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Aircraft reliability data asset risk total factor construction method and device

A technology of data assets and construction methods, applied in data processing applications, electrical digital data processing, special data processing applications, etc., can solve problems such as lack of relevance, data transfer and daily communication that cannot effectively carry out information transfer and task communication, etc. Achieve the effect of easy task management

Pending Publication Date: 2021-06-29
BEIJING SHENGTAOPING TEST ENG TECH RES INST
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Problems solved by technology

[0002] In the existing analysis of aircraft reliability, the three aspects of availability, reliability and maintainability are independent work systems, that is, each has an independent communication system, which lacks correlation with each other. In the transfer of data and daily communication, information transfer and task communication cannot be effectively carried out

Method used

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  • Aircraft reliability data asset risk total factor construction method and device
  • Aircraft reliability data asset risk total factor construction method and device
  • Aircraft reliability data asset risk total factor construction method and device

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Embodiment Construction

[0031] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the present invention. Obviously, the described embodiments are part of the embodiments of the present invention , but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0032] figure 1 It is a schematic flow chart of the aircraft reliability data asset risk all-factor construction method provided by the present invention, such as figure 1 shown, including:

[0033] S1, obtaining the historical raw data set of aircraft operation reliability;

[0034] S2. Based on the preset architectural language model, decompose the structure of the historical origin...

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Abstract

The invention provides an aircraft reliability data asset risk total factor construction method and device. The method comprises the steps of obtaining an aircraft operation reliability historical original data set; and based on a preset architecture language model, carrying out structural decomposition on the aircraft operation reliability historical original data set, and outputting a total element model of aircraft reliability basic data. According to the method, data related to asset risk control in aircraft reliability data is decomposed and coded in a unified mode, a set of perfect coding system based on metadata is designed, the uniformity of a concept layer and a logic layer is improved, and follow-up task management is facilitated.

Description

technical field [0001] The invention relates to the technical field of aviation equipment, in particular to a method and device for constructing all elements of aircraft reliability data asset risk. Background technique [0002] In the existing analysis of aircraft reliability, the three aspects of availability, reliability and maintainability are independent work systems, that is, each has an independent communication system, which lacks correlation with each other. In the transfer of data and daily communication, information transfer and task communication cannot be effectively carried out. [0003] Therefore, it is necessary to propose a unified coding system to manage all aspects of the task in a unified manner. Contents of the invention [0004] The invention provides a method and device for constructing all elements of aircraft reliability data asset risk, which are used to solve the defects in the prior art. [0005] In the first aspect, the present invention prov...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06Q10/00G06Q10/06G06F119/02
CPCG06F30/20G06Q10/0635G06Q10/20G06F2119/02
Inventor 陈冬梅王群勇
Owner BEIJING SHENGTAOPING TEST ENG TECH RES INST
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