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    Dynamic Characteristics of Labyrinth Seal and Rotor Stability Considering Swirl Brakes 

    Source: Journal of Aerospace Engineering:;2023:;Volume ( 036 ):;issue: 005:;page 04023057-1
    Author(s): Dan Sun; Guozheng Su; Huan Zhao; Xiaowei Wang; Wenfeng Xu; Zemin Yang
    Publisher: ASCE
    Abstract: The numerical solution model of the labyrinth seal considering the multiple frequencies elliptical whirling of the rotor and swirl brake was established by the computational fluid dynamics (CFD) technique. Then, the dynamic ...
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    Buoyancy Effect of Bristles for a Brush Seal with Disturbance-Suppressing Holes 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006:;page 04024073-1
    Author(s): Dan Sun; JiSheng Sun; Huan Zhao; Ze-Min Yang; Haoyu Yin; Wen-feng Xu
    Publisher: American Society of Civil Engineers
    Abstract: Bristles in the first few rows float up from the rotor surface due to the radial airflow in the gap between the front plate and bristle pack, which directly affects seal performance and the service life of a brush seal. ...
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    Influence Factors of Honeycomb Seal Performance and Stability Analysis of Rotor System 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004:;page 04022042
    Author(s): Huan Zhao; Ran Zhang; Dan Sun; Min Zhou; Yu Li; Ping Wang
    Publisher: ASCE
    Abstract: Structural parameters and inlet preswirl have great influences on the static and dynamic characteristics of honeycomb seals. In this paper, a multifrequency elliptical vortex dynamic model of a honeycomb seal was established ...
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    Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth Seals 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 005
    Author(s): Dan Sun; Min Zhou; Huan Zhao; Jiang Lu; Cheng-Wei Fei; Huan Li
    Publisher: ASCE
    Abstract: The heat load caused by windage heating effect of labyrinth seals seriously influences the sealing of shaft air flow. To reveal the windage heating effect of labyrinth seals to reasonably design an aeroengine rotor, this ...
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