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Aircraft manufacturing configuration control accuracy detection system and method

A technology for aircraft manufacturing and accuracy, applied in electrical testing/monitoring and other directions, can solve the problem of lack of product configuration data comparison, detection and comparison regularity

Inactive Publication Date: 2016-08-24
SHANGHAI AIRCRAFT MFG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

There is a lack of methods for comparing and detecting the regularity of product configuration data in a specific field

Method used

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  • Aircraft manufacturing configuration control accuracy detection system and method
  • Aircraft manufacturing configuration control accuracy detection system and method
  • Aircraft manufacturing configuration control accuracy detection system and method

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Experimental program
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Embodiment 1

[0055] Such as Figure 5 As shown, this embodiment relates to an aircraft manufacturing configuration control accuracy detection system, including: a preprocessing module, a data comparison module, an accuracy identification module and a detection difference processing module, wherein: the preprocessing module is connected to the data comparison module And transmit the MBOM / SPSBOM, component type, section, quantity, and EBOM version information after filtering the part identification; the data comparison module is connected with the accuracy identification module and transmits the difference information; the accuracy identification module and the detection difference The processing is connected and transmits the judgment result information of normal difference and error difference; the detection difference processing module performs difference revision according to the difference category according to the information result transmitted by the accuracy identification module, so ...

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Abstract

The invention discloses a system and method for detecting aircraft manufacturing configuration control accuracy. The system comprises a preprocessing module, a data comparison module, an accuracy recognition module and a detection difference processing module. The preprocessing module is connected with the data comparison module and used for transmitting the information such as MBOM / SPSBOM, component types, belonging parts, the quantity and EBOM versions after component identifications are filtered. The data comparison module is connected with the accuracy recognition module and used for transmitting difference information. The accuracy recognition module is connected with the detection difference processing module and used for transmitting normal difference and false difference judgment result information. The detection difference processing module is used for conducting difference amendment according to the difference types and the information result transmitted by the accuracy recognition module so as to guarantee manufacturing configuration control accuracy. By means of the system and method for detecting aircraft manufacturing configuration control accuracy, configuration detection human errors can be effectively reduced, detecting algorithms and formats are unified, the completeness and accuracy for aircraft product manufacturing are guaranteed, meanwhile, the detecting state and result are analyzed and counted in an assisting mode, the strength of relevant work is lowered, detection time is shortened, so that product manufacturing quality is improved, the overall development cycle is obviously shortened, development cost is lowered, and the method is wide in coverage and easy to implement.

Description

technical field [0001] The present invention relates to a system and method in the technical field of aircraft manufacturing, in particular to a system and method for detecting the accuracy of aircraft manufacturing configuration control. Background technique [0002] Civil aircraft products have a long life cycle, multiple stages, a large amount of data, and complex relationships. A large amount of data involved in the configuration control of final assembly comes from the engineering design stage, such as aircraft product definition data, various design documents, drawings, standard parts, material selection, various standard specifications and management regulations, etc. Data such as final assembly process, tooling design documents, airworthiness documents, quality management and control documents, etc. These data are diverse and heterogeneous, and need to be closely integrated with the configuration, change information and development process of the aircraft model to ke...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
Inventor 王斌倪炎榕张尚体陆敏余翔匡翠杨路平
Owner SHANGHAI AIRCRAFT MFG