Fuel bypass system for gaseous-fueled engine
A method of operating a forced induction gaseous-fueled engine includes mixing gaseous-fuel and engine intake air to form a mixture at a fuel mixer. The method includes delivering the mixture to an intake manifold by at least partially bypassing a charge air cooler.
1. A method of operating a forced induction gaseous-fueled engine, the engine comprising a bypass line, a charge air cooler, a throttle valve, an intake manifold, and a plurality of cylinders, the method comprising:
delivering fuel during engine start through a bypass line to the intake manifold for delivery to the plurality of cylinders, completely bypassing the charge air cooler and the throttle valve during a bypass period.
2. The method of claim 1 , wherein the bypass period is a predetermined time interval, wherein the bypass period is less than or equal to 10 seconds.
3. The method of claim 1 , wherein the bypass period is a time interval determined by when the gaseous-fueled engine exceeds a predetermined RPM threshold.
4. The method of claim 1 , further comprising opening the throttle valve an increasing amount during the bypass period.
5. The method of claim 1 , further comprising closing the throttle valve when completely bypassing the charge air cooler.
6. The method of claim 1 , wherein the engine further comprises a bypass valve positioned in communication with the bypass line, and wherein the bypass valve is opened when completely bypassing the charge air cooler.
7. The method of claim 6 , further comprising closing the bypass valve when the gaseous-fueled engine exceeds a predetermined RPM threshold.
8. The method of claim 6 , further comprising opening the bypass valve for a predetermined bypass period time interval after an initiation of a starting sequence of the engine and closing the bypass valve after the bypass period time interval has elapsed.
9. The method of claim 1 , further comprising providing electricity to a building via an electricity generating system in communication with the gaseous-fueled engine, wherein normal power is restored to the building within 10 seconds from an initiation of a starting sequence of the gaseous-fueled engine.
10. The method of claim 1 , further comprising after completely bypassing the charge air cooler and throttle valve, opening the throttle valve to transition to primary fuel system operation.
11. A fuel bypass arrangement for a forced induction gaseous-fueled engine, the fuel bypass arrangement comprising:
a bypass line;
a charge air cooler;
a throttle valve;
an intake manifold; and
a plurality of cylinders,
wherein fuel is delivered during engine start through a bypass line to the intake manifold for delivery to the plurality of cylinders, completely bypassing the charge air cooler and the throttle valve.
12. The fuel bypass arrangement of claim 11 , wherein the fuel is delivered directly to the intake manifold.
13. The fuel bypass arrangement of claim 11 , wherein the charge air cooler is positioned between the throttle valve and an inlet of the fuel bypass line, the charge air cooler being configured to reduce the temperature of the fuel as the fuel travels from an inlet to an outlet of the charge air cooler.
14. The fuel bypass arrangement of claim 13 , wherein the throttle valve is positioned between, and in fluid communication with, the charge air cooler and the intake manifold, wherein the throttle valve is configured to control an amount of fuel that is delivered to the intake manifold from the charge air cooler.
15. The fuel bypass arrangement of claim 11 , further comprising a bypass valve in communication with the bypass line, the bypass valve being configured to selectively control the flow of the fuel through the bypass line.
16. The fuel bypass arrangement of claim 15 , further comprising a controller in communication with the bypass valve.
17. The fuel bypass arrangement of claim 16 , wherein the controller automatically opens the bypass valve at an initiation of a starting sequence of the gaseous-fueled engine.
18. The fuel bypass arrangement of claim 11 , further comprising after completely bypassing the charge air cooler and throttle valve, opening the throttle valve to transition to primary fuel system operation.
19. A power backup system comprising a forced induction gaseous-fueled engine, the engine comprising:
a bypass line, a charge air cooler, a throttle valve, an intake manifold, and a plurality of cylinders,
wherein fuel is delivered from a fuel source during engine start through a bypass line to the engine intake manifold for delivery to the plurality of cylinders, completely bypassing the charge air cooler and the throttle valve.
20. The power backup system of claim 19 , further comprising an electricity generating system in communication with the gaseous-fueled engine, wherein an external electrical load is connected to the electricity generating system within 10 seconds from an initiation of a starting sequence of the gaseous-fueled engine.
21. The power backup system of claim 19 , further comprising a battery bank.
22. The power backup system of claim 19 , further comprising after completely bypassing the charge air cooler and throttle valve, opening the throttle valve to transition to primary fuel system operation.