Product design reliability with consideration of material property changes during service

A material property, computer technology, applied in the field of product design reliability and durability analysis accuracy, can solve problems such as the influence of inaccuracy of use time and the inability to represent changes in material properties.

Inactive Publication Date: 2015-07-29
GM GLOBAL TECH OPERATIONS LLC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Current methods of durability analysis and life prediction (such as fatigue analysis or related life prediction) for cast components often resort to making simplifying assumptions—such as constant material properties—that cannot actually represent these changes that occur over time. Material properties change; analyzes based on such assumptions suffer from inaccuracies as parts age

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  • Product design reliability with consideration of material property changes during service
  • Product design reliability with consideration of material property changes during service
  • Product design reliability with consideration of material property changes during service

Examples

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Embodiment Construction

[0056] first reference figure 1 , shows a typical T6 and / or T7 heat treatment cycle for an aluminum alloy according to the prior art. In T5 aging, there are three aging conditions commonly referred to as (1) underaged, (2) peak aged, and (3) overaged. During the initial stages of aging, GP regions and finely shearable precipitates form, and the structure is considered to be underaged. At this stage, the material hardness and yield strength are generally low. Prolonged time at a given temperature or aging at a higher temperature further evolves the precipitate structure, increasing hardness and yield strength to a maximum, peak aging / hardness condition. Further aging reduces the hardness / yield strength and the structure becomes overaged due to coarsening of the precipitates and their transition to crystalline incoherence.

[0057] next reference figure 2 , shows an example of the aging response of cast aluminum alloy 319 aged at various temperatures. For the aging time p...

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Abstract

A method of computationally determining material property changes for a cast aluminum alloy component. Accuracy of the determination is achieved by taking into consideration material property changes over the projected service life of the component. In one form, the method includes accepting time-dependent temperature data and using that data in conjunction with one or more constitutive relationships to quantify the impact of various temperature regimes or conditions on the properties of heat-treatable components and alloys. Finite element nodal analyses may be used as part of the method to map the calculated material properties on a nodal basis, while a viscoplastic model may be used to determine precipitation hardening and softening effects as a way to simulate the time and temperature dependencies of the material. The combined approach may be used to determine the material properties over the expected service life of a cast component made from such material.

Description

technical field [0001] The present invention relates generally to changes in material properties during the service life of a cast part, and in particular to improved product design reliability and durability analysis accuracy by accounting for changes in material properties over the expected service life of a cast part. Background technique [0002] The most common Al-Si-based alloys used to make cast automotive engine blocks and cylinder heads are heat-treatable variants, including Alloy 319 (nominal composition by weight: 6.5% Si, 0.5% Fe, 0.3 % Mn, 3.5% Cu, 0.4% Mg, 1.0% Zn, 0.15% Ti and the balance Al) and alloy 356 (nominal composition by weight: 7.0% Si, 0.1% Fe, 0.01% Mn, 0.05% Cu, 0.3% Mg, 0.05% Zn, 0.15% Ti and the balance Al). Aluminum alloys like 319 and 356 are usually heat treated to a T6 or T7 temper prior to use by subjecting them to three main stages: (1) solution treatment at a relatively high temperature below the melting point of the alloy, often for Mo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F17/5018G06F30/23
Inventor Q. 王D. R. 赫斯M. J. 沃克H. W. 多蒂B. 肖
Owner GM GLOBAL TECH OPERATIONS LLC
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