• DocumentCode
    1890901
  • Title

    The Calibration Technical Investigation on Helicopter Rotor Standard Blade

  • Author

    Liang Yun ; Liang Tingwei ; Jiao Jian

  • Author_Institution
    Hong Kong Polytech. Univ., Kowloon, China
  • fYear
    2013
  • fDate
    16-17 Jan. 2013
  • Firstpage
    1153
  • Lastpage
    1156
  • Abstract
    The rotor system is the most important part for helicopter, the helicopter flight quality depends tightly on the rotor blade. The parameters of primary standard rotor bland had been identified by analyzing its parameters systematically basing on dynamic balance test. A new method is proposed to calibrate the parameters of primary standard rotor blade with designing series of calibration equipments. Some of verification test and simulation results indicate that the method is valid, the uncertainty of measurement accord with the technical requirements. It can solve the calibration problem of standard rotor blade, finish the metrological transfer process, and maintain the consistency and stability of helicopter rotor blades.
  • Keywords
    blades; calibration; dynamic testing; helicopters; rotors; stability; calibration equipment; calibration technical investigation; dynamic balance test; helicopter flight quality; helicopter rotor blade stability; helicopter rotor standard blade; metrological transfer process; rotor bland; verification testing; Aerodynamics; Blades; Calibration; Helicopters; Position measurement; Rotors; Standards; Dynamic Balance Test; Flapping Measurement and Calibration; Rotor Flapping;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Measuring Technology and Mechatronics Automation (ICMTMA), 2013 Fifth International Conference on
  • Conference_Location
    Hong Kong
  • Print_ISBN
    978-1-4673-5652-7
  • Type

    conf

  • DOI
    10.1109/ICMTMA.2013.282
  • Filename
    6493935