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A fluid handling system for a use with an engine is provided. The fluid-handling system may have a first turbine connected to receive a portion of an exhaust flow from the engine, a first compressor driven by the first turbine to pressurize an airflow, and a heat exchanger configured to receive a re

A fluid handling system for a use with an engine is provided. The fluid-handling system may have a first turbine connected to receive a portion of an exhaust flow from the engine, a first compressor driven by the first turbine to pressurize an airflow, and a heat exchanger configured to receive a remaining portion of the exhaust flow from the engine and the airflow from the first compressor. The fluid-handling system may also have a second turbine connected to receive the airflow from the heat exchanger, and a generator driven by the second turbine to generate power.

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1. A fluid-handling system for an engine, comprising: a first turbine connected to receive a first portion of an exhaust flow from the engine;a first compressor driven by the first turbine to pressurize a first airflow;a heat exchanger configured to receive a second portion of the exhaust flow from

1. A fluid-handling system for an engine, comprising: a first turbine connected to receive a first portion of an exhaust flow from the engine;a first compressor driven by the first turbine to pressurize a first airflow;a heat exchanger configured to receive a second portion of the exhaust flow from the engine and the first airflow;a second turbine connected to receive the first airflow from the heat exchanger;a generator driven by the second turbine to generate power; andwherein the second portion of the exhaust flow is directed into the engine for combustion. 2. The fluid-handling system of claim 1, further including a second compressor configured to pressurize a second airflow directed into the engine for combustion, wherein the first and second compressors receive inlet air in parallel. 3. The fluid-handling system of claim 2, further including a second heat exchanger configured to cool the second airflow. 4. The fluid-handling system of claim 3, wherein the second portion of the exhaust flow from the heat exchanger is directed to join the second airflow at a location upstream of the second heat exchanger. 5. The fluid-handling system of claim 2, further including a third turbine connected to receive the first portion of exhaust flow from the engine, wherein the second compressor is driven by the third turbine. 6. The fluid-handling system of claim 5, wherein the first and third turbines are disposed in series. 7. The fluid-handling system of claim 2, wherein the second compressor is driven by the first turbine. 8. The fluid-handling system of claim 1, wherein an outlet of the second turbine is fluidly connected with an outlet of the first turbine. 9. The fluid-handling system of claim 1, wherein the generator is configured to generate electrical power. 10. The fluid-handling system of claim 1, further including a bypass valve configured to selectively cause the first airflow to bypass the heat exchanger. 11. A method of handling exhaust from an engine, comprising: combusting a mixture of air and fuel to generate a mechanical output and an exhaust flow;mechanically removing energy, via a first turbine, from a first portion of the exhaust flow;using the energy to pressurize an airflow;transferring heat from a second portion of the exhaust flow to the airflow;mechanically removing energy, via a second turbine, from the airflow after transferring the heat;converting the energy mechanically removed from the airflow to one of electrical energy, hydraulic energy, and kinetic energy; anddirecting the second portion of the exhaust flow after the energy has been removed to join combustion air. 12. The method of claim 11, further including: mechanically removing additional energy from the first portion of the exhaust flow; andusing the additional energy to pressurize combustion air. 13. The method of claim 12, wherein the airflow and the combustion air are pressurized in parallel. 14. The method of claim 12, further including cooling the combustion air. 15. The method of claim 14, further including directing the second portion of the exhaust flow after the energy has been removed to join the combustion air before cooling of the combustion air. 16. The method of claim 12, wherein the energy and the additional energy are mechanically removed from the first portion of the exhaust flow in series. 17. The method of claim 11, further including selectively inhibiting the airflow from transferring heat with the second portion of the exhaust flow. 18. A power system, comprising: an engine having an air duct and an exhaust duct;a first turbine fluidly connected to the exhaust duct to receive a first portion of an exhaust flow from the engine;a first compressor fluidly connected to the air duct and driven by the first turbine to pressurize a first airflow directed into the engine;a first heat exchanger configured to cool the first airflow before it is received by the engine;a second compressor driven by one of the first turbine, or a third turbine fluidly connected to the exhaust duct to receive the first portion of the exhaust flow, the second compressor configured to pressurize a second airflow;a second heat exchanger configured to receive a second portion of the exhaust flow from the engine and the second airflow from the second compressor;a second turbine connected to receive the second airflow from the second heat exchanger;a generator driven by the second turbine to generate electricity; andwherein the second portion of the exhaust flow is directed to the air duct of the engine. 19. The power system of claim 18, wherein the first and second compressors receive inlet air in parallel and the third turbine is fluidly connected to the first turbine to receive the first portion of the exhaust flow from the first turbine in series.