After-fan system with electrical motor for gas turbine engines
An after-fan system for an engine may comprise an after-fan turbine an electrical generator operationally coupled to the after-fan turbine, and an electric motor electrically coupled to the electrical generator. The electrical generator may be configured to generate an electrical current in response to rotation of the after-fan turbine. The electric motor may be configured to generate torque.
1. An after-fan system for a gas turbine engine, comprising:
a fan driven by a low speed shaft via a gear assembly and a fan input shaft, the gear assembly rotationally coupled to the fan via the fan input shaft and configured to transfer torque from the low speed shaft to the fan;
an after-fan turbine located forward of a compressor and aft of the fan, wherein a fluid output of the fan drives a rotation of the after-fan turbine thereby rotating an after-fan turbine shaft;
an electrical generator mechanically coupled to the after-fan turbine via the after-fan turbine shaft at a location between the fan and the after-fan turbine and configured to generate an electrical current in response to rotation of the after-fan turbine shaft;
an electric motor electrically coupled to the electrical generator at a location between the electric generator and the fan, the electric motor configured to drive a motor shaft; and
the gear assembly rotationally coupled to a mechanical output of the electric motor via the motor shaft and configured to transfer torque from the motor shaft to the fan via the fan input shaft.
2. The after-fan system of claim 1 , further comprising a battery electrically coupled to an output of the electrical generator.
3. The after-fan system of claim 2 , wherein the battery is electrically coupled to the electric motor.
4. The after-fan system of claim 1 , further comprising a controller electrically coupled to the electrical generator and the electric motor, wherein the controller is configured to receive the electrical current from the electrical generator and output an electrical signal to the electric motor, and wherein the electrical signal is configured to cause the electric motor to generate torque.
5. The after-fan system of claim 4 , further comprising an exit guide vane assembly located at an inlet of the after-fan turbine.
6. The after-fan system of claim 5 , wherein the exit guide vane assembly is a variable exit guide vane assembly, and wherein the controller is configured to control a stagger angle of the variable exit guide vane assembly.
7. The after-fan system of claim 1 , wherein the electric motor comprises an asynchronous 3-phase alternating current motor or a switch reluctance motor.
8. A gas turbine engine, comprising:
a fan driven by a low speed shaft via a gear assembly and a fan input shaft, the gear assembly rotationally coupled to the fan via the fan input shaft and configured to transfer torque from the low speed shaft to the fan;
a compressor aft of the fan; and
an after-fan system located axially between the fan and the compressor, the after-fan system comprising:
an after-fan turbine located forward of the compressor and aft of the fan, wherein a fluid output of the fan drives a rotation of the after-fan turbine thereby rotating an after-fan turbine shaft;
a first electrical generator mechanically coupled to the after-fan turbine via the after-fan turbine shaft at a location between the fan and the after-fan turbine and configured to generate a first electrical current in response to rotation of the after-fan turbine shaft;
an electric motor electrically coupled to the first electrical generator at a location between the electric generator and the fan, the electric motor configured to drive a motor shaft; and
the gear assembly rotationally coupled to a mechanical output of the electric motor via the motor shaft and configured to transfer torque from the motor shaft to the fan via the fan input shaft.
9. The gas turbine engine of claim 8 , wherein the after-fan system further comprises an exit guide vane assembly located axially between the fan and the after-fan turbine.
10. The gas turbine engine of claim 9 , further comprising:
a turbine aft of the compressor; and
the low speed shaft rotationally coupled to the turbine, wherein the gear assembly further couples the low speed shaft to the fan.
11. The gas turbine engine of claim 9 , further comprising:
a turbine aft of the compressor;
the low speed shaft rotationally coupled to the turbine; and
a second electrical generator operationally coupled to the low speed shaft and configured to generate a second electrical current in response to rotation of the turbine, wherein the second electrical generator is electrically coupled to the electric motor.
12. The gas turbine engine of claim 11 , further comprising:
the gear assembly rotationally coupled between the low-speed shaft and the second electrical generator, wherein the gear assembly is configured to transfer torque from the low speed shaft to the fan via the fan input shaft.
13. The gas turbine engine of claim 12 , further comprising:
a battery electrically coupled to the electric motor and to at least one of the first electrical generator or the second electrical generator.
14. The gas turbine engine of claim 8 , wherein the electric motor comprises an asynchronous 3-phase alternating current motor or a switch reluctance motor.
15. The gas turbine engine of claim 14 , wherein the first electrical generator comprises an alternating current self-oscillation rotary generator.