Analysis of Sealing Properties of Coupled Gas Film Flow Field and Cantilever-Type Foil Deformation

Aimed at cantilever-type foil cylinder film seal system, finite element method analysis model was established to calculate the deformation of cantilever foil under the gas pressure based on the theory of plate bending. The paper proposed a method to solve fluid-solid interaction problems in cantilev...

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Bibliographic Details
Published inApplied Mechanics and Materials Vol. 670-671; no. Applied Mechanics, Materials and Manufacturing IV; pp. 856 - 859
Main Authors Du, Yun Long, Ma, Gang
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 01.10.2014
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Summary:Aimed at cantilever-type foil cylinder film seal system, finite element method analysis model was established to calculate the deformation of cantilever foil under the gas pressure based on the theory of plate bending. The paper proposed a method to solve fluid-solid interaction problems in cantilever-type foil cylinder film seal system based on the numerical analysis method of cylinder gas film seal. The calculation program using the finite element method to solve fluid-solid interaction problems was developed. Calculation simulation of the film mechanical properties and steady-state performance of sealing system was realized which improved the accuracy of the sealing system performance analysis and provided the basis for the multi-parameters matching design of sealing system. The impact of adding cantilever foil support structure to the steady-state performance of sealing system and the influence of flexible support parameters on the steady-state performance of the sealing system was calculated through the method.
Bibliography:Selected, peer reviewed papers from the 4th International Conference on Applied Mechanics, Materials and Manufacturing (ICA3M 2014, ICAMMM 2014), August 23-24, 2014, Shenzhen, China
ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 23
ISBN:3038352888
9783038352884
ISSN:1660-9336
1662-7482
1662-7482
DOI:10.4028/www.scientific.net/AMM.670-671.856