Fuel conditioning system and method configured to supply an aircraft turbine engine with fuel from a cryogenic tank
US-12162621-B2 · Dec 10, 2024 · US
US9447733B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9447733-B2 |
| Application number | US-201313886334-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 3, 2013 |
| Priority date | Mar 14, 2013 |
| Publication date | Sep 20, 2016 |
| Grant date | Sep 20, 2016 |
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A gas turbine engine fuel system has an ecology valve for withdrawing residual fuel from primary and secondary fuel manifolds upon engine shut-down. The ecology valve has primary and secondary reservoirs respectively connected in fluid flow communication with the primary and secondary fuel manifolds. The valve further has a reciprocating piston movable from a retracted position when engine start-up is initiated to an extended position which the piston assumes under normal engine running conditions. The movement of the reciprocating piston between the retracted and extended positions controls the flow of fuel from and to the primary and secondary reservoirs. A cross-bleed passage is defined in the reciprocating piston. The cross-bleed passage connects the primary and secondary reservoirs in fluid flow communication only when the piston is in its extended position. In this way, the cross-bleed flow between the primary and secondary fuel manifolds may be initiated only at the end of the engine start-up phase.
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The invention claimed is: 1. An ecology valve for withdrawing residual fuel from a primary fuel manifold and a secondary fuel manifold of a gas turbine engine upon the gas turbine engine shut-down, the ecology valve comprising: a variable volume primary reservoir having a primary port connectable in fluid flow communication with the primary fuel manifold; a variable volume secondary reservoir connectable in fluid flow communication with the secondary fuel manifold; a reciprocating piston movable within the variable volume primary reservoir and the variable volume secondary reservoir from a retracted position when engine start-up is initiated to an extended position which is assumed by the piston under normal engine running conditions, the movement of the reciprocating piston between the retracted position and the extended position reducing respective volumes of the variable volume primary reservoir and of the variable volume secondary reservoir, thereby flowing the fuel from the variable volume primary reservoir and the variable volume secondary reservoir to the primary fuel manifold and the secondary fuel manifold, respectively; and a cross-bleed passage defined in the reciprocating piston, the cross-bleed passage connecting the variable volume primary reservoir and the variable volume secondary reservoir in fluid flow communication only when the piston is in its extended position, the cross-bleed passage having an inlet and an outlet which are both in fluid flow communication with the variable volume primary reservoir when the reciprocating piston is in its retracted position. 2. The ecology valve defined in claim 1 , wherein the inlet of the cross-bleed passage is connected in fluid flow communication with the variable volume primary reservoir irrespective of the position of the reciprocating piston, the outlet being connected in fluid flow communication with the variable volume secondary reservoir only when the reciprocating piston reaches its extended position. 3. The ecology valve defined in claim 1 , wherein the cross-bleed passage establishes fluid flow communication between the primary fuel manifold and the secondary fuel manifold via variable volume primary reservoir and the variable volume secondary reservoir of the ecology valve. 4. The ecology valve defined in claim 1 , further comprising a pressure chamber adapted to be connected in fluid flow communication with a fuel supply line, the reciprocating piston being movable from the retracted position and the extended position by the fuel pressure in the pressure chamber. 5. The ecology valve defined in claim 1 , wherein the variable volume secondary reservoir is defined in part in a spring chamber defined in a stem portion of the reciprocating piston, the spring chamber having a spring urging the reciprocating piston towards its retracted position. 6. A gas turbine engine fuel system comprising: a fuel supply line; a flow divider valve having an inlet connected in fluid flow communication with the fuel supply line for receiving a fuel flow therefrom, the flow divider valve having at least a primary outlet and a secondary outlet and a valve member for controlling the flow of fuel from the inlet to the primary outlet and the secondary outlet; a primary fuel manifold having a primary inlet connected in fluid flow communication with the primary outlet of the flow divider valve for feeding a set of primary fuel nozzles arranged to spray fuel in a combustion chamber; a secondary fuel manifold having a secondary inlet connected in fluid flow communication with the secondary outlet of the flow divider valve for feeding a set of secondary fuel nozzles arranged to spray fuel in the combustion chamber; an ecology valve having a variable volume primary reservoir and a variable volume secondary reservoir, the variable volume primary reservoir having a primary port connected in fluid flow communication with the primary fuel manifold, the variable volume secondary reservoir having a secondary port connected in fluid flow communication with the secondary fuel manifold, the ecology valve further having a reciprocating piston moveable within the variable volume primary reservoir and the variable volume secondary reservoir between a retracted position to draw fuel from the primary fuel manifold and the secondary fuel manifold respectively into the variable volume primary reservoir and the variable volume secondary reservoir and an extended position to expel fuel out from the variable volume primary reservoir and the variable volume secondary reservoir back into the primary fuel manifold and the secondary fuel manifold respectively, wherein movement of the reciprocating piston between the retracted position and the extended position causes respective volumes of the variable volume primary reservoir and the variable volume secondary reservoir to go from an expanded volume to a reduced volume; and a cross-bleed passage defined in the reciprocating piston of the ecology valve, the cross-bleed passage establishing fluid flow communication from the primary fuel manifold to the secondary fuel manifold only when the reciprocating piston is in its extended position to allow a portion of the fuel from the primary outlet of the flow divider valve to be diverted to the secondary fuel manifold from the moment the reciprocating piston reaches its extended position. 7. The gas turbine engine fuel system defined in claim 6 , wherein the cross-bleed passage has an inlet and an outlet, the inlet being connected in fluid flow communication with the variable volume primary reservoir irrespective of the position of the reciprocating piston, the outlet being connected in fluid flow communication with the variable volume secondary reservoir only when the reciprocating piston reaches its extended position. 8. The gas turbine engine fuel system defined in claim 6 , wherein the cross-bleed passage establishes fluid flow communication between the primary fuel manifold and the secondary fuel manifold via the variable volume primary reservoir and the variable volume secondary reservoir of the ecology valve. 9. The gas turbine engine fuel system defined in claim 6 , wherein said ecology valve has a pressure chamber connected in fluid flow communication with the fuel supply line, the reciprocating piston being movable from the retracted position and the extended position by the fuel pressure in the pressure chamber. 10. The gas turbine engine fuel system defined in claim 9 , wherein a biasing member urges the reciprocating piston towards its retracted position, and wherein when the fuel pressure in the pressure chamber becomes greater than a biasing force of the biasing member, the reciprocating piston is displaced from its retracted position to its extended position. 11. A method of providing fuel cross-bleed between a primary fuel manifold and a secondary fuel manifold of a gas turbine engine including an ecology valve having a reciprocating piston movable within a variable volume primary reservoir and a variable volume secondary reservoir for withdrawing residual fuel from the primary fuel manifold and the secondary fuel manifold respectively upon engine shut-down, the method comprising: initiating an engine start-up phase, including directing a primary fuel flow to said primary fuel manifold; displacing the reciprocating piston from a retracted position at an engine shut-down position to an extended position at an engine running position so as to reduce respective volumes of the variable volume primary reservoir and the variable volume secondary reservoir; and only at the end of the engine start-up phase when the reciprocating piston reaches the extended position at its engine running p
Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title
Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for · CPC title
Dividing fuel between various burners · CPC title
Drainage · CPC title
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