Analysis of 3D dynamic response for TC4 blades by the FEM

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

Abstract

TC4 blades are one of the major parts of the aero engine, and the examples of engine invalid and even wrecked are common. In this paper, a 3D analysis system of the vibration behaviors of the TC4 blades is given. The 3D analysis model of blade was described using 20 nodes elements. The finite element procedure was worked out using the blade vibration behaviors analysis of the aero engine. At last, the modal shapes and stress nephograms of the first six frequencies are gotten which influenced the blade vibration characteristics. Results show that the program has offered an effective, flexible research means for analyzing dynamic response of TC4 blades.

Original languageEnglish
Title of host publicationApplied Mechanics, Materials, Industry and Manufacturing Engineering
Pages425-428
Number of pages4
DOIs
StatePublished - 2012
Externally publishedYes
Event2012 2nd International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME 2012 - Hefei, China
Duration: 23 Jun 201224 Jun 2012

Publication series

NameApplied Mechanics and Materials
Volume164
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2012 2nd International Conference on Mechanical Engineering, Industry and Manufacturing Engineering, MEIME 2012
Country/TerritoryChina
CityHefei
Period23/06/1224/06/12

Keywords

  • 3D FEM
  • Dynamics behaviors
  • TC4 blades

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