EPICYCLIC GEAR SYSTEM HAVING TWO ARRAYS OF PINIONS MOUNTED ON FLEXPINS WITH COMPENSATION FOR CARRIER DISTORTION

An epicyclic gear system (A) includes sun and ring gears (2, 4) and planet pinions (6, 8) arranged in two side-by-side arrays (a, b) between the sun and ring gears, there also being a carrier (10, 50) to which planet pinions are coupled through flexpins (30). The carrier has primary and secondary walls (20, 22) between which the pinions are located and webs (24) connecting the walls. The flexpins for one array of pinions are cantilevered from the primary wall and the flexpins for the other array of pinions are cantilevered from the secondary wall. When the gear system operates, the carrier along its primary wall is subjected to an externally applied torque which transfers through the system at the planet pinions of the two arrays. The load path (pa) for the pinions at the primary wall is shorter than the load path (pb) for the pinions at the secondary wall, and this disparity causes the carrier to distort. To compensate for this distortion so that the pinions of the two arrays will mesh more evenly with the sun and ring gears, the flexpins of the first array are offset angularly with respect to the flexpins of the second array, or the teeth of the pinions in the first array are narrower than the teeth of the pinions of the second array, or the primary wall of the carrier has areas (40, 44) of weakness where the flexpins of the first array are cantilevered from it, or the flexpins of the first array are more flexible than the flexpins of the second array. As a consequence, the pinions of the two arrays mesh better under load with the sun and ring gears and share the transfer of torque more evenly. L'invention concerne un train épicycloïdal (A) d'engrenages comprenant un planétaire et une couronne (2, 4) ainsi que des satellites (6, 8) disposés en deux rangées côte à côte (a, b) entre le planétaire et la couronne, et comprenant également un porte-satellites (10, 50) auquel les satellites sont couplés par l'intermédiaire d'axes flexibles (30). Le porte-satellites est doté de parois primaire et secondaire (20, 22) entre lesquelles sont situés les satellites et de toiles (24) reliant lesdites parois. Les axes flexibles d'une rangée de satellites s'étendent de façon autoporteuse à partir de la paroi primaire et les axes flexibles de l'autre rangée de satellites s'étendent de façon autoporteuse à partir de la paroi secondaire. Lorsque le train d'engrenages est en fonctionnement, le porte-satellites est soumis, le long de sa paroi primaire, à un couple appliqué de