Improved Rotor Smoothing for the U.S. Army CH-47D

SM_2008_CBM-3141

2/12/2008

Authors
Abstract
Content

Rotor smoothing for U.S. Army rotorcraft must provide both a time efficient and cost effective means for reducing once-per-revolution vibrations. Through anecdotal experience, rotor smoothing systems have proven to be relatively efficient for both UH-60 and AH-64 rotorcraft; however, these same systems have not been as efficient for the CH-47. Improving the rotor smoothing coefficients for the CH-47 will reduce both the time and cost needed to bring the rotorcraft to an appropriate performance level. This paper outlines the effort for improving the rotor smoothing process for the CH-47.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_2008_CBM-3141
Citation
Hasty, J., Krick, S., and Keller, J., "Improved Rotor Smoothing for the U.S. Army CH-47D," AHS International CBM Specialists Meeting, Huntsville, Alabama 2008, Huntsville, Alabama, February 12, 2008, https://doi.org/10.4050/SM_2008_CBM-3141.
Additional Details
Publisher
Published
2/12/2008
Product Code
SM_2008_CBM-3141
Content Type
Technical Paper
Language
English