Flow mechanism between purge flow and mainstream in different turbine rim seal configurations
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference23 articles.
1. Numerical investigation on the flow and heat transfer in a rotor-stator disc cavity;Liao;Appl Therm Eng,2015
2. Application of heat and mass transfer analogy on hot gas ingestion through rim seal;Liu;Appl Therm Eng,2016
3. Numerical investigation on the steady and unsteady flow characteristics of rim seal for the first stage in gas turbine;Wang;Appl Therm Eng,2016
4. Effect of rotor-mounted protrusion on sealing performance and flow structure in rotor-stator cavity;Cao;Chinese J Aeronaut,2018
5. Schuler P, Kurz W, Dullenkopf K, et al. The influence of different rim seal geometries on hot-gas ingestion and total pressure loss in a low-pressure turbine. New York: ASME; 2010. Report No.: GT2010-22205.
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1. Sealing efficiency performance of four different rim seals in turbine cavity;Chinese Journal of Aeronautics;2024-08
2. Parameter sensitivity analysis of the interaction between purge flow and mainstream;Applied Thermal Engineering;2024-04
3. Experimental and Numerical Investigations into the Effects of Rim Seal Structure on Endwall Film Cooling and Flow Field Characteristics;Energies;2023-12-08
4. Rotor Cascade Assessment at Off-Design Condition: An Aerodynamic Investigation on Platform Cooling;International Journal of Turbomachinery, Propulsion and Power;2023-07-22
5. Numerical investigation on effects of egress flow through different rim seals;Thermal Science and Engineering Progress;2023-02
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