FREQUENCIES AND MODES OF ROTATING FLEXIBLE BLADED DISC-SHAFT ASSEMBLIES: A GLOBAL CYCLIC SYMMETRY APPROACH

Authors: Jacquet-Richardet G.; Ferraris G.; Rieutord P.

Source: Journal of Sound and Vibration, Volume 191, Number 5, April 1996 , pp. 901-915(15)

Publisher: Academic Press

Buy & download fulltext article:

OR

Price: $52.63 plus tax (Refund Policy)

Abstract:

It is now increasingly necessary to predict accurately, at the design stage and without excessive computer costs, the dynamic behaviour of rotating parts of turbomachines, in order to avoid resonant conditions at operating speeds. In this study, the global non-rotating mode shapes of flexible bladed disc-shaft assemblies are used in a modal analysis method for evaluating the dynamic characteristics (frequencies and mode shapes) of the corresponding rotating systems. The non-rotating modes are calculated by using a finite element cyclic symmetry approach. Rotational effects, such as centrifugal stiffening and gyroscopic effects are accounted for, and all the possible couplings between the flexible parts are allowed. An application is presented in order to assess the mathematical model by comparison of the computed results with reference values.

Language: English

Document Type: Research article

Affiliations: Laboratoire de Mecanique des Structures URA CNRS 862, INSA de Lyon, 20 Avenue Albert Einstein, 69621 Villeurbanne Cedex, France

Publication date: 1996-04-01

Related content

Tools

Key

Free Content
Free content
New Content
New content
Open Access Content
Open access content
Subscribed Content
Subscribed content
Free Trial Content
Free trial content

Text size:

A | A | A | A
Share this item with others: These icons link to social bookmarking sites where readers can share and discover new web pages. print icon Print this page