Spiral-grooved gas face seal for steam turbine shroud tip leakage reduction: Performance and feasibility analysis

Author:

Xu Wanjun,Yang Jiangang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials

Reference30 articles.

1. Control of shroud leakage loss by reducing circumferential mixing;Rosic;J Turbomach,2008

2. Denton JD. Loss mechanisms in turbomachines. In: ASME 1993 international gas turbine and aeroengine congress and exposition. Ohio, USA; 24–27 May 1993, paper No. 93-GT-453.

3. Schaub UW, Vlasic E, Moustapha SH. Effect of tip clearance on the performance of a highly loaded turbine stage. In: AGARD conference proceedings of 82nd symposium, technology requirements for small gas turbine; 1994, paper No. AGARD-CP-537.

4. Optimized shroud design for axial turbine aerodynamic performance;Porreca;J Turbomach,2008

5. Making use of labyrinth interaction flow;Pfau;J Turbomach,2004

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