Patent ID: 9388862
Filing Date: 2016-07-12
CPC Classification: B64C,F16D,Y10S

Claim Text:
1. A constant velocity universal joint apparatus for connecting a rotor hub of a multi-bladed helicopter with a drive shaft, the rotor hub tiltable in two directions of freedom with respect to the drive shaft about a flapping axis and a feathering axis of the blades, the blades being fixed to the rotor hub, the constant velocity universal joint apparatus comprising: an internal universal ring couplable by a pair of pins to the drive shaft so as to rotate with the drive shaft; an external universal ring couplable by a pair of swivel pins so as to rotate with the rotor hub, said internal and external universal ring connected to each other by a pair of connection pins so as to allow relative motion of said external universal ring with respect to said internal universal ring substantially in quadrature with said pair of rotating pins and with said pair of swivel pins, at least one of said pair of connection pins having an extremity extending outwardly coaxial with another of said pair of connections pins; at least one bisector device having a first element and a second element, the bisector device connectable to the drive shaft and the rotor hub by a connecting rod, said first and second elements being coupled in a prismatic manner to each other, each of said first and second elements having at least one hole, the hole allowing a passing therein of the protruding extremity of the connector pin such that said first and second elements are connected in a sliding and swiveling manner on the protruding extremity of the connection pin, the bisector device maintaining an axis of the connection pin on a plane that bisects an angle between the drive shaft and the rotor hub so as to assure a constant transmission of a rotating motion between the drive shaft and the rotor hub when the rotor hub is tilted with respect to the drive shaft at an angle not equal to zero, said external universal ring comprising a first superior element and a second element each having two pairs of daps so as to form a site for permanent fitting of the respective connection pin and to form a site receiving a respective anti-friction bushing, the sites being aligned with each other, said internal universal ring having a superior element having four locations receiving an additional anti-friction bushing therein, said internal universal ring having a pair of elements each having a site for another anti-friction bushing and an additional pair of elements receiving anti-friction flanged bushings.