unit 480, such as various types of displays, a speaker, etc., a storage unit 490, such as a magnetic disk, an optical disk, etc., and a communication unit 4100, such as a network card, a modem, a wireless communication transceiver, etc. The communication unit 4100 allows the electronic device 410 to exchange information / data with other devices through a computer network, such as the Internet, and / or various telecommunication networks.

[0121] The processor 420 can be various general and / or special purpose processing components with processing and computing capabilities. Some examples of the processor 420 include, but are not limited to, a central processing unit (CPU), a graphics processing unit (GPU), various special-purpose artificial intelligence (AI) computing chips, various processors running machine learning model algorithms, a digital signal processor (DSP), and any appropriate processor, controller, microcontroller, etc. The processor 420 performs various methods and processes described above, such as the carbon footprint accounting method for aircraft tailplanes.

[0122] The method comprises:

[0123] determining full-amount processing information corresponding to the target aircraft tail fin based on preset design composition and preset total process route corresponding to the target aircraft tail fin;

[0124] generating a basic carbon emission inventory corresponding to the target aircraft tail fin based on the full-amount processing information and preset process logic; wherein the basic carbon emission inventory comprises full-amount part processes corresponding to the target aircraft tail fin;

[0125] determining basic carbon emission data corresponding to the target part process based on preset process basic information, and filling the basic carbon emission data corresponding to the full-amount target part process based on the basic carbon emission inventory to generate a target component carbon footprint;

[0126] processing the target component carbon footprint based on preset mapping logic to generate a full-process carbon footprint corresponding to the target aircraft tail fin; wherein the preset mapping logic is a mapping logic between the aircraft tail fin manufacturing process and the design process.

[0127] In some embodiments, the carbon footprint accounting method of the aircraft tail fin can be implemented as a computer program tangibly embodied in a computer readable storage medium, such as storage unit 490. In some embodiments, part or all of the computer program can be loaded and / or installed onto electronic device 410 via ROM 430 and / or communication unit 4100. When the computer program is loaded into RAM 440 and executed by processor 420, one or more steps of the carbon footprint accounting method of the aircraft tail fin described above can be performed. Alternatively, in other embodiments, processor 420 can be configured to perform the carbon footprint accounting method of the aircraft tail fin by any other suitable means, such as by means of firmware.

[0128] The various implementations of the systems and techniques described above can be realized in digital electronic circuitry, integrated circuitry, specially designed application specific integrated circuits (ASICs), field programmable gate arrays (FPGAs) computer hardware, firmware, software, and / or combinations thereof. These various implementations can include implementation in one or more computer programs that are executable and / or interpretable on a programmable system including at least one programmable processor, which can be special or general purpose, coupled to receive data and instructions from, and to transmit data and instructions to, a storage system, at least one input device, and at least one output device.

[0129] Computer programs for implementing the methods of the present application can be written in any combination of one or more programming languages. These computer programs can be provided to a processor of a general purpose computer, special purpose computer, or other programmable data processing apparatus, such that the computer program, when executed, can cause instructions defined in the flow charts and / or block diagrams to be implemented. The computer program can be executed entirely on a machine, partially on a machine, partially on a machine as a stand-alone software package, and partially on a remote machine or entirely on a remote machine or server.

[0130] In the context of the present application, a computer-readable storage medium can be a tangible medium that can contain or store a computer program for use by or in connection with an instruction execution system, apparatus, or device. A computer-readable storage medium can include, but is not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any suitable combination of the foregoing. Alternatively, a computer-readable storage medium can be a machine-readable signal medium. More specific examples of a machine-readable storage medium will include one or more lines of electrical connections, 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.

[0131] To provide for interaction with a user, the systems and techniques described here can be implemented on an electronic device having a display device (e.g., a CRT (cathode ray tube) or LCD (liquid crystal display) monitor) for displaying information to the user and a keyboard and a pointing device (e.g., a mouse or a trackball) by which the user can provide input to the electronic device. Other kinds of devices can be used to provide for interaction with a user as well; for example, feedback provided to the user can be any form of sensory feedback (e.g., visual feedback, auditory feedback, or tactile feedback); and input from the user can be received in any form, including acoustic, speech, or tactile input.

[0132] The systems and techniques described herein can be implemented in a computing system that includes a back end component, e.g., as a data server, or that includes a middleware component, e.g., an application server, or that includes a front end component, e.g., a user computer having a graphical user interface or a Web browser through which a user can interact with an implementation of the systems and techniques described herein, or any combination of such back end, middleware, or front end components. The components of the system can be interconnected by 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), a blockchain network, and the Internet.

[0133] The computing system can include clients and servers. A client and server are generally remote from each other and typically interact through a communication network. The relationship of client and server arises by virtue of computer programs running on the respective computers and having a client-server relationship to each other. A server can be a cloud server, also known as a cloud computing server or cloud host, which is a host product in the cloud computing service system, to solve the defects of large management difficulty and weak business scalability in traditional physical host and VPS service.

[0134] The embodiments of the present application further disclose a computer program product, which comprises a computer program, and the computer program, when executed by a processor, implements the aircraft tailplane carbon footprint accounting method provided in any of the embodiments of the present application. The program product and the aircraft tailplane carbon footprint accounting method disclosed in the embodiments of the present application belong to the same inventive concept, and thus will not be repeated here.

[0135] It should be understood that the various forms of flow shown above can be reordered, added to, or deleted from without departing from the scope of the present application. For example, the steps described in the present application can be executed in parallel, in sequence, or in a different order, and the present application is not limited herein.

[0136] The above detailed description does not constitute a limitation on the protection scope of the present application. Those skilled in the art should understand that various modifications, combinations, sub-combinations, and substitutions can be made according to design requirements and other factors. Any modification, equivalent replacement, and improvement within the spirit and principles of the present application shall be included in the protection scope of the present application.

Claims

1. A method for calculating the carbon footprint of an aircraft horizontal tail, characterized in that: include: Determine the full processing information corresponding to the horizontal tail of the target aircraft based on the preset design components and the preset overall process route corresponding to the horizontal tail of the target aircraft; Generate a basic carbon emission inventory corresponding to the horizontal tail of the target aircraft based on the full processing information and the preset process logic; wherein the basic carbon emission inventory includes the full number of parts and processes corresponding to the horizontal tail of the target aircraft; Determine the basic carbon emission data corresponding to the target part process based on the preset process basic information, and fill in the basic carbon emission data corresponding to the full target part process in combination with the basic carbon emission inventory to generate the carbon footprint of the target component; The carbon footprint of the target component is calculated and processed based on a preset mapping logic to generate a full-process carbon footprint corresponding to the target aircraft horizontal tail; wherein the preset mapping logic is the mapping logic between the manufacturing process and the design process of the aircraft horizontal tail.

2. The method according to claim 1, characterized in that Generating a basic carbon emission inventory corresponding to the horizontal tail of the target aircraft based on the full processing information and preset process logic includes: Determine the target process hierarchy corresponding to the horizontal tail of the target aircraft based on the preset process logic; The full processing information is sorted and processed based on the target process hierarchy to generate a basic carbon emission inventory corresponding to the horizontal tail of the target aircraft.

3. The method according to claim 1, characterized in that The determining of the basic carbon emission data corresponding to the target part process based on the preset process basic information includes: Determine the target emission source and target process parameters corresponding to the target part process based on the preset process basic information; Determine the corresponding target accounting model based on the target emission source, and determine the basic carbon emission data corresponding to the target part process based on the target accounting model and target process parameters.

4. The method according to claim 1, wherein The process of combining the basic carbon emission inventory with the basic carbon emission data corresponding to the process of processing all target parts to generate the carbon footprint of the target parts includes: Determine the data filling position corresponding to the target part process based on the basic carbon emission inventory; Fill in the basic carbon emission data corresponding to the target part process based on the data filling position to generate a basic component carbon footprint; Combine and process the carbon footprints of all basic components to generate the carbon footprint of the target components.

5. The method according to claim 1, wherein The step of calculating and processing the carbon footprint of the target component based on the preset mapping logic to generate the full-process carbon footprint corresponding to the horizontal tail of the target aircraft includes: Determine the target mapping logic between the manufacturing process and the design process corresponding to the horizontal tail of the target aircraft based on the preset mapping logic; Determining, based on the target mapping logic, candidate carbon footprints in the target component carbon footprint and the calculation superposition logic between the candidate carbon footprints; The candidate carbon footprints are processed based on the calculation superposition logic to generate a full-process carbon footprint corresponding to the horizontal tail of the target aircraft.

6. The method according to claim 5, characterized in that After the candidate carbon footprints are calculated and processed based on the calculation superposition logic to generate a full-process carbon footprint corresponding to the horizontal tail of the target aircraft, the method further includes: Determining the occupancy ratio corresponding to each of the candidate carbon footprints based on the full-process carbon footprint; Sorting the occupancy ratios corresponding to the candidate carbon footprints, and determining the target candidate carbon footprint corresponding to the highest occupancy ratio; An evaluation result corresponding to the target candidate carbon footprint is generated based on the highest occupancy ratio.

7. The method according to claim 1, characterized in that The full processing information includes: workstations, stations, assembly outlines, pre-assembly outlines, components, and parts processing information.

8. A carbon footprint calculation device for an aircraft horizontal tail, characterized in that: include: An information determination module is used to determine the full processing information corresponding to the horizontal tail of the target aircraft based on the preset design components and the preset overall process route corresponding to the horizontal tail of the target aircraft; An inventory generation module is configured to generate a basic carbon emission inventory corresponding to the horizontal tail of the target aircraft based on the full processing information and a preset process logic; wherein the basic carbon emission inventory includes the full number of parts and processes corresponding to the horizontal tail of the target aircraft; The first generation module is used to determine the basic carbon emission data corresponding to the target part process based on the preset process basic information, and fill in the basic carbon emission data corresponding to the full number of target part processes in combination with the basic carbon emission inventory to generate the carbon footprint of the target component; The second generation module is used to calculate and process the carbon footprint of the target component based on a preset mapping logic to generate a full-process carbon footprint corresponding to the target aircraft horizontal tail. The preset mapping logic is the mapping logic between the manufacturing process and the design process of the aircraft horizontal tail.

9. An electronic device, characterized in that: The electronic device comprises: at least one processor; and a memory communicatively connected to the at least one processor; wherein, The memory stores a computer program executable by the at least one processor. The computer program is executed by the at least one processor to enable the at least one processor to perform the carbon footprint calculation method for an aircraft horizontal tail according to any one of claims 1 to 7.

10. A computer-readable storage medium, characterized in that The computer-readable storage medium stores computer instructions, and the computer instructions are used to enable a processor to implement the carbon footprint calculation method for an aircraft horizontal tail according to any one of claims 1 to 7 when executed.

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