Fuel flow divider and ecology system for a gas turbine engine fuel flow control system

Patent metadata

Field	Value
Publication number	US-9234465-B2
Application number	US-201113085107-A
Country	US
Kind code	B2
Filing date	Apr 12, 2011
Priority date	Apr 12, 2011
Publication date	Jan 12, 2016
Grant date	Jan 12, 2016

Abstract

A flow divider valve for a gas turbine engine fuel supply system is provided. The flow divider valve is configured, whenever fuel pressure at its inlet port is between a first predetermined pressure and a second predetermined pressure, to supply the fuel to a start nozzle manifold outlet port at a substantially constant flow rate, and to direct any fuel flow in excess of the substantially constant flow rate to a run nozzle manifold outlet port.

First claim

What is claimed is:

1. A flow divider valve for controlling fuel flow to a gas turbine engine that includes a start nozzle manifold and a run nozzle manifold, the flow divider valve comprising:
a valve body including an inlet port, a start nozzle manifold outlet port, a run nozzle manifold outlet port, and an inner surface that defines a valve chamber;
a start flow orifice disposed between the inlet port and the start nozzle manifold outlet port; and
a flow divider valve element disposed within the valve chamber and movable therein between a closed position and a plurality of open positions, the flow divider valve element including an inner surface, an outer surface, and a flow regulation port, the inner surface defining an internal channel, the flow regulation port extending through the flow divider valve element between the inner surface and the outer surface and providing continuous fluid communication between the internal channel and the run nozzle manifold outlet port when the flow divider valve element is in the plurality of open positions;
wherein the flow divider valve element is configured such that:
when the flow divider valve element is in the closed position, the inlet port is fluidly isolated from the start nozzle manifold outlet port, the run nozzle manifold outlet port, and the internal channel, and
when fuel pressure at the inlet port is between a first predetermined pressure and a second predetermined pressure:
the flow divider valve element is in one or more of the open positions and the inlet port is in fluid communication with (i) the start nozzle manifold outlet port via the start flow orifice and (ii) the run nozzle manifold outlet port via the internal flow channel and the flow regulation port, and
fuel flow through the start flow nozzle manifold outlet port is substantially constant regardless of fuel flow into the inlet port; and

wherein:
the valve body and flow divider valve element are configured to define, within the valve chamber, an inlet chamber, a run nozzle manifold chamber, and a start nozzle manifold chamber,
the start nozzle manifold chamber is in fluid communication with the inlet chamber, via the start flow orifice, regardless of flow divider valve element position,
the run nozzle manifold chamber is in fluid communication with the inlet chamber, via the internal flow channel and the flow regulation port, when the flow divider valve element is in the plurality of open positions, and
the start nozzle manifold chamber and the run nozzle manifold chamber are in fluid communication with each other when fuel pressure at the inlet port exceeds the second predetermined pressure.

2. The flow divider valve of claim 1 , wherein the flow divider valve element is further configured such that when fuel pressure at the inlet port exceeds the second predetermined pressure, the flow divider valve element is in one or more of the open positions and the start nozzle manifold outlet port is in fluid communication with the run nozzle manifold outlet port via the valve chamber.

3. The flow divider valve of claim 1 , wherein:
the valve body and flow divider valve element are further configured to define a control chamber; and
the flow divider valve further comprises a valve bias spring disposed within the control chamber, the valve bias spring engaging the valve body and the flow divider valve element and urging the flow divider valve element toward the closed position.

4. The flow divider valve of claim 3 , wherein the control chamber is in continuous fluid communication with the inlet chamber, via the start flow orifice, and with the start nozzle manifold chamber.

5. The flow divider valve of claim 1 , further comprising:
an ecology valve body including a control pressure port, a burn flow port, a run nozzle port, and an inner surface that defines an ecology valve chamber, the burn flow port in fluid communication with the internal channel of the flow divider valve element, the run nozzle port in fluid communication with the run nozzle manifold outlet port; and
an ecology valve element disposed within the ecology valve chamber and movable therein between a plurality of positions, the ecology valve element dividing the ecology valve chamber into a variable volume control chamber and a variable volume fuel reservoir, the variable volume control chamber in fluid communication with the control pressure port, the ecology valve element configured, in response to fuel pressure at the control pressure port, to move and selectively place the variable volume fuel reservoir in fluid communication with one of the burn flow port and the run nozzle port.

6. The flow divider valve of claim 1 , wherein:
the flow divider valve is for controlling fuel flow to a gas turbine engine that additionally includes a staged nozzle manifold;
the valve body further includes a staged nozzle manifold outlet port; and
the flow divider valve element is further configured such that:
the staged nozzle manifold outlet port is fluidly isolated from the inlet port when (i) the flow divider valve element is in the closed position and (ii) when fuel pressure at the inlet port is between the first predetermined pressure and a third predetermined pressure, the third predetermined pressure greater than the second predetermined pressure, and
the staged nozzle manifold outlet port is in fluid communication with the start nozzle manifold outlet port and the run nozzle manifold outlet port, via the valve chamber, when fuel pressure at the inlet port exceeds the third predetermined pressure.

7. The flow divider valve of claim 6 , further comprising:
a chamber equalization channel in fluid communication with the run nozzle manifold outlet port and the staged nozzle manifold outlet port; and
a nozzle staging on/off device disposed within the chamber equalization channel and movable between a first position and a second position,
wherein:
when the nozzle staging on/off device is in the first position, fluid communication between the run nozzle manifold outlet port and the staged nozzle manifold outlet port, via the chamber equalization channel, is blocked, and
when the nozzle staging on/off device is in the second position, the run nozzle manifold outlet port and the staged nozzle manifold outlet port are in fluid communication, via the chamber equalization channel.

8. The flow divider valve of claim 7 , further comprising:
an ecology valve body including a control pressure port, a burn flow port, a run nozzle port, a staged nozzle port, and an inner surface that defines an ecology valve chamber, the burn flow port in fluid communication with the internal channel of the flow divider valve element, the run nozzle port in fluid communication with the run nozzle manifold outlet port, and the staged nozzle port in fluid communication with staged nozzle manifold outlet port; and
an ecology valve element disposed within the ecology valve chamber and movable therein between a plurality of positions, the ecology valve element dividing the ecology valve chamber into a variable volume control chamber and a variable volume fuel reservoir, the variable volume control chamber in fluid communication with the control pressure port, the ecology valve element configured, in response to fuel pressure at the control pressure port, to move and selectively place the variable volume fuel reservoir in fluid communication with one of the burn flow port, the run nozzle port, and the staged nozzle port.

9. A flow divider and ecology system for a gas turbine engine that includes a start nozzle manifold and a run nozzle manifold, the system comprising:
a flow divider valve body including an inlet port, a start nozzle manifold outlet port, a run nozzle manifold

Assignees

• Futa Paul
• Mcroberts Brad
• Lafferty Greg
• Honeywell Int Inc

Inventors

• Futa Paul
• Mcroberts Brad
• Lafferty Greg

Classifications

• F02C9/263 Primary

  by means of fuel metering valves · CPC title

• F02C7/232

  Fuel valves {(control of fuel supply by means of fuel metering valves F02C9/263)}; Draining valves or systems (valves in general F16K) · CPC title

• Y10T137/2524

  Flow dividers [e.g., reversely acting controls] · CPC title

• F02C9/34

  Joint control of separate flows to main and auxiliary burners · CPC title

• F02C7/228

  Dividing fuel between various burners · CPC title