Blade retention system

Details Blade retention system Blade retention system

B - Operations, Transporting

64

C

244/15

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

Patent

CA 1158622

ABSTRACT OF THE DISCLOSURE A blade retention system for use in a fully articulated rotor head of a rotary wing aircraft is described. The retention system comprises a separate elastomeric bearing means for carrying loads in com- pression and accommodating motions about the respective flapping, lead-lag, and pitching axes of the rotor head in shear for each type of motion about the respective flapping, lead-lag and pitching axes of the rotor head.

371176

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