Affiliation:
1. College of Petrochemical Engineering, Lanzhou University of Technology (LUT), Lanzhou 730050, China
Abstract
High-performance aeroengine design is an important component of modern industry, and advanced sealing technology is a key technology to meet the engine fuel consumption rate, thrust-to-weight ratio, pollutant emission, durability, and lifetime. Reducing the internal airflow leakage of the engine through a sealing technology can improve the performance and efficiency of the engine. In this paper, the typical sealing technology for an aeroengine is introduced in more detail, including the structural characteristics and use limitations of the labyrinth seal, brush seal, honeycomb seal, gas film face seal, and cylindrical gas film seal. It focuses on the development history, typical structure type, working principle, basic technology research method, steady-state performance, dynamic characteristics, multi-physical field coupling, structural deformation, experimental testing, processing technology. Finally, it summarizes the problems and future development trends of the current application of the cylindrical gas film seal in aeroengines, and points out that the seal performance test and evaluation based on advanced composite sensor technology and the innovative design of the seal based on new material, a new principle, and a new structure will be the new research direction.
Funder
Gansu Basic Research Program—Outstanding Doctoral Student Project
Outstanding Graduate Student “Innovation Star” Program of Gansu Provincial Education Department
Subject
Process Chemistry and Technology,Chemical Engineering (miscellaneous),Bioengineering
Reference207 articles.
1. Two- and Three-Dimensional Numerical Experiments Representing Two Limiting Cases of an In-Line Pair of Finger Seal Components;Braun;Int. J. Rotating Mach.,2002
2. Current seal designs and future requirements for turbine engine seals and bearings;Povinelli;J. Aircr.,1975
3. Prospects of Aeroengine Power Transmission System in the 21st Century;Shu;J. Aerosp. Power,2001
4. Steinetz, B.M., Hendricks, R.C., and Munson, J. (1999). Advanced Seal Technology Role in Meeting Next Generation Turbine Engine Goals, RTO AVT Symposium.
5. Application Research of Seal Technologies for Aeroengine;Aeroengine,2012
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