• DocumentCode
    3230760
  • Title

    Miniature rotating amplifier system for windtunnel application packs 256 pre-conditioning channels in 187 cubic inch

  • Author

    Versteeg, M.H.J.B. ; Slot, H.

  • Author_Institution
    Nat. Aerosp. Lab., Amsterdam, Netherlands
  • fYear
    1997
  • fDate
    29 Sep-2 Oct 1997
  • Firstpage
    195
  • Lastpage
    201
  • Abstract
    For a NASA windtunnel model NLR developed a 256 channel pressure sensor signal conditioning and amplifier system. This system was to be mounted within the rotating part of the model in a volume of 7 inch diameter and less than 6 inch long. The development of this system, called Rotating Amplifier System (RAS), required a close cooperation between electrical and mechanical designers to meet all customer requirements. For all 256 channels the bridge supply voltage, offset and gain are separately remote controllable to allow for adjustments during a running experiment. These configuration settings are loaded into the system using a dedicated serial link. For on-line calibration an R-Cal function is available with 3 separate resistor values. The mechanical construction of the RAS unit consists of a cylindrical unit that is mounted on the propeller shaft between gearbox and sliprings. The RAS unit is of modular design and consists 16 of identical modules, each containing 16 self contained amplifier channels, sensor power supplies and associated control logic. The amplifier system was realized using specially developed hybrid modules and packs the complete functionality in 187 cubic inch
  • Keywords
    aerospace testing; amplifiers; automatic test equipment; calibration; computerised control; microcomputer applications; pressure sensors; signal processing; signal processing equipment; wind tunnels; 6 in; 7 in; NASA; NLR; R-Cal function; Rotating Amplifier System; bridge supply voltage; dedicated serial link; hybrid modules; mechanical construction; miniature rotating amplifier; modular design; multichannel pressure sensor; on-line calibration; pre-conditioning channels; propeller shaft; wind tunnel; Bridge circuits; Calibration; Mechanical sensors; NASA; Power amplifiers; Propellers; Resistors; Sensor systems; Shafts; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on
  • Conference_Location
    Pacific Grove, CA
  • Print_ISBN
    0-7803-4167-8
  • Type

    conf

  • DOI
    10.1109/ICIASF.1997.644681
  • Filename
    644681