Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution

Presented herein is a mathematical model employing differential equations formulation for brush seals used in gas turbine engines. These components are used to seal the bearing chamber from the environment and reduce the loss of lubricant in the atmosphere, ensuring a MTBR long enough to have requir...

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Main Authors: Amin Changizi, Ion Stiharu, Bilal Outirba, Patrick Hendrick
Format: Article
Language:English
Published: SAGE Publishing 2021-09-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/16878140211043396
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spelling doaj-7d49628c5da740f4aaaa679e89bb5fab2021-09-14T23:33:32ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402021-09-011310.1177/16878140211043396Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solutionAmin Changizi0Ion Stiharu1Bilal Outirba2Patrick Hendrick3Intelliquip LLC, Bethlehem, PA, USAConcordia University, Montreal, QC, CanadaUniversité Libre De Bruxelles, Bruxelles, BelgiumUniversité Libre De Bruxelles, Bruxelles, BelgiumPresented herein is a mathematical model employing differential equations formulation for brush seals used in gas turbine engines. These components are used to seal the bearing chamber from the environment and reduce the loss of lubricant in the atmosphere, ensuring a MTBR long enough to have required the change the seals only during the engine overhaul operation. The model assumes a single curved bristle loop in the form of a curved-bridge beam subjected to the influences of complex external loads (static and dynamic). Further, a model for clustered bristles is proposed. Specifically, the static forces acting on the curved-bridge beam include the weight of the oil capillary attached to the beam, the weight of the beam itself, the capillary force developed between the surfaces of the bristles in the brush and the temperature gradient. The dynamic forces include the leakage oil pressure and the rotation of the shaft. This complex loading induces a nonlinear large deflection on the curved-bridge beam. Also, the temperature gradient present on the bristles during the gas turbine engine operation generates a change in the geometry of the beam and in the magnitude of the forces acting on the bristles modeled as beams. In the present model, the weights are assumed as uniformly distributed forces on the surface of the beam while the capillary forces and the force generated by the rotating shaft are considered to be non-uniform. The equation expressing the curvature of the beam under general loading force is developed and one can choose the appropriate method of solving the generated differential equation after the expression of the general force is defined. Hence, the ordinary differential equation describing the nonlinear large deflection of the curved-bridge beam will be derived using general nonlinear elasticity theory.https://doi.org/10.1177/16878140211043396
collection DOAJ
language English
format Article
sources DOAJ
author Amin Changizi
Ion Stiharu
Bilal Outirba
Patrick Hendrick
spellingShingle Amin Changizi
Ion Stiharu
Bilal Outirba
Patrick Hendrick
Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
Advances in Mechanical Engineering
author_facet Amin Changizi
Ion Stiharu
Bilal Outirba
Patrick Hendrick
author_sort Amin Changizi
title Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
title_short Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
title_full Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
title_fullStr Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
title_full_unstemmed Mathematical model of brush seals for gas turbine engines: A nonlinear analytical solution
title_sort mathematical model of brush seals for gas turbine engines: a nonlinear analytical solution
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2021-09-01
description Presented herein is a mathematical model employing differential equations formulation for brush seals used in gas turbine engines. These components are used to seal the bearing chamber from the environment and reduce the loss of lubricant in the atmosphere, ensuring a MTBR long enough to have required the change the seals only during the engine overhaul operation. The model assumes a single curved bristle loop in the form of a curved-bridge beam subjected to the influences of complex external loads (static and dynamic). Further, a model for clustered bristles is proposed. Specifically, the static forces acting on the curved-bridge beam include the weight of the oil capillary attached to the beam, the weight of the beam itself, the capillary force developed between the surfaces of the bristles in the brush and the temperature gradient. The dynamic forces include the leakage oil pressure and the rotation of the shaft. This complex loading induces a nonlinear large deflection on the curved-bridge beam. Also, the temperature gradient present on the bristles during the gas turbine engine operation generates a change in the geometry of the beam and in the magnitude of the forces acting on the bristles modeled as beams. In the present model, the weights are assumed as uniformly distributed forces on the surface of the beam while the capillary forces and the force generated by the rotating shaft are considered to be non-uniform. The equation expressing the curvature of the beam under general loading force is developed and one can choose the appropriate method of solving the generated differential equation after the expression of the general force is defined. Hence, the ordinary differential equation describing the nonlinear large deflection of the curved-bridge beam will be derived using general nonlinear elasticity theory.
url https://doi.org/10.1177/16878140211043396
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