Fault-tolerant fuel isolation from engine firebay
Fuel isolation systems, apparatuses and methods are described. In some embodiments, a system comprises a connector coupled inline with a fuel line on a cold side of the fuel line, a valve coupled to the connector, a fluid feed line coupled to a fluid source and to the valve. In the event of an engine fire condition, a control unit outputs signaling to stop pumping the fuel and to operate the valve to introduce fluid from the fluid source into the fuel line. The introduced fluid provides a siphon break in the fuel line such that the only fuel that can pass the firewall is the remaining fuel in the fuel line downstream of the connector and the introduced fluid.
1. A system for use in isolating fuel in a vehicle, the system comprising:
a connector coupled inline with a fuel feed line of the vehicle at a location of a cold side portion of the fuel feed line extending from a fuel tank to a firewall, wherein the fuel feed line includes a hot side portion extending through the firewall to an engine in a vehicle firebay;
a valve coupled to the connector;
a fluid feed line coupled to a fluid source and to the valve; and
a control unit configured to control operation of at least a fuel pump and the valve, wherein the control unit is configured to output control signaling to:
stop pumping the fuel through the fuel feed line; and
operate the valve to introduce a fluid from the fluid source into the fuel feed line, wherein the fluid introduced by the valve provides a siphon break in the fuel feed line such that the only fuel that can pass the firewall is the fuel remaining in the fuel feed line downstream of the connector and the fluid introduced.
2. The system of claim 1 , wherein the fuel feed line does not include a shut off valve in the cold side portion of the fuel feed line extending from the fuel pump to the firewall.
3. The system of claim 1 , wherein in the event of an engine fire, the control unit is configured to output control signaling to turn off the engine.
4. The system of claim 1 , wherein in the event of a engine fire, the control unit is configured to output control signaling to operate a jettison valve fluidly connected to the fuel tank for a period of time to reduce pressure in the system.
5. The system of claim 1 , wherein in the event of an engine fire is not an actual engine fire, the control unit is configured to output control signaling to:
start the engine;
turn on the fuel pump; and
operate the valve such that the fuel will resume flowing to the engine.
6. The system of claim 1 , wherein in the event of a failure of the valve when there is not an engine fire, the fuel continues to flow at a sufficient level through the fuel feed line and the connector from the fuel tank to the engine to allow for safe operation of the engine.
7. The system of claim 6 , wherein in the event of the failure of the valve when there is not an engine fire, a portion of the fuel flowing through the fuel feed line is diverted through the valve to the fuel tank via the fluid feed line.
8. The system of claim 1 , wherein the connector is coupled inline with the fuel feed line at a high elevation location of the cold side portion of the fuel feed line, the high elevation location at or above an elevation corresponding to a low elevation point of the fluid source.
9. The system of claim 1 , wherein the connector is coupled inline with the fuel feed line at a high elevation point location of the cold side portion of the fuel feed line.
10. The system of claim 1 , wherein the connector comprises a tee connector coupled inline with the fuel feed line and coupled to the valve.
11. The system of claim 1 , wherein the control unit is configured to receive sensor signaling from comprising one or more sensors proximate to the engine and configured to detect a condition indicative of an engine fire.
12. The system of claim 11 , wherein the control unit is configured to:
transmit a message to a vehicle operator indicate a detection of the condition indicative of the engine fire;
receive a command from the vehicle operator to initiate fuel isolation; and
output control signaling to stop pumping the fuel through the fuel feed line and to operate the valve to introduce the fluid into the fuel feed line.
13. The system of claim 11 , wherein the control unit is configured to:
determine, based on at least the sensor signaling received, that fuel isolation is needed; and
output control signaling to stop pumping the fuel through the fuel feed line and to operate the valve to introduce the fluid into the fuel feed line.
14. The system of claim 1 , wherein the vehicle comprises one of a manned aerial vehicle, an unmanned aerial vehicle, a watercraft, and a ground vehicle.
15. The system of claim 1 , wherein the vehicle comprises one of multi-engine vehicle and a single engine vehicle.
16. The system of claim 1 , wherein the fluid source coupled to the fluid feed line comprises an ullage portion of the fuel tank, a separate volume containing the fluid, and/or a vent box.
17. The system of claim 1 , wherein the fluid from the fluid source is maintained at a pressure or at atmospheric pressure.
18. The system of claim 1 , wherein the fluid from the fluid source comprises one of air, a gas and a liquid.
19. A method for isolating fuel in a vehicle, the method comprising:
outputting, by a control circuit, control signaling to stop pumping the fuel through a fuel feed line passing through a firewall to an engine within a vehicle firebay, wherein firewall separates the vehicle firebay from a volume containing a fuel pump and a fuel tank;
outputting, by the control circuit, control signaling to operate a valve coupled to a connector coupled inline with the fuel feed line at a location of a cold side portion of the fuel feed line, wherein the cold side portion of the fuel feed line extends from the fuel tank to the firewall, and wherein a hot side portion of the fuel feed line extends from the firewall to the engine; and
wherein through operation of the valve, fluid is introduced from a fluid source via a fluid feed line into the fuel feed line to provide a siphon break in the fuel feed line such that the only fuel that can pass the firewall is the fuel remaining in the fuel feed line downstream of the connector and the fluid introduced.
20. The method of claim 19 , wherein the fuel feed line does not include a shut off valve in the cold side portion of the fuel feed line extending from the fuel pump to the firewall.
21. The method of claim 19 , further comprising:
in the event of an engine fire,
outputting, by a control circuit, control signaling to turn off the fuel pump and to operate the valve.
22. The method of claim 19 , wherein in the event of an engine fire,
outputting, by the control circuit, control signaling to turn off the engine.
23. The method of claim 19 , further comprising:
in the event of an engine fire,
outputting, by the control circuit, control signaling to operate a jettison valve fluidly connected to the fuel tank for a period of time to reduce pressure in a fuel system.
24. The method of claim 19 , wherein in the event of an engine fire is not an actual engine fire, the method comprises:
outputting, by the control circuit, control signaling to start the engine, to turn on the fuel pump and to operate the valve such that the fuel will resume flowing to the engine.
25. The method of claim 19 ,
wherein in the event of a failure of the valve when there is not an engine fire,
outputting, by the control circuit, control signaling to flow fuel at a sufficient level through the fuel feed line and the connector from the fuel tank to the engine to allow for safe operation of the engine.
26. The method of claim 25 ,
wherein in the event of the failure of the valve when there is not an engine fire,
outputting, by the control circuit, control signaling to divert a portion of the fuel flowing through the fuel feed line through the valve back to the fuel tank via the fluid feed line.
27. The method of claim 19 , wherein the connector is coupled inline with the fuel feed line at a high elevation location of the cold side portion of the fuel feed line, the high elevation location at an elevation corresponding to a low elevation point of the fluid source.
28. The method of claim 19 , wherein the connector is coupled inline with the fuel feed line at a high elevation point location of the cold side portion of the fuel feed line.
29. The method of claim 19 , wherein the connector comprises a tee connector coupled inline with the fuel feed line and coupled to the valve.
30. The method of claim 19 , further comprising:
receiving, by the control circuit, sensor signaling from one or more sensors proximate to the engine based on a detected condition indicative of an engine fire.
31. The method of claim 30 , further comprising:
transmitting, by the control circuit, a message to a vehicle operator to indicate a detection of the detected condition indicative of the engine fire;
receiving, by the control circuit, a command from the vehicle operator to initiate fuel isolation; and
outputting, by the control circuit, control signaling to initiate steps of turning off the fuel pump, operating the valve, and introducing the fluid.
32. The method of claim 30 , further comprising:
determining, by the control circuit and based on at least the sensor signaling received, that fuel isolation is needed; and
outputting, by the control circuit, control signaling to initiate steps of turning off the fuel pump, operating the valve, and introducing the fluid.
33. The method of claim 19 , wherein the vehicle comprises one of a manned aerial vehicle, an unmanned aerial vehicle, a watercraft, and a ground vehicle.
34. The method of claim 19 , wherein the vehicle comprises one of a multi-engine vehicle and a single engine vehicle.
35. The method of claim 19 , wherein the fluid source coupled to the fluid feed line comprises an ullage portion of the fuel tank, a separate volume containing fluid, and/or a vent box.
36. The method of claim 19 , wherein the fluid from the fluid source is maintained at a pressure or at atmospheric pressure.
37. The method of claim 19 , wherein the fluid from the fluid source comprises one of air, a gas and a liquid.
38. An apparatus for isolating fuel in a vehicle, the apparatus comprising:
a non-transitory storage medium storing a set of computer readable instructions; and
control circuit configured to execute the set of computer readable instructions which causes to the control circuit to:
output control signaling to stop pumping the fuel through a fuel feed line from a fuel tank to an engine within a vehicle firebay and passing through a firewall that separates the vehicle firebay from a volume containing a fuel pump and the fuel tank; and
output control signaling to operate a valve coupled to a connector coupled in line with the fuel feed line at a location of a cold side portion of the fuel feed line, wherein the cold side portion of the fuel feed line extends from the fuel tank to the firewall, and wherein a hot side portion of the fuel feed line extends from the firewall to the engine, wherein fluid from a fluid source is introduced into the fuel feed line to provide a siphon break in the fuel feed line such that the only fuel passing the firewall is the fuel remaining in the fuel feed line downstream of the connector and the fluid introduced.
39. The apparatus of claim 38 , wherein the vehicle comprises one of a manned aerial vehicle, an unmanned aerial vehicle, a watercraft, and a ground vehicle.
40. The apparatus of claim 38 , wherein the fluid from the fluid source comprises one of air, a gas and a liquid.