Spiral-grooved gas face seal for steam turbine shroud tip leakage reduction: Performance and feasibility analysis
Authors:
- Wanjun XuWXWanjun Xu
- Jiangang YangJYJiangang Yang
- 1 June 2016
- journal article
- Published by Elsevier in Tribology International
- Vol. 98, 242-252
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51575105, 51275088)
This publication has 24 references indexed in Scilit:
- Effect of honeycomb seals on loss characteristics in shroud cavities of an axial turbineChinese Journal of Mechanical Engineering, 2013
- Optimized Shroud Design for Axial Turbine Aerodynamic PerformanceJournal of Turbomachinery, 2008
- Control of Shroud Leakage Loss by Reducing Circumferential MixingJournal of Turbomachinery, 2008
- Making Use of Labyrinth Interaction FlowJournal of Turbomachinery, 2004
- Development of Brush Seal Technology for Steam Turbine Retrofit Applications2003
- Effects of Labyrinth Seal Variation on Multistage Axial Turbine Flow2003
- Aeroelasticity Analysis of Air-Riding Seals for Aero-Engine ApplicationsJournal of Tribology, 2002
- The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow TurbineJournal of Turbomachinery, 2000
- Advanced seals for engine secondary flowpathJournal of Propulsion and Power, 1996
- Development of Film Riding Face Seals for a Gas Turbine EngineTribology Transactions, 1992