王锁芳
    博士生导师
  • 招生学科专业:
    动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
    航空宇航科学与技术 -- 【招收硕士研究生】 -- 能源与动力学院
    能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
  • 学位:工学博士学位
  • 职称:教授
  • 所在单位:能源与动力学院
博士生导师
教师英文名称:Suofang Wang
电子邮箱:
所在单位:能源与动力学院
学历:南京航空航天大学
办公地点:A10-407,340
性别:
联系方式:sfwang@nuaa.edu.cn

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标题:
Investigations of the leakage characteristic and the sealing effectiveness on turbine bite rim seals
点击次数:
所属单位:
能源与动力学院
发表刊物:
J. Therm. Sci. Technol.
摘要:
In order to meet the needs of designing for high performance secondary air system in the turbine, a new turbine bite engineering rim seal of type-A and the related test rig were designed and set up. The numerical investigation and the experimental verification of the leakage characteristic of rim seal were carried out based on k-ω SST turbulence model. The key feature of the engineering rim seal of type-A, a bite type, was extracted, hence the other three kinds of rim seal named type-B, type-C and type-D were proposed. The sealing mechanism of bite rim seal was revealed from two aspects of the leakage characteristic and the seal effectiveness. The results show that: the numerical results of the k-ω SST turbulence model agree well with the experimental ones, and the maximum error is less than 4.2% in the range of this paper. The leakage of turbine bite rim seal of type-C and type-D are less than that of conventional rim seal (type-B). Compared with type-C, the radial inward shoulder structure of type-D reduces the leakage in the cavity, however, it enhances the pumping effect of the rotor. The average sealing efficiency of type-C and type-D are increased by 8.9% and 8.82% compared with that of conventional rim seal of type-B, respectively. The effects of entrainment and diffusion of the vortex in the sealing channel are one of the important reasons for the ingestion. There are two kinds of vortex structure named recirculation zone vortex (RZV) and rotationally induced vortex (RIV). The RZV will be rapidly replaced by the RIV with the rotation speed increasing at a low flow rate of the hot gas. However, the RZV will be relatively stable while the hot gas mass flow rate is increased. © 2018 The Japan Society of Mechanical Engineers.
是否译文:
发表时间:
2018-01-01
合写作者:
Dong, Weilin,Li, Pengfei
通讯作者:
Dong, Weilin,王锁芳
发表时间:
2018-01-01
个人简介

“某型发动机进气防砂滤国产化性能试验”和“某型发动机红外抑制器研制试验研究”课题通过了省部级鉴定,“某型发动机红外抑制器地面样机研制试验研究”获省科技进步三等奖、国防科学技术二等奖。 “中小型航空发动机空气系统篦齿封严研究”获国防科学技术三等奖。发表论文100余篇,多篇被Sci,Ei收录。获优秀科技论文奖4项。 1985年及1988年于东南大学工程热物理专业获工学学士和硕士学位;2002年于南京航空航天大学航空宇航推进理论与工程专业获工学博士学位,2008至2009年,赴美国Minnesota大学高级访问学者,师从美国工程院资深院士R. J. Goldstein教授,从事流动和传热研究工作。1988年至今任南京航空航天大学助教、讲师、副教授、教授、博士生导师。

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