Abstract: The disclosure relates to an assembly for an aircraft turbomachine, having a speed reduction gear comprising an input pinion connected to a power shaft of the turbomachine and an output pinion connected to a propeller shaft of the turbomachine. According to the disclosure, the assembly includes two electric machines which are each configured to provide electrical power to the propeller shaft or to draw mechanical power from the propeller shaft, each electric machine comprising a rotor and a stator, the stator configured to be connected to a casing of the turbomachine. The speed reduction gear can include two substantially parallel intermediate transmission lines configured to transmit the torque from the input pinion to the output pinion, each rotor being driven in rotation respectively by a pinion of an intermediate line.

Abstract: A turbomachine includes a fan, a first casing with longitudinal axis X in which a motor shaft is rotated around the longitudinal axis X, a second casing surrounding and coaxial with the first casing, and a drive shaft connected to the motor shaft. The driveshaft is also connected to at least two electric machines via a power transmission angle gear device housed in a housing. The electric machines being intended are configured to take or inject power on the motor shaft. The housing has a coupling surface to which the two electric machines are coupled.

Abstract: An aircraft turbomachine includes a speed reduction gear having an input pinion connected to a power shaft and an output pinion connected to a propeller shaft. An electric machine is integrated into the speed reduction gear and is configured to provide electrical power to the propeller shaft or to take mechanical power from the propeller shaft. The electric machine has a rotor driven in rotation about an axis coaxial with a longitudinal axis of the turbomachine and a stator connected to a casing. The input pinion includes an input shaft offset from an axis of the output pinion, and the speed reduction gear has two parallel intermediate transmission lines configured to transmit the torque from the input pinion to the output pinion to drive the rotor in rotation.

Abstract: The disclosure relates to an assembly for an aircraft turbomachine, having a speed reduction gear comprising an input pinion connected to a power shaft of the turbomachine and an output pinion connected to a propeller shaft of the turbomachine. According to the disclosure, the assembly includes two electric machines which are each configured to provide electrical power to the propeller shaft or to draw mechanical power from the propeller shaft, each electric machine comprising a rotor and a stator, the stator configured to be connected to a casing of the turbomachine. The speed reduction gear can include two substantially parallel intermediate transmission lines configured to transmit the torque from the input pinion to the output pinion, each rotor being driven in rotation respectively by a pinion of an intermediate line.

Abstract: The implant (12) according to the invention comprises a tubular frame (16), a plurality of distal arms (18) capable of pressing on a first face of a tissue, and a plurality of proximal arms (20) having an end (62) connected to the frame and a free end (64) intended to press on a second face of the tissue to clamp the tissue. The implant comprises a first integral assembly including a first part (38) of the frame and the proximal arms (20), and a second integral assembly including a second part of the frame (40) and the distal arms (18), the first assembly and the second assembly being attached one on top of the other. The first part (38) of the frame is in the form of a proximal sleeve, extending longitudinally between a proximal end (41) and a distal end (43) of the sleeve. The connected end (62) of each proximal arm (20) is connected to the distal end (43) of the proximal sleeve (38), and the free end (64) of each proximal arm (20) extends beyond that distal end (43) of the proximal sleeve (38).

Abstract: The implant (12) according to the invention comprises a tubular frame (16), a plurality of distal arms (18) capable of pressing on a first face of a tissue, and a plurality of proximal arms (20) having an end (62) connected to the frame and a free end (64) intended to press on a second face of the tissue to clamp the tissue. The implant comprises a first integral assembly including a first part (38) of the frame and the proximal arms (20), and a second integral assembly including a second part of the frame (40) and the distal arms (18), the first assembly and the second assembly being attached one on top of the other. The first part (38) of the frame is in the form of a proximal sleeve, extending longitudinally between a proximal end (41) and a distal end (43) of the sleeve. The connected end (62) of each proximal arm (20) is connected to the distal end (43) of the proximal sleeve (38), and the free end (64) of each proximal arm (20) extends beyond that distal end (43) of the proximal sleeve (38).

Abstract: Rare earth glass-polishing compositions of improved homogeneity and reproducibility are prepared by (a) simultaneously continuously admixing a cerium salt solution, a basic solution and a solution of at least one acid and/or one salt, the anion or anions of which being adopted to form insoluble rare earth compounds, the number of equivalents of base being equal to or greater than the number of equivalents of cerium, and the pH of the reaction medium being greater than about 6; (b) filtering the precipitate which results from the reaction medium; (c) drying said recovered precipitate; and (d) calcining said dried precipitate.

Abstract: Cerium based glass polishing compositions, well adapted for the polishing, e.g., of optical glass, are comprised of (i) at least one crystalline phase of CeO.sub.2 type, and (ii) a crystalline phase which comprises a rare earth pyrosilicate having the formula Ln.sub.2-x Ce.sub.x Si.sub.2 O.sub.7, wherein Ln is at least one lanthanide or yttrium and x is a number ranging from zero to less than 2.

Abstract: Rare earth glass-polishing compositions of improved homogeneity and reproducibility are prepared by (a) simultaneously continuously admixing a cerium salt solution, a basic solution and a solution of at least one acid and/or one salt, the anion or anions of which being adopted to form insoluble rare earth compounds, the number of equivalents of base being equal to or greater than the number of equivalents of cerium, and the pH of the reaction medium being greater than about 6; (b) filtering the precipitate which reuslts from the reaction medium; (c) drying said recovered precipitate; and (d) calcining said dried precipitate.