Free turbine turbogenerator comprising a reversible electrical machine coupled to the free turbine

Patent metadata

Field	Value
Publication number	US-12467378-B2
Application number	US-202118251031-A
Country	US
Kind code	B2
Filing date	Oct 25, 2021
Priority date	Oct 29, 2020
Publication date	Nov 11, 2025
Grant date	Nov 11, 2025

Abstract

Disclosed is a turbogenerator, in particular for an electrically-driven rotary wing aircraft, comprising a gas generator equipped with a first shaft, at least one reversible electrical machine, and a free turbine provided with a second shaft and caused to rotate by a gas flow generated by the gas generator. The second shaft is coupled to the at least one electrical machine during all phases of operation of the turbomachine, and the turbomachine further comprises a single mechanical coupling means for coupling the first mechanical shaft to the second mechanical shaft when the electrical machine is operating in motor mode and mechanically uncoupling the first mechanical shaft from the second mechanical shaft when the electrical machine is operating in generator mode.

First claim

The invention claimed is:

1 . A turbomachine of a free turbine turbogenerator type, comprising a gas generator equipped with a first mechanical shaft, at least one reversible electrical machine and a free turbine provided with a second mechanical shaft and caused to rotate by a gas flow generated by the gas generator,
wherein said second mechanical shaft is mechanically connected to said at least one reversible electrical machine and the free turbine during all phases of operation of the turbomachine, and the turbomachine further comprises a single mechanical coupling means configured to mechanically couple said first mechanical shaft to said second mechanical shaft when said at least one reversible electrical machine is operating in motor mode and mechanically uncoupling said first mechanical shaft from said second mechanical shaft when said at least one reversible electrical machine is operating in generator mode, said at least one reversible electrical machine configured to drive the gas generator and the free turbine during start-up of the turbomachine, wherein said single mechanical coupling means comprises a free wheel and at least one intermediate pinion mounted between the free wheel and the first mechanical shaft, and wherein the at least one intermediate pinion includes a first wheel and a second wheel mounted between the first mechanical shaft and the free wheel, wherein a control unit of said at least one reversible electrical machine is configured to: measure a torque exerted by the second mechanical shaft on an output of the free wheel mechanically connected to the first mechanical shaft; determine the measured torque is less than a torque threshold; determine the gas generator is autonomous when the measured torque is less than the torque threshold; and place the at least one reversible electrical machine in the generator mode upon determining the gas generator is autonomous.

2 . The turbomachine according to claim 1 , in which the control unit of said at least one reversible electrical machine being configured to place said at least one reversible electrical machine in said motor mode during the start-up of the turbomachine, and to place said at least one reversible electrical machine in said generator mode when the gas generator becomes autonomous.

3 . The turbomachine according to claim 2 , in which the control unit of said at least one reversible electrical machine is configured to detect that the gas generator is autonomous when a speed of the first mechanical shaft exceeds a start-up phase output-speed threshold.

4 . The turbomachine according to claim 1 , in which the free wheel is configured so that the first mechanical shaft, when it is mechanically uncoupled from the second mechanical shaft, turns at a speed greater than a speed of rotation of the second mechanical shaft.

5 . The turbomachine according to claim 4 , further comprising the at least one intermediate pinion having a gear ratio different from one, said at least one intermediate pinion being mounted between the free wheel and second mechanical shaft and/or between the free wheel and the first mechanical shaft.

6 . The turbomachine according to claim 2 , wherein the free wheel is configured so that the first mechanical shaft, when it is mechanically uncoupled from the second mechanical shaft, turns at a speed greater than a speed of rotation of the second mechanical shaft, and in which the control unit of said at least one reversible electrical machine is configured to detect that the gas generator is autonomous when the torque exerted by said second mechanical shaft of the free turbine on the output of the free wheel exceeds the torque threshold.

7 . The turbomachine according to claim 2 , wherein the free wheel is configured so that the first mechanical shaft, when it is mechanically uncoupled from the second mechanical shaft, turns at a speed greater than a speed of rotation of the second mechanical shaft, and in which the control unit of said at least one reversible electrical machine is configured to detect that the gas generator is autonomous when an input and the output of the free wheel starts to rotate at different speeds.

8 . The turbomachine according to claim 1 , further comprising an accessories box mechanically coupled to the first mechanical shaft and to which items of equipment are mechanically coupled.

9 . The turbomachine according to claim 8 , in which said at least one reversible electrical machine comprises a single reversible electrical machine, said single reversible electrical machine being driven directly by the second mechanical shaft of the free turbine.

10 . The turbomachine according to claim 9 , in which said single reversible electrical machine has a nominal speed of rotation equal to or close to that of the free turbine.

11 . A turbomachine of a free turbine turbogenerator type, comprising a gas generator equipped with a first mechanical shaft, at least one reversible electrical machine and a free turbine provided with a second mechanical shaft and caused to rotate by a gas flow generated by the gas generator,
wherein said second mechanical shaft is mechanically connected to said at least one reversible electrical machine and the free turbine during all phases of operation of the turbomachine, and the turbomachine further comprises a single mechanical coupling means configured to mechanically couple said first mechanical shaft to said second mechanical shaft when said at least one reversible electrical machine is operating in motor mode and mechanically uncoupling said first mechanical shaft from said second mechanical shaft when said at least one reversible electrical machine is operating in generator mode, wherein said single mechanical coupling means comprises a free wheel configured to couple the first mechanical shaft and second mechanical shaft, wherein a control unit of said at least one reversible electrical machine is configured to: measure a torque exerted by the second mechanical shaft on an output of the free wheel mechanically connected to the first mechanical shaft; determine the measured torque is less than a torque threshold; determine the gas generator is autonomous when the measured torque is less than the torque threshold; and place the at least one reversible electrical machine in the generator mode upon determining the gas generator is autonomous.

12 . The turbomachine according to claim 11 , in which the control unit of said at least one reversible electrical machine being configured to place said at least one reversible electrical machine in said motor mode during the start-up of the turbomachine, and to place said at least one reversible electrical machine in said generator mode when the gas generator becomes autonomous.

13 . The turbomachine according to claim 12 , in which the control unit of said at least one reversible electrical machine is configured to detect that the gas generator is autonomous when a speed of the first mechanical shaft exceeds a start-up phase output-speed threshold.

14 . The turbomachine according to claim 11 , in which the free wheel is configured so that the first mechanical shaft, when it is mechanically uncoupled from the second mechanical shaft, turns at a speed greater than a speed of rotation of the second mechanical shaft.

15 . The turbomachine according to claim 14 , wherein the single mechanical coupling means comprises at least one intermediate pinion, the at least one intermediate pinion having a gear ratio different from one, said at least one intermediate pinion being mounted between the free wheel and secon

Assignees

• Safran Helicopter Engines

Inventors

• Vive Loïs Pierre Denis
• Drouin Thomas
• Bedrine Olivier

Classifications

• F02C3/10

  with another turbine driving an output shaft but not driving the compressor · 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

• F05D2220/76

  an electrical generator · CPC title

• F05D2220/323

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

• B64D41/00

  Power installations for auxiliary purposes · CPC title