Paper Title:
Analysis of Crankshaft Fatigue Strength Based on Integrated Finite Element Model
  Abstract

Aiming at the complex mechanical systems for the prediction of the fatigue limit load requirements, this paper examines the relationship among finite element analysis model and the performance models. And a finite element modeling method for fatigue analysis is proposed. The finite element model can support static, modal, fatigue, and multi-body dynamic response analysis in parallel and collaboration. This method helps improve the fatigue limit load analysis.

  Info
Periodical
Edited by
Ran Chen
Pages
1558-1562
DOI
10.4028/www.scientific.net/AMM.44-47.1558
Citation
X. P. Chen, R. F. Hu, S. H. Zheng, "Analysis of Crankshaft Fatigue Strength Based on Integrated Finite Element Model", Applied Mechanics and Materials, Vols. 44-47, pp. 1558-1562, 2011
Online since
December 2010
Export
Price
$32.00
Share

In order to see related information, you need to Login.

In order to see related information, you need to Login.

Authors: Cheng Jie Ye, Zao Liang Gao
Chapter 1: High Strength High Performance Materials and New Structural System
Abstract:In this paper,a two-way winding-beam space-harmonic excitation beam string under the action of the dynamic response has been studied to...
3
Authors: Lei Sun, Ming Hai Wang, Xiao Peng Li, Yue Sun
Chapter 11: Environmental Protection and Economic Development
Abstract:Taking moving trestle of machine tool as example,the modal analysis and harmonic response analysis were done by means of finite element...
1553
Authors: Li Bao, Xi Zhao Li
Chapter 2: Mechatronics
Abstract:The load spectrum of a frame, which is a key component of a motorcycle, can be used to frame loading experiment and life prediction of a...
150
Authors: Tong Ying Shang Guan, Yang Lian, Di Wu
Chapter 3: Materials Forming
Abstract:We have take the design of the complex machinery equipment DF900 erecting machine as an example discussed SolidWorks and its module...
678
Authors: Ji Yan Li, Zhi Bing Yang
Chapter 4: Mechanics, Thermal and Dynamics Systems, Vibration, Noise, Applied Mechanics and Numerical Simulation Applications
Abstract:Landing gear is the critical component for aircrafts’ flight safety. According to the statistics, the accidents caused by the structure of...
870