Rotor Track and Balance Improvements

##plugins.themes.bootstrap3.article.main##

##plugins.themes.bootstrap3.article.sidebar##

Published Oct 14, 2013
Eric Bechhoefer Austin Fang Ephrahim Garcia

Abstract

Vibration derived from the main rotor dynamics and imbalance causes premature wear to the aircraft components, and can cause pilot fatigue. While improvements have been made in rotor track and balance (RTB) techniques; there is room to enhance the quality of the recommended RTB adjustments.

One aspect that limits the development of RTB algorithms is the difficulty in quantifying the performance of new algorithms. This is because there are limited data sets to work on, and no agreed upon metrics on which to measure RTB performance.This paper develops a methodology to simulate the vibration due to injecting a fault into the rotor system, and demonstrates metrics to evaluate the performance of a RTB algorithm. A new Bayes RTB method is evaluated against a standard least squares technique. In addition, a technique is presented to automate the selection of active adjustments.

How to Cite

Bechhoefer, E. ., Fang, A. ., & Garcia, E. . (2013). Rotor Track and Balance Improvements. Annual Conference of the PHM Society, 5(1). https://doi.org/10.36001/phmconf.2013.v5i1.2216
Abstract 487 | PDF Downloads 426

##plugins.themes.bootstrap3.article.details##

Keywords

rotor track and balance, reducing helicopter vibration, track

References
Veca, A., (1973). Vibration Effects on Helicopter Reliability and Maintainability. U.S. Army Air Mobility Research and Development Laboratory Technical Report 73-11.
Rosen, A., Ben-Ari, R., (1997). Mathematical Modeling of Helicopter Rotor Track and Balance: Theory, Journal of Sound and Vibration, vol. 200, No. 5.
Ferrer, E., Aubourg, P., Krysinksi, T., Bellizzi S. (2001). New Methods for Rotor Tracking and Balance Tuning and Defect Detection Applied to Eurocopter Products, American Helicopter Society International, Forum 57.
Dimarco, W., Floyd, M., Hayden, R., Ventres, C., (1990) “Method and Apparatus for Reducing Vibration over the Full Operating Range of Rotor and a Host Device” US Patent 4937758/
FAA, (2008), Certification of Transport Category Rotorcraft, AC-29-2C.
Bechhoefer, E., Fang, A., and Van Ness, D., (2011). Improved Rotor Track and Balance Performance, American Helicopter Society, Annual Forum 67.
Ventres, S., Hayden, R., (2000) “Rotor Tuning Using Vibration Data Only” American Helicoper Society Annual Forum, Virginia Beach.
Fukunaga, K., (1990). Introduction to Statistical Pattern Recognition. Academic Press, San Diego.
Renzi, M., (2004). An Assessment of Modern Methods for Rotor Track and Balance. Air Force Institute of Technology, Wright-Patterson Air Force Base.
Keller, J., Brower, G., (2007). Coefficient Development for Linear Rotor Smoothing on the MH-6 Main Rotor. http://www.rmc98.com/Coefficient%20Development% 20for%20Linear%20Rotor%20Smoothing%20on%20th e%20MH-6%20Main%20Rotor.pdf
Wackerly, D., Mendenhall, W., and Scheaffer, R., (1996) Mathematical Statistics with Applications, Duxbury Press, Belmont. Pg. 451-453.
Section
Technical Research Papers

Most read articles by the same author(s)

<< < 1 2 3 > >>