Power generation and transfer using variable-pitch propeller
In one embodiment, a method includes determining a pitch value based on at least an energy goal. The energy goal may be at least one of bowed rotor motoring or an engine start. The method includes adjusting a pitch of a plurality of variable-pitch propeller blades based on the pitch value. The plurality of variable-pitch propeller blades are part of a variable-pitch propeller. The method includes, in response to a rotation of the plurality of variable-pitch propeller blades about a central axis based on the pitch of the plurality of variable-pitch propeller blades, activating an electric brake to reduce a speed of the rotation. The method further includes transferring electrical energy, generated by the electric brake reducing the speed of the rotation, to a component.
1. A method comprising:
receiving an indication of an energy goal, the energy goal being at least one of a bowed rotor motoring, an engine start for a first engine, an engine start for a second engine, energy storage onboard in an electric battery, or energy storage offboard in a power grid;
in response to receiving the indication of the energy goal that is the bowed rotor motoring:
identifying either the first engine or the second engine associated with the bowed rotor motoring; and
causing a first electrical energy to be transferred to a first shaft associated with the identified engine;
in response to receiving the indication of the energy goal that is the engine start for the first engine, causing a second electrical energy to be transferred to the first engine;
in response to receiving the indication of the energy goal that is the engine start for the second engine, causing a third electrical energy to be transferred to the second engine;
in response to receiving the indication of the energy goal that is energy storage onboard in the electric battery:
generating a fourth electrical energy; and
transferring the generated fourth electrical energy to the electrical battery; and
in response to receiving the indication of the energy goal that is energy storage offboard in the power grid:
generating a fifth electrical energy; and
transferring the generated fifth electrical energy to the power grid;
determining a pitch value based on at least the energy goal;
adjusting a pitch of a plurality of variable-pitch propeller blades based on the pitch value, the plurality of variable-pitch propeller blades being part of a variable-pitch propeller; and
in response to receiving the indication of the energy goal that is one or more of the bowed rotor motoring, the engine start for the first engine, or the engine start for the second engine:
in response to a rotation of the plurality of variable-pitch propeller blades about a central axis based on the pitch of the plurality of variable-pitch propeller blades, activating an electric brake to reduce a speed of the rotation; and
transferring a sixth electrical energy generated by the electric brake reducing the speed of the rotation to a component.
2. The method of claim 1 , wherein the component is one of:
a second shaft of a third engine;
the electric battery; or
the power grid.
3. The method of claim 1 , wherein activating the electric brake to reduce the speed of the rotation is in response to at least one of:
the speed of rotation reaching a predetermined speed value;
user input; or
sensor data.
4. The method of claim 1 , wherein the engine start is for starting at least one of:
a turbo engine, wherein the turbo engine includes the variable-pitch propeller; or
a second turbo engine, wherein the second turbo engine is coupled to the turbo engine.
5. The method of claim 1 , wherein determining the pitch value is based on at least one of:
environmental conditions; or
characteristics of an aircraft, wherein the aircraft includes a turbo engine, and the turbo engine includes the variable-pitch propeller.
6. The method of claim 1 , further comprising:
generating the sixth electrical energy from the rotation.
7. The method of claim 1 , wherein determining the pitch value is in response to at least one of:
user input; or
sensor data.
8. A system, comprising:
a variable-pitch propeller, the variable-pitch propeller includes a plurality of variable-pitch propeller blades;
a processor;
a non-transitory memory storing machine-readable instructions that, when executed by the processor, cause the processor to:
receive an indication of an energy goal, the energy goal being at least one of a bowed rotor motoring, an engine start for a first engine, an engine start for a second engine, energy storage onboard in an electric battery, or energy storage offboard in a power grid;
in response to receiving the indication of the energy goal that is the bowed rotor motoring:
identify either the first engine or the second engine associated with the bowed rotor motoring; and
cause a first electrical energy to be transferred to a shaft associated with the identified engine;
in response to receiving the indication of the energy goal that is the engine start for the first engine, cause a second electrical energy to be transferred to the first engine;
in response to receiving the indication of the energy goal that is the engine start for the second engine, cause a third electrical energy to be transferred to the second engine;
in response to receiving the indication of the energy goal that is energy storage onboard in the electric battery:
generate a fourth electrical energy; and
transfer the generated fourth electrical energy to the electrical battery; and
in response to receiving the indication of the energy goal that is energy storage offboard in the power grid:
generate a fifth electrical energy; and
transfer the generated fifth electrical energy to the power grid;
determine a pitch value based on at least the energy goal;
adjust a pitch of the plurality of variable-pitch propeller blades based on the pitch value; and
in response to receiving the indication of the energy goal that is one or more of the bowed rotor motoring, the engine start for the first engine, or the engine start for the second engine:
in response to a rotation of the plurality of variable-pitch propeller blades about a central axis based on the pitch of the plurality of variable-pitch propeller blades, activate an electric brake to reduce a speed of the rotation; and
transfer a sixth electrical energy generated by the electric brake reducing the speed of the rotation to a component.
9. The system of claim 8 , wherein the component is one of:
a second shaft of a third engine;
the electric battery; or
the power grid.
10. The system of claim 8 , wherein the machine-readable instructions further include instructions that when executed by the processor cause the processor to:
activate the electric brake to reduce the speed of the rotation in response to at least one of:
the speed of rotation reaching a predetermined speed value;
user input; or
sensor data.
11. The system of claim 8 , wherein the engine start is for starting at least one of:
a turbo engine, wherein the turbo engine includes the variable-pitch propeller; or
a second turbo engine, wherein the second turbo engine is coupled to the turbo engine.
12. The system of claim 8 , wherein the machine-readable instructions further include instructions that when executed by the processor cause the processor to:
determine the pitch value based on at least one of:
environmental conditions; or
characteristics of an aircraft, wherein the aircraft includes a turbo engine, and the turbo engine includes the variable-pitch propeller.
13. The system of claim 8 , wherein the machine-readable instructions further include instructions that when executed by the processor cause the processor to: generate the sixth electrical energy from the rotation.
14. The system of claim 8 , wherein the machine-readable instructions further include instructions that when executed by the processor cause the processor to:
determine the pitch value is in response to at least one of:
user input; or
sensor data.
15. A non-transitory computer-readable medium including instructions that, when executed by a processor, cause the processor to:
receive an indication of an energy goal, the energy goal being at least one of a bowed rotor motoring, an engine start for a first engine, an engine start for a second engine, energy storage onboard in an electric battery, or energy storage offboard in a power grid;
in response to receiving the indication of the energy goal that is the bowed rotor motoring:
identify either the first engine or the second engine associated with the bowed rotor motoring; and
cause a first electrical energy to be transferred to a shaft associated with the identified engine;
in response to receiving the indication of the energy goal that is the engine start for the first engine, cause a second electrical energy to be transferred to the first engine;
in response to receiving the indication of the energy goal that is the engine start for the second engine, cause a third electrical energy to be transferred to the second engine;
in response to receiving the indication of the energy goal that is energy storage onboard in the electric battery:
generate a fourth electrical energy; and
transfer the generated fourth electrical energy to the electrical battery; and
in response to receiving the indication of the energy goal that is energy storage offboard in the power grid:
generate a fifth electrical energy; and
transfer the generated fifth electrical energy to the power grid;
determine a pitch value based on at least the energy goal;
adjust a pitch of a plurality of variable-pitch propeller blades based on the pitch value, the plurality of variable-pitch propeller blades being part of a variable-pitch propeller; and
in response to receiving the indication of the energy goal that is one or more of the bowed rotor motoring, the engine start for the first engine, or the engine start for the second engine:
in response to a rotation of the plurality of variable-pitch propeller blades about a central axis based on the pitch of the plurality of variable-pitch propeller blades, activate an electric brake to reduce a speed of the rotation; and
transfer a sixth electrical energy generated by the electric brake reducing the speed of the rotation to a component.
16. The non-transitory computer-readable medium of claim 15 , wherein the component is one of:
a second shaft of a third engine;
the electric battery; or
the power grid.
17. The non-transitory computer-readable medium of claim 15 , wherein the instructions include instructions to activate the electric brake to reduce the speed of the rotation in response to at least one of:
the speed of rotation reaching a predetermined speed value;
user input; or
sensor data.
18. The non-transitory computer-readable medium of claim 15 , wherein the engine start is for starting at least one of:
a turbo engine, wherein the turbo engine includes the variable-pitch propeller; or
a second turbo engine, wherein the second turbo engine is coupled to the turbo engine.
19. The non-transitory computer-readable medium of claim 15 , wherein the instructions include instructions to determine the pitch value based on at least one of:
environmental conditions; or
characteristics of an aircraft, wherein the aircraft includes a turbo engine, and the turbo engine includes the variable-pitch propeller.
20. The non-transitory computer-readable medium of claim 15 , wherein the instructions include instructions to generate the sixth electrical energy from the rotation.