封严环的不平衡量及配合关系对低压系统振动的影响分析
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  • 英文篇名:Influence of the Imbalance and Matching Relationship of the Sealing Ring on the Vibration of the Low Pressure System
  • 作者:王洪明 ; 孙汕民 ; 李希顺
  • 英文作者:Wang Hongming;Sun Shanmin;Li Xishun;AECC Shenyang Liming Aero-engine Co., Ltd.;
  • 关键词:低压涡轮转子部件 ; 低压系统 ; 不平衡量 ; 配合间隙 ; 发动机振动
  • 英文关键词:low-pressure turbine rotor;;low-pressure system;;unbalance;;clearance;;aero-engine vibration
  • 中文刊名:HKKX
  • 英文刊名:Aeronautical Science & Technology
  • 机构:中国航发沈阳黎明航空发动机有限责任公司;
  • 出版日期:2018-08-15
  • 出版单位:航空科学技术
  • 年:2018
  • 期:v.29;No.200
  • 语种:中文;
  • 页:HKKX201808005
  • 页数:5
  • CN:08
  • ISSN:11-3089/V
  • 分类号:26-30
摘要
为研究低压系统振动的影响因素,通过结构平面简化和数据统计,分析盘间封严环不平衡量、盘间封严环与低压一级涡轮盘配合间隙值等因素对低压系统振动的影响,提出盘间封严环的不平衡量越大则低压系统振动的可能性越大、盘间封严环与低压一级涡轮盘配合间隙值越大则低压系统振动的可能性越大。因此,控制盘间封严环不平衡量和盘间封严环与低压一级涡轮盘的配合间隙值是控制低压系统振动的有效措施。
        In order to study factors affecting the vibration of low pressure system, through structural plane simplification and statistical analysis, the influence of the unbalance between the disc seal ring, the gap between the disc seal ring and the low pressure turbine disk on the vibration of the low pressure system was analyzed. It is proposed that the greater imbalance of disc seal ring, the greater possibility of the vibration of the low pressure system, and the greater clearance between the seal ring and the low pressure first turbine disk, the greater the possibility of the vibration of the low pressure system. Therefore, it is an effective measure to control the vibration of the low pressure system by controlling the unbalance between the disc seal ring and the gap between the disc seal ring and the low-pressure first level turbine disk.
引文
[1]罗立,唐庆如.航空发动机振动与平衡研究[J].中国民航飞行学院学报,2014(5):57-60.Luo Li, Tang Qingru. Research on vibration and balance of aero-engine[J].Journal of Civil Aviation Flight University of China,2014(5):57-60.(in Chinese)
    [2]岳聪,任兴民,邓旺群,等.航空发动机转子突加不平衡参数分析及LQR控制技术应用[J].振动与冲击,2015,34(17):174-179.YueCong,RenXingmin,Deng Wangqun,etal.Parametric analysis due to sudden unbalance change and LQR control application for aeroengine rotor systems[J].Journal of Vibration and Shock,2015,34(17):174-179.(in Chinese)
    [3]张群岩,史建邦,符娆.基于多元线性回归方法的试验条件对发动机振动的影响分析[J].机械研究与应用,2016,29(4):114-117.Zhang Qunyan, Shi Jianbang, Fu Yao. Influence analysis of testing conditions on engine vibration base on MLR[J].Mechanical Research&Application,2016,29(4):114-117.(in Chinese)
    [4]朱亚夫,丁宏刚,曹光光.汽车起重机发动机振动分析[C]//中国工程机械学会工程起重机械分会第17届年会会刊,2015:201-207.Zhu Yafu,DingHonggang,CaoGuangguang.Vibrationanalysis of motor crane engine[C]//Association Journal of the 17th Annual Conference of China Construction Machinery Academy,Council of Hoisting Machiney,2015:201-207.(in Chinese)
    [5]周骏,潘晓铭,周哲为.转子动平衡的技术研究[J].机械设计与制造,2007(04):151-153.Zhou Jun, Pan Xiaoming, Zhou Zhewei. Rotator dynamic balance technology studies[J]. Machinery Design&Manufacture,2007(04):151-153.(in Chinese)
    [6]张大林.离心泵不平衡振动的故障诊断分析[J].建设机械技术与管理,2015,28(12):67-69.Zhang Dalin. Diagnosis and analysis of unbalance vibration fault for the centrifugal pump[J].Machinery Technology&Management,2015,28(12):67-69.(in Chinese)
    [7]刘静宇.CFM56-7B发动机振动指示高故障分析[J].航空维修与工程,2012(01):58-59.LiuJingyu. AnalysisofCFM56-7Benginevibrationhigh fault[J].Aviation Maintenance and Engineering, 2012(01):58-59.(in Chinese)
    [8]王宇飞,谢永鹏.旋转机械转子不平衡故障的诊断与分析[J].湖南工业职业技术学院学报,2009,9(05):6-7.Wang Yufei, Xie Yongpeng. Fault diagnosis and analysis of rotor imbalance of rotationmachinery[J]. Journal of Hunan Industry Polytechnic,2009,9(05):6-7.(in Chinese)
    [9]刘翠红,王克明,夏锟,等.转子系统不平衡响应的逆向分析[J].沈阳航空航天大学学报,2016,33(4):30-37.Liu Cuihong, Wang Kepeng, Xia Kun,et al. Reverse analysis of rotor unbalance response[J]. Journal of Shengyang Aerospace Uniwersity,2016,33(4):30-37.(in Chinese)
    [10]王娟,史新宇,王文宇.发动机转子平衡测量稳定性技术研究[J].航空科学技术,2015,26(07):17-21.WangJuan,ShiXinyu, Wang Wenyu.Researchonthemeasurementstabilitytechnologyofenginerotorbalancing[J].Aeronautical Science&Technology,2015,26(07):17-21.(in Chinese)
    [11]王娟,史新宇.航空发动机低压涡轮转子平衡工艺研究[J].航空科学技术, 2016,27(02):25-28.Wang Juan, Shi Xinyu. Research on the balancing technology of aeroengine low-pressure turbine rotor[J].Aeronautical Science&Technology,2017,27(02):25-28.(in Chinese)

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