• DocumentCode
    2071874
  • Title

    Torquemeter on sites of gyrodines

  • Author

    Skorykh, V.J. ; Gormakov, A.N. ; Plotnikov, I.A.

  • Author_Institution
    Tomsk Polytech. Univ., Russia
  • Volume
    1
  • fYear
    2001
  • fDate
    26 Jun-3 Jul 2001
  • Firstpage
    42
  • Abstract
    The basic sources of vibration, noise and torques, transmitted case from a gyrodine, are dynamical unbalance of a rotor, errors of manufacturing of bearings and finite rigidity of the shaft. The requirements on these parameters for electric motors are not so stiff. But for gyrodines these requirements become paramount. The perturbing torques of the gyrodine, which is the effector of system of orientation, cause additional vibrations of a space vehicle, as multimass elastic system, that reduces accuracy of its orientation. For development and serial manufacture of gyrodines it is necessary to have a torquemeter for constant and alternate torques. The maximal torque of such a torquemeter -0.2 Nm, threshold of sensitivity -0.5·10-4 Nm. Constant and slowly varying torques with frequency up to 5 Hz can be measured on a torquemeter constructed on the principle of power compensation. The platform of a torquemeter has one measuring axis and is mounted on elastic three-tape supports which are set up on a quasi-zero torsional rigidity. For measurement of torque variation with frequency more than 5 Hz, the stand is equipped with the second measuring channel constructed on the basis of an accelerometer with a wide passband (up to 500 Hz). The accelerometer is mounted near to a site of the gyrodine. The signal from an accelerometer is proportional a high-frequency component of torque, which is not compensated by system of power compensation. Thus, the torquemeter covers the whole range of frequencies interesting for the consumer. The block diagram of the torquemeter, its frequency characteristic and conditions of setup of supports with quasi-zero torsional rigidity are shown
  • Keywords
    accelerometers; aerospace instrumentation; angular measurement; attitude control; compensation; space vehicles; torquemeters; transfer functions; accelerometer signal; angular acceleration; bearing manufacturing errors; central moments of inertia; dynamical rotor unbalance; elastic three-tape supports; finite shaft rigidity; frequency characteristic; gyrodyne sites; high-frequency component; multimass elastic system; noise; orientation system; power compensation system; quasi-zero torsional rigidity; space vehicle; torquemeter; transfer function; vibration; Accelerometers; Electric motors; Frequency measurement; Manufacturing; Passband; Power measurement; Rotors; Shafts; Space vehicles; Torque measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Science and Technology, 2001. KORUS '01. Proceedings. The Fifth Russian-Korean International Symposium on
  • Conference_Location
    Tomsk
  • Print_ISBN
    0-7803-7008-2
  • Type

    conf

  • DOI
    10.1109/KORUS.2001.975049
  • Filename
    975049