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| | Hub for rotor head of rotary-wing aircraft and rotor head with such hub - US Patent 6200097 (Site not responding. Last check: 2007-10-20) |
 | | Hence, with such a known hub, in the production of the rotor head, it is necessary to integrate each spherical stop of a rigid loop with the associated blade, then to insert the stops, thus integrated with their blades, through said apertures into said cage and, finally, to fix the stops to the hub. |
 | | In order to fix and articulate each blade on the hub, laminated spherical stops 8 of a known type are provided, the centre of rotation 11 of which lies on the axis L--L of the corresponding blade, these spherical stops serving as the sole articulation in flapping, in drag and in pitch. |
 | | Moreover, the flapping-pitch coupling of the invention improves the behaviour of the aircraft from the point of view of stability and of entry into autorotation and the inclination of the pitch rods, by virtue of the pitch-drag coupling, affords favourable aerodynamic damping from the point of view of ground-air resonance. |
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