A comparison of blade tip timing data analysis methods

被引:108
作者
Carrington, IB [1 ]
Wright, JR [1 ]
Cooper, JE [1 ]
Dimitriadis, G [1 ]
机构
[1] Univ Manchester, Sch Engn, Dynam & Aeroelast Res Grp, Manchester M13 9PL, Lancs, England
关键词
blade tip timing; non-intrusive stress measurement system; vibration analysis; turbomachinery; bladed assemblies; autoregressive methods;
D O I
10.1243/0954410011533293
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The experimental determination of the vibration characteristics of rotating engine blades is very important for fatigue failure considerations. One of the most promising techniques for measuring the frequency of blade vibrations is blade tip timing. In this paper, three vibration analysis methods were specifically formulated and applied to the tip timing problem for the first time, using data obtained from a simple mathematical blade tip timing simulation. The results from the methods were compared statistically in order to determine which of the techniques is more suitable. One of the methods, the global autoregressive instrumental variables approach, produced satisfactory results at realistic noise levels. However, all of the techniques produced biased results under certain circumstances.
引用
收藏
页码:301 / 312
页数:12
相关论文
共 9 条
  • [1] SYSTEM IDENTIFICATION - SURVEY
    ASTROM, KJ
    EYKHOFF, P
    [J]. AUTOMATICA, 1971, 7 (02) : 123 - +
  • [2] COOPER JE, 1989, INT J ANAL EXPT MODA, V4, P51
  • [3] HEATH S, 1997, AGARD C P, V598
  • [4] Heath S., 1997, INT GAS TURB AER ENG, P1
  • [5] HEATH S, 1999, INT GAS TURB AER C E
  • [6] COMPARISON OF PARAMETER ESTIMATION ALGORITHMS FOR DISCRETE SYSTEMS
    JAMES, PN
    SOUTER, P
    DIXON, DC
    [J]. CHEMICAL ENGINEERING SCIENCE, 1974, 29 (02) : 539 - 547
  • [7] ROBINSON WW, 1991, P 37 S INSTR SOC AM, P91
  • [8] ROBINSON WW, 1999, 45 INT INSTR S ALB N
  • [9] ZIELINSKI M, 1997, AGARD C P, V598