• DocumentCode
    1740192
  • Title

    Remote control structural exciters for structural data acquisition system calibrations

  • Author

    Banaszak, David

  • Author_Institution
    Air Force Res. Lab., Air Vehicles Directorate, WPAFB, OH, USA
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    95
  • Lastpage
    104
  • Abstract
    The Air Force invented a new calibration technique, which allows one person to perform multiple end-to-end mechanical calibrations of structural dynamics measurement systems. An end-to-end calibration means a full calibration of instrumentation from the physical input to the transducer to the output where the analog or digital signal is normally analyzed. It is difficult to stimulate mounted and embedded transducers with known physical inputs. Normally two people calibrate-one at the transducer holds or attaches the exciter and one operates the recorder. This new technique uses remote control structural exciters to stimulate measurement transducers contained in structures, with a measurable input level, and the output signal is communicated to a data recorder. The Air Force demonstrated this patented technique by using accelerometers in the laboratory. A commercial off-the-shelf vibration paging system sends a signal from a master control unit to individual exciters that stimulate accelerometers mounted on structures. A reference accelerometer measures the input. Engineers validated the technique using eight different exciters in a completely randomized block design experiment consisting of three 2-level factors: material, structural thickness and excitation mode. The engineers measured amplitude, frequency and transfer function between the accelerometers. This paper describes the invention and looks at potential field applications to insure data integrity in structural data acquisition systems on aging commercial and military vehicles
  • Keywords
    accelerometers; calibration; condition monitoring; data acquisition; data integrity; design of experiments; strain gauges; telecontrol; transfer functions; accelerometers; aging vehicles; commercial vehicles; data integrity; data recorder; excitation mode; experimental design; flight tests; master control unit; measurement transducers; military vehicles; multiple end-to-end mechanical calibrations; off-the-shelf vibration paging system; remote control structural exciters; strain gauges; structural data acquisition system calibration; structural dynamics measurement systems; structural thickness; transfer function; Accelerometers; Calibration; Data acquisition; Force measurement; Instruments; Mechanical variables measurement; Performance evaluation; Signal analysis; Transducers; Vehicle dynamics;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    National Aerospace and Electronics Conference, 2000. NAECON 2000. Proceedings of the IEEE 2000
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-6262-4
  • Type

    conf

  • DOI
    10.1109/NAECON.2000.894897
  • Filename
    894897