Device for driving a generator of an aircraft turbomachine and method for regulating the speed of such a generator
AssigneeSafran Aircraft Engines
InventorHuguette De Wergifosse
Life of this patent
Estimating the term…
Abstract
A device for driving an integrated generator from an accessories relay box of a turbomachine. The device includes first and second electric motors arranged to transfer electric power from one to the other, one or more controllers configured for controlling said electric motors, and an epicyclic reduction gear train. The gear train includes a first element intended to be coupled to the accessories relay box, a second element intended to be coupled to the generator, and a third element driven to rotate by said first electric motor. The control means are configured to modify the speed of rotation of the third element in such a way that the second element is driven to rotate at a constant speed.
Claims10
A driving device for driving an input shaft of an integrated generator of an aircraft turbomachine from an output shaft of an accessory gear box of the turbomachine, the driving device comprising:
- first and second electric motors each being a motor/generator;
- control means configured to control said first and second electric motors, said first and second electric motors being arranged to transfer electrical power from one to the other;
- and
- an epicyclic reduction gear train comprising three elements:
- a central planetary gear,
- an external ring gear, and
- a planet carrier,
- wherein said planet carrier carries planet gears which mesh with said central planetary gear and said external ring gear,
- wherein said three elements are rotatable about an axis of the epicyclic reduction gear train, a first one of said three elements being coupled to the output shaft of the accessory gear box, a second one of said three elements being coupled to the input shaft of the integrated generator, and a third one of said three elements being suitable to be driven in rotation by said first electric motor,
- and wherein said control means are configured to change a rotational speed of the third one of said three elements so that the second one of said three elements is driven in rotation at a constant speed.
A device for driving an input shaft of an integrated generator of an aircraft turbomachine from an output shaft of an accessory gear box of the turbomachine, the driving device comprising:
- first and second electric motors each being a motor/generator, the first and second electric motors being arranged to transfer electrical power from one to the other;
- and
- an epicyclic reduction gear train comprising three elements:
- a central planetary gear,
- an external ring gear, and
- a planet carrier
- wherein said planet carrier carries planet gears which mesh with said central planetary gear and said external ring gear,
- wherein said three elements being rotatable about an axis of the epicyclic reduction gear train, a first one of said three elements being coupled to the output shaft of the accessory gear box, a second one of said three elements coupled to the input shaft of the integrated generator, and a third one of said three elements being driven in rotation by said first electric motor,
- wherein the first and/or second motor is controllable to change a rotational speed of the third of said three elements so that the second of said three elements is driven in rotation at a constant speed.
Dependencies are inferred from the claim text.