The leakage characteristics and hysteresis effect of different axial width of pressure relief chamber of 0
04 mm and 06 mm with the conventional and low hysteresis brush seals were studied under the static and dynamic tests of pressure difference rise and drop and the rotor speed rise and drop. The results showed that: the dynamic leakage coefficient was about 14%-20% lower than the static one
when the pressure drop was more than 02MPa. The sealing performance of low hysteresis brush seals was better
and the leakage coefficient was up to about 20% lower than the conventional brush seal. The hysteresis effect was the strongest in the process of pressure difference rise and drop cycle with the static condition when axial width of pressure relief chamber was 06 mm. The hysteresis effect of conventional brush seal was the strongest in the process of pressure difference rise and drop cycle with the dynamic condition. After the rotor speed rise and drop cycle
the leakage coefficient decrease by about 15% when the axial width of pressure relief chamber was 06 mm
and there was basically no hysteresis effect when the axial width was 04 mm. In addition
for the three structures
the brush seal with the axial width 04 mm had the best sealing performance and the weakest hysteresis effect.
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Related Author
Hao LI
Yuzhong FENG
Huan ZHAO
Dan SUN
Wei MU
Guochen ZHANG
Jindao GUO
Dan SUN
Related Institution
Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System,School of Aero⁃engine,Shenyang Aerospace University
Key Lab for Power Transmission of Aero Engine,Shenyang Engine Research Institute,Aero Engine Corporation of China
Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University
Collaborative Innovation Center of Machine Manufacturing in Liaoning,Shenyang Blower Works Group Company Limited
Key Laboratory of Advanced Measurement and Test Technology for;Aviation Propulsion System,Liaoning Province,School of Aero⁃engine,Shenyang Aerospace University