• DocumentCode
    2643301
  • Title

    Ceramic strain gages for propulsion health monitoring

  • Author

    Gregory, Otto J. ; Luo, Qing

  • Author_Institution
    Dept. of Chem. Eng., Rhode Island Univ., Kingston, RI, USA
  • Volume
    2
  • fYear
    2000
  • fDate
    2000
  • Abstract
    A robust ceramic strain gage has been developed for propulsion health monitoring which is capable of measuring both static and dynamic strains at temperatures up to 1400°C. These thin film sensors are ideally suited for in-situ strain measurement in harsh environments such as those encountered in the hot sections of gas turbine engines. The sensors are non-intrusive and robust enough to withstand the high “g” loading associated with rotating engine components. Since gage thickness is considerably less than the boundary layer thickness, these sensors do not adversely affect the gas flow path through the engine. Results of recent laboratory tests have shown that these strain gages can meet many of the current demands of high performance propulsion engines. Specifically, static strain tests have been performed at temperatures as high as 1400°C, which have resulted in a relatively large and reproducible piezoresistive response. In addition, high frequency dynamic strain tests were performed at temperatures up to 500°C and at frequencies up to 2000 Hz to simulate conditions that would be encountered during high cycle fatigue. The results indicated that not only did these sensors survive severe testing conditions, including an applied strain of ±500 με, but that they were sensitive enough to isolate possible causes of high cycle fatigue. The results of both the static and dynamic strain measurements at elevated temperature using these ceramic strain gages are presented and the prospects of using these strain gages for structural health monitoring are discussed
  • Keywords
    aerospace engines; aerospace instrumentation; aerospace propulsion; aerospace testing; condition monitoring; electric sensing devices; fatigue testing; gas turbines; piezoresistive devices; strain gauges; strain measurement; 1400 C; 500 C; ITO based strain sensors; dynamic strains; gas turbine engine hot sections; harsh environments; high cycle fatigue; high performance propulsion engines; high temperatures; in-situ strain measurement; propulsion health monitoring; reproducible piezoresistive response; robust ceramic strain gage; static strains; structural health monitoring; thin film sensors; Capacitive sensors; Ceramics; Engines; Monitoring; Performance evaluation; Propulsion; Robustness; Strain measurement; Temperature sensors; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
  • Conference_Location
    Philadelphia, PA
  • Print_ISBN
    0-7803-6395-7
  • Type

    conf

  • DOI
    10.1109/DASC.2000.884914
  • Filename
    884914