Research Status and Development Trend of Cylindrical Gas Film Seals for Aeroengines

被引:5
作者
Jiang, Haitao [1 ]
Yu, Shurong [1 ]
Wang, Shengshun [1 ]
Ding, Xuexing [1 ]
Jiang, Andi [1 ]
机构
[1] Lanzhou Univ Technol LUT, Coll Petrochem Engn, Lanzhou 730050, Peoples R China
关键词
aeroengine sealing technology; cylindrical gas film seal; dynamic characteristics; multi-physical field coupling; structural deformation; experimental testing; development trend; FLOATING RING SEAL; ROTORDYNAMIC COEFFICIENTS; LEAKAGE PERFORMANCE; LABYRINTH SEAL; FLUID-FLOW; HIGH-SPEED; TEMPERATURE; MODEL; ROTOR; SYSTEMS;
D O I
10.3390/pr12010069
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
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.
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页数:43
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