This paper provides an overview of current vibration methods used to identify the health of helicopter transmission gears. The gears are critical to the transmission system that provides propulsion, lift and maneuvering of the helicopter. This paper reviews techniques used to process vibration data to calculate conditions indicators (CI's), guidelines used by the government aviation authorities in developing and certifying the Health and Usage Monitoring System (HUMS), condition and health indicators used in commercial HUMS, and different methods used to set thresholds to detect damage. Initial assessment of a method to set thresholds for vibration based condition indicators applied to flight and test rig data by evaluating differences in distributions between comparable transmissions are also discussed. Gear condition indicator FM4 values are compared on an OH58 helicopter during 14 maneuvers and an OH58 transmission test stand during crack propagation tests. Preliminary results show the distributions between healthy helicopter and rig data are comparable and distributions between healthy and damaged gears show significant differences.


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    Title :

    Investigation of Current Methods to Identify Helicopter Gear Health


    Contributors:


    Publication date :

    2007-03-01


    Size :

    944915 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Investigation of Current Methods to Identify Helicopter Gear Health

    Dempsey, Paula J. / Lewicki, David G. / Le, Dy D. | NTRS | 2007


    Investigation of Current Methods to Identify Helicopter Gear Health

    Dempsey, Paula J. / Lewicki, David G. / Le, Dy D. | NTRS | 2007


    Investigation of Current Methods to Identify Helicopter Gear Health

    P. J. Dempsey / D. G. Lewicki / D. D. Le | NTIS | 2007


    Investigation of Current Methods to Identify Helicopter Gear Health

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