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Aircraft full-life-cycle configuration management system

A technology of full life cycle and configuration management, applied in the direction of manufacturing computing systems, instruments, data processing applications, etc., can solve problems such as small production batches, and achieve the effect of facilitating status query and problem tracing

Active Publication Date: 2016-01-20
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In my country's aerospace field, the development of traditional aerospace models has the characteristics of independent tasks, complex development processes, and small production batches. The research on configuration management technology for the life cycle of model products is still in its infancy

Method used

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  • Aircraft full-life-cycle configuration management system
  • Aircraft full-life-cycle configuration management system
  • Aircraft full-life-cycle configuration management system

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Embodiment Construction

[0022] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0023] Such as figure 1 As shown in the system composition block diagram, the aircraft life cycle configuration management system of the present invention includes a product coding and identification subsystem, a product information input subsystem, an aircraft assembly subsystem, an aircraft maintenance subsystem and a database.

[0024] (1) Product coding and identification subsystem

[0025] In order to systematically manage the entire life cycle of the aircraft, the present invention divides products with a Field Replaceable Unit (LRU) as the smallest unit. In the product coding and identification subsystem, coding rules are set to code all purchased products to obtain identification codes corresponding to the products one by one, and then mark the identification codes on each product one by one.

[0026] Aircraft product coding adopts the...

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PUM

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Abstract

The invention provides an aircraft full-life-cycle configuration management system. The aircraft full-life-cycle configuration management system comprises a product coding and identifying subsystem, a product information entering subsystem, an aircraft general assembly subsystem, an aircraft maintenance subsystem and a database. The aircraft full-life-cycle configuration management system compiles identification codes for aircraft products, records information data of the all processes of product warehousing, aircraft generally assembling, component maintenance and product replacing, and realizes the configuration state management in the full life cycle of the aircraft. The system manages all the products by means of identification codes, so that uniform management of the aircraft in processes of product warehousing, generally assembling, maintenance and replacing is facilitated, the technical states and maintenance information of all aircraft products are recorded, and state querying and problem tracing are convenient.

Description

technical field [0001] The invention relates to the technical field of integrated flight support, in particular to an aircraft life-cycle configuration management system, which is used to perform life-cycle configuration management on components on the aircraft during the model development process. Background technique [0002] The composition of aerospace vehicle systems is very complex, and the products involved have the characteristics of large amounts of information, complex associations and processing rules. How to quickly and accurately decompose the information of hundreds or even thousands of parts of aircraft components and components into each process, Each operator has a one-to-one correspondence with each work result. This requires an information carrier that runs through the entire life cycle of the aircraft to realize real-time collection of information in the process of aircraft assembly and maintenance, and to ensure the operation of all products on the aircra...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/06G06Q50/04
CPCY02P90/30
Inventor 杜刚代京陈洪波曹霄辉曹晓瑞郑宏涛李昊赵兴朱红詹景坤满益明黄喜元曹熙炜王福忠彭小波
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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