Blade braking load stop

Details Blade braking load stop Blade braking load stop

B - Operations, Transporting

64

C

244/15, 202/6

B64C 27/37 (2006.01) B64C 27/32 (2006.01) B64C 27/35 (2006.01)

Patent

CA 1117091

ELASTOMERIC ROTOR LOAD REACTION SYSTEM ABSTRACT OF THE DISCLOSURE In a helicopter rotor in which the blades are supported for rotation and articulation from the hub by elastomeric bearings and including a lead-lag damper which acts to cause radially inward blade motion during rotor braking and including the improvement of utilizing members which move pivotally in response to centrifugal force and which serve blade flapping and droop stop functions both statically and dynamically and which further are programmed as a function of rotor speed to prevent or limit radial inward motion of the blade during the rotor braking operation. S-3044

326993

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