Exit loss model for plain axial seals in multi-stage centrifugal pumps

K.A.J. Bruurs, B.P.M. van Esch, M.S. van der Schoot

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

1 Citation (Scopus)

Abstract

Plain axial seals are often used in centrifugal pumps as a means to achieve acceptable sealing against leakage flow without the much higher friction losses that are associated with mechanical seals. Examples of their application are the front seals in shrouded radial and mixed-flow pumps and the inter-stage seals in multi-stage pumps. Knowledge about the relation between leakage flow rate and pressure drop over the seal is vital, not only for estimating the volumetric losses, but also for calculating the axial thrust and shaft power of a pump. Investigations up till now have mainly concentrated on the frictional pressure drop in the seal (e.g. Yamada [1], Weber [2]), and hardly on the expansion losses at the exit of the seal. These exit losses are commonly modelled by a kinetic loss coefficient equal to or close to 1, but recent measurements by Storteig [3] have shown that exit loss coefficients can have values well above 1. This paper presents an analytical method to compute the exit loss coefficient of a plain axial seal. It is derived from energy and momentum balances and assumes power-law profiles for the velocity distribution in the seal. The power-law coefficients are computed using CFD and are found to only depend on the Reynolds numbers based on axial flow, Reax, and Couette flow in circumferential direction, ReW. The resulting exit loss coefficients are shown to range between 1 and 2, depending on the ratio of Reax and ReΩ. Results of the analytical model are compared with measurements and CFD calculations. This new analytical model can help improve the prediction of rotor dynamic stability, efficiency and axial thrust of turbomachinery without the need for dedicated CFD calculations in these tight clearances.

Original languageEnglish
Title of host publicationASME 2017 Fluids Engineering Division Summer Meeting
Subtitle of host publicationVolume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery
Place of Publications.l.
PublisherAmerican Society of Mechanical Engineers
Number of pages9
ISBN (Print)978-0-7918-5804-2
DOIs
Publication statusPublished - 1 Jan 2017
Event2017 ASME Fluids Engineering Division Summer Meeting (FEDSM 2017) - Waikoloa, United States
Duration: 30 Jul 20173 Aug 2017

Conference

Conference2017 ASME Fluids Engineering Division Summer Meeting (FEDSM 2017)
CountryUnited States
CityWaikoloa
Period30/07/173/08/17

Fingerprint

Centrifugal pumps
Seals
Computational fluid dynamics
Pumps
Pressure drop
Analytical models
Turbomachinery
Axial flow
Leakage (fluid)
Velocity distribution
Momentum
Reynolds number
Rotors
Flow rate
Friction
Kinetics

Cite this

Bruurs, K. A. J., van Esch, B. P. M., & van der Schoot, M. S. (2017). Exit loss model for plain axial seals in multi-stage centrifugal pumps. In ASME 2017 Fluids Engineering Division Summer Meeting: Volume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery [FEDSM2017-69251] s.l.: American Society of Mechanical Engineers. https://doi.org/10.1115/FEDSM2017-69251
Bruurs, K.A.J. ; van Esch, B.P.M. ; van der Schoot, M.S. / Exit loss model for plain axial seals in multi-stage centrifugal pumps. ASME 2017 Fluids Engineering Division Summer Meeting: Volume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery. s.l. : American Society of Mechanical Engineers, 2017.
@inproceedings{c6775f99012848f2b846b43122e237a4,
title = "Exit loss model for plain axial seals in multi-stage centrifugal pumps",
abstract = "Plain axial seals are often used in centrifugal pumps as a means to achieve acceptable sealing against leakage flow without the much higher friction losses that are associated with mechanical seals. Examples of their application are the front seals in shrouded radial and mixed-flow pumps and the inter-stage seals in multi-stage pumps. Knowledge about the relation between leakage flow rate and pressure drop over the seal is vital, not only for estimating the volumetric losses, but also for calculating the axial thrust and shaft power of a pump. Investigations up till now have mainly concentrated on the frictional pressure drop in the seal (e.g. Yamada [1], Weber [2]), and hardly on the expansion losses at the exit of the seal. These exit losses are commonly modelled by a kinetic loss coefficient equal to or close to 1, but recent measurements by Storteig [3] have shown that exit loss coefficients can have values well above 1. This paper presents an analytical method to compute the exit loss coefficient of a plain axial seal. It is derived from energy and momentum balances and assumes power-law profiles for the velocity distribution in the seal. The power-law coefficients are computed using CFD and are found to only depend on the Reynolds numbers based on axial flow, Reax, and Couette flow in circumferential direction, ReW. The resulting exit loss coefficients are shown to range between 1 and 2, depending on the ratio of Reax and ReΩ. Results of the analytical model are compared with measurements and CFD calculations. This new analytical model can help improve the prediction of rotor dynamic stability, efficiency and axial thrust of turbomachinery without the need for dedicated CFD calculations in these tight clearances.",
author = "K.A.J. Bruurs and {van Esch}, B.P.M. and {van der Schoot}, M.S.",
year = "2017",
month = "1",
day = "1",
doi = "10.1115/FEDSM2017-69251",
language = "English",
isbn = "978-0-7918-5804-2",
booktitle = "ASME 2017 Fluids Engineering Division Summer Meeting",
publisher = "American Society of Mechanical Engineers",
address = "United States",

}

Bruurs, KAJ, van Esch, BPM & van der Schoot, MS 2017, Exit loss model for plain axial seals in multi-stage centrifugal pumps. in ASME 2017 Fluids Engineering Division Summer Meeting: Volume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery., FEDSM2017-69251, American Society of Mechanical Engineers, s.l., 2017 ASME Fluids Engineering Division Summer Meeting (FEDSM 2017), Waikoloa, United States, 30/07/17. https://doi.org/10.1115/FEDSM2017-69251

Exit loss model for plain axial seals in multi-stage centrifugal pumps. / Bruurs, K.A.J.; van Esch, B.P.M.; van der Schoot, M.S.

ASME 2017 Fluids Engineering Division Summer Meeting: Volume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery. s.l. : American Society of Mechanical Engineers, 2017. FEDSM2017-69251.

Research output: Chapter in Book/Report/Conference proceedingConference contributionAcademicpeer-review

TY - GEN

T1 - Exit loss model for plain axial seals in multi-stage centrifugal pumps

AU - Bruurs, K.A.J.

AU - van Esch, B.P.M.

AU - van der Schoot, M.S.

PY - 2017/1/1

Y1 - 2017/1/1

N2 - Plain axial seals are often used in centrifugal pumps as a means to achieve acceptable sealing against leakage flow without the much higher friction losses that are associated with mechanical seals. Examples of their application are the front seals in shrouded radial and mixed-flow pumps and the inter-stage seals in multi-stage pumps. Knowledge about the relation between leakage flow rate and pressure drop over the seal is vital, not only for estimating the volumetric losses, but also for calculating the axial thrust and shaft power of a pump. Investigations up till now have mainly concentrated on the frictional pressure drop in the seal (e.g. Yamada [1], Weber [2]), and hardly on the expansion losses at the exit of the seal. These exit losses are commonly modelled by a kinetic loss coefficient equal to or close to 1, but recent measurements by Storteig [3] have shown that exit loss coefficients can have values well above 1. This paper presents an analytical method to compute the exit loss coefficient of a plain axial seal. It is derived from energy and momentum balances and assumes power-law profiles for the velocity distribution in the seal. The power-law coefficients are computed using CFD and are found to only depend on the Reynolds numbers based on axial flow, Reax, and Couette flow in circumferential direction, ReW. The resulting exit loss coefficients are shown to range between 1 and 2, depending on the ratio of Reax and ReΩ. Results of the analytical model are compared with measurements and CFD calculations. This new analytical model can help improve the prediction of rotor dynamic stability, efficiency and axial thrust of turbomachinery without the need for dedicated CFD calculations in these tight clearances.

AB - Plain axial seals are often used in centrifugal pumps as a means to achieve acceptable sealing against leakage flow without the much higher friction losses that are associated with mechanical seals. Examples of their application are the front seals in shrouded radial and mixed-flow pumps and the inter-stage seals in multi-stage pumps. Knowledge about the relation between leakage flow rate and pressure drop over the seal is vital, not only for estimating the volumetric losses, but also for calculating the axial thrust and shaft power of a pump. Investigations up till now have mainly concentrated on the frictional pressure drop in the seal (e.g. Yamada [1], Weber [2]), and hardly on the expansion losses at the exit of the seal. These exit losses are commonly modelled by a kinetic loss coefficient equal to or close to 1, but recent measurements by Storteig [3] have shown that exit loss coefficients can have values well above 1. This paper presents an analytical method to compute the exit loss coefficient of a plain axial seal. It is derived from energy and momentum balances and assumes power-law profiles for the velocity distribution in the seal. The power-law coefficients are computed using CFD and are found to only depend on the Reynolds numbers based on axial flow, Reax, and Couette flow in circumferential direction, ReW. The resulting exit loss coefficients are shown to range between 1 and 2, depending on the ratio of Reax and ReΩ. Results of the analytical model are compared with measurements and CFD calculations. This new analytical model can help improve the prediction of rotor dynamic stability, efficiency and axial thrust of turbomachinery without the need for dedicated CFD calculations in these tight clearances.

UR - http://www.scopus.com/inward/record.url?scp=85033598888&partnerID=8YFLogxK

U2 - 10.1115/FEDSM2017-69251

DO - 10.1115/FEDSM2017-69251

M3 - Conference contribution

AN - SCOPUS:85033598888

SN - 978-0-7918-5804-2

BT - ASME 2017 Fluids Engineering Division Summer Meeting

PB - American Society of Mechanical Engineers

CY - s.l.

ER -

Bruurs KAJ, van Esch BPM, van der Schoot MS. Exit loss model for plain axial seals in multi-stage centrifugal pumps. In ASME 2017 Fluids Engineering Division Summer Meeting: Volume 1A, Symposia: Keynotes; Advances in Numerical Modeling for Turbomachinery Flow Optimization; Fluid Machinery; Industrial and Environmental Applications of Fluid Mechanics; Pumping Machinery. s.l.: American Society of Mechanical Engineers. 2017. FEDSM2017-69251 https://doi.org/10.1115/FEDSM2017-69251