Dynamic response of coupled shaft torsion and blade bending in rotor blade system

Hwanhee Lee, Ji Seok Song, Seog Ju Cha, Sung Soo Na

Research output: Contribution to journalArticle

13 Citations (Scopus)

Abstract

This study develops a computational model for the dynamic characteristics of a rotor-blade system. The rotor-blade coupled model with pre-twisted blade attached to a rigid disk driven by a shaft is developed using the Lagrange equation in conjunction with the assumed mode method to discretize the blade deformation. The effects of axial shortening due to blade lagging deformation, centripetal force caused by the rotating blade, and gravity are included in the model. The coupled equation of motion is formulated based on the small deformation theory for the blade and shaft torsional deformation to obtain the dynamic characteristics of the system for various system parameters. Numerical simulations show that the pre-twist angle of the blade and the shaft torsional flexibility strongly influence the dynamic behavior of the rotor-blade system.

Original languageEnglish
Pages (from-to)2585-2597
Number of pages13
JournalJournal of Mechanical Science and Technology
Volume27
Issue number9
DOIs
Publication statusPublished - 2013 Sep 1

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Torsional stress
Turbomachine blades
Dynamic response
Rotors
Equations of motion
Gravitation
Computer simulation

Keywords

  • Assumed mode method
  • Lagrange equation
  • Natural frequency
  • Pre-twist angle
  • Rotor-blade system
  • Shaft torsional flexibility

ASJC Scopus subject areas

  • Mechanical Engineering
  • Mechanics of Materials

Cite this

Dynamic response of coupled shaft torsion and blade bending in rotor blade system. / Lee, Hwanhee; Song, Ji Seok; Cha, Seog Ju; Na, Sung Soo.

In: Journal of Mechanical Science and Technology, Vol. 27, No. 9, 01.09.2013, p. 2585-2597.

Research output: Contribution to journalArticle

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