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 electric engine for an aircraft, 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; and
an after-fan system located aft of the fan, the after-fan system comprising:
an exit guide vane assembly located at an outlet of the fan;
an after-fan turbine located forward of a compressor and aft of the exit guide vane assembly, 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;
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 electric engine of claim 1 , further comprising:
a sensor operably coupled to the after-fan turbine; and
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 a signal corresponding to a rotations per minute of the after-fan turbine from the sensor, and wherein the controller is configured to output an electrical signal to the electric motor based on the signal corresponding to the rotations per minute of the after-fan turbine.
3. The electric engine of claim 2 , further comprising:
a battery electrically coupled to the electrical generator and to the electric motor; and
an alternating current to direct current convertor electrically coupled between the electrical generator and the battery.
4. The electric engine of claim 3 , wherein the exit guide vane assembly is a variable vane assembly, and wherein the controller is configured to control a stagger angle of the variable vane assembly.