Compressor bypass

1. A method of operating a power system, comprising:

generating a flow of compressed intake air;

injecting natural gas into the flow of compressed intake air to form an air/fuel mixture;

burning the air/fuel mixture in a natural gas engine;

directing a combustion exhaust from the engine to a turbine downstream of the engine sensing an intake manifold pressure associated with the engine;

comparing the sensed intake manifold pressure to a threshold pressure; and

adjusting a valve assembly in a bypass system to selectively direct a portion of the flow of compressed intake air to the turbine when the sensed intake manifold pressure is greater than the threshold pressure, wherein the portion of the compressed intake air includes no natural gas and assists in rotating the turbine.

2. The method of claim 1 , further comprising directing the portion of the flow from a first location having a first fluid pressure to a second location having a second fluid pressure less than the first fluid pressure.

3. A power system, comprising:

a natural gas engine; a first turbine receiving an exhaust from the engine;

a second turbine having an inlet fluidly connected to an outlet of the first turbine;

a compressor driven by the first turbine, the compressor having an outlet fluidly connected to the engine;

a bypass system, comprising a valve assembly configured to selectively direct a fluid from the outlet of the compressor to the inlet of the second turbine;

a sensor configured to sense an intake manifold pressure associated with the engine; and

a controller operably connected to the valve assembly of the bypass system, wherein the controller is configured to compare the sensed intake manifold pressure to a threshold pressure and selectively control the valve assembly to effect fluid communication between the compressor outlet and the inlet of the second turbine when the sensed intake manifold pressure is greater than the threshold pressure.

4. The power system of claim 1 , wherein the valve assembly comprises a valve element moveable between an open position permitting a flow of the fluid between the compressor and the inlet of the second turbine, and a closed position blocking the flow of the fluid between the compressor and the inlet of the second turbine, and an actuator operably connected to the valve element.

5. The power system of claim 1 , wherein the valve assembly is fluidly connected to a first passageway extending from the compressor to the inlet of the second turbine.

6. The power system of claim 5 , further comprising a second passageway extending from the outlet of the first turbine to the inlet of the second turbine, wherein an outlet of the first passageway is fluidly connected to the second passageway.

7. The power system of claim 6 , wherein a fluid pressure within the second passageway is less than a fluid pressure proximate the outlet of the compressor.

8. The power system of claim 1 , further including an injector configured to inject fuel at a location downstream of an inlet of the bypass system.

9. The power system of claim 1 , wherein the second turbine is connected to an output member of the engine such that rotation of the second turbine assists in rotating the output member.

10. A power system, comprising:

a natural gas engine;

an air induction system including a compressor having an outlet fluidly connected to the engine;

an exhaust system including a first turbine connected to the compressor, and a second turbine downstream of the first turbine and connected to an output member of the engine;

a bypass system including a valve assembly configured to regulate a flow of compressed air from the compressor to the second turbine; and

a control system including a controller and at least one sensor, wherein the sensor is configured to sense an intake manifold pressure associated with the engine, and the controller is configured to compare the sensed intake pressure to a threshold pressure and to control the valve assembly of the bypass system to selectively effect fluid communication between the compressor outlet and the second turbine when the sensed intake manifold pressure is greater than the threshold pressure.

11. The power system of claim 10 , wherein the valve assembly comprises a valve element moveable between an open position permitting flow between the compressor and the second turbine, and a closed position blocking flow between the compressor and the second turbine, and an actuator operably connected to the valve element.

12. The power system of claim 10 , wherein the bypass system further comprises a passageway extending from the compressor to the second turbine, wherein the valve assembly is configured to regulate passage of the flow of compressed air through the passageway.

13. The power system of claim 10 , further including an injector configured to inject fuel at a location downstream of an inlet of the bypass system.

14. The power system of claim 10 , wherein the location downstream of the inlet of the bypass system comprises one of a combustion chamber of the engine and a port of the engine.