Load reduction mechanism of cone wall fuse caused by fan blade off

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

2 Scopus citations

Abstract

The purpose of this paper is to study the effect of the cone wall fuse of an aeroengine caused by fan blade off. Firstly, the load reduction mechanism of cone wall fuse was analyzed. Then, the finite element model was established. Finally, the steady calculation and transient calculation was carried out. The results show that the mechanism of the cone wall fuse is that the relative value between the critical speed and the blade off speed was changed because of the decrease of the support stiffness. The key parameters which influence the cone wall fuse phenomenon is the response time of the fuse process and the support stiffness after the fuse.

Original languageEnglish
Title of host publication2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages193-197
Number of pages5
ISBN (Electronic)9781728155357
DOIs
StatePublished - Jul 2019
Event10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, Belgium
Duration: 22 Jul 201925 Jul 2019

Publication series

Name2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

Conference

Conference10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Country/TerritoryBelgium
CityBrussels
Period22/07/1925/07/19

Keywords

  • Fan blade off
  • Fuse
  • Load reduction
  • Stiffness

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