TURBOMACHINE DRIVE ARRANGEMENT
An example arrangement for driving a turbomachine includes an input shaft that is configured to rotate a rotor of the turbomachine through a hydraulic log and gear differential rotatable coupled to the input shaft. A motor-generator is rotatably coupled to the differential. The motor-generator has a motor mode of operation and a generator mode of operation. The motor-generator is configured to drive the input shaft through the hydraulic log and differential when the motor-generator is in the motor mode of operation. The input shaft is configured to drive the motor-generator through the hydraulic log and differential when the motor-generator is in the generator mode of operation.
1 ) An arrangement for driving a turbomachine, comprising:
an input shaft that is configured to rotate a turbomachine rotor;
a hydraulic log assembly rotatably coupled to the input shaft; and
a motor-generator rotatably coupled to the hydraulic log assembly, the motor-generator having a motor mode of operation and a generator mode of operation, wherein the motor-generator is configured to drive the input shaft through the hydraulic log assembly when the motor-generator is in the motor mode of operation, and the input shaft is configured to drive the motor-generator through the hydraulic log assembly when the motor-generator is in the generator mode of operation.
2 ) The arrangement of claim 1 , wherein the hydraulic log assembly is configured to adjust the rotational input from the motor-generator to drive the input shaft when the motor-generator is in the motor mode of operation.
3 ) The arrangement of claim 1 , wherein the hydraulic log assembly is configured to adjust the rotational input from the input shaft to provide a rotational output that drives the motor-generator when the motor-generator is in the generator mode of operation.
4 ) The arrangement of claim 1 , including a first plurality of pistons and a second plurality of pistons within the hydraulic log assembly, wherein a stroke of the first plurality of pistons is configured to be adjusted with a first wobbler plate and a stroke of the second plurality of pistons is configured to be adjusted with a second wobbler plate.
5 ) The arrangement of claim 4 , wherein the first wobbler plate selectively adjusts the stroke of the first plurality of pistons to provide a rotational output from the hydraulic log assembly that is different than a rotational input to the hydraulic log provided by the motor-generator.
6 ) The arrangement of claim 4 , wherein the second wobbler plate selectively adjusts the stroke of the second plurality of pistons to provide a rotational output from the hydraulic log that is different than a rotational input to the hydraulic log provided by the input shaft.
7 ) The arrangement of claim 1 , wherein the hydraulic log assembly comprises a differential.
8 ) A gas turbine engine arrangement, comprising:
a motor-generator;
a compressor rotor; and
a hydraulic log configured to adjust a rotational input from one of the motor-generator or the compressor rotor, and to provide a rotational output to the other of the motor-generator or the compressor rotor.
9 ) The gas turbine engine of claim 8 , wherein the hydraulic log comprises a first plurality of pistons and a second plurality of pistons, the first plurality of pistons configured to selectively adjust a rotation input from one of the motor-generator or the compressor rotor, and the second plurality of pistons configured to selectively adjust a rotational input from the other of the motor-generator or the compressor rotor.
10 ) The gas turbine engine of claim 9 , including a first wobbler plate configured to adjust the first plurality of pistons and a second wobbler plate configured to adjust the second plurality of pistons.
11 ) The gas turbine engine of claim 10 , including control piston assemblies configured to adjust the position of the first and second wobbler plates.
12 ) The gas turbine engine of claim 11 , wherein the control piston assemblies are controlled by hydraulic pressure and spring biasing.
13 ) The gas turbine engine of claim 12 , including a controller configured to adjust the hydraulic pressure biasing of the control piston assemblies.
14 ) The gas turbine engine of claim 8 , wherein the motor-generator is configured to provide a first rotational input to the hydraulic log, and the hydraulic log is configured to adjust the first rotational input to provide a second rotational input to the compressor rotor.
15 ) The gas turbine engine of claim 12 , wherein the compressor rotor is configured to be driven by the rotational input provided by the hydraulic log until the engine reaches self-sustaining operation.
16 ) A method of driving components within a turbomachine, comprising:
providing a first rotational input to a hydraulic log using a motor-generator when the motor-generator is in a motor mode of operation;
adjusting the first rotational input to provide a second rotational input that drives a compressor rotor;
providing a third rotational input to the hydraulic log using the compressor rotor when the motor-generator is in a generator mode of operation; and
adjusting the third rotational input and to provide a fourth rotational input that drives the motor-generator.
17 ) The method of claim 16 , including using a hydraulic log to perform the adjusting.
18 ) The method of claim 17 , wherein the hydraulic log comprises more than one wobbler plate.
19 ) The method of claim 17 , wherein the hydraulic log comprises a first plurality of pistons adjusted by a first wobbler plate and a second plurality of pistons adjusted by a second wobbler plate.
20 ) The method of claim 17 , including spring-biasing at least one of the first wobbler plate or the second wobbler plate.
21 ) The method of claim 19 , wherein the adjusting comprises tilting at least one of the first wobbler plate and the second wobbler plate relative a rotational axis of the hydraulic log.