Nozzles with internal manifolding

Patent metadata

Field	Value
Publication number	US-10876477-B2
Application number	US-201615268211-A
Country	US
Kind code	B2
Filing date	Sep 16, 2016
Priority date	Sep 16, 2016
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A nozzle includes a nozzle body defining a liquid circuit extending from a liquid inlet to a liquid outlet. The liquid circuit includes a plurality of spiral liquid passages spiraling radially inward relative to a spray axis. The spiral liquid passages all lie in a plane normal to the spray axis. A manifold assembly includes a plurality of such nozzles. A manifold ring is in fluid communication with the liquid inlet of each of the nozzles to deliver liquid to the nozzles. The nozzles are circumferentially spaced apart around the manifold ring.

First claim

What is claimed is:

1. A nozzle comprising:
a nozzle body defining a liquid circuit extending from a liquid inlet to a liquid outlet, wherein the liquid circuit includes at least one spiral liquid passage spiraling radially inward relative to a spray axis, wherein each of the at least one spiral liquid passages lies in a plane normal to the spray axis, wherein each of the at least one spiral liquid passage defines a respective outlet orifice of the liquid outlet, wherein each outlet orifice defines an orifice axis that is tangential relative to the spray axis and lies in the plane normal to the spray axis, wherein a radial cross-section through the nozzle body, relative to the spray axis, cuts through all spiral liquid passages, namely a cross-section as viewed in a cross-sectional side-elevation view, viewing toward the spray axis, which runs in a direction going across the view, wherein each spiral liquid passage is defined in and issues from a plane perpendicular to the spray axis into a respective air passage that follows a path parallel to the spray axis.

2. A nozzle as recited in claim 1 , wherein the nozzle body includes an inner air circuit passing inboard of the liquid outlet.

3. A nozzle as recited in claim 2 , wherein the inner air circuit extends radially inward with a tangential swirl from an inlet thereof and turns in an axial direction to an outlet thereof radially inboard of the liquid outlet.

4. A nozzle as recited in claim 2 , further comprising a radial air swirler mounted to the nozzle body, wherein radial air slots defined in the radial air swirler define an inlet of the inner air circuit.

5. A nozzle as recited in claim 2 , wherein the inner air circuit and liquid circuit are in a co-swirling configuration.

6. A nozzle as recited in claim 1 , wherein the nozzle body includes an outer air circuit passing outboard of the liquid outlet.

7. A nozzle as recited in claim 6 , wherein the outer air circuit extends radially inward from an inlet thereof and turns in an axial direction to an outlet thereof radially outboard of the liquid outlet.

8. A nozzle as recited in claim 1 , wherein the nozzle body includes inner and outer manifold ring segments, wherein at least one of the ring segments includes a liquid manifold passage in fluid communication with the liquid inlet of the liquid circuit.

9. A nozzle as recited in claim 8 , wherein at least one of the ring segments includes a bayonet feature configured to receive a corresponding bayonet feature of a combustor wall or combustor sliding support.

10. A nozzle comprising:
a nozzle body defining a liquid circuit extending from a liquid inlet to a liquid outlet, wherein the liquid circuit includes at least one spiral liquid passage spiraling radially inward relative to a spray axis, wherein each of the at least one spiral liquid passages lies in a plane normal to the spray axis, wherein a radial cross-section through the nozzle body, relative to the spray axis, cuts through all spiral liquid passages, namely a cross-section as viewed in a cross-sectional side-elevation view, viewing toward the spray axis, which runs in a direction going across the view, wherein the nozzle body includes an outer air circuit passing outboard of the liquid outlet, wherein the nozzle body includes a plurality of spacers extending from an annular face of the nozzle body in a parallel direction to the spray axis, and further comprising a heat shield mounted to the nozzle body, spaced apart from the nozzle body by the plurality of spacers, wherein the outer air circuit is defined between the nozzle body, the plurality of spacers, and heat shield, wherein each spiral liquid passage is defined in and issues from a plane perpendicular to the spray axis into a respective air passage that follows a path parallel to the spray axis.

11. A nozzle as recited in claim 10 , wherein the spacers define a non-tangential flow path for non-swirling flow of air through the outer air circuit.

Assignees

• Delavan Inc

Inventors

• Prociw Lev Alexander
• Ryon Jason A

Classifications

• F23R3/283 Primary

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

• F23D14/78

  Cooling burner parts · CPC title

• B05B7/10

  producing a swirling discharge · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C7/222 Primary

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