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齿形结构对迷宫密封泄漏与动力特性影响

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建立齿在静子上迷宫密封(TOSLS)、齿在转子上迷宫密封(TORLS)与交错式迷宫密封(ILS)三维数值分析模型,并采用多频椭圆涡动轨迹模型与计算流体力学方法阐明4种齿形角(θ=0°,15°,30°,45°)对3种迷宫密封泄漏与动力特性的影响。结果表明:在转子转速15 000r/min与进口压力6。9 ×105 Pa的运行工况下,ILS具有最小的泄漏量,但是若采用过小的齿形角(θ=0°,15°)易引发转子失稳;TORLS具有最差的封严性能;TOS LS具有最好的系统稳定性。在齿形角从0°增加至45°时:TOSLS、TORLS与ILS的泄漏量分别降低5。6%、5。1%与16。8%;中间腔室负气流切向力的绝对值分别增加60。2%、133。9%与470。3%;整个密封段的有效阻尼分别增加44。9%~61。9%、30。7%~53。6%与90。4%~445。3%,系统稳定性均得到显著加强。
Effect of tooth profile on the leakage and dynamic characteristics of labyrinth seals
The three-dimensional numerical analysis models of teeth-on-stator labyrinth seal(TOS LS),teeth-on-rotor labyrinth seal(TOR LS)and interlocking labyrinth seal(ILS)were established.The effects of four tooth profile angles(θ=0°,15°,30°,45°)on the leakage and dynamic characteristics of three labyrinth seals were investigated by applying multi-frequency elliptical whirling orbit model and computational fluid dynamics method.Under the operating conditions of 15 000 r/min rotational speed and 6.9 × 105 Pa inlet pressure,although ILS leaked the least,it was easy to cause rotor instability if the tooth profile angle was too small(θ=0°,15°);TOR LS had the worst sealing performance,while TOS LS had the best system stability.As the tooth profile angle increased from 0° to 45°:the leakage flow rate of TOS LS,TOR LS and ILS decreased by 5.6%,5.1%and 16.8%;the absolute value of negative flow-induced tangential force for the middle cavity increased by 60.2%,133.9%and 470.3%;the effective damping of the whole seal section increased by 44.9%-61.9%,30.7%-53.6%and 90.4%-445.3%,respectively,indicating the system stability was significantly enhanced.

labyrinth sealcomputational fluid dynamicsleakage flow ratedynamic characteristicstooth profile angle

叶强生、张万福、周庆辉、李春

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上海理工大学能源与动力工程学院,上海 200093

上海理工大学上海市动力工程多相流动与传热重点实验室,上海 200093

迷宫密封 计算流体力学 泄漏量 动力特性 齿形角

国家自然科学基金上海市自然科学基金

5187536120ZR1439200

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(6)
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