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An engine may have a recuperator that may be powered by an electrical generator driven by the engine. The recuperator may be disposed within or incorporated into a compressor discharge of the engine, such as in the form of a vane or tube. The engine may be configured to operate in a variety of modes

An engine may have a recuperator that may be powered by an electrical generator driven by the engine. The recuperator may be disposed within or incorporated into a compressor discharge of the engine, such as in the form of a vane or tube. The engine may be configured to operate in a variety of modes at least some of which may use thermal energy from the recuperator to heat a fluid flow stream of the engine. An energy storage device may be used with an electrical generator to provide power to a load.

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1. A system comprising: an engine having:a compressor and a turbine coupled together with a flow path there between by which a fluid flow stream is flowable from the compressor to the turbine, the compressor having a compressor discharge through which the fluid flow stream exits the compressor, the

1. A system comprising: an engine having:a compressor and a turbine coupled together with a flow path there between by which a fluid flow stream is flowable from the compressor to the turbine, the compressor having a compressor discharge through which the fluid flow stream exits the compressor, the turbine being configured to generate power;a combustor located between the compressor and the turbine, the combustor being configured to provide heat to the fluid flow stream before entering the turbine;at least one recuperator disposed downstream of the compressor, the recuperator being configured to transfer heat with the fluid flow stream en route to the combustor;an electric generator operatively coupled to the turbine to receive at least a portion of the power generated by the turbine, the electric generator further being in communication with the at least one recuperator; anda controller configured to operate the engine in a low power mode, a high power mode, and at least one intermediate speed/power mode, the controller configured to selectively distribute energy from the electric generator between the at least one recuperator and a load, the controller configured to direct energy to the at least one recuperator while reducing a fuel flow to the engine when in the intermediate speed/power mode to maintain a speed/power setting of the engine;wherein the recuperator is configured in an off condition in the low power mode. 2. The system of claim 1 wherein the compressor discharge has a first terminal and a second terminal in communication with the at least one recuperator, the first terminal and the second terminal being configured to subject a potential difference to the recuperator to enable the heat transfer with the fluid flow stream. 3. The system of claim 2 wherein the first terminal and the second terminal are located at a radially inner end of the recuperator and a radially outer end of the recuperator, respectively. 4. The system of claim 3 wherein the at least one recuperator includes an electrical conduit routed from the radially inner end through the fluid flow stream. 5. The system of claim 1 wherein the recuperator is configured in an off condition in the low power mode and the high power mode. 6. The system of claim 1 further comprising an energy storage device configured to provide energy to the load when the engine transitions from the low power mode to the high power mode. 7. The system of claim 6 wherein the load is configured to receive power from at least one of the electric generator and the energy storage device. 8. The system of claim 7 wherein the controller is further configured to selectively supply power to the load from at least one of the electric generator and the energy storage device. 9. The system of claim 1 wherein the engine further comprises a low pressure spool to which the turbine is connected. 10. A method comprising: supplying fuel at a flow rate to an engine such that the engine operates in a high power mode, the engine including a compressor, a combustor, a turbine, and a recuperator;decreasing the fuel flow rate while supplying energy to the recuperator from the turbine such that the engine continues to maintain a speed/power setting during an intermediate speed/power mode; andpowering a load by:reducing energy supplied to the recuperator; andtransmitting power from an energy storage device to the load. 11. The method of claim 10 further comprising further increasing the fuel flow rate after supplying energy to the recuperator. 12. The method of claim 11 further comprising accelerating the compressor of the engine prior to powering the load. 13. The method of claim 10 wherein the recuperator is electrically driven, and wherein energy is supplied to the recuperator via an electrical generator. 14. The system of claim 1, wherein the controller during the intermediate speed/power mode is configured to reduce the fuel flow to a flow rate approximately equal to a fuel flow rate at the low power mode. 15. The system of claim 10, wherein the fuel flow rate is decreased during the intermediate speedpower mode to be approximately equal to a fuel flow rate at a low power mode. 16. The system of claim 1, wherein the controller is in communication with at least one sensor, the sensor configured to measure or calculate sensor data comprising one or more of static temperature, static pressure, total temperature, total pressure, equivalent airspeed, altitude, and Mach number; wherein the controller is configured to distribute energy to the at least one recuperator based on the sensor data.