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24789

THEORY AND EXPERIMENT OF DISK FLEXIBILITY INFLUENCES ON TURBOROTOR VIBRATIONS

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Last updated: 04 Jan 2025

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Abstract

This paper investigates the vibration problems associated with the attachment of flexible disks to high speed, flexible rotors. A semi-analytical finite element method has been employed to model two flexible disks attached to a flexible rotor supported by three ball bearings. A two-nodes beam element of 8-DOF is used to model the flexural vibrations of the flexible rotor while a four-node (arranged on two perpendicular diameters) annular circular plate element of 8-DOF is used to model the transverse vibrations of the flexible disks. The system natural frequencies and critical speeds are computed in a speed rang up to a 5000 RPM. An experimental test rig has been employed to validate the theoretical findings. An acceptable matching has been found between the experimental and the simulation results. Most importantly, the results reveal that the rotor natural frequencies and critical speeds are marginally influenced by the disk flexibility. The main contribution of this work is that the inclusion of disk flexibility in the modeling process effectively reduces the modeling error, which seems to be crucial for some applications.

DOI

10.21608/asat.2001.24789

Authors

First Name

GAFFER

Last Name

I.

MiddleName

H.

Affiliation

Lecturer, Dept. of Production Engineering and Mechanical Design, Faculty of Engineering, Menoufia University, Shebin ElKom, Egypt.

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First Name

ELBEHEIRY

Last Name

M.

MiddleName

E.

Affiliation

Lecturer, Dept. of Production Engineering and Mechanical Design, Faculty of Engineering, Menoufia University, Shebin ElKom, Egypt.

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Volume

9

Article Issue

ASAT Conference, 8-10 May 2001

Related Issue

4547

Issue Date

2001-05-01

Receive Date

2019-01-15

Publish Date

2001-05-01

Page Start

1

Page End

17

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_24789.html

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https://asat.journals.ekb.eg/service?article_code=24789

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24

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

THEORY AND EXPERIMENT OF DISK FLEXIBILITY INFLUENCES ON TURBOROTOR VIBRATIONS

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Article

Created At

22 Jan 2023