Budi Chandra
Mechanisms for Residence Volume Reduction in Shallow Sump
Chandra, Budi; Simmons, Kathy; Murphy, Andrew
Authors
Professor KATHY JOHNSON KATHY.JOHNSON@NOTTINGHAM.AC.UK
PROFESSOR OF MECHANICAL AND AEROSPACE ENGINEERING
Andrew Murphy
Abstract
© 2018 by ASME. Gas turbine aero-engines employ fast rotating shafts that are supported by bearings at several axial locations along the engine. Due to extreme load and heat, oil is injected to the bearings to aid lubrication and cooling. The oil is then shed to the bearing chamber before it is extracted out by a scavenge pump. Scavenging oil from the bearing chamber is challenging due to high windage induced by the fast rotating shafts as well as the two-phase nature of the flow. A deep sump has been found to increase scavenge performance due to its ability to shelter the pooled oil from the bulk rotating air flow thus minimizing two-phase mixing. However, in many cases, a deep sump is not an option due to conflicting space requirements. The space limitation becomes more stringent with higher bypass ratio engines as the core becomes smaller. Therefore, it is imperative to have a high performing shallow sump. However, shape modification of a shallow sump is too constrained due to limited space and, therefore, has minimal impact on the scavenge performance. This research presents several alternative concepts to improve scavenge performance of a generic baseline shallow sump by augmenting it with attachments or inserts. These augmentations attempt to exploit two known mechanisms for reducing the residence volume: momentum reduction and sheltering. The experimental results show that some augmentations are able to reduce the residence volume of a shallow sump by up to 50% or more in some cases.
Citation
Chandra, B., Simmons, K., & Murphy, A. (2018). Mechanisms for Residence Volume Reduction in Shallow Sump. Journal of Engineering for Gas Turbines and Power, 140(3), Article 032601. https://doi.org/10.1115/1.4037871
Journal Article Type | Article |
---|---|
Acceptance Date | Jul 10, 2017 |
Online Publication Date | Oct 17, 2017 |
Publication Date | 2018-03 |
Deposit Date | Sep 12, 2017 |
Publicly Available Date | Oct 18, 2018 |
Journal | Journal of Engineering for Gas Turbines and Power |
Print ISSN | 0742-4795 |
Electronic ISSN | 1528-8919 |
Publisher | American Society of Mechanical Engineers |
Peer Reviewed | Peer Reviewed |
Volume | 140 |
Issue | 3 |
Article Number | 032601 |
DOI | https://doi.org/10.1115/1.4037871 |
Public URL | https://nottingham-repository.worktribe.com/output/872174 |
Publisher URL | http://gasturbinespower.asmedigitalcollection.asme.org/article.aspx?articleid=2654069 |
Contract Date | Sep 11, 2017 |
Files
GTP-17-1185 (pdf).pdf
(1.1 Mb)
PDF
You might also like
Characterising Horizontal Two-Phase Flows Using Structured-Planar Laser-Induced Fluorescence (S-PLIF) Coupled With Simultaneous Two-Phase PIV (S2P-PIV)
(2024)
Presentation / Conference Contribution
GT2022-82180 Experimental investigation into oil film thickness and behaviour near an aero-engine bearing
(2022)
Presentation / Conference Contribution
COUPLED EULERIAN THIN FILM MODEL AND LAGRANGIAN DISCRETE PHASE MODEL TO PREDICT FILM THICKNESS INSIDE AN AERO-ENGINE BEARING CHAMBER
(2022)
Presentation / Conference Contribution
Experimental Investigation Into Oil Shedding From a Rotating Cup Geometry
(2022)
Presentation / Conference Contribution
Downloadable Citations
About Repository@Nottingham
Administrator e-mail: discovery-access-systems@nottingham.ac.uk
This application uses the following open-source libraries:
SheetJS Community Edition
Apache License Version 2.0 (http://www.apache.org/licenses/)
PDF.js
Apache License Version 2.0 (http://www.apache.org/licenses/)
Font Awesome
SIL OFL 1.1 (http://scripts.sil.org/OFL)
MIT License (http://opensource.org/licenses/mit-license.html)
CC BY 3.0 ( http://creativecommons.org/licenses/by/3.0/)
Powered by Worktribe © 2025
Advanced Search