# US 2008/0184707 A1 · Fuel manifold for combustion systems

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- Number: US 2008/0184707 A1
- Document ID: US20080184707A1
- Status: Published application
- Kind: A1
- Application number: 11/588,893
- Filed: 2006-10-27
- Published: 2008-08-07
- Earliest claimed: 2006-10-27
- Assignees: Honeywell International Inc.
- Inventors: Frank J. Zupanc; Ian L. Critchley
- Web page: https://patentgrep.com/patent/US20080184707A1

## CPC

- F02C 7/222: {Fuel flow conduits, e.g. manifolds}
- F02C 3/145: {the combustion chamber being in the reverse flow-type}
- F23R 3/38: comprising rotary fuel injection means
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F23R: GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (fluidised bed combustion apparatus specially adapted for operation at superatmospheric pressures F23C10/16)

## Abstract

A fuel manifold is provided for receiving a flow of fuel from a fuel source and delivering the flow of fuel to a rotary fuel slinger. The fuel manifold can include a housing having an end face and defining a cavity for receiving the flow of fuel; at least one exit orifice formed in the housing end face and in fluid communication with the cavity; and a fuel drip guide extending from the end face.

## Claims

### Claim 1

A combustion system, comprising;
a fuel manifold adapted to receive a flow of fuel from a fuel source, the fuel manifold including at least one exit orifice from which the received fuel is discharged;
a rotary fuel slinger disposed adjacent to, and adapted to receive the flow of fuel from, the fuel manifold and to atomize the received fuel;
a combustor including at least a forward radial liner and an aft radial liner spaced apart from one another to form a combustion chamber therebetween that receives the atomized fuel from the rotary fuel slinger, the forward and aft radial liners each including a plurality of openings for receiving compressed air into the combustion chamber to mix with the atomized fuel;
an igniter extending at least partially into the combustion chamber and configured to ignite the atomized fuel and the compressed air mixture; and
a fuel drip guide disposed adjacent the fuel manifold exit orifice.

### Claim 2 (depends on 1)

The combustion system of claim 1, wherein the fuel manifold is configured such that,
during normal operating conditions, the flow of fuel exits the at least one exit orifice and flows directly onto the rotary fuel slinger, and
during low flow operating conditions, the flow of fuel exits the at least one exit orifice, flows down the fuel drip guide, and onto the rotary fuel slinger.

### Claim 3 (depends on 1)

The combustion system of claim 1, wherein a rotary fuel slinger includes
a coupler shaft adapted to receive a rotational drive force,
a vertical shoulder extending substantially perpendicular from the coupler shaft, and
a slinger extending substantially perpendicular from the vertical shoulder and including a plurality of evenly spaced openings extending therethrough,
wherein the rotary fuel slinger is adapted to receive the flow of fuel from the fuel manifold and, upon receipt of the rotational drive force, to centrifuge the received fuel into the combustion chamber to atomize the fuel.

### Claim 4 (depends on 1)

The combustion system of claim 1, wherein the rotary fuel slinger has a substantially cup-shaped radial cross section.

### Claim 5 (depends on 1)

The combustion system of claim 1, wherein the fuel drip guide has a length of about 0.05 to about 0.08 inches.

### Claim 6 (depends on 1)

The combustion system of claim 1, wherein the fuel manifold includes an end face, the fuel drip guide is parallel to the end face, and the fuel drip guide having a first side that, during low flow operating conditions, directs the flow of fuel onto the rotary fuel slinger and a second side that does not contact fuel.

### Claim 7 (depends on 1)

The combustion system of claim 1, wherein the fuel manifold has an annular shape with a circumference, and the drip guide extends around the circumference of the fuel manifold.

### Claim 8 (depends on 1)

The combustion system of claim 1, wherein the fuel drip guide is a knife-edge guide.

### Claim 9 (depends on 1)

The combustion system of claim 1, wherein the rotary fuel slinger primarily receives the flow of fuel directly from the at least one exit orifice.

### Claim 10

A fuel manifold for receiving a flow of fuel from a fuel source and delivering the flow of fuel to a rotary fuel slinger, the fuel manifold comprising:
a housing having an end face and defining a cavity for receiving the flow of fuel;
at least one exit orifice formed in the housing end face and in fluid communication with the cavity; and
a fuel drip guide extending from the end face.

### Claim 11 (depends on 10)

The fuel manifold of claim 10, wherein the fuel manifold is configured such that,
during normal operating conditions, the flow of fuel exits the at least one exit orifice and flows directly onto the rotary fuel slinger, and
during low flow operating conditions, the flow of fuel exits the at least one exit orifice, flows down the fuel drip guide, and onto the rotary fuel slinger.

### Claim 12 (depends on 10)

The fuel manifold of claim 10, wherein the fuel drip guide has a length of about 0.05 to about 0.08 inches.

### Claim 13 (depends on 10)

The fuel manifold of claim 10, wherein the fuel drip guide is parallel to the end face, the fuel drip guide having a first side that, during low flow operating conditions, directs the flow of fuel onto the rotary fuel slinger and a second side that does not contact fuel.

### Claim 14 (depends on 10)

The fuel manifold of claim 10, wherein the end face has a circumferential shape and the drip guide extends around the circumference of the end face.

### Claim 15 (depends on 10)

The fuel manifold of claim 10, wherein the fuel drip guide is a knife-edge guide.

### Claim 16 (depends on 10)

The fuel manifold of claim 10, wherein the fuel manifold is configured to primarily deliver the flow of fuel directly from the at least one exit orifice.

### Claim 17

A method of delivering a flow of fuel to a rotary fuel slinger from a fuel manifold having at least one exit orifice and a fuel drip guide, the method comprising:
during normal operating conditions, providing the flow of fuel directly from the at least one exit orifice to the rotary fuel slinger; and
during low flow operating conditions, directing the flow of fuel from the at least one exit orifice to the rotary fuel slinger via the fuel drip guide.

### Claim 18 (depends on 17)

The method of claim 17, wherein the fuel drip guide has a length of about 0.05 to about 0.08 inches.

### Claim 19 (depends on 17)

The method of claim 17, wherein the fuel manifold has a end face, and wherein the fuel drip guide is parallel to the end face, the fuel drip guide having a first side that, during low flow operating conditions, directs the flow of fuel onto the rotary fuel slinger and a second side that does not contact fuel.

### Claim 20 (depends on 17)

The method of claim 17, wherein the fuel drip guide is a knife-edge guide.