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Helicopter key and important parts wear rate prediction method

A technology of helicopter closing and forecasting method, which is applied in forecasting, special data processing applications, complex mathematical operations, etc., to achieve good results and reduce workload.

Inactive Publication Date: 2018-06-01
CHINA HELICOPTER RES & DEV INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The object of the present invention is to provide a method for predicting the wear rate of heavy-duty parts of a helicopter, to solve at least one problem existing in the quantitative prediction method for the wear rate of heavy-duty parts of helicopters

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  • Helicopter key and important parts wear rate prediction method
  • Helicopter key and important parts wear rate prediction method
  • Helicopter key and important parts wear rate prediction method

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[0035] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The present invention relates to the usage and maintenance guarantee technology field, in particular to a helicopter key and important parts wear rate prediction method. The method comprises the following steps of determining the helicopter key and important parts wear influence factors, and acquiring the wear quantity data; converting the visual wear quantity into a wear rate of unit time; usinga main effect, a secondary effect and an interaction effect of the wear influence factors to form an independent variable set, forming a sample data table with a dependent variable set, and carrying out the correlation analysis; extracting the components; utilizing the partial least squares to extract the components until a regression equation reaches the predetermined precision; converting into aregression equation between the original independent variables and the dependent variables in the original data table; analyzing a model and verifying the effects. The helicopter key and important parts wear rate prediction method of the present invention applies an orthogonal test design method, enables the workload to be reduced, and fully considers the mutual effects between the multiple factors and multiple levels, thereby really achieving the purposes of being high in efficiency and being fast and economic.

Description

technical field [0001] The invention relates to the technical field of service maintenance support, in particular to a method for predicting the wear rate of critical parts of a helicopter. Background technique [0002] At present, the helicopters that have been in service for many years in the field of the army have various degrees of aging and weakening of functions in multiple systems. The problems are mainly concentrated in several large mechanical systems, which are prone to component sticking, vibration, speeding, and line detachment and desoldering. And other problems, at its root, wear is one of the main reasons for this type of failure. [0003] For the wear problem, quantitative prediction has always been an important and difficult point in its research; at present, the multi-factor orthogonal test method is mainly used to extract the wear data, and according to the statistical law of the wear data, a more suitable mathematical statistical method is sought. Establ...

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Application Information

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IPC IPC(8): G06Q10/04G06F17/50G06F17/18
CPCG06F17/18G06Q10/04G06F30/20
Inventor 刘松宇沈亚斌辛冀
Owner CHINA HELICOPTER RES & DEV INST