Helicopter rotor lead-lag damper

Details Helicopter rotor lead-lag damper Helicopter rotor lead-lag damper

B - Operations, Transporting

64

C

244/15

B64C 27/35 (2006.01) B64C 27/51 (2006.01)

Patent

CA 1078354

IMPROVED HELICOPTER ROTOR LEAD LAG DAMPER ABSTRACT OF THE DISCLOSURE A helicopter rotor lead-lag hydraulic fluid damper has an internal anti-torque shaft preventing rotary motion of the dynamic fluid retaining seal. An independent fluid reservoir under centrifugal force supplies lubrication to the low-pressure side of the seal. At rest, the fluid returns to the lower reservoir chamber by gravity.

281544

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