共查询到18条相似文献,搜索用时 109 毫秒
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采用RNG k-ε两方程紊流模型、Simple算法和结构化网格,利用Fluent软件数值分析不同间隙、压比和转速条件下,蜂窝芯格尺寸对蜂窝密封内泄漏流动的影响。结果表明:蜂窝密封特殊的六边形结构可以将泄漏流分割成许多小涡流,漏汽在蜂窝腔内呈逆时针螺旋式三维紊流运动;芯格尺寸越大,漏汽量越大;同一密封间隙下,随着芯格尺寸的增大,泄漏量增大的趋势在升高;随着压比的增大,蜂窝密封的泄漏量增大,但泄漏量增加的趋势在减小;随着转速的增加,转轴表面形成强烈的气旋效应,有利于阻滞泄漏流动。 相似文献
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为提高压气机级间气路封严密封性能,在传统六边形蜂窝的基础上,改变其结构得到方形蜂窝和圆形蜂窝,数值研究不同间隙、压比和转速下蜂窝结构对篦齿-蜂窝密封封严性能的影响。结果表明:间隙增加时,篦齿密封、六边形蜂窝密封、方形蜂窝密封、圆形蜂窝密封4种密封方式泄漏量均线性增加,但由于蜂窝破坏了流场透气效应,故篦齿-蜂窝密封泄漏量增速最慢,其中圆形蜂窝密封封严效果最好;压比增加时,4种密封方式泄漏量均增加,但篦齿及蜂窝腔室内形成漩涡亦随压比增加而愈发强烈,耗散更多能量,故泄漏量增速逐渐变缓;转子转速增加时,流体环向速度增加,4种密封方式泄漏量均减小,而蜂窝环向切割流体形成漩涡耗散能量,故篦齿-蜂窝密封减小幅度较大。在大间隙高压比高转速的工况下,篦齿-蜂窝衬套结构封严效果更好,其中篦齿-圆形蜂窝密封最具优势。 相似文献
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考虑闭合效应的刷式密封泄漏特性研究 总被引:3,自引:0,他引:3
采用基于非线性Darcian多孔介质模型的Reynolds-Averaged Navier-Stokes(RANS)方程的数值方法研究实验测量的零间隙和具有间隙的刷式密封在不同压比和转速下的泄漏特性,提出针对刷式密封闭合效应的间隙修正公式。考虑闭合效应后具有间隙的刷式密封泄漏量的预测结果与实验数据吻合,验证所建立刷式密封闭合效应修正模型的有效性。研究结果表明:刷丝束顶部与转轴间的间隙导致刷丝束内部压力降低且具有较为明显的径向压差,径向压差的存在导致刷丝束产生闭合效应,进而减小了刷式密封的有效密封间隙;闭合效应使得刷式密封有效间隙随着压比升高而减小,数值计算刷式密封泄漏特性时考虑闭合效应可以显著提高预测精度;在相同压比和转速下,具有间隙的刷式密封的泄漏量明显大于零间隙刷式密封的泄漏量;刷式密封的泄漏量随着压比的增大而增大;在所研究的转速范围内转速对刷式密封的泄漏特性的影响有限。 相似文献
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根据某型汽轮机迷宫轴封的泄漏特性进行了蜂窝轴封的改进设计,以及蜂窝轴封的泄漏特性和影响因素的研究。介绍了透平机械密封技术的研究进展。根据汽轮机迷宫轴封的结构特点,对高低齿迷宫密封的短齿部分改进设计成蜂窝结构,将传统的迷宫轴封设计成蜂窝轴封,并采用数值方法研究改进的蜂窝轴封泄漏特性。数值分析了传统迷宫轴封的泄漏特性。比较了不同间隙、不同芯格尺寸的蜂窝密封的泄漏特性,得出了最佳蜂窝密封尺寸。蜂窝轴封的最佳设计方案是径向间隙0.50mm,蜂窝芯格直径是2.75mm。 相似文献
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针对直升机减速器润滑油泄漏问题,选取某直升机减速器径向石墨密封环为研究对象,应用FLUENT软件对其内部流场和泄漏特性进行数值模拟,研究径向间隙、密封块豁口间隙、压比、被密封轴椭圆度及密封环分块数对径向石墨密封泄漏特性的影响。结果表明,在其他条件相同时,密封装置的泄漏量随径向间隙、椭圆度的增大而增大,且增大速度有加快的趋势;密封装置的泄漏量随豁口间隙的增大而增大,且增大速度有减慢的趋势;密封装置的泄漏量随压比的增大近似呈线性增大;密封装置的泄漏量与密封环分块数没有明显关系。 相似文献
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采用计算流体动力学软件、RNG k-ε模型、Simple算法和结构化网格,研究不同间隙、压比、转速等工况下密封表面凹槽结构对凹槽迷宫密封三维流场和泄漏流动特性的影响。结果表明:凹槽迷宫密封的凹槽结构可以更加充分地耗散气体的动能,从而有效地阻滞气体流动,减小气体的泄漏;迷宫密封的泄漏量随间隙的增大而增大,但凹槽迷宫密封泄漏量和泄漏量增加率都小于普通迷宫密封;随着压比的增大,凹槽迷宫密封的泄漏量有所增加,但相比于普通迷宫密封,其泄漏量增加的趋势在逐渐减小;随着转速的增加,凹槽迷宫密封更容易在凹槽内形成气旋效应,从而使其封严性能显著提高。 相似文献
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反旋流对密封静力与动力特性影响的理论与试验研究 总被引:4,自引:0,他引:4
设计加工无/有反旋流共4种密封结构,从理论与实验两个方面研究反旋流对密封静力与动力特性的影响规律。建立反旋流密封静力特性CFD模型,理论分析反旋流对密封间隙流体切向速度、周向压力分布以及泄漏特性的影响;设计搭建反旋流密封动力特性试验台,试验测试无/有反旋流密封的泄漏特性,应用不平衡同频激励法试验研究反旋流对密封动力特性的影响。研究结果表明:反旋流可减小密封间隙流体的切向速度,进而降低密封间隙流体的周向压力差,且密封间隙流体周向压差随切向速度的减小而降低,这是反旋流抑制密封气流激振力的主要原因;密封的泄漏量随进出口压比的增加而增大,两者近似呈线性关系;与无反旋流密封相比,反旋流密封增加了密封的泄漏量,且随着进出口压比的增加,两者泄漏量差异增大;密封的动力特性系数的随密封进出口压比与转速的增加而增大。在相同工况下,主刚度大于交叉刚度约一个数量级,主阻尼与交叉阻尼数量级相同,且主阻尼大于交叉阻尼;反旋流可有效降低密封的等效刚度,增加密封的等效阻尼,提高密封的稳定性。 相似文献
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Effect of honeycomb seals on loss characteristics in shroud cavities of an axial turbine 总被引:1,自引:0,他引:1
The loss in efficiency due to shroud leakage or tip clearance flow accounts for a substantial part of the overall losses in turbomachinery.It is important to identify the leakage loss characteristics in order to optimize turbomachinery.At present,little information is available in the open literature concerning the effect of honeycomb seals on the loss characteristics in shroud cavities of an axial turbine,despite of the widespread use of the honeycomb seals.Therefore,interaction between rotor labyrinth seal leakage flow with and without honeycomb facings and main flow is investigated to provide the loss characteristics of the mixing process of the re-entering leakage flow into the main flow.The effects of honeycomb seals on the flow in shroud cavities and interaction with the main flow are analyzed.An additional study on the impact of subtle shroud cavity exit geometry is also presented.The investigation results indicate that the honeycomb seal affects the over tip leakage flow and reduces mixing losses when compared to the solid labyrinth seal.The leakage flow interactions with the main flow have considerably changed the flow fields in the endwall regions.The proposed research reveals the effects of honeycomb seals on the loss characteristics in shroud cavities and the impact of subtle shroud cavity exit geometry,and it is helpful for the design optimization of turbomachinery. 相似文献
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Xin Yan Xinbo Dai Kang Zhang Jun Li Kun He 《Journal of Mechanical Science and Technology》2018,32(10):4697-4709
To achieve higher aerodynamic performance, turbine usually works at tight clearance, which results in inevitable rub between the rotor and stator parts of labyrinth seal due to vibrations, misalignment, mechanical force, thermal stress, etc. In the rubbing events, contact between labyrinth fin and rotor part will commonly induce the teeth bending and mushrooming damages, which significantly affect the discharge performance of a labyrinth seal. To account for the influence of teeth bending and mushrooming on leakage performance of a straight-through labyrinth seal, the leakage rates and flow fields in the worn labyrinth seal are measured and also compared with the original design cases. With numerical methods, the discharge behaviors of the labyrinth seal with different degrees of bending and mushroom damages are analyzed. It shows that the predicted leakage performance and flow fields in the labyrinth seals match well with the experimental tests. For the bending cases, the leakage rates and flow patterns in labyrinth seals are dependent on the effective clearance and bending angle. The leakage ratio of forward bending case is smaller than that of backward bending case with the same geometrical dimensions. However, for the mushroomed labyrinth seals, the leakage rates and flow patterns are much dependent on the effective clearance but slightly dependent on the mushroom radius. 相似文献
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