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A rotor blade retention system connects an elongated rotor blade to a rotor hub that is rotatable about its central axis. The connected rotor blade normally extends generally radially from the hub and is rotatable with the hub. The retention system includes a pair of bearings that are interconnected

A rotor blade retention system connects an elongated rotor blade to a rotor hub that is rotatable about its central axis. The connected rotor blade normally extends generally radially from the hub and is rotatable with the hub. The retention system includes a pair of bearings that are interconnected in parallel load transmitting relationship. Both bearings are connected in serial load transmitting relationship with a flap hinge. One bearing is relatively stiff along the longitudinal axis of the rotor blade and is less stiff in directions transverse to the longitudinal blade axis. The other bearing is most stiff in directions transverse to the rotor blade axis and is less stiff along the axis. Both bearings define effective elastic centers which are located along the longitudinal blade axis, but the two elastic centers are spaced from each other. The two bearings accommodate lead-lag motions of the rotor blade. Because of the relative stiffnesses of the bearings in directions transverse to the longitudinal axis of the rotor blade, the axis about which lead-lag motion occurs is displaced from the effective elastic center of the bearing that has its greatest stiffness along the longitudinal blade axis. The displacement of the lead-lag axis causes the bearing, and the retention system, to appear relatively stiff in response to lead-lag motions. The stiffness of the blade retention system in response to flapping motions of the rotor blade is not affected, however, because the serially connected flap hinge accommodates most of the flapping motion in preference to the bearings. Since the retention system is relatively stiff in response to lead-lag motions, less damping is required at the natural frequencies of lead-lag motion. The required damping may be provided entirely by material incorporated into the bearings and without the use of an auxiliary lead-lag damper.

대표청구항 ▼

A rotor blade retention system for connecting at least one elongated rotor blade to a rotor hub that is rotatable about a central axis, the connected rotor blade normally extending generally radially from the hub and being rotatable with the hub about its central axis, said retention system comprisi

A rotor blade retention system for connecting at least one elongated rotor blade to a rotor hub that is rotatable about a central axis, the connected rotor blade normally extending generally radially from the hub and being rotatable with the hub about its central axis, said retention system comprising: (a) first bearing means disposed between the rotor blade and the rotor hub, the first bearing means having an axis of greatest stiffness along a longitudinal axis of the rotor blade and having axes of lesser stiffnesses transverse to the longitudinal axis of the rotor blade, the first bearing means defining a first effective elastic center on the longitudinal axis of the rotor blade and restraining the rotor blade against centrifugal forces imposed on the blade during rotation of the blade with the rotor hub; (b) second bearing means disposed beteen the rotor blade and the rotor hub and connected with the first bearing means in parallel load transmitting relationship at least with respect to said centrifugal forces imposed on the rotor blade, the second bearing means having axes of greatest stiffness transverse to the longitudinal axis of the rotor blade and an axis of lesser stiffness coincident with the axis of greatest stiffness of the first bearing means and the longitudinal axis of the rotor blade, the second bearing means defining a second effective elastic center which is located on the longitudinal axis of the rotor blade and which at all times is spaced from the first effective elastic center of the first bearing means; (c) hinge means for permitting and deflecting in response to flapping motions of the rotor blade about a flapping axis which is oriented transverse to the longitudinal axis of the rotor blade and more nearly perpendicular than parallel to the central axis of the rotor hub, the hinge means being disposed between the rotor hub and the first and second bearing means and being connected to the rotor hub and to the first and second bearing means; (d) first substantially inflexible means for rigidly interconnecting the first and second bearing means and for rigidly connecting said first and second bearing means to the rotor blade; and (e) second substantially inflexible means for rigidly interconnecting the first and second bearing means, the first and second interconnecting means cooperating to mount the bearing means in parallel load transmitting relationship, the second interconnecting means also connecting said first and second bearing means to the hinge means in serial load transmitting relationship so that the hinge means acts in series with the first bearing means to restrain the rotor blade against centrifugal forces imposed on the blade, the stiffness of the hinge means in response to flapping motions of the rotor blade about said flapping axis being in comparison to corresponding stiffnesses of the first and second bearing means such that the hinge means accommodates a majority of the flapping motion of the rotor blade, the relative stiffnesses of the first and second bearing means in directions transverse to the longitudinal axis of the rotor blade being such that a lead-lag axis which is oriented transverse to the longitudinal axis of the rotor blade and more nearly parallel than perpendicular to the central axis of the rotor hub and about which oscillatory lead-lag motions of the rotor blade occur is located closer to the Second elastic center than to the first elastic center within an area longitudinally bounded by and including the first and second elastic centers, the blade retention system being constructed so as to cause the natural frequency of oscillation of the rotor blade about the lead-lag axis to be less than the normal operating speed of rotation of the rotor blade and hub.