A variant “Stepped Double Notched Tooth” for conventional sharp teeth of a labyrinth seal has been proposed and investigated by three-dimensional CFD numerical modeling of the flow field. The purpose is to reduce total leakage through the seal. The tooth is numerically tested with both solid and honeycomb lands. CFD assumptions and analysis were validated by comparison with leakage data from stationary labyrinth seal experiments conducted by Stocker [1]. The baseline model considered for comparison study consists of the conventional straight-through four sharp knife shaped teeth in combination with solid and honeycomb land. The variant tooth is also straight having a sharp tip but has a stepped inclined notch opposing the flow at both sides of the tip. CFD analyses revealed that this double notched tooth reduces seal leakage by ∼10.7% when used with solid land and ∼12.5% when used with honeycomb land compared to a conventional baseline tooth.
Skip Nav Destination
ASME Turbo Expo 2014: Turbine Technical Conference and Exposition
June 16–20, 2014
Düsseldorf, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4573-8
PROCEEDINGS PAPER
CFD Simulation of Single Step and Double Notched Tooth for Labyrinth Seals
Hasham H. Chougule,
Hasham H. Chougule
Honeywell Technology Solutions, Bangalore, India
Search for other works by this author on:
Alexander Mirzamoghadam,
Alexander Mirzamoghadam
Honeywell International, Phoenix, AZ
Search for other works by this author on:
Douglas Ramerth
Douglas Ramerth
Honeywell International, Phoenix, AZ
Search for other works by this author on:
Hasham H. Chougule
Honeywell Technology Solutions, Bangalore, India
Alexander Mirzamoghadam
Honeywell International, Phoenix, AZ
Douglas Ramerth
Honeywell International, Phoenix, AZ
Paper No:
GT2014-26286, V05CT16A028; 9 pages
Published Online:
September 18, 2014
Citation
Chougule, HH, Mirzamoghadam, A, & Ramerth, D. "CFD Simulation of Single Step and Double Notched Tooth for Labyrinth Seals." Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Volume 5C: Heat Transfer. Düsseldorf, Germany. June 16–20, 2014. V05CT16A028. ASME. https://doi.org/10.1115/GT2014-26286
Download citation file:
19
Views
0
Citations
Related Proceedings Papers
Related Articles
Development of a Two-Dimensional Computational Fluid Dynamics Approach for Computing Three-Dimensional Honeycomb Labyrinth Leakage
J. Eng. Gas Turbines Power (October,2004)
Numerical Investigations for Leakage and Windage Heating in Straight-Through Labyrinth Seals
J. Eng. Gas Turbines Power (January,2016)
A Bulk Flow Model for Off-Centered Honeycomb Gas Seals
J. Eng. Gas Turbines Power (January,2007)
Related Chapters
Numerical Simulations of Tip Leakage Vortex Cavitation Flows Around a NACA0009 Hydrofoil
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
System Automation
Pipeline Operation & Maintenance: A Practical Approach, Second Edition
But the Graphics Are Pretty
Hot Air Rises and Heat Sinks: Everything You Know about Cooling Electronics Is Wrong