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基于压缩和油脂逃逸试验的盾尾刷密封性分析
引用本文:钟小春,黄思远,竺维彬,陈乔松,游智. 基于压缩和油脂逃逸试验的盾尾刷密封性分析[J]. 西南交通大学学报, 2023, 58(1): 125-132. DOI: 10.3969/j.issn.0258-2724.20210814
作者姓名:钟小春  黄思远  竺维彬  陈乔松  游智
作者单位:1.河海大学土木与交通学院,江苏 南京 2100982.广州地铁集团有限公司,广东 广州 5102203.广州轨道交通建设监理有限公司,广东 广州 510010
基金项目:国家自然科学基金(52178387,51678217)
摘    要:为研究盾尾刷质量问题对盾尾刷密封系统工作性能的影响,基于动态压缩试验与油脂逃逸试验,探讨了盾尾刷长期挤压、磨损程度、砂浆渗入对盾尾刷密封性能的影响机理.首先,通过动态压缩试验,获得各个影响因素下盾尾刷贴合力变化规律;其次,利用油脂逃逸试验获取不同工况下盾尾刷的油脂逃逸量;最后,以贴合力为媒介,将影响盾尾刷质量的因素与油脂逃逸量联系起来,探讨盾尾刷的密封性能.研究结果表明:长期挤压、盾尾刷磨损程度、砂浆渗入等因素对盾尾刷弹性性能的影响显著,尤其是砂浆渗入,盾尾刷弹性性能损失最大可达90%;油脂压力存在一临界压力,盾尾间隙为50、70、90 mm的临界油脂压力分别为0.4、0.3、0.2 MPa,低于临界压力时油脂逃逸量极少,超过临界压力时油脂逃逸量陡增,油脂压力增加0.1 MPa,油脂逃逸量增加4倍以上;在盾构平均盾尾间隙(70 mm)条件下,当保护板磨损超过1/2与砂浆渗入比超过10%时,油脂逃逸将超过工程容许上限.

关 键 词:盾构隧道  盾尾刷  动态压缩  油脂逃逸  密封
收稿时间:2021-11-03

Analysis of Sealing Performance of Shield Tail Brush Based on Compression and Grease Escape Test
ZHONG Xiaochun,HUANG Siyuan,ZHU Weibin,CHEN Qiaosong,YOU Zhi. Analysis of Sealing Performance of Shield Tail Brush Based on Compression and Grease Escape Test[J]. Journal of Southwest Jiaotong University, 2023, 58(1): 125-132. DOI: 10.3969/j.issn.0258-2724.20210814
Authors:ZHONG Xiaochun  HUANG Siyuan  ZHU Weibin  CHEN Qiaosong  YOU Zhi
Affiliation:1.College of Civil and Transportation Engineering, Hohai University, Nanjing 210098, China2.Guangzhou Metro Group Co., Ltd., Guangzhou 510220, China3.Guangzhou Rail Transit Construction Engineering Consulting Co., Ltd., Guangzhou 510010, China
Abstract:In order to study the effect of the quality of shield tail brush on the working performance of shield tail sealing system, based on dynamic compression test and grease escape test, the influence mechanism of long-term extrusion, wear degree of shield tail brush and mortar penetration on sealing performance of shield tail brush are revealed. Firstly, the variation law of the adhesion force of shield tail brush under various influencing factors is discussed based on the dynamic compression test. Secondly, the grease escape volume of shield tail brush under different working conditions is obtained by grease escape test. Finally, taking the adhesion force as the medium, the factors affecting the quality of shield tail brush are connected with the volume of grease escape, and the sealing performance of shield tail brush is discussed. The results show that, long-term extrusion, wear degree of shield tail brush and mortar penetration ratio have significant effects on the elastic properties of shield tail brush, especially the mortar penetration ratio can cause the elastic property loss up to 90%. There is a critical pressure in the grease pressure, and the critical grease pressure with shield tail clearance of 50, 70, 90 mm is 0.4, 0.3, 0.2 MPa respectively. When grease pressure is lower than the critical pressure, the volume of grease escape is very small. When it exceeds the critical pressure, the volume of grease escape increases sharply. The grease pressure further increases by 0.1 MPa, the volume of grease escape increases by more than 4 times. Under the condition of average shield tail clearance (70 mm), the volume of grease escape exceeds the allowable upper limit when the wear of protective plate exceeds 1/2 and the mortar penetration ratio exceeds 10%. 
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