Device for driving a generator of an aircraft turbomachine and method for regulating the speed of such a generator

Patent metadata

Field	Value
Publication number	US-11859558-B2
Application number	US-202017619362-A
Country	US
Kind code	B2
Filing date	Jul 23, 2020
Priority date	Jul 26, 2019
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

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.

First claim

The invention claimed is:

1. 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.

2. The driving device according to claim 1 , wherein the first electric motor is a motor/generator adapted to operate without power transfer with a second motor and to be equipped with a battery.

3. The driving device according to claim 1 , wherein said first and second electric motors are asynchronous.

4. The driving device according to claim 1 , comprising at least one reversible power converter arranged between said first and second electric motors so as to transfer electrical power reversibly from one to the other.

5. The driving device according to claim 1 , wherein the first one of said three elements is the planet carrier coupled to the output shaft of the accessory gear box, the second one of said three elements is the external ring gear coupled to the integrated generator, and the third one of said three elements is the central planetary gear coupled to the first electric motor, and wherein the second one of said three elements is also coupled to said second electric motor.

6. The driving device according to claim 1 , wherein the first one of said three elements is the planet carrier coupled to the output shaft of the accessory gear box, the second one of said three elements is the external ring gear coupled to the integrated generator, and the third one of said three elements is the central planetary gear being intended to be coupled to the first electric motor, and wherein the first one of said three elements is also coupled to said second electric motor.

7. The driving device according to claim 1 , wherein the first one of said three elements is the external ring gear being coupled to the output shaft of the accessory gear box, the second one of said three elements is the central planet carrier coupled to the integrated generator, and the third one of said three elements is the central planetary gear coupled to the first electric motor, and wherein the second one of said three elements is also coupled to said second electric motor.

8. A turbomachine, comprising:
an accessory gear box having an output shaft;
an integrated generator having an input shaft; and
the driving device according to claim 1 .

9. A method for regulating a speed of an integrated generator of a turbomachine in an aircraft, the turbomachine having an accessory gear box with an output shaft, an integrated generator with an input shaft, and the driving device according to claim 1 , the method comprising a step of modifying the speed of the third of the three elements by controlling the first electric motor so that the second of said three elements is driven in rotation at a constant speed.

10. 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.

Assignees

• Safran Aircraft Engines

Inventors

• De Wergifosse Huguette

Classifications

• F02C7/32 Primary

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2220/76

  an electrical generator · CPC title

• F05D2220/766

  via a direct connection, i.e. a gearless transmission · CPC title