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刷式密封刷丝摩擦磨损特性实验研究

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建立了基于柱面圆周摩擦的直接测力法与间接转矩法两种刷式密封摩擦因数实验识别模型,设计搭建了刷式密封摩擦磨损特性实验装置,设计加工了 8种不同结构参数的刷式密封实验件,实验对比分析了两种摩擦因数识别模型的实验结果,研究了结构参数对刷丝与转子表面正压力影响、工况参数对刷丝摩擦因数影响、干涉量对刷丝磨损影响。结果表明:直接测力法与间接转矩法测得的刷丝摩擦因数彼此相差较小,直接测力法稳定性优于间接转矩法。刷式密封刷丝与转子表面静态和动态正压力均随后挡板保护高度的增加而增大,随刷丝径向长度的增加而减小,随刷丝束厚度的增加而增大;相同干涉量下,静态正压力大于动态正压力;刷式密封刷丝与转子表面正压力在干涉加载阶段大于干涉卸载阶段,在转速升高阶段大于转速降低阶段,刷丝表现出滞后效应。刷式密封刷丝摩擦因数随刷丝与转子间干涉量的增加而降低,随转子转速的增加而降低;随摩擦时长增加,摩擦因数在磨损初期先迅速降低,之后基本保持稳定。刷式密封刷丝磨损量随刷丝与转子间干涉量的增加而增大,刷丝与转子间干涉量由0。3 mm增加至0。4mm时,刷丝磨损量增大了 296。66%。
Experimental investigation on friction and wear characteristics of brush seal bristle
Two brush seal friction coefficient experimental identification models were established based on cylindrical circumferential friction,direct force measurement and indirect torque method,an experimental device for friction and wear characteristics of brush seals was designed and built,and eight brush seal test pieces with different structural parameters were designed and processed.The experimental results of two kinds of friction coefficient identification models were compared and analyzed,and the influence of structural parameters on the positive pressure of the brush bristle and rotor surface,the influence of working conditions on the friction coefficient of the brush bristle,and the influence of interference on the wear of the brush bristle were studied.The research results showed that the friction coefficients of brush bristle measured by the direct force measurement method and the indirect torque method were less different from each other,and the stability of the direct force measurement method was better than that of the indirect torque method.Both the static and dynamic positive pressures on the surface of the brush seal and the rotor increased with the increase of the protection height of the baffle,decreased with the increase of the radial length of the brush,and increased with the increase of the thickness of the brush pack;at the same interference under the condition of measurement,the static positive pressure was greater than the dynamic positive pressure;the positive pressure of the brush seal filament and the rotor surface was greater in the interference loading phase than in the interference unloading phase,and the speed increase phase was greater than the speed reduction phase,the brush filament exhibited a hysteresis effect.The friction coefficient of the brush seal bristle decreased with the increase of the interference between the brush bristle and the rotor,and also decreased with the increase of the rotor speed;with the increase of the friction time,the friction coefficient decreased rapidly at the initial stage of wear,and then kept basically stable.The wear amount of the brush bristle of the brush seal increased with the increase of the interference between the brush bristle and the rotor.When the interference between the brush bristle and the rotor increased from 0.3 mm to 0.4 mm,the wear amount of the brush bristle increased by 296.66%.

brush sealpositive pressurefriction coefficientwear extentwear surface morphology

赵欢、冯毓钟、孙丹、张国臣、李玉、李浩

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沈阳航空航天大学航空发动机学院辽宁省航空推进系统先进测试技术重点实验室,沈阳 110136

刷式密封 正压力 摩擦因数 磨损量 磨损形貌

国家自然科学基金辽宁省"兴辽英才计划"项目辽宁省教育厅基础研究项目

52075346XLYC2007077JYT2020047

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(4)
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