Annular fuel manifold with a deflector

Patent metadata

Field	Value
Publication number	US-10746101-B2
Application number	US-201715621367-A
Country	US
Kind code	B2
Filing date	Jun 13, 2017
Priority date	Jun 13, 2017
Publication date	Aug 18, 2020
Grant date	Aug 18, 2020

Abstract

An annular fuel manifold includes an annular fuel plenum defined within the annular fuel manifold, an axial inlet into the annular fuel plenum, and a deflector downstream of the axial inlet, the deflector oriented such that fluid flow into the annular fuel plenum from the axial inlet is deflected by the deflector at least partially along a circumference of the annular fuel plenum.

First claim

What is claimed is:

1. An annular fuel manifold comprising:
an annular fuel plenum defined within the annular fuel manifold;
an axial inlet into the annular fuel plenum; and
a deflector downstream of the axial inlet, the deflector oriented such that fluid flow into the annular fuel plenum from the axial inlet is deflected by the deflector at least partially along a circumferential direction defined by the annular fuel plenum;
wherein the deflector comprises a deflector nipple downstream of the axial inlet, the deflector nipple defining an oblique conduit in fluid communication with the annular fuel manifold, the oblique conduit configured to direct fluid flow from the axial inlet partially along the circumferential direction.

2. The annular fuel manifold of claim 1 , further comprising a forward wall, an aft wall axially spaced from the forward wall, and a cylindrical outer surface extending between the forward wall and the aft wall.

3. The annular fuel manifold of claim 2 , further comprising a plurality of radial outlets circumferentially arranged along the cylindrical outer surface.

4. The annular fuel manifold of claim 3 , further comprising an axial conduit between the annular fuel plenum and each radial outlet of the plurality of radial outlets.

5. The annular fuel manifold of claim 1 , wherein the axial inlet is a first axial inlet and the deflector is a first deflector, further comprising a second axial inlet into the annular fuel plenum and a second deflector downstream of the second axial inlet, the second deflector circumferentially oriented such that fluid flow into the annular fuel plenum from the second axial inlet is deflected by the second deflector along the circumferential direction.

6. A fuel nozzle for a combustor of a turbomachine, comprising:
a liquid fuel supply conduit connected to a source of liquid fuel;
an annular fuel manifold, the liquid fuel supply conduit connected to an axial inlet of the annular fuel manifold and in fluid communication with an annular fuel plenum defined within the annular fuel manifold via the axial inlet, the annular fuel manifold further comprising a deflector downstream of the axial inlet, the deflector oriented such that liquid fuel flow into the annular fuel plenum from the axial inlet is deflected at least partially along a circumferential direction defined by the annular fuel plenum;
wherein the deflector comprises a deflector nipple downstream of the axial inlet, the deflector nipple defining an oblique conduit in fluid communication with the annular fuel manifold, the oblique conduit configured to direct fluid flow from the axial inlet partially along the circumferential direction.

7. The fuel nozzle of claim 6 , wherein the annular fuel manifold further comprises a forward wall, an aft wall axially spaced from the forward wall, and a cylindrical outer surface extending between the forward wall and the aft wall.

8. The fuel nozzle of claim 7 , wherein the annular fuel manifold further comprises a plurality of radial outlets circumferentially arranged along the cylindrical outer surface.

9. The fuel nozzle of claim 8 , wherein each of the plurality of radial outlets comprises an atomizer in fluid communication with an air plenum for spraying atomized liquid fuel from the annular fuel plenum into the air plenum.

10. The fuel nozzle of claim 8 , wherein the annular fuel manifold further comprises an axial conduit between the annular fuel plenum and each radial outlet of the plurality of radial outlets.

11. The fuel nozzle of claim 6 , wherein the axial inlet is a first axial inlet and the deflector is a first deflector, further comprising a second axial inlet into the annular fuel plenum and a second deflector downstream of the second axial inlet, the second deflector circumferentially oriented such that fluid flow into the annular fuel plenum from the second axial inlet is deflected by the second deflector along the circumferential direction.

12. The fuel nozzle of claim 6 , further comprising a center tube, a pilot tip disposed at a downstream end of the center tube, the annular fuel plenum upstream of the pilot tip within the center tube, an outer sleeve that circumferentially surrounds at least a portion of the center tube, and an air plenum defined between the outer sleeve and the center tube.

Assignees

• Gen Electric

Inventors

• Johnson Thomas Edward
• Graham Kaitlin Marie
• Myers Geoffrey David

Classifications

• F02C7/222 Primary

  Fuel flow conduits, e.g. manifolds · CPC title

• F23R3/286

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• F23R3/283

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F23R3/46

  Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings · CPC title

• F23R3/343

  Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title