Flex coupler for hybrid gas turbine engine powerplant
An engine system is provided that includes an engine rotating structure, an electric machine rotating structure and a flex coupler. The flex coupler rotatably connects the electric machine rotating structure to the engine rotating structure. The flex coupler includes a first mount, a second mount and a flex plate. The first mount includes a plurality of first mount fingers arranged circumferentially about an axis. The second mount includes a plurality of second mount fingers arranged circumferentially about the axis. The flex plate connects the first mount to the second mount. The flex plate includes a plurality of first flex plate fingers and a plurality of second flex plate fingers. Each of the first flex plate fingers is attached to a respective one of the first mount fingers. Each of the second flex plate fingers is attached to a respective one of the second mount fingers.
1. An engine system, comprising:
a gas turbine engine including an engine rotating structure, a compressor section, a combustor section, a turbine section and a flowpath extending through the compressor section, the combustor section and the turbine section, the engine rotating structure comprising a turbine rotor within the turbine section;
an electric machine comprising an electric machine rotating structure; and
a flex coupler rotatably connecting the electric machine rotating structure to the engine rotating structure, the flex coupler including
a first mount including a plurality of first mount fingers arranged circumferentially about an axis;
a second mount including a plurality of second mount fingers arranged circumferentially about the axis; and
a flex plate connecting the first mount to the second mount, the flex plate including a plurality of first flex plate fingers and a plurality of second flex plate fingers, each of the plurality of first flex plate fingers attached to a respective one of the plurality of first mount fingers, and each of the plurality of second flex plate fingers attached to a respective one of the plurality of second mount fingers.
2. The engine system of claim 1 , wherein the flex coupler is configured to accommodate axial shifting between the engine rotating structure and the electric machine rotating structure.
3. The engine system of claim 1 , wherein the flex coupler is configured to accommodate misalignment between a rotational axis of the engine rotating structure and a rotational axis of the electric machine rotating structure.
4. The engine system of claim 1 , wherein the plurality of first flex plate fingers are interspersed with the plurality of second flex plate fingers circumferentially about the axis.
5. The engine system of claim 1 , wherein each of the plurality of first flex plate fingers is arranged circumferentially between a respective circumferentially adjacent pair of the plurality of second flex plate fingers.
6. The engine system of claim 5 , wherein each of the plurality of second flex plate fingers is arranged circumferentially between a respective circumferentially adjacent pair of the plurality of first flex plate fingers.
7. The engine system of claim 1 , wherein
the first mount further includes a first mount base;
each of the plurality of first mount fingers projects radially out from the first mount base to a respective first mount finger distal end; and
each of the plurality of first mount fingers is attached to the respective one of the plurality of first flex plate fingers at the respective first mount finger distal end.
8. The engine system of claim 7 , wherein each of the plurality of first mount fingers further projects axially out from the first mount base towards the respective first mount finger distal end.
9. The engine system of claim 1 , wherein
the flex plate further includes a flex plate base;
each of the plurality of first flex plate fingers projects radially out from the flex plate base to a respective first flex plate finger distal end, and each of the plurality of first flex plate fingers is attached to the respective one of the plurality of first mount fingers at the respective first flex plate finger distal end; and
each of the plurality of second flex plate fingers projects radially out from the flex plate base to a respective second flex plate finger distal end, and each of the plurality of second flex plate fingers is attached to the respective one of the plurality of second mount fingers at the respective second flex plate finger distal end.
10. The engine system of claim 1 , wherein
each of the plurality of first mount fingers has a minimum first mount finger thickness; and
each of the plurality of first flex plate fingers has a minimum first flex plate finger thickness that is less than the minimum first mount finger thickness.
11. The engine system of claim 1 , wherein
each of the plurality of first flex plate fingers is attached to the respective one of the plurality of first mount fingers by a respective first fastener; and
each of the plurality of second flex plate fingers attached to the respective one of the plurality of second mount fingers by a respective second fastener.
12. The engine system of claim 1 , further comprising a driveshaft rotatably connecting the flex coupler to one of the electric machine rotating structure or the engine rotating structure.
13. The engine system of claim 12 , further comprising:
a second flex coupler rotatably connecting the driveshaft to the electric machine rotating structure;
the flex coupler comprising a first flex coupler that rotatably connects the driveshaft to the engine rotating structure; and
the second flex coupler having a different configuration than the first flex coupler.
14. The engine system of claim 12 , further comprising:
a second flex coupler rotatably connecting the driveshaft to the electric machine rotating structure;
the flex coupler comprising a first flex coupler that rotatably connects the driveshaft to the engine rotating structure; and
the second flex coupler having a common configuration with the first flex coupler.
15. The engine system of claim 1 , wherein the flex coupler is directly attached to at least one of the engine rotating structure or the electric machine rotating structure.
16. The engine system of claim 1 , further comprising a propulsor rotor rotatably connected to the engine rotating structure and the electric machine rotating structure.
17. An engine system, comprising:
a propulsor rotor;
an electric machine comprising an electric machine rotating structure; and
a drivetrain configured to transfer mechanical power between the electric machine rotating structure and the propulsor rotor, the drivetrain comprising a flex coupler including
a first mount including a plurality of first mount fingers arranged circumferentially about an axis;
a second mount including a plurality of second mount fingers arranged circumferentially about the axis; and
a flex plate connecting the first mount to the second mount, the flex plate including a plurality of first flex plate fingers and a plurality of second flex plate fingers, each of the plurality of first flex plate fingers attached to a respective one of the plurality of first mount fingers, and each of the plurality of second flex plate fingers attached to a respective one of the plurality of second mount fingers.
18. The engine system of claim 17 , further comprising:
a gas turbine engine comprising an engine rotating structure;
the drivetrain rotatably connecting the electric machine rotating structure to the engine rotating structure.