NASA NTRS · 19870031988
Total rotor isolation system (TRIS) flight test results
Abstract
The total rotor isolation system (TRIS) is a six-degree-of-freedom helicopter rotor vibration isolation system that has been installed on a 206LM helicopter in order to demonstrate a better-than-90-percent isolation of the fuselage from main rotor forces and moments. The results thus far obtained indicate a 95-percent suppression of vibration levels from the rotor hub to the pilot's seat, with considerable weight savings over traditional antiresonant isolation concepts.
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Halwes, D. R., Cline, J. H.. 1986-01-01. Total rotor isolation system (TRIS) flight test results. https://ntrs.nasa.gov/citations/19870031988
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