Fatigue notch coefficient data processing method considering corrosion and residual stress

A technology of residual stress and data processing, applied in the direction of electrical digital data processing, special data processing applications, CAD numerical modeling, etc. Improve prediction accuracy and good universal applicability

Active Publication Date: 2020-09-04
恒创联拓(青岛)航空科技有限公司
View PDF3 Cites 8 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] Through the above analysis, the problems and defects in the prior art are: (1) the current analysis method of the fatigue notch coefficient cannot consider the influence of corrosion damage; (2) the current existing analysis method of the fatigue notch coefficient cannot Consider the influence of residual stress caused by shot peening; (3) The existing analysis method of fatigue notch coefficient cannot consider surface defects
The above factors lead to inaccurate calculation results of the traditional fatigue notch coefficient calculation method, which leads to inaccurate fatigue life evaluation results and affects the safety of the structure.
[0009] The difficulty of solving the

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Fatigue notch coefficient data processing method considering corrosion and residual stress
  • Fatigue notch coefficient data processing method considering corrosion and residual stress
  • Fatigue notch coefficient data processing method considering corrosion and residual stress

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0050] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the examples. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0051] Aiming at the problems existing in the prior art, the present invention provides a fatigue notch coefficient data processing method considering corrosion and residual stress. The present invention will be described in detail below in conjunction with the accompanying drawings.

[0052] In the present invention, the fatigue notch coefficient data processing method considering the influence of corrosion and residual stress is based on the theory of fracture mechanics, and can be obtained through theoretical derivation, which can consider the microstructure of materials (including grain size and internal microscopic defe...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention belongs to the technical field of structural life reliability evaluation in a corrosive environment, and discloses a fatigue notch coefficient data processing method considering corrosion and residual stress. The method includes: reconstructing a notch surface geometric model; actually measuring the residual stress distribution of the notch part of the structural simulation piece byadopting an ultrasonic residual stress tester; obtaining a fitting calculation formula of the residual compressive stress along the depth direction through data fitting; establishing a finite elementtheoretical analysis model by adopting a reverse modeling technology, carrying out mesh generation, and obtaining a stress concentration coefficient through analysis; and obtaining the stress concentration coefficient under the corrosion condition based on analysis. The theoretical calculation method provided by the invention better conforms to the actual condition of structure service, and the prediction precision of the fatigue life is obviously improved. According to the method, the influences of corrosion damage and residual stress caused by the microstructure, the structural boundary dimension and the environment of the material can be considered, and the fatigue notch coefficient calculation method provided by the invention is wider in application range and good in universality.

Description

technical field [0001] The invention belongs to the technical field of structural life reliability evaluation in a corrosive environment, and relates to a fatigue notch coefficient data processing method considering corrosion and residual stress. Background technique [0002] At present, accurate prediction of structural fatigue life under service corrosive environmental conditions is crucial for safe use. Fatigue notch factor K f is a very important parameter in structural fatigue life assessment, and its definition is [0003] [0004] Determining the fatigue notch factor K f The most direct and reliable method is to pass the fatigue test. Due to the different structural forms, the size of the structural simulation parts is different, and the surface finish is different. K f They are different, and it takes a lot of manpower, material and financial resources to carry out such a test, so the fatigue notch coefficient K is determined through the test f is unrealistic....

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): G06F30/23G06F119/02G06F111/10G06F119/14
CPCG06F30/23G06F2119/02G06F2111/10G06F2119/14Y02P10/20
Inventor 谭晓明张丹峰钱昂于光辉贺小帆赵培仲陈新波
Owner 恒创联拓(青岛)航空科技有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products