Turbomachine with an electric machine assembly and method for operation
A turbomachine and method for operating a turbomachine comprising a first rotatable component and a second rotatable component each defining a rotatable speed mechanically independent of one another, and an electric machine electrically coupled to the first rotatable component and the second rotatable component such that a load level relative to the first rotatable component and the second rotatable component is adjustable is generally provided. The method includes adjusting a first load at a first rotor assembly of the electric machine electrically coupled to the first rotatable component such that a first speed of the first rotatable component is increased or decreased based on an engine condition and the first load; adjusting a second load at a second rotor assembly of the electric machine electrically coupled to the second rotatable component such that a second speed of the second rotatable component is decreased or increased based on the engine condition and the second load; and transferring electrical energy generated from at least one of the first rotatable component or the second rotatable component.
1. A method for operating a turbomachine, the method comprising:
adjusting a first load at a first rotor assembly of an electric machine electrically coupled to a first rotatable component comprising at least a portion of a first compressor, a first turbine, or a first shaft, wherein the electric machine is electrically coupled to the first rotatable component such that a first speed of the first rotatable component is increased or decreased based on an engine condition and the first load;
adjusting a second load at a second rotor assembly of the electric machine electrically coupled to a second rotatable component comprising at least a portion of a second compressor, a second turbine, or a second shaft, and wherein the electric machine is electrically coupled to the second rotatable component such that a second speed of the second rotatable component is decreased or increased based on the engine condition and the second load; and
transferring electrical energy generated from at least one of the first rotatable component or the second rotatable component.
2. The method of claim 1 , wherein adjusting the first load level at the first rotor assembly is in inverse relationship relative to adjusting the second load level at the second rotor assembly.
3. The method of claim 1 , wherein transferring electrical energy generated from at least one of the first rotatable component or the second rotatable component includes transmitting electrical energy to one or more apparatuses electrically coupled to the turbomachine.
4. The method of claim 1 , further comprising:
rotating the second rotatable component at the second speed defining a minimum steady state second speed.
5. The method of claim 4 , further comprising:
increasing the first load level at the first rotor assembly.
6. The method of claim 5 , further comprising:
decreasing the first speed of the first rotatable component via the increased first load level.
7. The method of claim 4 , wherein rotating the second rotatable component at the second speed is based on at least one of a fuel-air ratio, a compressor exit pressure, an inter-turbine temperature, a turbine exit temperature, or an exhaust gas temperature.
8. The method of claim 1 , further comprising:
generating electrical energy via the first rotor assembly and the first rotatable component;
transmitting electrical energy from the first rotor assembly to the second rotor assembly; and
rotating the second rotatable component at the second speed based at least in part on the electrical energy from the second rotor assembly.
9. The method of claim 8 , further comprising:
decreasing a fuel flow at a combustion chamber such that rotating the second rotatable component at the second speed based at least in part on the electrical energy from the second rotor assembly results in approximately no change in the second speed.
10. The method of claim 1 , further comprising:
rotating the second rotatable component at the second speed;
generating electrical energy via the second rotor assembly and the second rotatable component;
transmitting electrical energy from the second rotor assembly to the first rotor assembly; and
rotating the first rotatable component at the first speed based at least in part on the electrical energy from the first rotor assembly.
11. The method of claim 10 , further comprising:
increasing the second load level at the second rotor assembly; and
decreasing the second speed of the second rotatable component via the increased second load level.
12. The method of claim 11 , wherein transferring energy electrical energy includes transmitting electrical energy to one or more apparatuses electrically coupled to the turbomachine.
13. The method of claim 12 , wherein decreasing the second speed of the second rotatable component is further based on one or more of a stall margin, a surge margin, an operating pressure ratio, a rotational speed.
14. A turbomachine, the turbomachine comprising:
a first rotatable component comprising one or more of a first compressor, a first turbine, or a first shaft, wherein the first rotatable component is rotatable to a first speed;
a second rotatable component comprising one or more of a second compressor, a second turbine, or a second shaft, wherein the second rotatable component is rotatable to a second speed mechanically independent of the first speed;
an electric machine assembly comprising:
a first rotor assembly disposed at the first rotatable component;
a second rotor assembly disposed at the second rotatable component; and
a stator assembly disposed between the first rotatable component and the second rotatable component; and
a controller comprising one or more processors and one or more memory devices, the one or more memory devices storing instructions that when executed by the one or more processors cause the one or more processors to perform operations, the operations comprising:
adjusting a first load at a first rotor assembly of the electric machine electrically coupled to the first rotatable component such that a first speed of the first rotatable component is increased or decreased based on an engine condition and the first load;
adjusting a second load at a second rotor assembly of the electric machine electrically coupled to the second rotatable component such that a second speed of the second rotatable component is decreased or increased based on the engine condition and the second load; and
transferring electrical energy generated from at least one of the first rotatable component or the second rotatable component.
15. The turbomachine of claim 14 , the operations further comprising:
decreasing the first speed of the first rotatable component via an increase in the first load level at the first rotor assembly.
16. The turbomachine of claim 14 , the operations further comprising:
generating electrical energy via the first rotor assembly and the first rotatable component;
transmitting electrical energy from the first rotor assembly to the second rotor assembly; and
rotating the second rotatable component at the second speed based at least in part on the electrical energy from the second rotor assembly.
17. The turbomachine of claim 16 , the operations further comprising:
decreasing a fuel flow at a combustion chamber such that rotating the second rotatable component at the second speed based at least in part on the electrical energy from the second rotor assembly results in approximately no change in the second speed.
18. The turbomachine of claim 14 , the operations further comprising:
rotating the second rotatable component at the second speed;
generating electrical energy via the second rotor assembly and the second rotatable component;
transmitting electrical energy from the second rotor assembly to the first rotor assembly; and
rotating the first rotatable component at the first speed based at least in part on the electrical energy from the first rotor assembly.
19. The turbomachine of claim 18 , the operations further comprising:
increasing the second load level at the second rotor assembly.
20. The turbomachine of claim 14 , the operations further comprising:
rotating the second rotatable component at the second speed defining a minimum steady state second speed.